N855FT
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
1,068 reports on file, 1995-04-03 – 2000-06-23.
Part: PANEL — DELAMINATED (HORIZONTAL STAB) · airframe 62,122 hrs · 20,784 cycles
LEFT HORIZONTAL STABILIZER UNDERSIDE PANEL 334KBL DELAMINATED. REMOVED DAMAGE, REPLACED CORE, POTTED, APPLIED GLASS OVERLAYS AND APPLIED FINISH PER SRM 51-40-06.
Part: FITTING — CRACKED (RT WING) · airframe 62,122 hrs · 20,784 cycles
FUEL FEED LINE FITTING CRACKED BETWEEN NR 3 AND NR 4 MAIN TANKS BY THE NR 3 PYLON BULKHEAD. REPLACED FITTING WITH NEW PART PER MM 28-22-05.
Part: PANEL — CRACKED (LT WING) · airframe 62,122 hrs · 20,784 cycles
WS 400 LEFT SIDE OVERWING PANEL JUST OUTBOARD OF ALTERNATE LANDING GEAR EXTENSION ACTUATOR. UNDER SIDE OF PANEL HAS 14 INCH CRACK WITH DELAMINATION. REMOVED DAMAGED, POTTED CORE, APPLIED GLASS OVERLAYS AND RESTORED FINISH.
Part: SKIN — DELAMINATED (ELEVATOR) · airframe 62,122 hrs · 20,784 cycles
LEFT INBOARD ELEVATOR UPPER SURFACE TRAILING EDGE HAS 9 INCHES OF DELAMINATION. REMOVED DAMAGE, POTTED CORE, APPLIED GLASS OVERLAYS AND RESTORED FINISH PER SRM 51-40-14.
Part: SKIN — DELAMINATED (LT WING) · airframe 62,122 hrs · 20,784 cycles
LEFT WING UNDERSIDE AFT OF OUTBOARD LANDING LIGHT PREVIOUS REPAIR HAS 13 INCH CRACK AND DELAMINATION. REMOVED REPAIR AND CORE, POTTED CORE, APPLIED GLASS OVERLAYS AND RESTORED FINISH PER SRM 51-40-09.
Part: SKIN — CHAFED (NR 4 PYLON)
NR 4 PYLON INBOARD SIDE LOWER EDGE OF THE SKIN DAMAGED (CHAFED). FOUND DURING ENGINE CHANGE. SUBMITTER SUGGESTED FREQUENT INSPECTION OF AREA WHEN COWLING IS REMOVED. REPAIRED PER EAC ECRA N855FT-54-001-EAC. (X)
Earlier reports · 1995–1999 · 1062 reports
1999
Part: SEAT TRACK — CORRODED (BS 1808)
LEVEL 1 CORROSION FOUND AT BS 1808 TO 1814 RBL 11 SEAT TRACK INBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01 AND 53-10-01.
Part: SPAR — CRACKED (NR 1 PYLON)
NR 1 PYLON LOWER SPAR WEB HAS CRACK APPROX 2 INCHES LONG AT NAC STA 232 RT SIDE. REPAIRED PER SRM 54-10-03.
Part: TRACK — CORRODED (BS 460-540)
LEVEL 1 CORROSION FOUND AT BS 460 TO 540 LBL 33 TIE DOWN TRACK. CORROSION REMOVED PER SRM 51-10-01 AND 53-10-01.
Part: TRACK — CORRODED (BS 1140-1160)
LEVEL 1 CORROSION FOUND ON MAIN DECK BS 1140 TO 1160 RBL 13 TIE DOWN TRACK LOWER FACE. CORROSION REMOVED PER SRM 51-10-01 AND 53-10-01.
Part: SPAR — CRACKED (NR 4 PYLON)
NR 4 PYLON LOWER SPAR WEB FOUND CRACKED AT NAC STA 230 TO 234. EPAIRED PER SRM 54-10-03 FIG 2 AND 3.
Part: SUPPORT — CORRODED (BS 1360)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1360 LBL 33 FLOOR SUPPORT LOWER FACE. CORRSOSION REMOVED PER SRM 51-10-01 AND 53-10-01.
Part: SUPPORT — CORROSION (BS 1920-1940)
LEVEL 1 CORROSION FOUND ON MAIN DECK BS 1920 TO 1940 LBL 114 FLOOR SUPPORT. FLOOR SUPPORT REPAIRED PER SRM 51-40-03 FIG 2.
Part: FLOORBEAM — CORRODED (BS 1580)
LEVEL 1 CORROSION ON FLOORBEAM MAIN DECK BS 1580 LBL 9. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 1.
Part: FLOORBEAM — CORRODED (BS 1580)
LEVEL 1 CORROSION FOUND ON FLOORBEAM AT MAIN DECK BS 1580 LBL 34 TO 75. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 1.
Part: FLOORBEAM — CORRODED (BS 1580)
LEVEL 1 CORROSION FOUND ON FLOORBEAM AT BS 1580 LBL 82 TO 96. FLOORBEAM REPAIRED PER SRM 51-40-04 FIG 1.
Part: STRINGER — CRACKED (BS 1348)
MAIN DECK CROWN BS 1348 STR 11L STRINGER END FOUND CRACKED. CRACKED STRINGER REPAIRED PER SRM 53-10-03 FIG 5.
Part: FRAME — CRACKED (BS 860)
MAIN DECK BS 860 CRACKED AT S13L CUTOUT AREA. FRAME REPAIRED PER RS R53-27-34052.
Part: SKIN — DAMAGED (CARGO DOOR)
FUSELAGE FWD CARGO DOOR AFT CUTOUT LOWER CORNER EXTERIOR SKIN FOUND DAMAGED. SKIN REPAIRED PER RS 53-21-340531.
Part: FLOORBEAM — CORRODED (BS 680)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 680 LBL 12 FLOORBEAM LOWER FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 542)
LEVEL 1 CORROSION FOUND AT UPPER DECK BS 542 LBL 11 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 750)
LEVEL 1 CORROSION FOUND AT UPPER DECK BS 750 LBL 44 SEAT TRACK CROWN. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SKIN — CORRODED (WS 197)
LEVEL 1 CORROSION FOUND RIGHT WING LOWER SKIN OUTER SURFACE, REAR SPAR WBL 197. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 57-30-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 560-561)
LEVEL 1 CORROSION FOUND AT UPPER DECK BS 560 TO 561 RBL R46 SEAT TRACK. SEAT TRACK REPLACED FROM BS 480 TO 600 PER SRM 51-10-01 PG 18.
Part: SEAT TRACK — CORRODED (BS 750)
LEVEL 1 CORROSION FOUND AT UPPER DECK BS 750 RBL 10 SEAT TRACK CROWN. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 1261)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1261 RBL 33 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 650-690)
LEVEL 1 CORROSION FOUND AT UPPER DECK BS 650 TO 690 RBL 66 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1372)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1372 RBL 57 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — BROKEN (BS 640)
FORWARD CARGO BS 640 LBL 45 FLOORBEAM UPPER CHORD FOUND BROKEN. CRACKED AREA TRIMMED OFF AS PER SRM 51-10-01 AND TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 675-690)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 624, 675-690 LBL 25 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 552-560)
LEVEL 1 CORROSION FOUND AT UPPER DECK BS 552 TO 560 LBL 11 FLOOR SUPPORT. SEAT TRACK LBL 9 STA 550 TO 590 REPAIRED AS PER SRM 53-10-05 FIG 4.
Part: SEAT TRACK — CORRODED (BS 610-613)
LEVEL 1 CORROSION FOUND AT UPPER DECK BS 610 TO 613 RBL R66 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 660-670)
LEVEL 1 CORROSION FOUND AT UPPER DECK BS 660 TO 670 RBL R46 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FITTING — CORRODED (BS 360)
LEVEL 1 CORROSION FOUND MAIN DECK BS 360 LBL 40 FLOOR HANDLING FITTING AFT SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 2320)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2320 LBL 38 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 382)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 382 LBL 45 TIE DOWN TRACK INBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 1800)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1800 LBL 10 TO RBL 11 LATERAL FLOOR SUPPORT FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1394)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1394 RBL 11 SEAT TRACK CROWN. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 1170-1260)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1170 TO 1260 LBL 11 TO RBL 11 TIE DOWN TRACK FLANGE AROUND ANCHOR NUTS. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 2105-2108)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2105 TO 2108 RBL 87 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 2123)
LEVEL 1 CORROSION ON BS 2123 LBL 89 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01.
Part: FLOORBEAM — CORRODED (BS 800)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 800 LBL 82 TO 95 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 760)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 760 LBL 75-98 FLOORBEAM UPPER SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1802)
LEVEL 1 CORROSION ON SEAT TRACK BS 1802 TO 1812 LBL 11. CORROSION REMOVED PER SRM 51-10-01.
Part: SEAT TRACK — CORRODED (BS 1910-1920)
LEVEL 1 CORROSION ON MD SEAT TRACK BS 1910 TO 1920 LBL 33. CORROSION REMOVED PER SRM 51-10-01.
Part: SEAT TRACK — CORRODED (BS 1770)
LEVEL 1 CORROSION ON SEAT TRACK BS 1770 LBL 97. CORROSION REMOVED PER SRM 51-10-01.
Part: SEAT TRACK — CORRODED (BS 480-520)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 480 TO 520 LBL 69 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FITTING — CORRODED (BS 1800)
LEVEL 1 CORROSION ON TIE DOWN FITTING BS 1800 LBL 55. CORROSION REMOVED PER SRM 51-10-01.
Part: FLOORBEAM — CORRODED (BS 2140)
LEVEL 1 CORROSION FOUND MAIN DECK BS 2140 RBL 85 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 2180)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2180 RBL 76 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 940-980)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 940 TO 980 RBL 11 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 2038-2250)
LEVEL 1 CORROSION FOUND ON SEAT TRACKS FROM BS 2038 TO 2250 LBL10 TO 11. CORROSION REMOVED PER SRM 51-10-01.
Part: FLOORBEAM — CORRODED (BS 2100)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2100 LBL 92 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 2040)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2040 LBL 91 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1416-1500)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1416 TO 1500 LBL 11-33 FLOORBEAM AND ATTACH TIE DOWN FITTING. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: ANGLE — CORRODED (BS 890)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 890 LBL 117 FLOOR SUPPORT ANGLE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1950-1970)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1950 TO 1970 RBL 11 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 940)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 940 LBL 30 TIE DOWN PLATE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 710-790)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 710 TO 790 LBL 11 TIE DOWN TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 520)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 520 LBL 33 TO 70 FLOORBEAM AT UPPER SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SHEAR PANEL — CORRODED (BS 1100-1010)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1100 TO 1010 LBL 11 TO RBL 11 BELOW FLOOR SHEAR PANEL AT BOTH FACES. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FITTING — CORRODED (BS 320)
LEVEL 1 CORROSION FOUND MAIN DECK BS 320 LBL 50 FLOOR HANDLING FITTING AFT SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FITTING — CORRODED (BS 260)
LEVEL 1 CORROSION FOUND MAIN DECK BS 260 LBL 60 HANDLING FLOOR FITTING AFT SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 2123)
LEVEL 1 CORROSION FOUND ON SEAT TRACK AT BS 2123 LBL 97. CORROSION REMOVED PER SRM 51-10-01.
Part: SEAT TRACK — CORRODED (BS 220-240)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 220 TO 224 LBL 26 SEAT TRACK CROWN SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1912)
LEVEL 1 CORROSION ON SEAT TRACK BS 1912 LBL 97. CORROSION REMOVED PER SRM 51-10-01.
Part: SEAT TRACK — CORRODED (BS 570-660)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 570 TO 660 LBL 11 SEAT TRACK CROWN. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1700)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1700 LBL 85 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: WEB — CORRODED (BS 420-440)
LEVEL 1 CORROSION FOUND MAIN DECK BODY STATION 420 TO 440, RBL 90, VERTICAL WEB SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 53-10-02.
Part: SEAT TRACK — CORRODED (BS 2138)
LEVEL 1 CORROSION ON SEAT TRACK BS 2138 LBL 75. CORROSION REMOVED PER SRM 51-10-01.
Part: TIE DOWN — CORRODED (BS 960)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 960 LBL 17 TIE DOWN PLATE LOWER FACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 500)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 500 LBL 20-30 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 640-674)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 640 TO 674 LBL 75 TIE DOWN TRACK INBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 865)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 865 LBL 97 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 980)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 980 LBL 8295 FLOORBEAM LOWER FACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 320)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 320 LBL 11 TO 33 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 980)
LEVEL 1 CORROSION FOUND MAIN DECK BS 980 RBL 55 TO 77 FLOORBEAM UPPER TEE CHORD LOWER FACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 360)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 360 LBL 33 FLOOR HANDLING AFT SUPPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 520)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 520 LBL 11 TIE DOWN CRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 240-260)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 240 TO 260 LBL 36 SEAT TRACK CROWN SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1780)
LEVEL 1 CORROSION AT BS 1780 LBL 75 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01.
Part: TIE DOWN — CORRODED (BS 378)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 378 LBL 80 TIE DOWN TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 520)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 520 RBL 87 TIE DOWN PLATE SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 910)
LEVEL 1 CORROSION FOUND MAIN DECK BS 910 LBL 19 FLOOR SUPPORT HAT SECTION. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 760)
LEVEL 1 CORROSION FOUND MAIN DECK BS 760 RBL 95-98 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FITTING — CORRODED (BS 1320)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1320 RBL 33 TIE DOWN FITTING ATTACH FLANGE LOWER FACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1920)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1920 LBL 90 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 460-480)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 460 TO 480 LBL 11 AND 22. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 1689)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1689 LBL 114 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1967)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1967 RBL 33 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 2140)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2140 LBL 22 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 680)
LEVEL 1 CORROSION FOUND AT BS 680 RBL 56 TIE DOWN PLATE SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 520-550)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 520 TO 550 LBL 11 SEAT TRACK CROWN SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1940)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1940 RBL 97 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 420-440)
LEVEL 1 CORROSION FOUND MAIN DECK BS 420 TO 440, RBL 104, FLOOR PANEL SUPPORT RAIL. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 270-340)
LEVEL 1 CORROSION FOUND MAIN DECK BS 270-340, RBL 94, FLOOR PANEL SUPPORT RAIL. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: WEB — CORRODED (BS 240)
LEVEL 1 CORROSION FOUND MAIN DECK BS 240 LBL 17 TO RBL 14, HORIZONTAL WEB SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 460)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 460 LBL 68-95 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 324)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 324 LBL 36 TIE DOWN TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: WEB — CORRODED (BS 160)
LEVEL 1 CORROSION FOUND MAIN DECK BS 160 LBL 11 HORIZONTAL WEB SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-02 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1940)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1940 RBL 50 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 980)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 980 LBL 11 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 640-670)
LEVEL 1 CORROSION FOUND MAIN DECK BS 640 TO 670, RBL 104, FLOOR PANEL SUPPORT RAIL. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 2178-2180)
LEVEL 1 CORROSION FOUND MAIN DECK BS 2178 TO 2180 RBL 98 TO 102 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 480-520)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 480 TO 520 RBL 68 SEAT TRACK CROWN SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 910-914)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 910 TO 914 LBL 33 TIE DOWN TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 2140)
LEVEL 1 CORROSION FOUND MAIN DECK BS 2140 LBL 10 TO RBL 10 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 2040)
LEVEL 1 CORROSION FOUND MAIN DECK BS 2040 LBL 10 TO RBL 10 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SHEAR PANEL — CORRODED (BS 1170-1260)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1170 TO 1260 CENTER BELOW FLOOR SHEAR PANEL. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 665)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 665 LBL 76 TIE DOWN TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 600-610)
LEVEL 1 CORROSION FOUND AT UPPER DECK LEFT HAND BS 600 TO 610 LBL 66 SEAT TRACK CROWN FLANGE. SEAT TRACK REPAIRED AT LBL 66 STA 560 AND 640 PER SRM 53-10-05.
Part: FITTING — CORRODED (BS 1780)
LEVEL 1 CORROSION ON BS 1780 LBL 88 TIE DOWN FITTING. CORROSION REMOVED PER SRM 51-10-01.
Part: SEAT TRACK — CORRODED (BS 1804)
LEVEL 1 CORROSION ON SEAT TRACK BS 1804 LBL 35. CORROSION REMOVED PER SRM 51-10-01.
Part: TIE DOWN — CORRODED (BS 420-460)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 420 TO 460 LBL 68 TIE DOWN TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 2140)
LEVEL 1 CORROSION FOUND MAIN DECK BS 2140 RBL 38 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 360)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 360 LBL 33 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 660)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 660 LBL 11 TO RBL 11 FLOORBEAM SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FITTING — CORRODED (BS 1800)
LEVEL 1 CORROSION ON TIE DOWN FITTING BS 1800 LBL 12. CORROSION REMOVED PER SRM 51-10-01.
Part: TIE DOWN — CORRODED (BS 290)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 290 LBL 70 TIE DOWN TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1924)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1294 RBL 33 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1888)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1888 RBL 11 SEAT TRACK INBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1900)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1900 RBL 75 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 2040)
LEVEL 1 CORROSION FOUND MAIN DECK BS 2040 RBL 21 FLOORBEAM UPPER CHORD LOWER FACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 400)
LEVEL 1 CORROSION FOUND MAIN DECK BS 400 RBL 38 FLOORBEAM SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 761)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 761 LBL 97 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 2140)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2140 LBL 73 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FITTING — CORRODED (BS 1800)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 800 RBL 15-16 TIE DOWN FITTING FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1500-1508)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1500 TO 1508 RBL 11 SEAT TRACK. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 2220)
LEVEL 1 CORROSION FOUND ON MD BS 2220 LBL 97 TIE DOWN TRACK. CORROSION REMOVED PER SRM 51-10-01.
Part: SEAT TRACK — CORRODED (BS 2234-2236)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2234 TO 2236 RBL 64 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 770)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 770 RBL 10 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1540-1560)
LEVEL 1 CORROSION ON SEAT TRACK BS 1540 TO 1560 LBL 75. REMOVED CORROSION PER SRM 51-10-01.
Part: SEAT TRACK — CORRODED (BS 560-590)
LEVEL 1 CORROSION FOUND AT UPPER DECK SEAT TRACK EDGE ATTACH HOLE LOWER AREA, BS 560 TO 590 LBL 40 AND 60. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1510-1560)
LEVEL 1 CORROSION FOUND ON M/D BS 1510 TO 1560 LBL 10 SEAT TRACK FLANGE. REMOVED CORROSION, BLENDED OUT AND TREATED PER SRM 51-10-01.
Part: STRINGER — CORRODED (BS 2000)
LEVEL 1 CORROSION FOUND MAIN DECK BS 2000 STRINGER 17L AROUND RIVIT AREA. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: STRINGER — CORRODED (BS 2220)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2220 STR 2R. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 1220)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1220, RBL 60 TO 74 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FITTING — CORRODED (BS 1760)
LEVEL 1 CORROSION ON MD BS 1760 LBL 88 TIE DOWN FITTING FLANGE PLATE. CORROSION REMOVED PER SRM 51-10-01.
Part: SUPPORT — CORRODED (BS 1000-1100)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1000 TO 1100 LBL L11-R11 TIE DOWN TRACK FLOOR SUPPORT LOWER FACE ANCHOR NUT ATTACH AREA. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 2226-2228)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2226 TO 2228 RBL 32 SEAT TRACK INBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: BRACKET — CORRODED (BS 680)
LEVEL 1 CORROSION FOUND MAIN DECK BS 680, WL 200, LT FRAME ATTACH BRACKET UPPER SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1830)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1830 RBL 75 SEAT TRACK CROWN AND FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1800)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1800 LBL 83 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FRAME — CRACKED (BS 1760)
MAIN DECK BS 1760 STR 14 TO 15R FRAME FLANGE FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-10-04.
Part: TIE DOWN — CORRODED (BS 1140-1160)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1140 TO 1160 RBL 32 TIE DOWN TRACK LOWER FACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: STRINGER — CRACKED (BS 2360)
MAIN DECK BS 2360 STRINGER 15L STRINGER END FOUND CRACKED. REPAIRED STRINGER AS PER SRM 53-10-03 FIG 2.
Part: FLOORBEAM — CORRODED (BS 1500)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1500 LBL 11 TO RBL 11 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 770-790)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 770 TO 790 LBL 10 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 2140-2148)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2140 TO 2148 RBL 11 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FORGING — CORRODED (BS 1980-2020)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1980 TO 2020, STR 20R-22R WINDOW FORGING (SEVERAL LOCATIONS). CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 56-20-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1900-1980)
LEVEL 1 CORROSION FOUND ON SEAT TRACK FROM BS 1900 TO 1980 LBL75 TO 77. CORROSION REMOVED PER SRM 51-10-01.
Part: SEAT TRACK — CORRODED (BS 670-690)
LEVEL 1 CORROSION FOUND AT UPPER DECK BS 670 TO 690 LBL 22 SEAT TRACK SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 463)
LEVEL 1 CORROSION FOUND UPPER DECK FLOOR SUPPORT UPPER CHORD BS 463 RBL R40. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 2240)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2240 LBL 75 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 440)
LEVEL 1 CORROSION FOUND MAIN DECK BS 440 RBL 47 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1752-1754)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1752 TO 1754 RBL 11 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: STRINGER — CORRODED (BS 1800)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1800 STRINGER 15L. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FORGING — CORRODED (BS 1416-1438)
LEVEL 1 CORROSION FOUND MAIN DECK FS 1416 TO 1438, RT WINDOW FORGING FORWARD CORNER. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 56-20-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1500)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1500 RBL 84 TO 94 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FORGING — CORRODED (BS 638)
LEVEL 1 CORROSION FOUND MAIN DECK BS 638 STR 20L-21L, WINDOW FORGING AFT EDGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 56-20-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE CLIP — CORRODED (BS 2160)
LEVEL 1 CORROSION FOUND MAIN DECK BS 2160 STR 21L TIE CLIP. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1540)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1540 LBL 20 TO RBL 10 FLOORBEAM LOWER CHORD UPPER SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1775-1780)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1775 TO 1780 RBL 75 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 2198-2200)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2198 TO 2200 RBL 34 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 2240)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2240 RBL 66 TO 69 LATERAL FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1500)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1500 LBL 82-96 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 1140)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1140, RBL 11 TO 33, FLOOR SUPPORT LOWER FACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: BRACKET — CORRODED (BS 2080)
LEVEL 1 CORROSION FOUND MAIN DECK BS 2080 STR 26R, FRAME ATTACH BRACKET AT HI-LOK AREA. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 2231-2240)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 2231 TO 2240 RT WL 200 O/B FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: DECK — CORRODED (BS 1416-1372)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1416 TO 1372, RBL 11, PRESSURE DECK SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1413)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1413 RBL 10 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 1670)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1670 LBL 55 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 960-980)
LEVEL 1 CORROSION FOUND MAIN DECK FLOOR SUPPORT LOWER FACE, BS 960 TO 980 RBL 18. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 789)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 789 LBL 10 TO RBL 10 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1530)
LEVEL 1 CORROSION ON SEAT TRACK BS 1530 LBL 77. REMOVED CORROSION PER SRM 51-10-01.
Part: FLOORBEAM — CORRODED (BS 1560)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1560 LBL 10 FLOORBEAM LOWER CHORD UPPER AND LOWER SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 1208-1223)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1208 TO 1223 RBL 32 TIE DOWN TRACK CROWN OUTBOARD EDGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 160-180)
LEVEL 1 CORROSION FOUND MAIN DECK BS 160 TO 180 RBL 44 FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 2166-2168)
LEVEL 1 CORROSION FOUND MAIN DECK BS 2166 TO 2168 RBL 97 LONGIT FLOOR SUPPORT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1500)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1500 LBL 60-75 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1916-1920)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1916 TO 1920 RBL 75 SEAT TRACK FLANGE AND CROWN. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1810-1812)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1810 TO 1812 RBL 11 SEAT TRACK OUTBOARD FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 520-528)
LEVEL 1 CORROSION FOUND AT UPPER DECK FLOOR SUPPORT BS 520 TO 528 RBL R80. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 460-480)
LEVEL 1 CORROSION FOUND MAIN DECK TIE DOWN TRACK FLANGE, BS 460 TO 480 LBL 32 WL 200. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1500)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1500 RBL 11 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: TIE DOWN — CORRODED (BS 380-460)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 380 TO 460 LBL 80 TIE DOWN TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FITTING — CORRODED (BS 1900)
LEVEL 1 CORROSION FOUND ON TIE DOWN FITTING MD BS 1900 LBL 82. CORROSION REMOVED PER SRM 51-10-01.
Part: SKIN — CORRODED (BS 520-740)
LEVEL 1 CORROSION FOUND MAIN DECK BS 520-740, STR 23L UPPER LAP JOINT. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. TREATED AREA PER SRM 51-10-01.
Part: WEB — CRACKED (BS 2220)
MAIN DECK BS 2220 BELOW STR 22R, WEB FOUND CRACKED. WEB REPAIRED IAW SRM 51-40-03 FIG 1.
Part: FITTING — CORRODED (BS 2240)
LEVEL 1 CORROSION ON MD BS 2240 LBL 3 TIE DOWN FITTING FLANGE PLATE. REMOVED CORROSION PER SMR 51-10-01.
Part: SKIN — DELAMINATED (RT WING)
RIGHT WING L/E CAVITY LOWER SKIN HAS AREA OF DELAMINATION JUST AFT OF NR 15 K/FLAP. FIBER GLASS REPAIRED AS PER SRM 51-40-05 FIG 7.
Part: KEEL BEAM — CORRODED (LT MLG WW)
LEVEL 1 CORROSION FOUND LEFT HAND WING GEAR WHEEL WELL KEEL BEAR UPPER SURFACE. CORROSION REMOVED AND AREA TREATED AS PER SRM 51-10-01 AND 51-10-02.
Part: ANGLE — CORRODED (BS 2140-2160)
LEVEL 1 CORROSION FOUND ON SUPPORT ANGLE, BULK CARGO COMPARTMENT CEILING AREA RT STA 2140 TO 2160. SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 18.
Part: SHEAR TIE — CRACKED (BS 1960)
BULK CARGO STATION 1960 RBL 10 SHEAR TIE FOUND CRACKED AND CORRODED. CRACKED AREA TRIMMED PER SRM 51-10-01 AND SHEAR TIE REPAIRED PER SRM 53-10-04.
Part: KEEL BEAM — CORRODED (BS 1480-1420)
LEVEL 1 CORROSION FOUND AT LEFT HAND BODY GEAR WHEEL WELL KEEL BEAM UPPER WEB ADJACENT BS 1480 AND 1420. CORROSION REMOVED AND AREA TREATED AS PER SRM 51-10-01 AND 51-10-02.
Part: FITTING — CORRODED (BS 1800)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1800 RBL 77 TIE DOWN FITTING. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: WALL — CORRODED (LT MLG WW)
LEVEL 1 CORROSION FOUND LEFT HAND BLG W/W, OUTER WALL CAVITY ABOVE U/C DOOR SEQUENCE VALVE. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02.
Part: FITTING — CORRODED (BS 1780)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1780 RBL 77 TIE DOWN FITTING. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SKIN — CORRODED (WS 429)
LEVEL 1 CORROSION FOUND RIGHT HAND WING UPPER SKIN OUTER SURFACE AT MID SPAR WL 429 STR 14. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM LIMITS 57-30-01. TREATED AREA PER SRM 51-10-02.
Part: FITTING — CORRODED (BS 1840)
LEVEL 1 CORROSION FOUND BS 1840 LBL 53 TIE DOWN FITTING. CORROSION REMOVED PER SRM 51-10-01.
Part: SHEAR TIE — CORRODED (BS 2080)
LEVEL 1 CORROSION FOUND AT SHEAR TIE, BULK CARGO STA 2080, STR 43-44R. CORROSION REMOVED AND AREA TREATED AS PER SRM 51-10-01 AND 51-10-02.
Part: SEAT TRACK — CORRODED (BS 240-260)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 240 TO 260 RBL 36 SEAT TRACK CROWN SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1580)
LEVEL 1 CORROSION FOUND MAIN DECK BS 1580 RBL 84 TO 94 FLOORBEAM. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 640)
LEVEL 1 CORROSION FOUND MAIN DECK BS 640 RBL 48 FLOORBEAM SURFACE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 817)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 817 LBL 87 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: SEAT TRACK — CORRODED (BS 1800)
LEVEL 1 CORROSION FOUND AT MAIN DECK BS 1800 RBL 75 SEAT TRACK FLANGE. CORROSION REMOVED PER SRM 51-10-01, WITHIN SRM 53-10-01 LIMITS. AREA TREATED PER SRM 51-10-02.
Part: STRINGER — CRACKED (BS 1354)
MAIN DECK BS 1354 STRINGER 18R STRINGER END FOUND CRACKED. STRINGER END REPAIRED PER SRM 53-10-03 FIG 2.
Part: FAIRING — DAMAGED (NR 1 FLAP TRACK)
NR 1 FLAP TRACK MOVABLE CANOE FAIRING HAS SEVERAL AREAS OF DAMAGE. REPAIRED DAMAGE PER SRM 51-40-15 FIG 7.
Part: SKIN — LOOSE (BS 2658-2742)
EMP TAIL CONE LT SKIN ATTACHED RIVETS FOUND LOOSE. TOTAL 140 FROM BS 2658 TO 2742 LEFT SIDE. RIVETS REPAIRED PER SRM 51-30-02.
Part: COWL — CRACKED (NR 3 ENGING)
NR 3 ENGINE TRANSLATING COWL INNER SKIN IS CRACKED AT T/E AT 7 TO 8 O'CLOCK POSITION. SLIGHTLY CRACKED SMOOTHED OUT PER SRM 51-10-02 AND TREATED PER SRM 51-10-02.
Part: ANGLE — CORRODED (BS 1283)
LEVEL 1 CORROSION FOUND ON RIGHT WING WHEEL WELL BS 1283 RBL90 APPROX CEILING ANGLE END PLATE. REMOVED CORROSION AND TREATED PER SRM 51-10-01 AND 51-10-02 WITHIN LIMITS.
Part: WEB — CRACKED (BS 660-680)
FWD CARGO STA 660-680 LBL30 FLOOR AREA WEB FOUND CRACKED. FLOOR WEB REPAIRED AT STA 660-680 LBL 30 AS PER SRM 51-40-02 FIG 1.
Part: SKIN — CORRODED (RT WING)
LEVEL 1 CORROSION FOUND ON RIGHT WING UPPER SURFACE AT WS440, 443, 586, 947, 992, 1026, 1480, 1482, 1512, 1513, 1519 AND 1528. CORROSION REMOVED PER SRM 51-10-01 AND BLENDED OUT WITHIN SRM LIMITS PER 57-30-01. TREATED AREAS PER SRM 51-10-02.
Part: HINGE — CORRODED (APU DOOR)
RIGHT APU DOOR HINGE MOUNT BOLT AREA SKIN SURFACE CORROSION. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02.
Part: WALK WAY — CORRODED (BS 1820)
AFT CARGO RIGHT SIDE STA 1820 WALK WAY PANEL FOUND CORROSION. REMOVED CORROSION AND REPROTECTED PER SRM 51-20-01 AND 51-10-02.
Part: FAIRING — DELAMINATED (NR 6 FLAP TRACK)
RIGHT WING NR 6 CANOE FAIRING FOUND DELAMINATION AT TWO LOCATIONS. REPAIRED DEFECTED AREA WITH FIBERGLASS LAYUP AT 150 DEGREES F CURED. REPAIRED PER SRM 51-40-15 FIG 7.
Part: FAIRING — DELAMINATED (NR 3 PYLON)
NR 3 PYLON V FAIRING HAS 2 AREAS OF DISBONDING. REPAIRED DELAMINATION PER SRM 51-10-02, 51-10-01 AND 57-30-01.
Part: SUPPORT — CRACKED (BS 789)
MAIN DECK BODY STATION 789 RBL33 FLOOR SUPPORT CRACKED. SUPPORT REPLACED PER SRM 51-10-01.
Part: SKIN — CRACKED (LT ELEVATOR)
LEFT INBOARD ELEVATOR TRAILING EDGE HAS DAMAGED AND CRACKED AREA. FIBERGLASS WET LAYUP REPAIR PER SRM 51-40-15.
Part: SKIN — CORRODED (BS 2658)
EMP LT SIDE BUTT JOINT SKIN SURFACE CORROSION AT BS2658. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (APU INLET DOOR)
EMP APU AIR INLET DOOR CUT OUT FWD EDGE SKIN HAS SURFACE CORROSION. REPAIRED CORROSION PER SRM 51-10-01 AND 51-10-02.
Part: STRINGER — CRACKED (BS 2360)
MAIN DECK BS 2360 STR 14L STRINGER END FOUND CRACKED. MINOR CRACK TRIMMED OFF PER SRM 53-10-01 AND 51-10-02.
Part: SKIN — CORRODED (WS 807)
LEVEL 1 CORROSION FOUND ON UPPER SURFACE AT FRONT SPAR WS 807 WBL 584L. CORROSION REMOVED AND TREATED PER SRM 57-30-01, 51-10-01, 51-10-02 AND 57-30-01.
Part: SKIN — CORRODED (WS 614)
LEVEL 1 CORROSION LEFT HAD WING SURFACE AT WS 614 BETWEEN MID TO REAR SPAR AREA. CORROSION REMOVED AND TREATED PER SRM 57-30-01, 51-10-01 AND 51-10-02.
1998
Part: COMPRESSOR — STALLED (ENGINE)
ON TAKEOFF ROLL, A LOUD BANG OCCURRED AT SPEED OF 80 KNOTS. RETURNED TO BLOCKS. VISUAL INSPECTION OF ALL ENGINE INTAKES, AND EXHAUST PER MM 72-00-00, FOUND NOTHING. CHECKED EXTERIOR OF A/C AND FOUND NOTHING ABNORMAL. AIRCRAFT DEPARTED ON TIME.
Part: FRAME — DAMAGED (CARGO DOOR)
MAIN DECK CARGO DOOR FRAME LOWER FWD END IS DAMAGED. REPAIRED PER SRM 51-10-01 AND 51-30-02.
Part: SKIN — LOOSE (NR 1 PYLON)
NR 1 PYLON INBOARD AFT LOWER SKIN HAS LOOSE FASTENERS. FASTENERS REMOVED AND REPAIRED PER SRM 51-30-02.
Part: PANEL — DELAMINATED (LT WING)
LEFT WING FLYING PANEL HAS PROTECTIVE SEALANT PEELING. RESEALED PER SRM 51-21-03.
Part: RIVETS — SHEARED (NR 3 EXHAUST)
NR 3 ENGINE EXHAUST PLUG MOUNT BRACKET SHEARED RIVETS. REPLACED SHEARED RIVETS PER SRM 51-30-02.
Part: COWL — BROKEN (NR 3 ENGINE)
NR 3 ENGINE OUTBOARD POWER COWL RIB ANGLE BROKEN. REPAIRED PER SRM 51-30-02.
Part: CHAFE STRIP — CRACKED (NR 2 ENG COWL)
NR 2 ENG CORE COWL CHAFE STRIP DAMAGED/CRACKED. REPAIRED PER SRM 51-30-02.
Part: SKIN — LOOSE (NR 2 PYLON)
NR 2 PYLON INBOARD SIDE HAS MANY LOOSE FASTENERS. REMOVED AND REPLACED PER SRM 51-30-02.
Part: SKIN — LOOSE (NR 2 PYLON)
NR 2 ENGINE PYLON, EXTERNAL SKIN, LOOSE AND WORKING FASTENERS. REPAIRED PER SRM 51-30-02.
Part: SLEEVE — GOUGED (NR 1 FAN)
NR 1 FAN REVERSER SLEEVE ASSY. AFT INBOARD SIDE HAS GOUGE. REPAIRED PER SRM 51-24-11.
Part: RIVETS — SHEARED (RT MLG HINGE PIN)
RIGHT BODY GEAR STEERING HINGE PIN BRACKET HAS SHEARED RIVETS. REMOVED AND REPLACED RIVETS PER SRM 51-30-02.
Part: ANGLE — CRACKED (CARGO DOOR)
LOWER FORWARD CORNER OF MAIN DECK CARGO DOOR HAS CRACKED T ANGLE. REPAIRED PER SRM 51-10-01.
Part: FLOOR — DELAMINATED (COCKPIT)
COCKPIT AREA, FLOOR PANEL UNDER F/E TABLE IS DELAMINATED. REPAIRED PER SRM 51-10-01 AND SRM 51-10-02.
Part: COWL — CRACKED (NR 3 ENGINE)
NR 3 ENGINE INBOARD CORE COWL HINGE BRACKET HAS CRACKED MOUNT. REPAIRED PER SRM 51-30-02.
Part: BRACE — CHAFED (NR 2 ENG PYLON)
NR 2 ENGINE PYLON DIAGONAL BRACE FORWARD LOWER END HAS CHAFE MARKS. BLENDED PER SRM 54-40-01 FIG 3. TREATED/PAINT PER SRM 51-10-02.
Part: SKIN — LOOSE (NR 1 PYLON)
NR 1 PYLON OUTBOARD AFT LOWER SKIN HAS LOOSE FASTENERS. REMOVED AND REPLACED FASTENERS PER 51-30-20.
Part: COWL — CRACKED (NR 2 ENGINE)
NR 2 INBOARD POWER COWL PREVIOUS REPAIR CRACKED. REPAIRED PER SRM 51-10-01.
Part: FIRE DET PANEL — SPARKING (COCKPIT)
AFTER ENGINE START WHEN POWER WAS TRANSFERRED TO AIRCRAFT POWER AN ACRID SMELL WAS NOTICED IN COCKPIT. SPARKS WERE SEEN COMING FORM FIRE DETECTION PANEL BEHIND P6 PANEL. REPLACED CARD INDEX PANEL PER M/M 26-11-05 AND OPERATIONAL CHECKED PER M/M 26-11-00.
Part: FOREFLAP — DAMAGED (RT TE FLAP)
ON POST FLT WALKAROUND, FOUND APPROX 13 FT OF OUTBD FOREFLAP MISSING FROM RIGHT SIDE OF AIRCRAFT. REPAIRED BY BOEING PER WORK DOCUMENT NR 6-117-RE-706.
Part: INU — FAILED (COCKPIT)
AFTER TAKEOFF, NR 2 INS WARNING LIGHT ILLUMINATED WITH THE FOLLOWING CODES 34, 42, 102 AND 56. REPLACED NR 2 INU SYSTEM ALIGNED TO 05, OK NO FAULT PER M/M 34-41-03.
Part: CONNECTOR — CONTAMINATED (NR 1 ENGINE)
DURING CLIMB AT APPROX 37,000 FT, NR 1 ENG FLAMED OUT. AFTER SEVERAL ATTEMPTS AT A RESTART THE ENGINE LIT OFF AND FLAMED OUT AGAIN. ENGINE FIREWALL PLUG DOO14J FOUND CONTAMINATED. CLEANED PLUG AND RESEATED PIN NR 17. ELECTRICALLY CHECKED OUT PER WDM 76-11-11.
Part: PANEL — LOOSE (LT WING)
L/W FLYING PANEL Z572 I/B BRACKET, O/B FASTENER HOLE DRILLED OVERSIZED FITTING. FITTING REPLACED IAW 51-10-01, HFEC CHECK OK.
Part: PANEL — SPLIT (NR 4 SPOILER)
NR 4 SPOILER PANEL, T/E HAS SPLIT IN REPAIR. CLEANED DAMAGED AREA APPLIED FILLER, BONDED CURED SANDED SMOOTH IAW SRM 51-40-06.
Part: PANEL — DELAMINATED (NR 11 SPOILER)
NR 11 SPOILER PANEL, UPPER SURFACE DELAMINATED. REMOVED DAMAGED AREA, APPLIED FILLER AND DOUBLED IAW SRM 51-40-06.
Part: FASTENERS — MISINSTALLED (LT TE MID FLAP)
LEFT WING INBOARD TRAILING EDGE MIDFLAP HAS BLIND FASTENER INSTALLED IN STRESS PANEL. REMOVED AND REPAIRED FASTENER IAW SRM 51-30-02.
Part: PANEL — DELAMINATED (NR 6 SPOILER)
R/W PANEL FORWARD OF NR 6 SPOILER DELAMINATED. REPAIRED PANEL IAW SRM 51-40-15.
Part: PANEL — DELAMINATED (NR 6 SPOILER)
NR 6 SPOILER PANEL DELAMINATED AT I/B AND O/B EDGE BAND. REMOVED DELAMINATION UPPER SKIN, FABRICATED AND BONDED REPAIR SKIN AND DOUBLER IAW SRM 51-40-06.
Part: FUEL LINE — LOOSE (NR 1 PYLON)
FUEL LINE LOOSE ON NR 1 PYLON BULKHEAD AFT UPPER BLOW OUT PANEL. RE-TORQUED B-NUTS IAW MM 20-11-05.
Part: FASTENERS — MISSING (LT TE MIDFLAP)
L/W O/B T/E MIDFLAP FOUND MISSING FASTENERS. REPLACED MISSING FASTENERS IAW SRM 51-30-02.
Part: R-RAIL — CRACKED (NR 3 ENGINE)
NR 3 ENGINE R RAIL AT 60 DEGREE POSITION LIGHTENING HOLE OD RADIAL CRACK. WELDED IAW PWA 72-53-01 REPAIR NR 14.
Part: SUPPORT — BROKEN (BS 1820)
AFT CARGO BS 1820 LT SIDE WALL BROKEN SUPPORT. REPAIRED IAW SRM 51-30-02.
Part: SKIN — GOUGED (LT TE FOREFLAP)
GOUGE IN L/W I/B T/E FOREFLAP IN LOWER SURFACE. REPARIED FOREFLAP BY USING FIBERGLASS OVERLAYS IAW SRM 51-40-09.
Part: SKIN — CORRODED (LT TE FOREFLAP)
LEVEL 1 CORROSION FOUND ON L/W O/B T/E FOREFLAP SURFACE. REMOVED CORROSION AND TREATED IAW SRM 51-10-06.
Part: FLYING PANEL — LOOSE (LT WING)
L/W FLYING PANEL INCOMPLETE FASTENERS INSTALLATION. REMOVED AND REPLACED FASTENERS IAW ARM 51-30-02.
Part: PANEL — DAMAGED (FUSELAGE)
HOLE FOUND IN PANEL 191B. REPAIRED PUNCTURE WITH FIBERGLASS OVERLAYS IAW 747 SRM 51-40-14.
Part: FLYING PANEL — LOOSE (RT WING)
R/W FLYING PANEL O/B DOUBLER ATTACH POINT WORKING FASTENERS. REPAIRED IAW SRM 51-40-14.
Part: FASTENERS — WORKING (RT WING)
RT WING FLYING PANEL OUTBD ATTACH POINT HAS WORKING FASTENERS. REPAIRED DAMAGED FASTENER HOLES WITH POTTING COMPOUND AND FIBERGLASS OVERLAYS IAW SRM 51-40-14.
1997
Part: PANEL — DISBONDED (LT TE FLAP)
ON WALKARROUND INSPECTION, FOUND 8 X 14 DELAMINATION ON LEFT INBOARD MID FLAP LOWER STRESS PANEL. REPLACED PANEL PER BOEING SRM 51-10-01.
Part: CANOE — DAMAGED (TE FLAPS)
DAMAGED NR 8 CANOE, BOTTOM SIDE DEPRESSED. REPAIRED PER SRM 51-40-07 AND MM 27-51-45.
Part: ACTUATOR — BROKEN (LT MLG TILT)
BROKEN LEFT WING LANDING GEAR TILT ACTUATOR END FITTING. REMOVED AND REPLACED TILT ACTUATOR PER BOEING M/M 32-11-20.
Part: ANTI-SKID MODULE — CRACKED (RT MLG)
CRACKED RIGHT BODY GEAR ANTI-SKID MODULE FOUND ON CREW PREFLIGHT. REPLACED MODULE PER BOEING MAINTENANCE MANUAL 32-42-02.
Part: FRAME — CRACKED (NR 3 PYLON)
NR 3 PYLON - AFT MOUNT FRAME AFT OUTBOARD WEB CRACKED PAST PREVIOUS STOP DRILL. REPAIRED PER BOEING SERVICE BULLETIN 747-54-2065 R-6.
Part: BULKHEAD CHORD — CRACKED (FUSELAGE)
FIVE CRACKS IN THE NOSE LANDING GEAR CANTED BULKHEAD OUTER CHORDS. PERFORMED PERMANENT REPAIR OF THE BULKHEAD CHORDS PER MAE ENGINEERING AUTHORIZATION 47-5316-15-A0292.
Part: FRAME — ELONGATED HOLES (CARGO DOORWAY)
ELONGATED HOLES IN BS 1900 FRAME FOR AFT CARGO DOOR AFT ROTARY ACTUATOR MOUNTING BOLT HOLES. INSTALLED FREEZE PLUG PER BOEING SRM 51-10-08 AND ENGINEERING AUTHORIZATION 47-5310-A0289.
Part: TURBINE CASE — CRACKED (NR 3 ENGINE)
CRACK AT 90Ã POSITION R RAIL NR 3 ENGINE, RADIUS CRACK TRAVELING TO CASE OUTSIDE DIAMETER. REPAIRED PER PW M/M 72-53-01 REPAIR 14.
Part: TURBINE CASE — CRACKED (NR 4 ENGINE)
CRACKED R RAIL NR 4 ENGINE AT 300Ã POSITION, RADIUS CRACK TRAVELING TO OUTSIDE DIAMETER. REPAIRED PER PW M/M 72-53-01 REPAIR NR 14.
Part: TURBINE CASE — CRACKED (NR 2 ENGINE)
CRACKED S RAIL NR 2 ENGINE AT 300Ã POSITION, RADIUS CRACK TRAVELING TO FILLER RADIUS, CRACK CONTAINED. REPAIRED PER PW M/M 72-53-01 REPAIR 14.
Part: SKIN — DELAMINATED (RT ELEVATOR)
DELAMINATION RIGHT INBOARD ELEVATOR LOWER SIDE. REPAIRED PER BOEING SRM 51-40- 15.
Part: PANEL — DELAMINATED (LT HORIZ STAB)
DELAMINATED PANEL LEFT HORIZONTAL STABILIZER, PANEL NUMBER 334GBL. REPAIRED PER BOEING SRM 51-40-09.
Part: PANEL — HOLE (LT WING)
LT UPPER WING TIP PANEL HAS HOLE NEAR EDGE. REPAIRED PER BOEING SRM 51-40-09.
Part: SKIN — DELAMINATED (RT ELEVATOR)
RT INBOARD ELEVATOR OUTBOARD END OF LOWER SURFACE DELAMINATED. REPAIRED PER BOEING SRM 51-40-15.
Part: SKIN — DELAMINATED (RT AILERON)
RT INBOARD AILERON TRAILING EDGE SEPARATED AT OUTBOARD EDGE.
Part: BLKHD SHROUD — DELAMINATED (BS 2360)
APU DUCT SHROUD AT BS 2360 AFT PRESS BULKHEAD IS DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.
Part: PANEL DOOR — DELAMINATED (NR 3 PYLON)
NR 3 PYLON 473 CL PANEL DOOR DELAMINATED. REPAIRED PER BOEING SRM 51-40-06.
Part: SKIN — DAMAGED (LT TE MID FLAP)
LT INBOARD TRAILING EDGE MIDFLAP INBD CORNER HAS SEVERAL SMALL HOLES. REPAIRED PER BOEING SRM 51-40-09.
Part: SKIN — DELAMINATED (LT ELEVATOR)
LT INBOARD ELEVATOR TRAILING EDGE DELAMINATED 24 INCHES INBOARD. REPAIRED PER BOEING SRM 51-40-15.
Part: ANGLE — CRACKED (WS 470)
CRACKED WING LEADING EDGE STIFFENER WEB AT NR 18 LEADING EDGE DEVICE. REPAIRED PER BOEING SRM 51-30-02.
Part: SKIN — DELAMINATED (RT ELEVATOR)
RT INBOARD ELEVATOR LOWER SURFACE DELAMINATED 30 INCHES IN FROM INBOARD END. REPAIRED PER BOEING SRM 51-40-15.
Part: SKIN — DAMAGED (BS 1940)
BS 1940 S48 TO S47 R SKIN CREASED. FILLER AND DOUBLER INSTALLED PER BOEING SRM 53-30-03.
Part: SKIN — CRACKED (BS 1980)
GROUND DAMAGE FOUND ON BOTTOM OF FUSELAGE AREA BELOW REAR CARGO DOOR BS 1980 BETWEEN S46R TO S50L, DEEPEST GOUGE APPROXIMATELY .025 AT S49R WHERE CRACK IN SKIN DETECTED BY HFEC CHECK. REPAIRED CRACK PER BOEING SRM 53-30-03 FIGURE 1 BLENDED GOUGES PER 51-10-01.
Part: BULL NOSE — MISSING (NR 6 LE FLAP)
ON POST FLIGHT, FOUND NR 6 LEADING EDGE FLAP BULL NOSE MISSING. AIRCRAFT DISPATCHED PER CDL 27-81-3. BULL NOSE TO BE REPLACED.
Part: FUEL CONTROL — FAILED (NR 2 ENGINE)
DURING CRUISE FLIGHT, NR 2 ENGINE STALLED. ALL INDICATIONS SHOWED THRUST LOSS. ATTEMPTED RESTART, ENGINE DID RELIGHT BUT DID NOT STABILIZE. ACCOMPLISHED ENGINE SHUT DOWN PROCEDURE. POSITIVE OIL PRESSURE AT ALL TIMES. FCU CYCLED 1 MIN EACH 30 MIN. REMOVED AND REPLACED FUEL CONTROL PER MAINTENANCE MANUAL 73-21-01. REPLACED FUEL PUMP PER MAINTENANCE MANUAL 73-11-01, PRECAUTIONARY. PERFORMED LEAK AND POWER RUNS PER MAINTENANCE MANUAL 71-00-00.
Part: SPAR CHORD — CRACKED (LT WING)
FRONT SPAR LOWER CHORD CRACKS AT FSSO 1440 AND 1425 RHS. REPAIRED PERMANENTLY BY REPLACING CRACKED CHORD SECTIONS WITH NEW CHORD SECTIONS AND SPLICE STRAPS AT FSSO 1395 RHS PER RS NR 57-21-33404.
Part: SPAR CHORD — CRACKED (LT WING)
FRONT SPAR LOWER CHORD CRACKS AT FSSO 1446 LHS. REPAIRED PERMANENTLY BY REPLACING CRACKED CHORD SECTION WITH NEW CHORD SECTION AND SPLICE STRAP AT FSSO 1425 LHS AS PER RS NR R-57-21-33403.
Part: TENSION TIE — CRACKED (BS 900)
CRACK IN MAIN DECK TENSION TIE FORWARD CHANNEL AT STA 900, LHS. TRIMMED OUT CRACK AND THE TRIM LINE WAS HFEC INSPECTED TO ENSURE NO OTHER DISCREPANCIES EXIST. ACTION CARRIED OUT PER RS NR R-53-15-33394.
Part: SKIN — CORRODED (BS 1720)
LEVEL 2, CORROSION AT BS 1720 AFTER EDGE OF MED NR 4 CUTOUT, AT TWO LOCATIONS, S-18R AND S-19R AND AT S-22R. TRIMMED OUT DAMAGED SKIN AND INSTALLED FILLER AND EXTERNAL DOUBLERS PER RS NR R53-11-33400, R-53-11-33399.
Part: STRINGER — CORRODED (BS 1860)
LEVEL 2, STRINGER 44 HEAVILY CORRODED AT STA 1860, STA 1900 AND STA 1920. ALSO, CORROSION AREA HAD BEEN CRACKED THROUGH THE STRINGER. CORROSION REMOVED, 2 STRINGER SECTIONS ARE TO BE SPLICED IN AT BS 1850 AND BS 1910, USING HALF CHANNEL SPLICE AND STRAP AT EACH SPLICE LOCATION PER RS NR R-53-61-33414.
Part: STRINGER — CORRODED (BS 1880-1890)
LEVEL 2, AFT CARGO STR 48R FOUND CORRODED AT BS 1880 TO 1890. REPAIRED STRINGER AT BS 1870 TO BS 1890 PER BOEING SRM 53-10-03.
Part: BULKHEAD WEB — CORRODED (BS 1245)
LEVEL 2, LT WLG W/W CANTED BULHEAD WEB BULGED UP AT BS 1245, LBL 10. TRIMMED WEB BONDSKIN AREA 4 BY 6 AND DOUBLER REPAIRED PER BOEING SRM 51-40-02.
Part: SEAT TRACK — CORRODED (BS 520-550)
LEVEL 2, U/D SEAT TRACK FOUND DAMAGE AT BS 520 TO BS 550 LBL 65. REPLACED SEAT TRACK AT BS 530 EXISTING SPLICE TO BS 560 PER BOEING SRM 53-10-05.
Part: SUPPORT — CORRODED (BS 1468)
LEVEL 2, FX KEEL BEAM BOX LWR ACCESS PANEL SUPPORT BEAM FOUND CORRODED ON BS 1468 LBL 14 TO RBL 14. REPLACED SUPPORT BEAM PER BOEING SRM 51-10-01, (P/N 65B14058-1).
Part: SEAT TRACK — CORRODED (BS 530-550)
LEVEL 2, U/D BS 530 TO BS 550 LBL 65 SEAT TRACK CORRODED ON FLANGE AREA. REPLACED SEAT TRACK AT BS 530 EXISTING SPLICE TO BS 560 PER BOEING SRM 53-10-05.
Part: STRUT — CHAFED (RT MLG)
RT WING LANDING GEAR SHOCK STRUT INNER CYLINDER O/B BRAKE EQUALIZING ROD ATTACH LUG DEEP CHAFE MARK. REF BOEING TELEX PAO-HKG-97-0008RE, 0011RE LOCAL BLENDING C/O, NDT INSPECTED SHOT PEENING AND STYLUS CADIUM PLATED. THE CYLINDER AND BRAKE ROD REQ OVERHAUL WITHIN 6 MONTHS OR 1000 CYCLES.
Part: SKIN — WORN (BS 520-526)
SKIN LAP BS 520 TO BS 526 S12L EXISTING COUNTERSUNK HOLES OVERSIZED. REPAIRED SKIN LAP AT BS 520 TO BS 526 PER BOEING SRM 53-30-03.
Part: FITTING — CRACKED (NR 5 SPOILER ACT)
LHW NR 5 SPOILER ACTUATOR MOUNT FTG FOUND CRACKED AT I/B LWR SECTION LENGTH 1.5 INCHES LONG. REPLACED FITTING (P/N 65B08099-) PER DWG 65B08099.
Part: ANGLE — DELAMINATED (NR 4 PYLON)
NR 4 PYLON FWD ENG MOUNT BHD CHAFE MARK FOUND ON I/B RADIUS ANGLE LWR SECTION. ORIGINAL THICKNESS 0.059 REMAIN 0.046 REF BOEING TELEX PAO - HKG- 97 - 0014RE FOR REPAIR.
Part: STRINGER — CRACKED (BS 1330-1350)
M/D BS 1346 S10L STRINGER END AREA FOUND CRACKED .75 INCH LONG. REPAIRED STRINGER BETWEEN BS 1330 TO BS 1350 PER BOEING SRM 53-10-03.
Part: CHANNEL — CRACKED (BS 800)
M/D TENSION TIE AT BS 800 LT SIDE FOUND CHANNEL CRACKED .0625. REPAIRED TENSION TIE PER SB 747-53-2371.
Part: LOWER GATE — CORRODED (L4 DOOR)
LEVEL 2, L4 DOOR LOWER GATE SEVERE CORROSION FOUND. REMOVED CORROSION PER BOEING SRM 51-10-01 AND REPROTECTED PER BOEING SRM 51-10-02. TOUCH UP PAINT PER MM 51-24-11.
Part: UPPER GATE — CRACKED (L3 DOOR)
CRACKED REVEALED AT L3 DOOR UPPER GATE (2 EA). REINSTALLED RIVETS PER BOEING SRM 51-30-02, REMOVED AND REPLACED L3 DOOR UPPER GATE PER MM 52-11-07.
Part: TIE DOWN TRACK — CORRODED (BS 1090-1210)
LEVEL 2, M/D TIE DOWN TRACK AT BS 1100 RBL 75 FOUND CRACK 4 INCHES LONG. REPLACED TIE DOWN TRACK BETWEEN BS 1090 TO BS 1210 PER BOEING SRM 53-10-05.
Part: SKIN — CORRODED (R4 DOORWAY)
LEVEL 2, CABIN R4 DOOR AFT CUTOUT SKIN CORRODED SPOTS AT 2 LOCATIONS, REF BOEING TELEX PAO-HKG-97-0005RE AND 0006RE FOR REPAIR.
Part: SPAR — CRACKED (LT WING)
LHW FRONT SPAR LOWER CHORD CRACK FOUND 9 INCHES LONG AT OLES 1440, REF BOEING PAO-HKG-97-0021RE FOR REPAIR.
Part: SPAR — CRACKED (RT WING)
RHW FRONT SPAR LWR CHORD CRACK FOUND 2 INCH LONG AT OLES 1430, REF BOEING PAO-HKG-97-0021RE FOR REPAIR.
Part: SKIN — CORRODED (WS 966-976)
LEVEL 2, RHW LOWER SKIN AT WS 966 TO WS 976 AT REAR SPAR EXTENSION CORROSION FOUND EXCEEDS BOEING SRM 57-30-01 AFTER BLENDING. REF BOEING TELEX PAO-HKG-97-0015TE FOR REPAIR.
Part: TRUNNION — CRACKED (NLG)
NOSE LANDING GEAR LT TRUNNION FTG CRACKED ABOUT 2 INCHES LONG REVEALED AT AFT ATTACH FLANGE. REPLACED TRUNNION FTG (P/N 65B10081-7) PER DWG 65B10081.
Part: BRACE — DELAMINATED (NR 3 PYLON)
NR 3 PYLON DIAGONAL BRACE AFT SECTION DEEP CHAFE MARK FOUND EXCEED SRM 54-40-01, REF BOEING TELEX PAO-HKG-97-0009RE FOR REPAIR.
Part: PANEL — CRACKED (RT SPOILER)
A .5 INCH CRACK REVEALED ON ACTUATOR ATTACH HINGE FITTING I/B FILLET AREA. REPLACED NR 9 SPOILER PANEL PER MM 27-61-02.
Part: FLOORBEAM — CORRODED (BS 480)
LEVEL 2, U/D BS 480 RBL 42 RBL 65 FLOORBEAM FOUND CORRODED. REPAIRED FLOORBEAM AT RBL 36 TO RBL 56 PER BOEING SRM 53-10-07. ALSO BLENDED OUT AND REPROTECTED AT RBL 56 TO RBL 65 PER BOEING SRM 51-10-01.
Part: TENSION TIE — CRACKED (BS 900)
CABIN, TENSION TIE AT BS 900 LT SIDE CRACKED .125 INCH LONG, REF BOEING TELEX PAO-HKG-97-0010RE REPAIR SCHEME.
Part: SKIN — CORRODED (BS 741-1000)
LEVEL 1 CORROSION, M/D SKIN LAP FAYING EDGE BS 741 TO 1000, STR R12. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: PANEL — CRACKED (RT SPOILER)
2 CRACKS REVEALED ON LOWER SURFACE ACTUATOR ATTACH FITTING O/B AREA. REPLACED NR 7 SPOILER PANEL PER MM 27-62-01.
Part: BRACKET — BROKEN (BS 840)
M/D BS 840 BARRIER NET LT MOST O/B VERT SUPPORT TOP ATT BRACKET BROKEN. REPLACED PER BOEING SRM 51-10-07.
Part: SKIN — CRACKED (BS 820-840)
BS 820 TO 840 S12L SKIN LAP JOINT TOP ROW FASTENER HOLES FOUND (2 EA) CRACKED. REPAIRED SKIN LAP JOINT AT BS 820 TO BS 840 SILL PER BOEING SRM 53-30-03.
Part: SKIN — MISDRILLED (BS 860-880)
U/D SKIN LAP JOINT BETWEEN BS 880 TO BS 860 FOUND MANY FASTENER HOLES FOUND INSUFFICIENT EDGE MARGIN AT S12L TOP ROW. REPAIRED SKIN LAP BETWEEN BS 880 TO BS 960 PER BOEING SRM 53-30-03.
Part: BLKHD STIFFENER — SHEARED RIVITS (NR 4 PYLON)
EIGHTEEN RIVETS SHEARED ON NR 4 PYLON AFT BULKHEAD STIFFENER AT NACELLE STATION 268.4 NACELLE WATER LINE 153.6. NEW RIVETS INSTALLED AND DETAILED INSPECTION WAS PERFORMED AT AFT BULKHEAD SUPPORTING STRUCTURE. NO OTHER DAMAGE FOUND. NOTE: PYLON MODIFICATION PER 54A2159 COMPLETED IN JANUARY 1996 AT 53048 HOURS AND 18684 CYCLES.
Part: RIB — CRACKED (WS 852)
RT WING L/E CAVITY AT STA 852.45 SUPPORT RIB AFT END UPPER POSITION CRACKED. REPAIRED PER BOEING SRM 57-20-03.
Part: FLOOR PANEL — SPONGY (BS 520-600)
U/D BS 520 TO 600 MOST LT O/B FLOOR PNL FOUND SPONGY. REPLACED/REINSTALLED SVC TAG NR 2042412.
Part: AIR INLET — CRACKED (NR 2 PACK)
NR 2 AIR COND RAM AIR INLET AFT DOOR FOUND CRACKED AFTER HINGE REMOVED. REPLACED AIR INLET AFT DOOR ASSY PER MM 21-62-02.
Part: FLOOR PANEL — SPONGY (BS 520-580)
U/D FLOOR PNL FOUND SPONGY BET BS 520 TO 580 LBL 40 TO 65 IPC 53-21-17-01. REPLACED/REINSTALLED SVC TAG NT 2042488.
Part: RIVETS — SHEARED (NR 4 PYLON)
NR 4 PYLON TORQUE B/HEAD STIFFENER RIVETS FOUND SHEARED. REPLACED AND DETAILED INSP AT SURROUNDING STRUCTURE CARRIED OUT NIL FURTHER DAMAGE FOUND, REF NR 867322.
Part: SKIN — DENTED (BS 1790)
FX EXT SKIN FOUND DENT MARKS AT BS 1790 S43L TO 44L AND S38L AREA. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: STRINGER — CRACKED (BS 2184-2186)
AFT OF BULK CARGO COMPT BS 2184 TO 2186 STR 38L STRINGER SPLICE FOUND CRACKED. REPLACED PER BOEING SRM 51-10-01.
Part: FAIRING — CRACKED (NR 4 PYLON)
NR 4 PYLON TO WING GLOVE FAIRING FOUND CRACKED AND TORN. REPAIRED CARRIED OUT IAW SRM 51-40-15, REF NR 860341.
Part: TIE DOWN TRACK — CRACKED (BS 650-660)
FWD CARGO TIE DOWN TRACK CRACKED AT BS 650 TO BS 660 RBL 44. REPLACED TIE DOWN TRACK AT BS 640 TO BS 700 PER BOEING SRM 53-10-05.
Part: FITTING — CORRODED (MLG DOOR ACT)
LEVEL 2, LT WING LANDING GEAR DOOR ACTUATOR SUPPORT FITTING CORRODED AT FORWARD LOWER WEB. REPLACED CORRODED FITTINGS PER BOEING SRM 51-10-01.
Part: FLOOR PANEL — DAMAGED (BS 520-540)
U/D BS 520 TO 540 MID FLOOR PNL DAMAGE. REPLACED/REINSTALLED PER SV TAG NR 2042488.
Part: FAIRING — CRACKED (FUSELAGE)
FX - BODY FAIRING 193F FOUND CRACKED. FIBERGLASS REPAIR PER BOEING SRM 51-40-14, FIG 9.
Part: BULKHEAD — CORRODED (BS 1241)
LEVEL 1 CORROSION, M/D CANTED PRESSURE BULKHEAD TO WING CTR SECTION TOP SKIN JOINT WITH ATTACHMENT FTG REMOVED BS 1241, LBL L11. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SKIN — TORN (LT TE FORE FLAP)
LHW - I/B FORE FLAP O/B SURFACE PANEL UPPER AREA FOUND SKIN PORTION TORN OUT. REPAIRED, SKIN HOT BOND PER BOEING SRM 51-40-06.
Part: FITTING — CORRODED (NLG DOOR)
LEVEL 2 CORROSION NLG AFT DOOR HINGE FUSELAGE MOUNT FITTING TWO SERRATED PLATE. REPLACED PER CSN 7179.
Part: SKIN — MISDRILLED (BS 880-960)
U/D SKIN LAP BETWEEN BS 880 TO BS 960 TOP ROW FASTENER HOLES INSUFFICIENT EDGE MARGIN BETWEEN HOLES AT S-12L. SKIN REPAIRED PER BOEING SRM 53-30-03. SRWS S/N 911821 FOR RELATED WORKS.
Part: SKIN — CORRODED (FUSELAGE)
LEVEL 1 - FUS SKIN LAP CORRODED ALONG PAYING SURFACE OF SKIN JOINT WITH SKIN LIFTED UP PER SB 53-2307. CORROSION REMOVED PER BOEING SRM 51-10-01 AND REPROTECTED PER SRM 51-10-02., MM 51-24-11.
Part: DUCT — CHAFING (NR 3 PYLON)
NR 3 PYLON PNEUMATIC T-DUCT CHAFING AGAINST THE MAIN FUEL SUPPLY LINE JUST FORWARD OF WING FRONT SPAR. THE SAME T-DUCT WAS ALSO CHAFING AGAINST THE ELECTRICAL WIRING LOOM COVER. REPLACED FUEL LINE AND ADJUSTED THE ELECTRICAL WIRING LOOM COVER. REPOSITIONED THE MAIN PNEUMATIC DUCTING, INCLUDING THE T-DUCT, TO OBTAIN ENOUGH CLEARANCE BETWEEN THE DUCT AND THE FUEL SUPPLY LINE. REFERENCE MAINTENANCE MANUAL 54-10-01. PYLON MODIFICATION COMPLETED JANUARY 96, AT 53048 HOURS AND 18684 CYCLES.
Part: SKIN — DELAMINATED (BS 910/918/928)
U/D SKIN LAP BELT STA 910, STA 918, STA 928 INNER SKIN AT S-12L. TRIMMED OFF AT SEVERAL PLACES ADJACENT TO TOP ROW FASTENER HOLES. REPAIRED PER BOEING SRM 53-30-03, S/N 911821.
Part: DOOR — DENTED (APU COMPT)
APU LT ACCESS DOOR DENT MARKS. SMOOTHED OUT PER BOEING SRM 51-10-01 AND REPROTECTED PER SRM 51-10-02 PAINT TOUCH UP PER MM 51-24-11.
Part: HINGE FITTING — CORRODED (NLG DOOR)
LEVEL 1 NLG AFT DOOR ALL 4 HINGE FITTING SURFACE REVEALED CORROSION. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: BRACKET — DELAMINATED (CARGO DOOR)
M/D SIDE CARGO DOOR BRACKET FOUND DAMAGED AT STA 1900 LWR AFT NR 2. REPLACED BRACKET PER BOEING SRM 51-10-01.
Part: SLOPE PANEL — DELAMINATED (FUSELAGE)
LT REAR W/W CUTOUT SLOPE PNL, DEFORMED AS MARKED, PNL BELOW TRUNNION FITTING. REFORMED SLOPE PNL PER BOEING SRM 51-40-01.
Part: FAIRING — DELAMINATED (FUSELAGE)
RT REAR W/W CUTOUT SLOPE FAIRING DAMAGED AND DEFORMED. SMOOTHED OUT SLOPE FAIRING PER BOEING SRM 51-10-01 AND REPROTECTED PER SRM 51-10-01 AND REFORMED PER SRM 51-40-00.
Part: PANEL — DELAMINATED (NLG WW CUTOUT)
NLG LT REAR W/W CUTOUT PNL DEFORMED PNL BELOW TRUNNION FITTING. REFORMED NLG LT REAR PER BOEING SRM 51-40-01.
Part: FITTING — CORRODED (BS 480)
LEVEL 1 CORROSION, M/D TIE DOWN FITTING FLANGE, BS 480, LBL L11. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-0, TREATED PER 51-10-02 AND MM 51-24-11.
Part: FLOOR BEAM — CORRODED (BS 2140)
LEVEL 1 CORROSION, M/D LT BS 2140, WL 200, LBL 75, FLOORBEAM UPPER CHORD. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SEAT TRACK — CORRODED (BS 520)
LEVEL 2, U/D BS 480 TO BS 520 RBL 46.5 SEAT TRACK FOUND HEAVILY CORRODED. REPLACED SEAT TRACK AT BS 480 EXISTING SPLICE TO BS 529 EXISTING SPLICE PER BOEING SRM 51-10-01.
Part: WEB — DAMAGED (LT TE MID FLAP)
LHW-O/B MIDFLAP MOST O/B FORE FLAP TRACK POSITION I/B WEB FOUND PREVIOUS REPAIRED AREA DAMAGED. REPARIED PER BOEING SRM 51-40-03.
Part: WEB — CRACKED (LT TE MID FLAP)
LHW-O/B MIDFLAP MOST O/B FORE FLAP TRACK POSITION, I/B WEB I/B ATT ANGLE CRACKED. REPLACED PER BOEING SRM 51-10-01.
Part: WEB — CRACKED (LT TE FORE FLAP)
LHW-I/B FORE FLAP I/B ACCESS PNL AFTER REMOVAL FOUND RT ATT WEB CRACKED. REPAIRED PER BOEING SRM 51-10-01.
Part: TIE DOWN FTG — CORRODED (BS 420)
LEVEL 2 - M/D BS 420 LBL 17 TIE DOWN FITTING FOUND CORRODED/CRACKED. REPLACED AND INSTALLED WITH SCREWS AS PER MM 20-51-01 AND SVC TAG NR FF 008407.
Part: TIE DOWN FTG — CORRODED (BS 480)
LEVEL 1 - M/D TIE DOWN FITTING FOUND CORRODED AT BS 480 LBL 35. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01, 51-10-02.
Part: WEB — CRACKED (LT TE FORE FLAP)
LHW-I/B FORE FLAP MOST I/B ACCESS PNL I/B SUPPORT WEB CRACKED AT UPPER EDGE POSITION. REPLACED PER BOEING SRM 51-10-01.
Part: SEAT TRACK — CORRODED (BS 530-600)
LEVEL 2, U/D BS 530 TO BS 590 RBL 65 SEAT TRACK CROWN FOUND CORRODED. REPLACED SEAT TRACK BETWEEN BS 530 TO BS 600 PER BOEING SRM 53-10-05.
Part: FITTING — CORRODED (BS 500)
LEVEL 1 CORROSION, M/D TIE DOWN FITTING, BS 500, RBL R11 TO L11. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: INTERCOSTAL — CRACKED (BS 420)
M/D-BS 420 LBL 55 BELOW FLOOR PNL INTERCOASTAL WEB FOUND CRACKED. REPLACED PER BOEING SRM 51-10-01.
Part: SEAT TRACK — CORRODED (BS 530-710)
LEVEL 2, U/D BS 530 TO BS 710 RBL 46 SEAT TRACK CORRODED. REPLACED SEAT TRACK BETWEEN BS 530 TO BS 710 PER BOEING SRM 53-10-05.
Part: SEAT TRACK — CORRODED (BS 440-450)
LEVEL 1 CORROSION, M/D SEAT TRACK BS 440 TO 450, WL 200, RBL R92 TO R94. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SEAT TRACK — CORRODED (BS 498-520)
LEVEL 2, U/D BS 498 TO BS 520 LBL 65 SEAT TRACK FLANGE CORRODED. REPLACED SEAT TRACK AT BS 480 EXISTING SPLICE TO BS 529 EXISTING SPLICE PER BOEING SRM 51-10-01.
Part: FLOORBEAM — CORRODED (BS 460)
LEVEL 1 CORROSION, M/D FLOORBEAM, BS 460, LBL L80. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: FLOORBEAM — CORRODED (BS 2240)
LEVEL 1 CORROSION, M/D FLOORBEAM UPPER CHORD, BS 2240, WL 200, LBL L82. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: TIE DOWN FTG — CORRODED (BS 440)
LEVEL 1 - M/D TIE DOWN FITTING FOUND CORRODED AT BS 440 LBL 45. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01, 51-10-07.
Part: SEAT TRACK — CORRODED (BS 450)
LEVEL 1 CORROSION, M/D TIE DOWN TRACK FLANGE, BS 450, RBL R82. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: FLOORBEAM — CORRODED (BS 460)
LEVEL 1 CORROSION, M/D BS 460, LBL 40 TO 60 FLOORBEAM. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SEAT TRACK — CORRODED (BS 460)
LEVEL 1 CORROSION, M/D TIE DOWN TRACK FLANGE, BS 460, LBL L61. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SEAT TRACK — CORRODED (BS 460-485)
LEVEL 1 CORROSION, M/D TIE DOWN TRACK FLANGE, BS 460 TO 485, LBL L33. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SKIN — CORRODED (BS 520-741)
LEVEL 1 CORROSION, FX SKIN LAP BETWEEN BS 520 TO 741 S19R AT SURFACE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-0, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SEAT TRACK — CORRODED (BS 480-502)
LEVEL 2, U/D BS 480 TO BS 502 RBL 65 SEAT TRACK CORRODED. REPLACED SEAT TRACK AT BS 480 EXISTING SPLICE TO BS 529 EXISTING SPLICE PER BOEING SRM 51-10-01.
Part: TIE DOWN FTG — CORRODED (BS 460)
LEVEL 1 - M/D TIE DOWN FITTING AND FLANGE FOUND CORRODED AT BS 460 LBL 40. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01, 51-10-02.
Part: TIE DOWN — CORRODED (BS 2200)
LEVEL 1 CORROSION, M/D FLOORBEAM TIE DOWN PLATE, BS 2200, WL 200, LBL L80 TO L85. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: GUIDE FRAME — CRACKED (BS 1330)
M/D-BS 1330 CENTER GUIDE FRAME BODY FOUND CRACKED. REPLACED PER MM 25-58-00 SVC TAG NR FF002167.
Part: SEAT TRACK — CORRODED (BS 512)
LEVEL 1 CORROSION, M/D BS 512, LBL L11 TIE DOWN TRACK. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-0, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SEAT TRACK — CORRODED (BS 537)
LEVEL 1 CORROSION, M/D BS 537 RBL R10, SEAT TRACK FLANGE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 1043)
LEVEL 2 FX BS 1043 RBL 18 TO RBL 24 A/COND BAY ACCESS PANEL SUPPORT BEAM FOUND CORRODED. CORRODED SUPPORT REPAIRED PER BOEING SRM 53-50-04.
Part: SEAT TRACK — CORRODED (BS 2180)
LEVEL 1 CORROSION, M/D BS 2180, RBL 98 TIE DOWN TRACK SURFACE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: PANEL — DELAMINATED (NR 3 PYLON)
NR 3 PYLON ACCESS PANEL 472BL IS DEBONDED. REBONDED IAW BOEING SRM 51-40-06 REF TO CWS NR 834288.
Part: SEAT TRACK — CORRODED (BS 2250)
LEVEL 1 CORROSION, M/D SEAT TRACK UPPER SURFACE AT STA 2250, LBL 33. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SEAT TRACK — CORRODED (BS 512)
LEVEL 1 CORROSIO, M/D BS 512, RBL 11 TIE DOWN TRACK. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SEAT TIE DOWN — CORRODED (BS 440)
LEVEL 2 M/D BS 440 LBL 11-0 TIE DOWN FITTING FOUND CORRODED. CORROSION REMOVED PER BOEING SRM 51-10-01.
Part: FLOOR PANEL — DAMAGED (BS 460-480)
M/D-BS 460 TO 480 LBL 33 O/B FLOOR PNL DAMAGED. REPLACED/REINSTALLED PER BOEING SRM 51-10-01, SVC TAG NR 2042691.
Part: SUPPORT — CORRODED (BS 480)
LEVEL 1 CORROSION, M/D LADDER CUTOUT MOVEABLE PLATFORM SUPPORT BEAM, BS 480, RBL 50. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: FAIRING — DELAMINATED (RT WING)
RT WING NR 8 CANNON FAIRING FOUND DELAMINATION AT LWR MID PORTION. REPAIRED NR 8 CANNOE FAIRING FIBERGLASS AS PER BOEING SRM 51-40-15.
Part: LONGERON — CORRODED (BS 755)
LEVEL 1 CORROSION, FWD CARGO STR 35R AT STA 755. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-0, TREATED PER 51-10-02 AND MM 51-24-11.
Part: CASCADE WEB — CRACKED (NR 4 ENGINE)
NR 4 ENG 6R CASCADE WEB IS CRACKED. BLENDED OUT IAW MM 78-31-07, REF CWS NR 854171.
Part: SKIN — TORN (LT TE FORE FLAP)
LHW - I/B FLAP NR 2 FORE FLAP TRACK CUTOUT FOUND SURFACE TORN. FIBERGLASS REPAIR C/OUT PER BOEING SRM 51-40-15, FIG 7.
Part: SUPPORT — CORRODED (BS 1235)
LEVEL 2 FX BS 1235 LBL 69 RBL 69 A/COND BAY ACCESS PANEL SUPPORT BEAM LWR SURFACES FOUND CORRODED. REPAIRED SUPPORT PER BOEING SRM 51-40-04.
Part: BRACKET — CRACKED (RT WING)
RT WING T/E LWR ACCESS PNL 671AB I/B SUPPORT WEB ATT BRACKET CRACKED. REPAIRED BRACKET PER BOEING SRM 51-10-01.
Part: SEAL — DELAMINATED (NR 3 PYLON)
NR 3 PYLON SLOT SEAL IS SPLIT. REPLACED PER AMM 54-51-00.
Part: WEB — CRACKED (RT TE MID FLAP)
RHW - I/B MID FLAP O/B DEFLECTION ROLLER GUIDE TRACK ATT WEB CRACKED AT RIVET HOLE AREA. REPAIRED WEB PER BOEING SRM 51-40-02.
Part: SUPPORT — CORRODED (BS 2280)
LEVEL 1 CORROSION, M/D FLR SUPPORT HEAD SECTION, BS 2280, WL 200, RBL 22 TO 33. REMOVED CORROSION PER BOEING SRM 51-10-0, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BRACKET — CRACKED (RT WING)
RT WING T/E LWR ACCESS PNL 671AB MID SUPPORT AFT ATT BRACKET CRACKED. REPAIRED BRACKET PER BOEING SRM 51-10-01.
Part: FAIRING — DELAMINATED (RT WING)
RT WING NR 7 CANNOE FAIRING I/B LWR MID PORTION DENT MARK FOUND. REPAIRED FIBERGLASS PER BOEING SRM 51-40-15.
Part: SKIN — CRACKED (NR 3 PYLON)
NR 3 PYLON VALVE ACCESS PNL CUTOUT IS DEFORMED AND CRACKED. TRIMMED OFF PER BOEING SRM 51-10-01 REF NR 854302.
Part: SKIN — DELAMINATED (ACCESS DOOR)
FWD CARGO STN 470 LT ACCESS DOOR SKIN FOUND DELAMINATED. REPAIRED ACCESS DOOR PER BOEING SRM 51-40-15.
Part: BRACKET — CRACKED (WS 683)
RT WING AUX BEAM FWD FACE AT WS 683 (APPX) UPP LONG SUPPORT ATT BRACKED CRACKED. REPAIRED PER BOEING SRM 51-10-01.
Part: COWL — GOUGED (NR 2 ENGINE)
NR 2 ENG LT SIDE COWL FWD LWR CORNER IS BADLY GOUGED. TRIMMED OFF AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: COWL HINGE — CRACKED (NR 4 PYLON)
NR 4 PYLON FAN COWL HINGE SUPPORT RT AFT HINGE CUT OUT IS CRACKED. TRIMMED OFF IAW BOEING SRM 51-10-02 REF CWS NR 854169.
Part: COWL — CRACKED (NR 2 ENGINE)
NR 2 ENG RT SIDE COWL BREATHER AIR EXHAUST SHROUD IS CRACKED AND HOLED AT FLANGE AREA. REPAIRED CARRIED OUT SERV TAG S/N FF001948, REF NR 860128 FOR DETAILS.
Part: SUPPORT — CORRODED (CABIN)
LEVEL 1 M/D DIAGONAL FLOOR SUPPORT CORRODED. CORROSION REMOVED PER BOEING SRM 51-10-01.
Part: BULKHEAD ANGLE — CRACKED (BS 250-260)
LWR FX INTERIOR STA 250 TO 260 FWD BULKHEAD FWD FACE ATT VERT ANGLE. REPAIRED PER BOEING SRM 51-40-04.
Part: FLOORBEAM — CORRODED (BS 2360)
LEVEL 1 CORROSION, M/D FLOORBEAM UPPER AND LOWER SURFACES BS 2360, WL 200, BBL R70 TO L70. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: FAIRING — CRACKED (FUSELAGE)
FX - BODY FAIRING 291B EXT SKIN PREVIOUS REPAIRED AREA FOUND CRACKED. FIBERGLASS REPAIR PER BOEING SRM 51-40-15, FIG 7.
Part: SKIN — CORRODED (BS 2720)
LEVEL 1 CORROSION, AFT FUSELAGE RT SIDE SURFACE AT ELEVATOR INDEX PLATE BS 2720, RBL 30. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BRACKET — CRACKED (WS 685)
RT WING REAR SPAR AFT FACE AT WS 685 (APPX) UPP LONG SUPPORT ATT BRACKET CRACKED. REPAIRED PER SRM 51-10-01.
Part: SUPPORT — CORRODED (BS 2230)
LEVEL 1 CORROSION, M/D FLOOR SUPPORT PLATE, BS 2320, WL 200, LBL 72. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BLOWOUT PANEL — DELAMINATED (BS 600-640)
DELAMINATION FWD CARGO LT SIDEWALL BLOWOUT PNL, SKIN FOUND TEAR/LIFT UP AT STA 600 TO 640. REPLACED PER MM 25-52-05.
Part: SKIN — DELAMINATED (AFT TE FLAP)
RT WING O/B AFT FLAP L/E PORTION DELAMINATED. REPAIRED PER BOEING SRM 51-40-15.
Part: SKIN — CRACKED (BS 680-700)
CRACKED RT SIDE GUIDE AT STA 680 AND 700. REPLACED PER MM 28-84-00.
Part: SUPPORT — CRACKED (BS 570)
CRACKED FLOOR SUPPORT WEB AT LT STA 570 LBL 48 APPROX. REPAIRED PER BOEING SRM 51-40-03.
Part: SUPPORT — CORRODED (BS 500)
LEVEL 1 FWD CARGO FLOOR SUPPORT UPP SURFACE FOUND CORRODED AT STN 500 LBL 35 TO 45. CORROSION CLEANED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SEAL FAIRING — CRACKED (NR 4 PYLON)
NR 4 PYLON UPPER FWD SLOT SEAL FAIRING IS CRACKED AT RT FWD CORNER. REPAIRED PER BOEING SRM 51-40-03.
Part: BRACKET — CRACKED (WS 590)
LT WING LWR T/E PNL SUPPORT FWD MOUNT BRACKET (1 EA) CRACKED AT WS 590. REPAIRED PER BOEING SRM 51-10-01.
Part: COWL SKIN — DELAMINATED (NR 2 ENGINE)
NR 2 ENG RT SIDE COWL TRIMMER ACCESS PNL ATTACHED INNER SKIN IS DISBONDED FROM SKIN. REPAIRED PER BOEING SRM 51-10-01 REF NR 867374.
Part: TIE DOWN — CORRODED (BS 2285)
LEVEL 1 CORROSION, M/D FLOORBEAM TIE DOWN PLATE, BS 2285, WL 200, RBL 45 TO 50. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-0, TREATED PER 51-10-02 AND MM 51-24-11.
Part: COWL FRAMES — BENT (NR 2 ENGINE)
NR 2 ENG LT SIDE COWL 1ST AND 2ND HINGE ATTACH FRAMES ARE BENT AND DEFORMED. SMOOTHED OUT AND DEFORMED AREA REFORMED PER BOEING SRM 51-10-01 AND 51-40-01.
Part: ANGLE — CRACKED (BS 680)
M/D DOOR UPPER SILL/FRAME AFT ANGLE CARCKED AT BS 860 S16R. REPAIRED PER BOEING SRM 51-10-01.
Part: SEAL — DELAMINATED (NR 4 ENGINE)
NR 4 ENG SLOT SEAL IS SPLIT. REPLACED SEAL PER AMM 54-51-00.
Part: LONGERON — CORRODED (BS 515)
LEVEL 1 CORROSION, FWD CARGO STR 34R AND 36R FOUND AT STA 515. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: MOUNT LUG — BROKEN (NR 3 ENGINE)
NR 3 ENG HIGH STG BLEED CONTROLLER HAS ONE MOUNT LUG BROKEN. REPLACED AND TEST REF NRC 5821.
Part: FLOOR PANEL — BROKEN (BS 380-440)
M/D BS 380 TO 440 CTR FLOOR PNL CORNER BROKEN. REPLACED/INSTALLED PER MM 53-21-02.
Part: TIE DOWN — CORRODED (BS 460)
LEVEL 1 CORROSION, M/D BS 460 LBL 3 TIE DOWN FITTING FOUND. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: ANGLE — CORRODED (BS 260)
LEVEL 1 CORROSION, LWR FX INTERIOR STR 30L END ATT ANGLE AT STA 260. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: FLAP — SPONGY (LT TE FLAP)
LT WING I/B FLAP I/B EDGE AREA LWR SURFACE FOUND SPONGY. REPAIRED PER BOEING SRM 51-40-15.
Part: FAIRING — BROKEN (FUSELAGE)
FX - BODY FAIRING 1920 FWD UPPER CORNER FOUND BROKEN. FIBERGLASS REPAIR PER BOEING SRM 51-40-15, FIG 7.
Part: FLOORBEAM — CORRODED (BS 400)
LEVEL 1 CORROSION, M/D-BS 400 RBL 30 TO 40 FLOORBEAM. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: WEB — CORRODED (BS 420)
LEVEL 1 CORROSION, M/D BS 420 RBL 11 TO 33 FLOOR SUPPORT WEB. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SKIN — TORN (RT TE FORE FLAP)
RHW - I/B MID FLAP PANEL AT MID FORE FLAP TRACK CUTOUT FOUND TORN. FIBERGLASS REPAIR PER BOEING SRM 51-40-15, FIG 7.
Part: STRINGER — CORRODED (BS 515)
LEVEL 1 - FWD CARGO STR 34R AND 36R FOUND CORRODED AT STA 515. REMOVED CORROSION PER BOEING SRM 51-10-01, 51-10-02.
Part: SUPPORT — CORRODED (BS 1167-1235)
LEVEL 1 FX BS 1167 TO 1235 LBL 69 A/COND BAY ACCESS PANEL SUPPORT CHORD LWR SURFACE FOUND CORRODED. CORROSION CLEANED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: TIE DOWN FITTING — CORRODED (BS 420)
LEVEL 2 M/D BS 420 LBL 6 TIE DOWN FITTING FOUND CORRODED. CORROSION REMOVED PER BOEING SRM 51-10-01.
Part: ANGLE — CORRODED (BS 293)
LEVEL 1 CORROSION, LWR FX INTERIOR SKIN ATT ANGLE FOUND AT STA 293 AND RBL 36 TO 40. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BRACKET — CORRODED (BS 400)
LEVEL 1 LOWER LOBE INTERIOR BRACKET ATT TO STR 44R FOUND CORRODED AT STA 400. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SEAT TRACK — CORRODED (BS 460)
LEVEL 1 CORROSION, M/D BS 460 RBL 40 TIE DOWN FITTING FLANGE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: WEB — CRACKED (RT TE MIDFLAP)
RT WING I/B MID FLAP T/E O/B WEB CRACKED. REPLACED PER BOEING SRM 51-10-01.
Part: BRACKET — CRACKED (WS 670)
RT WING REAR SPAR AFT FACE AT WS 670 (APPX) LONG SUPPORT ATT BRACKET CRACKED. REPAIRED PER BOEING SRM 51-10-01.
Part: FRAME — CORRODED (BS 400)
LEVEL 1 LWR LOBE INTERIOR STA 400 FRAME LWR CHORD CORRODED AT STR 43R TO 44R. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: FLOOR PANEL — DELAMINATED (BS 460-480)
M/D BS 460 TO 480 RBL 33TO O/B FLOOR PNL CORNER AREA. REPLACED/REINSTALLED SVC NR 2042301.
Part: SUPPORT — CORRODED (BS 1320)
LEVEL 1 CORROSION, M/D ZONE-D STA 1320 RBL 80 TO 95 SUPPORT CHANNEL. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: COWL — DISBONDED (NR 1 ENGINE)
NR 1 ENG LT FAN COWL UPPER FWD CORNER INNER SKIN IS DISBONDED FROM CORE. REPAIR CARRIED OUT IAW BOEING SRM 51-40-06, REF CWS NR 860243.
Part: SKIN — CORRODED (BS 1845-1855)
LEVEL 1 CORROSION AFT CARGO SKIN SURFACE AT STA 1845 TO 1855 AND STR 42R TO 43R. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BRACKET — CRACKED (NR 3 ENGINE)
CRACKED NR 3 ENG FLOW DIVIDER SUPPORT BRACKET. WELDED AND REINSTALLED, SERVICEABLE LABEL S/N FF011895, REF NR 854055.
Part: FLOORBEAM — CORRODED (BS 440)
LEVEL 2 - M/D BS 440 LBL 11 TO RBL 11 FLOORBEAM LOWER CHORD DRIP SHIELD SURFACE FOUND CORRODED. CORROSION REPAIRED PER BOEING SRM 51-10-01 AND 51-40-02.
Part: SKIN — SPONGY (LT TE FORE FLAP)
LHW - I/B FORE FLAP L/E FOUND SPONGY AT MOST I/B AREA. FIBERGLASS REPAIR PER BOEING SRM 51-40-15, FIG 7.
Part: SUPPORT — CORRODED (BS 580)
LEVEL 1 FWD CARGO FLOOR SUPPORT UPP SURFACE CORROSION REVEAL AT STN 580 RBL 12 LBL 40. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SEAT TRACK — CORRODED (BS 400-410)
LEVEL 1 CORROSION, M/D BS 400 TO 410 RBL 11 TIE DOWN TRACK. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: PANEL — CRACKED (RT WING)
RT WING O/B OF NR 8 SPOILER T/E UPP FIXED PNL I/B EDGE AFT PORTION CRACKED. RT WING O/B OF NR 8 SPOILER T/E UPP FIXED PNL I/B EDGE AFT PORTION FIBERGLASS REPAIRED PER BOEING SRM 51-40-12.
Part: FAIRING — CORRODED (FUSELAGE)
LEVEL 1 - FX - BODY FAIRING 191F EXT SKIN FOUND SURFACE CORRODED. REMOVED CORROSION AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: BRACKET — CRACKED (RT WING)
RT WING T/E LWR ACCESS PNL 672GB MID SUPPORT AFT END ATT BRACKET CRACKED. REPAIRED BRACKET PER BOEING SRM 51-10-01.
Part: BRACKET — CRACKED (WS 520)
RHW-WS 520 T/E MOST AFT LWR ACCESS PNL I/B SUPPORT AFT BRACKET CRACKED. REPAIRED AS PER BOEING SRM 51-10-01.
Part: SKIN — CORRODED (BS 800-860)
LEVEL 1 CORROSION, M/D L2 ENTRY DOOR CUTOUT SCUFF PLATE ATTACH AREA, BS 800 TO 860, LBL 118. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: COWL — DEBONDED (NR 1 ENGINE)
NR 1 ENG RT FAN COWL FWD TOP CORNER INNER SKIN IS DISBONDED FROM CORE. REPAIR CARRIED OUT PER BOEING SRM 51-40-06, REF CWS NR 560244.
Part: BRACKET — CRACKED (LT WING)
LT WING UPPER/LOWER T/E PNL SUPPORT MOUNTING BRACKED CRACKED (3 EA). REPAIRED PER BOEING SRM 51-10-01.
Part: CHANNEL — DAMAGED (NR 2 ENGINE)
NR 2 ENG RT SIDE COWL BOTTOM CHANNEL IS HOLED AT THE 3RD 'U' BOLT ATTACH POINT AREA. REPAIRED CARRIED OUT IAW BOEING SRM 51-40-02, REF NR 854316.
Part: SUPPORT — BROKEN (BS 670)
FWD CARGO BROKEN SLOP SIDEWALL SUPPORT STRIP ATT FRAME AREA AT RT STA 670 ABOVE CARGO FLOOR LEVEL. REPLACED PER BOEING SRM 51-10-01.
Part: SUPPORT — CORRODED (BS 2350)
LEVEL 1 CORROSION, M/D LATERAL FLOOR SUPPORT HAT SECTION BS 2350, WL 200, LBL 60 TO 70. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 460)
LEVEL 1 CORROSION, M/D LADDER CUTOUT MOVEABLE PLATFORM SUPPORT BEAM, BS 460, RBL 0 TO 24. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SKIN — CORRODED (BS 240-250)
LEVEL 1 CORROSION, LWR FX INTERIOR SKIN SURFACE AT STA 240 TO 250 AND LBL 25 TO 35. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: COWL — SCRATCHED (NR 2 ENGINE)
NR 2 ENG LT SIDE COWL SKIN EXT SURFACE HAS ONE 10 LONG SCRATCH AT FWD MID SECT AREA. SMOOTHED OUT SCRATCHED AREA AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DELAMINATED (NR 3 PYLON)
NR 3 PYLON LWR SPAR SKIRT FAIRINGS I/B AND O/B HAVE LOOSE FASTENERS DEBONDED INNER SKIN AND INTERLINKING RIBS WITH LOOSE FAST FROM AFT MOUNT TO NAC STA 260. REPAIRED IAW BOEING SRM 54-30-03, REF NR 854328.
Part: SUPPORT — CORRODED (BS 500)
LEVEL 1 CORROSION, M/D LADDER CUTOUT MOVEABLE PLATFORM SUPPORT BEAM, BS 500, RBL 10. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: MOUNT RING — BROKEN (FUSELAGE)
BELLY AREA NR 2 FWD LRRA ANT MOUNTING RING BROKEN. REPLACED MOUNTING RING SCREW NUT PER MM 34-33-00.
Part: SUPPORT — CORRODED (BS 420)
LEVEL 1 CORROSION, M/D LADDER CUTOUT MOVEABLE PLATFORM SUPPORT BEAM, BS 520, RBL 10. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: ANGLE — CRACKED (RT WING)
RHW FWD OF I/B AIL T/E FIXED PANEL LWR I/B WEB I/B FACE UPP 'L' ANGLE CRACKED. REPLACED PER BOEING SRM 51-10-01.
Part: SKIN — CORRODED (BS 800-860)
LEVEL 1 CORROSION, M/D R2 DOOR CUTOUT SCUFF PLATE AREA, BS 800 TO 860, RBL 118. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SKIN — CORRODED (LWR FUSELAGE)
LEVEL 1 CORRODED LWR BELLY BOTH DME ANT BASE (A/C SKIN). REMOVED CORROSION AND REPORTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: FRAME — CRACKED (NR 4 PYLON)
NR 4 PYLON FWD FAIRING 3RD FRAME FROM FRONT IS CRACKED. REPAIRED IAW BOEING SRM 51-40-02 REF CWS NR 854342, PROCESS SHEET S/N DY 0204.
Part: SEAT TRACK — CORRODED (BS 380-390)
LEVEL 1 CORROSION, M/D BS 380 TO 390 RBL 11 TIE DOWN TRACK FLANGE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BRACKET — CRACKED (WS 670)
RT WING AUX BEAM FWD FACE AT WS 670 (APPX) UPP LONG SUPPORT ANGLE REAR ATT BRACKET CRACKED. REPAIRED PER BOEING SRM 51-10-01.
Part: SUPPORT — CORRODED (BS 2370)
LEVEL 1 CORROSION, M/D FLOOR SUPPORT, BS 2370, WL 200, RBL 11 TO 30. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BRACKETS — CORRODED (FUSELAGE)
LEVEL 1 FX KEEL BEAM ACCESS PNL NR 193U INT ATT BRACKETS FOUND CORRODED. CORROSION CLEANED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: LONGERON — CORRODED (BS 1770-1800)
LEVEL 1 CORROSION AFT CARGO STR 50L AT STA 1770 TO 1800. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SKIN — DENTED (FUSELAGE)
LT BLG W/W EXT BODY SKIN FOUND A DENT MARK AT AFT LWR AREA JUST ABOVE O/B STRUT DOOR AS MARKED. SMOOTHED OUT PER BOEING SRM 51-10-01 AND REPROTECTED PER BOEING SRM 51-10-02, PAINTED PER MM 81-24-11.
Part: SUPPORT BRACKET — CORRODED (BS 1097)
LEVEL 1, FX BS 1097 LBL 9 KEEL BEAM PANEL SUPPORT BRACKET FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: ACCESS PANEL — CORRODED (FUSELAGE)
CORROSION KEEL BEAM ACCESS PNL NR 191HH EXT AND INT STRUCTURE FOUND. CORROSION CLEANED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: LONGERON — CORRODED (BS 1770-1790)
LEVEL 1 CORROSION, AFT CARGO STR 51R AT STA 1770 TO 1790. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: COWL RUB STRIP — DAMAGED (NR 3 ENGINE)
NR 3 ENG RT SIDE COWL VERT UPPER EDGE IS DEFORMED AND THE EDGE RUB STRIP IS DAMAGED AT NUMEROUS LOCATIONS. REPLACED AND REFORMED EDGE PER BOEING SRM 51-10-01, REF CWS NR 854080.
Part: COWL — DAMAGED (NR 3 ENGINE)
NR 3 ENG LT SIDE COWL FWD VERT EDGE IS DAMAGED AND DISTROTED. REPLACED LUBE STRIP AND DISTROTION REFORMED IAW BOEING SRM 51-40-01 REF TO CWS NR 854079.
Part: ACCESS PANEL — CORRODED (FUSELAGE)
CORROSION KEEL BEAM ACCESS PNL NR 191KK EXT AND INT STRUCTURE FOUND. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1404)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT BEAM FOUND CORRODED ON BS 1404 LBL 15 RBL 15. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: STRINGER — CORRODED (BS 2210)
LEVEL 1 CORROSION S51R AT BS 2210. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: ANGLE — CORRODED (AIR COND DOOR)
LEVEL 2, FX AIR COND BAY ACCESS DOOR 192E AFT HINGE LWR HALF ATT ANGLE FOUND CORRODED. REPLACED ANGLE PER MM 52-48-01.
Part: FRAME — CORRODED (L5 DOORWAY)
LEVEL 1 CORROSION, M/D L5 DOOR FWD FRAME REVEAL AT STR L22, WL 230. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: LONGERON — CORRODED (BS 1750)
LEVEL 1 CORROSION, AFT CARGO STR 46R AT STA 1750. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: FITTING — CRACKED (L2 DOORWAY)
CRACKED M/D L2 DOOR CUTOUT AFT LOWER CORNER FTG. REINSTALLED EXISTING FTGS PER BOEING SRM 51-30-02.
Part: LONGERON — CORRODED (BS 1740-1760)
LEVEL 1 CORROSION, AFT CARGO STR 47R AT STA 1740 TO 1760. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BRACKET — CRACKED (NR 1 PYLON)
NR 1 PYLON O/B SAIL FAIRING DOOR THE 5TH LATCH AFT ATTACH AND BRACKET. REPAIRED NR 5 LATCH PER BOEING SRM 51-10-01, IAW MM 54-32-00, REF NR 854014.
Part: PANEL — CORRODED (FUSELAGE)
LEVEL 1 FX KEEL BEAM ACCESS PNL NR 191GG INT AND EXT STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — GOUGED (NR 1 PYLON)
NR 1 PYLON O/B SAIL FAIRING DOOR INNER SKIN IS GOUGED AT NUMEROUS PLACES. REPAIRED HOT BOND IAW BOEING 51-40-06, REF NR 854012.
Part: LONGERON — CORRODED (BS 1760-1770)
LEVEL 1 CORROSION, AFT CARGO STR 45L AT STA 1760 TO 1770. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 1437)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT CHANNEL ON BS 1437 LBL 15 RBL 15 FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: FLOOR PANEL — SPONGY (BS 2240-2280)
M/D FLOOR PANEL FOUND SPONGY AT STA 2240 TO 2280 LBL 33 TO 90. REPLACED/REINSTALLED PER MM 53-21-02, SVC TAG NR 2042203.
Part: LONGERON — CORRODED (BS 1750-1800)
LEVEL 1 CORROSIO, AFT CARGO STR 51L AT STA 1750 TO 1800. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: HINGE — CORRODED (AIR COND DOOR)
LEVEL 2, FX AIR COND BAY ACCESS DOOR 191M MID HINGE LWR HALF ATT ANGLE FOUND CORRODED. REPLACED MID HINGE ASSY PER MM 54-48-01.
Part: SKIN — CRACKED (L5 DOOR)
M/D L5 DOOR INNER SKIN CRACK FROM MID UPPER LIGHTENING HOLE. REPAIRED LIGHTENING HOLE PER BOEING SRM 51-40-02.
Part: BRACKET — CORRODED (FUSELAGE)
LEVEL 1 FX KEEL BEAM ACCESS PNL NR 193U INT ATT BRACKETS FOUND CORRODED. CORROSION CLEANED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT BEAM — CORRODED (BS 983)
LEVEL 1, FX BS 983 LBL 9 TO RBL 9 KEEL BEAM BOX ACCESS PANEL SUPPORT BEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CRACKED (BS 1880)
AFT CARGO CEILING PANEL SUPPORT CRACKED AT STA 1880 AND RBL. REPAIRED PER BOEING SRM 51-40-03.
Part: BRACKET — CORRODED (BS 989-995)
LEVEL 1, FX BS 989 TO 995 RBL 9 KEEL BEAM BOX LWR ACCESS PANEL SUPPORT BRACKET FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CRACKED (BS 1920)
AFT CARGO FRAME ATT VERT 'U' SUPPORT FOUND CRACKED AT LT STA 1920 ABOVE STR 40. REPLACED 'U' SUPPORT PER BOEING SRM 51-10-01.
Part: TIE DOWN TRACK — CRACKED (BS 650-660)
FWD CARGO TIE DOWN TRACK FOUND CRACKED AT RT STN 650 TO 660 RBL 44 APPX. REPAIRED TRACK PER BOEING SRM 53-10-05.
Part: COWL CHANNEL — CRACKED (NR 1 ENGINE)
NR 1 ENG LT SIDE COWL BOTTOM CHANNEL IS EITHER TORN OR CRACKED AND DEFORMED AT LATCH HOLE AREA. REFORMED IAW BOEING SRM 51-40-01 AND DRESSED OUT IAW BOEING SRM 51-10-01, REF CWS NR 860119.
Part: SKIN — CRACKED (L5 DOOR)
M/D L5 DOOR INNER SKIN CRACKED FROM MID LWR LIGHTENING HOLE. REPAIRED CRACK SKIN PER BOEING SRM 51-40-02.
Part: SKIN — CRACKED (L 5 DOOR)
M/D L5 DOOR VERT BEAM CRACKED BTN OUTER/INNER SKIN AT 2ND ROW/AFT NR 4 LIGHTENING HOLE. DRILLED STOP HOLE PER BOEING SRM 51-10-01.
Part: FLOORBEAM — CRACKED (BS 1820)
AFT CARGO FLOORBEAM WEB CRACKED AT STA 1820 AND LBL 47. REPAIRED WEB PER BOEING SRM 51-40-02.
Part: COWL FAIRING — DELAMINATED (NR 3 ENGINE)
NR 3 ENG AFT 'V' FAIRING FWD OUTBD EDGE HAS CHAFED THROUGH. REPAIRED OUTBD EDGE IAW BOEING SRM 51-40-03, REF CWS NR 867371.
Part: ANGLE — CRACKED (BS 1620)
AFT CARGO FRAME ATT VERTICAL 'L' ANGLE STRIP FOUND CRACKED AT LT STN 1620 BTN STR 36 TO 37 AND S38-39 ABOVE AREA. REPLACED ANGLE PER BOEING SRM 51-10-01.
Part: STRINGER — CORRODED (BS 2205)
LEVEL 1 CORROSION S30L AT BS 2205. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: STRINGER — CORRODED (BS 2200)
LEVEL 1 CORROSION S50R AT BS 2200. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: SUPPORT BEAM — CORRODED (BS 1109)
LEVEL 1, FX BS 1109 LBL 9 TO RBL 9 KEEL BEAM BOX LWR ACCESS PANEL SUPPORT BEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1468)
LEVEL 2 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT BEAM FOUND CORRODED ON BS 1468 LBL 14 RBL 14. REPLACED SUPPORT BEAM PER BOEING SRM 51-10-01.
Part: SKIN — TORN (LT TE MID FLAP)
LHW - O/B MID FLAP MOST I/B L/E FOUND EDGE TORN. FIBERGLASS REPAIR PER BOEING SRM 51-40-15.
Part: LONGERON — CORRODED (BS 1770-1800)
LEVEL 1 CORROSION, AFT CARGO STR 49L AT STA 1770 TO 1800. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BRACKET — CRACKED (PYLON)
CRACKED BRACKET AT NAC 180 LOWER HOR FIRE WALL, METAL SEAL ATT ON LT AND RT SIDE. REPLACED BRACKET PER BOEING SRM 51-10-01.
Part: PLATE — CRACKED (NR 2 PYLON)
CRACKED RETAINING PLATE NR 2 PYLON SLOT SEAL PNL LT SIDE, NAC 150 APP. REPLACED RETAINING PLATE PER BOEING SRM 51-10-01.
Part: SUPPORT BEAM — CORRODED (BS 1043)
LEVEL 1, FX BS 1043 LBL 9 TO RBL 9 KEEL BEAM BOX LWR ACCESS PANEL SUPPORT BEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: RIB — CRACKED (NR 2 PYLON)
CRACKED NR 2 PYLON RT SIDE RIB AT NAC 230, ACCESS FROM NR 483GL. REPAIRED CARRIED OUT IAW BOEING SRM 54-10-03, REF NR 854454 AND PROCESS SHEET S/N 240206.
Part: COWL RUB STRIP — DAMAGED (NR 4 ENGINE)
NR 4 ENG LT SIDE COWL UPPER EDGE RUB STRIP IS DAMAGED AND DISBONDED. REPLACED AND RESECURED RUB STRIP WITH RIVETS PER BOEING SRM 51-30-02.
Part: COWL — TORN (NR 1 ENGINE)
NR 1 ENG LT SIDE COWL LATCH THROUGH HOLE SKIN EDGE IS EITHER TORN OR DEFORMED (ALL 5 LOCATIONS). DRESSED OUT PER BOEING SRM 51-10-01, REPROTECTED PER BOEING SRM 51-10-02 AND REFORMED PER BOEING SRM 51-40-01.
Part: PRESS PANEL — CORRODED (BS 1350-1360)
LEVEL 1 RBLG W/W STA 1350 TO 1360 RBL 75 UPPER PRESSURE PANEL SURFACE SLIGHTLY CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02. PAINT TOUCH UP PER MM 51-24-00.
Part: LONGERON — CORRODED (BS 1670-1680)
LEVEL 1 CORROSION, AFT CARGO STR 51L AT STA 1670 TO 1680. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: LONGERON — CORRODED (BS 1780-1800)
LEVEL 1 CORROSION, AFT CARGO STR 48R AT STA 1780 TO 1800. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT BRACKET — CORRODED (BS 1075)
LEVEL 2, FX BS 1075 LBL 9 KEEL BEAM PANEL SUPPORT BRACKET FOUND CORRODED. REPLACED BRACKET PER BOEING SRM 51-10-01.
Part: COWL BRACKET — CRACKED (NR 4 ENGINE)
NR 4 ENG RT SIDE COWL 1ST RIB FROM AFT END HAS AN ANGLE BRACKET CRACKED AT THE UPPER MOST PART OF THIS RIB. REPLACED ANGLE IAW BOEING SRM 51-10-01, REF CWS NR 854049.
Part: STRAP — BROKEN (BS 1960)
BULK CARGO STA 1960 BROKEN STRAP ATT TO FRAME ABOVE STR 40L. REPAIRED STRAP PER BOEING SRM 51-40-03.
Part: FLOORBEAM — CRACKED (BS 1780)
AFT CARGO FLOORBEAM WEB CRACKED AT STA 1780 AND LBL 48. REPAIRED WEB PER BOEING SRM 51-40-02.
Part: LONGERON — CORRODED (BS 1680-1700)
LEVEL 1 CORROSION, AFT CARGO STR 51L AT STA 1680 TO 1700. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: COWL FILLER — CRACKED (NR 3 ENGINE)
NR 3 ENG LT FAN COWL INNER SURFACE PREVIOUS FILLER REPAIRS HAVE CRACKED. REPAIRED FILLER IAW BOEING SRM 51-40-06, REF CWS NR 834270.
Part: COWL — DELAMINATED (NR 4 ENGINE)
NR 4 ENG LT SIDE COWL INNER SKIN DOUBLER IS PUNCTURED. REPLACED INNER DOUBLER IAW BOEING SRM 51-10-01 REF CWS NR 854253.
Part: LONGERON — CORRODED (BS 1720-1740)
LEVEL 1 CORROSION, AFT CARGO STR 44L AT STA 1720 TO 1740. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 400-420)
LEVEL 1 CORROSION, U/D-CREW ENTRY DOOR SUPPORT BEAM SURFACE BS 400 TO 420, RBL R80. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: LONGERON — CORRODED (BS 1740)
LEVEL 1 CORROSION, AFT CARGO SPLICE STRAP AT STA 1740 TO STR 42L TO 43L. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: PANEL — CORRODED (FUSELAGE)
LEVEL 1 FX KEEL BEAM ACCESS PNL NR 191HH EXT AND INT STRUCTURE FOUND CORRODED. CORROSION CLEANED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1390)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT CHANNEL FOUND CORRODED ON BS 1390 LBL 15 RBL 15. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: STRINGER — CORRODED (BS 2202)
LEVEL 1 CORROSION S46R AT BS 2202. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: SKIN — DELAMINATED (NR 4 PYLON)
NR 4 PYLON ACCESS PANEL CUTOUTS 483CL, 483EL ARE DAMAGED AND DEFORMED. TRIMMED OFF AND SMOOTHED DAMAGE OUT IAW BOEING SRM 51-10-01 REF CWS NR 854261.
Part: SKIN — TORN (LT TE MID FLAP)
LHW - I/B MID FLAP T/E FOUND SKIN TORN AT MIDDLE 2 EA AFT SPINDLE AREA. FIBERGLASS REPAIR PER BOEING SRM 51-40-15.
Part: STRINGER — CORRODED (BS 2187)
LEVEL 1 CORROSION S33L BS 2187. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: SUPPORT — CRACKED (LT WING)
LHW T/E CAVITY UPPER AND LOWER T/E PANEL SUPPORT ATT ANGLES (4 EA) FOUND CRACKED JUST O/B AND I/B SIDE OF NR 5 SPOILER SERVO. REPLACED PANEL SUPPORT PER BOEING SRM 51-10-01.
Part: TRUNNION FITTING — CRACKED (NLG)
NLG LT TRUNNION FITTING AFT END CRACKED. REPLACED NLG LT TRUNNION SUPPORT FITTING. ALIGNMENT CHECKED OUT PER BOEING SRM 51-10-08.
Part: SKIN — DETERIORATED (LT AILERON)
DETERIORATED I/B AILERON LOWER SURFACE PREVIOUS FILLER REPAIR PATCH AREA NEAR I/B AFT CORNER. REPAIRED PER BOEING SRM 51-40-15.
Part: COWL — DELAMINATED (NR 1 ENGINE)
NR 1 ENG LT SIDE COWL UPPER INNER SKIN IS OVERHEATED AND BULGED AT MID SECTION AREA. REPAIRED FIRE SHIELD IAW BOEING SRM 54-30-03, REF NR 860121.
Part: COWL — CRACKED (NR 3 ENGINE)
NR 3 ENG LT SIDE COWL BOTTOM CHORD IS CRACKED AND DISTORTED WITH LOOSE AND MISSING FASTENERS. REPAIRED COWL BOTTOM CHORD IAW BOEING SRM 51-40-03, REF CWS NR 854178.
Part: SUPPORT — CORRODED (BS 1390)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PANEL SUPPORT CHANNEL FOUND CORRODED ON BS 1390 LBL 1 RBL 15. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — GOUGED (NR 1 PYLON)
DELAMINATION NR 1 PYLON INNER SKIN IS GOUGED BY ACCESS PNL 453 EL LATCHES. REPAIR CARRIED OUT IAW BOEING SRM 54-30-03, REF NR 860254.
Part: DOOR REVEAL — CORRODED (L4 DOORWAY)
LEVEL 1 CORROSION, M/D L4 DOOR CUTOUT FWD LOWER REVEAL STR L24 TO L25, WL 210. REMOVED CORROSION PER BOEING SRM 51-10-0, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: LONGERON — CORRODED (BS 1720)
LEVEL 1 CORROSION, AFT CARGO STR 42L AT STA 1720. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SKIN — CORROSION (PYLON)
CORROSION AND PAINT PEELING AT FASTENER HOLES UNDER PYLON SADDLE FAIRING. REMOVED AND REPROTECTION CARRIED OUT IAW BOEING SRM 51-10-01, MM 51-24-00, REF NR 867338.
Part: COWL — DELAMINATED (NR 3 ENGINE)
NR 3 ENG LT SIDE COWL INTERCOSTAL BETWEEN 5TH AND 7TH RIB AND SEPARATING 2 PRECOOLER EXHAUST CUTOUTS IS CHAFED THROUGH. REPLACED IAW BOEING SRM 51-30-02, REF CWS NR 858944.
Part: KEEL BEAM — CORRODED (BS 1058-1070)
LEVEL 1 CORROSION BS 1058 TO 1070 LBL 7 TO LBL 8 KEEL BEAM BOX LOWER SURFACE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: SKIN — CORRODED (BS 2230-2290)
LEVEL 1 CORROSION, M/D L5 DOOR CUTOUT OUTER SKIN REVEAL JUST BEHIND SCUFF PLATE AREA BS 2230 TO 2290, WL 190 TO 200. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: PANEL — DELAMINATED (RT HORIZ STAB)
RT STAB PANEL 344QBR DELAMINATED AT PREVIOUS REPAIR (MOST O/B PANEL). REPAIRED PER BOEING SRM 51-40-06. PAINT TOUCH UP PER MM 51-24-11.
Part: BRACKET — CRACKED (NR 2 PYLON)
CRACKED BRACKET NR 2 PYLON RT STRUT DOOR MOST AFT LATCH FITTING. REPLACED BRACKET IAW BOEING SRM 51-10-01, REF NR 854048.
Part: WEB — CRACKED (BS 1485)
AFT CARGO HORIZ WEB AT FLOOR LEVEL CRACKED AT STA 1485 AND LBL 56. REPAIRED PER BOEING SRM 51-40-02.
Part: WING TIP — DELAMINATED (LT WING)
LWH, O/B WING TIP AFT LOWER CORNER RIVETS SHEARED. REPLACED RIVETS PER BOEING SRM 51-30-02.
Part: SUPPORT — CORRODED (BS 1404)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT BEAM FOUND CORRODED ON BS 1404 LBL 15 RBL 15. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (BS 520-741)
LEVEL 1 CORROSION ON UPPER FUSELAGE SKIN LAP FAYING SURFACE S12L BS 520 TO BS 741. REPAIRED PER SB 747-53-2307.
Part: SUPPORT — CORRODED (BS 1480)
LEVEL 1 FX KEEL BEAM BOX LOWER ACCESS PNL SUPPORT ANGEL FOUND CORRODED ON BS 1480 LBL 15 TO RBL 15. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (RT HORIZ STAB)
LEVEL 1 RT STAB PANEL 344NBR SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: ANGLE — CORRODED (BS 1480)
LEVEL 1 FX KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT ANGLE FOUND CORRODED ON BS 1480 LBL 15 RBL 15. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: COWL — CRACKED (NR 3 ENGINE)
NR 3 ENG RT SIDE COWL AFT EDGE IS CRACKED 12 FT FROM THE TOP. REPAIRED CARRIED OUT IAW BOEING SRM 51-40-02, REF CWS NR 854294.
Part: FLOORBEAM — CRACKED (BS 1280)
AFT CARGO FLOORBEAM WEB CRACKED AT STA 1280 AND LBL 23. REPAIRED WEB PER BOEING SRM 51-40-02.
Part: SUPPORT — CORRODED (BS 1437)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT CHANNEL ON BS 1437 LBL 15 RBL 15 FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1459)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PANEL SUPPORT CHANNEL FOUND CORRODED ON BS 1459 LBL 9 RBL 9. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1426-1437)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT CHANNEL ON BS 1426 TO 1437 LBL 15 FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1426)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT BEAM FOUND CORRODED ON BS 1426 LBL 15 RBL 15. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1426)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT CHANNEL ON BS 1426 TO 1437 LBL 15 FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (R1 DOOR)
LEVEL 1 CORROSION, M/D R1 DOOR I/B LONG SCUFF PLATE SUPPORT CHANNEL TOP, STR R26, WL 200. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 1449)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT BEAM FOUND CORRODED ON BS 1449 LBL 9 RBL 9. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — CRACKED (L5 DOORWAY)
M/D L5 DOOR CUTOUT INNER SKIN CRACKED AT LIGHTENING HOLE BTN S24L/S25L. TRIMMED OFF AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: COWL — DELAMINATED (NR 3 ENGINE)
NR 3 ENG LT SIDE COWL UPPER VERT EDGE HAS DISBONDED FOR APPROX 3 FEET. RESECURED WITH RIVETS PER BOEING SRM 51-40-02.
Part: SHEAR TIE — CORRODED (BS 1500/1540)
LEVEL 1 AFT CARGO SHEAR TIE ATT LINER CORRODED AT STA 1500 AND 1540 AND STR 50R TO 51R. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: STRINGER — CORRODED (BS 2202)
LEVEL 1 CORROSION S48R AT BS 2202. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: COWL — DELAMINATED (NR 3 ENGINE)
NR 3 ENG LT SIDE COWL PRESS RELIEF DOOR INNER SKIN IS PUNCTURED. REPAIRED INNER SKIN IAW BOEING SRM 51-40-05, REF CWS NR 854099.
Part: SKIN — CRACKED (FUSELAGE)
FX NR 2 PACK H/X HEADER INT SKIN FOUND CRACKED. REPAIRED PER BOEING SRM 51-40-15.
Part: PANEL — CORRODED (FUSELAGE)
LEVEL 1 FX KEEL BEAM ACCESS PANEL NR 191JJ EXT AND INT STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND SRM 51-10-02.
Part: SUPPORT — CHAFING (BS 1032)
FX - BS 1032 LBL 68 AIR COND BAY ACCESS DOOR SUPPORT BEAM UPPER CHORD FOUND DEEP CHAFFING. REPAIRED PER BOEING SRM 51-40-04 FIG. 1.
Part: ANGLE — CRACKED (BS 1920)
AFT CARGO FRAME ATT VERT 'L' ANGLE STRIP FOUND CRACKED AT LT STN 1920 ABOVE STR 39. CRACKED AREA TRIMMED OFF AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — MISREPAIRED (LT TE FORE FLAP)
LHW - I/B FORE FLAP O/B L/E AREA FOUND SPONGY ON PREVIOUS REPAIR AREA. FIBERGLASS REPAIRED PER BOEING SRM 51-40-75, FIG 7.
Part: LONGERON — CORRODED (BS 1770-1800)
LEVEL 1 CORROSION, AFT CARGO STR 48L AT STA 1770 TO 1800. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: PANEL — CORRODED (FUSELAGE)
LEVEL 1 FX KEEL BEAM ACCESS PNL NR 191GG INT AND EXT STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — GOUGED (NR 1 PYLON)
NR 1 PYLON AFT I/B SAIL FAIRING DOOR INNER SKIN IS GOUGED AT SEVERAL PLACES FWD SECTION AREA. REPAIRED HOT BOND PER BOEING SRM 51-40-06, REF NR 854011.
Part: WEB — CORRODED (CREW DOOR)
LEVEL 1 CORROSION CREW ENTRY DOOR AFT REVEAL LOWER WEB. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: BRACE — CHAFED (NR 3 PYLON)
DEEP CHAFE MARK ON NR 3 DIAGONAL BRACE. REP 0-1R OF BLEND OUT CARRIED OUT IAW BOEING FAX S/N 206-266-6878, REF CWS NR 867323, 867324. ALSO RS R54-54-33401.
Part: FITTING — CRACKED (L3 DOORWAY)
CRACKED M/D L3 DOOR CUTOUT FWD LOWER CORNER FTG. REPLACED FTG PER BOEING SRM 51-10-01, SVC TAG NR FF008136.
Part: SUPPORT — CORRODED (BS 983-1023)
LEVEL 1 FX BS 983 TO 1023 LBL 68 AIR/COND BAY ACCESS PANEL SUPPORT BEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: LONGERON — CORRODED (BS 1670)
LEVEL 1 CORROSION, AFT CARGO STR 50L AT STA 1670. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BULKHEAD — CORRODED (NR 1 PYLON)
LEVEL 1 NR 1 PYLON FWD BULKHEAD EXTERNAL SURFACE HAS LIGHT FRETTING CORROSION ON L/R SIDE AT NAC STA 128 AREA. CORROSION REMOVED IAW BOEING SRM 51-10-01 REF TO CWS NR 844412.
Part: CAM PLATES — RUSTED (PAX DOOR)
LEVEL 1 ALL DOOR GUIDE ARM CAM PLATES RUSTED. CLEANED PER BOEING SRM 51-10-01.
Part: FLOORBEAM — CORRODED (BS 520)
LEVEL 2, U/D BS 520 LBL 54 TO LBL 61 FLOORBEAM FOUND CORRODED. REPLACED FLOORBEAM AT LBL 45 EXISTING SPLICE TO LT O/B END PER BOEING SRM 51-10-01.
Part: SUPPORT — CORRODED (BS 1426)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT BEAM FOUND CORRODED ON BS 1426 LBL 15 RBL 15. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: CONTROL CABLE — WORN (WS 1300)
LHW - O/B AILERON CONTROL CABLE AA-15, AA-13 FOUND WORN OUT OF LIMIT AT WS 1300 FAIRLEAD AREA AND WS 1260 PULLEY AREA. LHW O/B AILERON CONTROL CABLE AA-15, AA-13 REPLACED PER MM 20-11-03.
Part: CHANNEL — CRACKED (AILERON)
CRACKED I/B AILERON POWER PACKAGE COMPT I/B VERT WEB ATT SUPPORT CHANNEL. REPLACED V-CHANNEL SUPPORT PER BOEING SRM 51-10-01.
Part: SKIN — CORRODED (LT TE AFT FLAP)
LEVEL 1 - LHW O/B AFT FLAP UPPER SURFACE O/B AREA FOUND SURFACE CORROSION AT SEVERAL AREAS. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1459)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT CHANNEL FOUND CORRODED ON BS 1459 LBL 9 RBL 9. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DAMAGED (LT TE MID FLAP)
LHW - I/B MID FLAP LOWER SURFACE AT NR 4 FLAP TRACK AND O/B AREA FOUND SKIN PEELED UP. FIBERGLASS REPAIR PER BOEING SRM 51-40-15.
Part: PANEL — CORRODED (FUSELAGE)
LEVEL 1 FX KEEL BEAM ACCESS PNL NR 191KK EXT AND INT STRUCTURE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DAMAGED (NR 4 PYLON)
DAMAGED NR 4 PYLON ACCESS PANEL CUTOUTS 483CL, 483EL. TRIMMED OFF AND SMOOTHED OUT IAW BOEING SRM 51-10-01, REF NR 854261.
Part: SKIN — CORRODED (NR 4 PYLON)
CORROSION AND PAINT PEELING AT NR 4 PYLON FASTENER HOLES UNDER PYLON SADDLE FAIRING. CORROSION REMOVED AND REPROTECTION CARRIED OUT IAW BOEING SRM 51-10-01, MM 51-24-00, REF NR 867338.
Part: SUPPORT — CORRODED (BS 1449)
LEVEL 1 FX KEEL BEAM BOX LWR ACCESS PNL SUPPORT BEAM FOUND CORRODED ON BS 1449 LBL 9 RBL 9. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: EXHAUST HOUSING — CORRODED (NR 1 PACK)
LEVEL 1 FX NR 1 PACK H/X EXHAUST HOUSING AFT FACE FOUND CORRODED. CORROSION CLEANED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: LONGERON — CORRODED (BS 1770-1790)
LEVEL 1 CORROSION, AFT CARGO STR 50R AT STA 1770 TO 1790. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: ACCESS PANEL — CRACKED (FUSELAGE)
KEEL BEAM ACCESS PANEL NR 191HH MOUNTING BOLT HOLES FOUND WORN/CRACKED. REPAIRED PER BOEING SRM 51-40-03.
Part: ANGLE — CRACKED (LT WING)
LHW UPPER T/E PNL SUPPORT 'T' ANGLE CRACKED JUST I/B OF I/B AILERON POWER PACKAGE. REPLACED 'T' ANGLE SUPPORT PER BOEING SRM 51-10-01.
Part: FLOORBEAM — CRACKED (BS 1820)
AFT CARGO FLOORBEAM WEB CRACKED AT STA 1820 AND RBL 4 TO 6. REPAIRED WEB PER BOEING SRM 51-40-02.
Part: PANEL — DELAMINATED (LT HORIZ STAB)
LT STAB PANEL 344JBL DELAMINATED. REPAIRED PER BOEING SRM 51-40-06. PAINT TOUCH UP PER MM 51-24-11.
Part: PANEL — CORRODED (BS 440-460)
LEVEL 2 U/D BS 440 TO 460 CTR FLOOR PANEL SURFACE FOUND CORRODED. REPLACED PER MM 3-21-02, SVC TAG NR 2042498.
Part: SPAR STRAP — SHEARED (WS 450)
LT WING UPPER SURFACE FRONT SPAR UPPER STRAP ATT RIVETS (1 EA) SHEARED AT WS 450. REPLACED PER BOEING SRM 51-30-02.
Part: SPAR STRAP — CORRODED (WS 1454)
LEVEL 1 CORROSION LT WING UPPER SURFACE FRONT SPAR UPPER STRAP BULGED UP AT WS 1454. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SPAR STRAP — CORRODED (WS 485)
LEVEL 1 LT WING UPPER SURFACE FRONT SPAR UPPER STRAP BULGED UP AT WS 485. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 1900-1920)
FX EXT SKIN BS 1900 TO 1920 S50L TO S50R AREA FOUND DENT MARKS. DRESSED OUT AND REPROTECTED PER BOEING SRM 51-10-02.
Part: NOSE COWL — DELAMINATED (NR 4 ENGINE)
NR 4 ENG NOSE COWL INLET ACCOUSTIC PANEL BETWEEN 7 AND 10 O'CLOCK IS DEBONDED. REPAIRED PER BOEING SRM 54-30-03.
Part: SKIN — CORRODED (RT HORIZ STAB)
LEVEL 1 RT STAB 344LBR PANEL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: FAIRING — CRACKED (NR 2 PYLON)
NR 2 PYLON FWD FAIRING O/B BOTTOM INNER RUB STRIP IS TORN AND ATTACH ANGLE IS CRACKED. REPLACED RUB STRIP IAW BOEING SRM 51-10-01 REF CWS NR 867283.
Part: PANEL — DELAMINATED (NR 2 PYLON)
NR 2 PYLON ACCESS PANEL 463CL INNER HONEY COMB FOUND DISBONDED FROM SKIN. REBONDED IAW BOEING SRM 51-40-06, REF CWS NR 834291.
Part: TENSION TIE — CRACKED (BS 800)
M/D TENSION TIE LT O/B END AFT SECTION CRACKED AT BS 800. REPAIRED PER SB 53-2371, BOEING SRM 51-10-02.
Part: SKIN — CORRODED (RT HORIZ STAB)
LEVEL 1 RT STAB PANEL 344PBR SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (LT HORIZ STAB)
LEVEL 1 LT STAB PANEL 334MBL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: PANEL — CORRODED (LT HORIZ STAB)
LEVEL 1 LT STAB PANEL 334NBL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (RT HORIZ STAB)
LEVEL 1 RT STAB PANEL 344JBR SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CRACKED (BS 1140)
M/D FLOOR SUPPORT FOUND CRACK AT STA 1140 LSL 116. REPAIRED FLOOR SUPPORT PER BOEING SRM 51-40-03.
Part: BEAM — CORRODED (BS 1260)
LEVEL 1 RT WING GEAR W/W CANTED BULKHEAD CORRODED AT HORIZ BEAM STA 1260 RBL 15. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02. PAINT TOUCH UP PER MM 51-24-00.
Part: SPAR CHORD — CORRODED (WS 395)
LEVEL 1 LT WING UPPER SURFACE FRONT SPAR UPPER CHORD STRAP BULGED UP AT WS 395. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: BEAM — CORRODED (BS 1250)
LEVEL 1 RT WING GEAR W/W CORRODED AT LOWER FACE OF HORIZ BEAM STA 1250 RBL 90. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02. PAINT TOUCH UP PER MM 51-24-00.
Part: PAN — DELAMINATED (NR 2 PYLON)
NR 2 PYLON SLOT SEAL FWD UPPER PAN IS DELAMINATED AT NUMEROUS PLACES. REPAIRED IAW BOEING SRM 54-54-03, REF CWS NR 854125.
Part: PANEL — CORRODED (LT HORIZ STAB)
LEVEL 1 LT STAB PNL 334HBL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02. PAINT TOUCH UP PER MM 51-24-11.
Part: PANEL — DELAMINATED (NR 1 PYLON)
NR 1 PYLON ACCESS PANEL HONEY COMB IS DISBONDED FROM SKIN AT 1 PLACES. REBONDED IAW BOEING SRM 51-40-06, REF CWS NR 834290.
Part: PANEL — CORRODED (BS 460-480)
LEVEL 2 U/D BS 460 TO 480 CTR FLOOR PANEL SURFACE FOUND CORRODED. REPLACED PER MM 53-21-02, SVC TAG NR 2042499.
Part: PANEL — DELAMINATED (NR 1 PYLON)
NR 1 PYLON ACCESS PANEL 453EL INNER SKIN AND HONEY COMB DISBONDED AT NUMEROUS PLACES. REBONDED PER BOEING SRM 51-40-06, REF CWS NR 834289.
Part: SPAR STRAP — CRACKED (WS 840)
LT WING UPPER SURFACE FRONT SPAR UPPER STRAP CRACKED AT WS 840. REPAIRED PER BOEING SRM 51-40-15.
Part: FAIRING — DAMAGED (LT HORIZ STAB)
LT STAB UPPER AIRGATE FAIRING L/E DAMAGED. REPAIRED PER BOEING SRM 51-40-15. PAINT TOUCH UP PER MM 51-24-11.
Part: PANEL — CORRODED (BS 480-520)
LEVEL 2 U/D BS 480 TO 520 CTR FLOOR PANEL SURFACE FOUND CORRODED. CORROSION REPLACED/INSTALLED PER MM 53-21-02, SVC TAG NR 2042496.
Part: SKIN — DELAMINATED (RT HORIZ STAB)
RT STAB PANEL 344LBR SURFACE DELAMINATED. REPAIRED PER BOEING SRM 51-40-15. PAINT TOUCH UP PER MM 51-24-11.
Part: SKIN — DELAMINATION (LT HORIZ STAB)
LT STAB PANEL 344GBL DENT AND DELAMIATED AT PREVIOUS REPAIR. REPAIRED PER BOEING SRM 51-40-06. PAINT TOUCH UP PER MM 51-24-11.
Part: SKIN — CORRODED (BS 520-741)
LEVEL 1 CORROSION, UPPER FUSELAGE SKIN LAP INTERFACE REVEALED ALONG LAPS BETWEEN BS 520 TO 741, STR R12. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SKIN — DELAMINATED (NR 4 SPOILER)
LHW - NR 4 SPOILER UPPER SURFACE DELAMINATION FOUND NEAR O/B T/E CORNER. NR 4 SPOILER HOT BOND REPAIRED PER BOEING SRM 51-40-06.
Part: SKIN — DELAMINATED (NR 1 SPOILER)
LHW - NR 1 SPOILER UPPER SURFACE DELAMINATION FOUND AT CENTER AREA. REPAIRED, HOT BOND PER BOEING SRM 51-40-06 FIG 13. SPOILER PANEL REMOVAL/INSTALLATION PER MM 27-61-02, DUP C/N 048 RAISED.
Part: ANGLE — CORRODED (WS 1271)
LEVEL 1 RHW L/E CAVITY FWD LOWER 'L' ANGLE FWD FACE SLIGHTLY CORRODED SURFACE FOUND FROM OLES 1271 TO TIP. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: FAIRING — DAMAGED (RT HORIZ STAB)
RT STAB UPPER AIRGATE FAIRING L/E DAMAGED. REPAIRED PER BOEING SRM 51-40-15, PAINT TOUCH UP PER MM 51-24-11.
Part: SKIN — DELAMINATED (LT HORIZ STAB)
LT STAB PANEL 334HBL O/B FWD CORNER DELAMINATED. REPAIRED PER BOEING SRM 51-40-06. PAINT TOUCH UP PER MM 51-24-11.
Part: CANTED BULKHEAD — CORRODED (BS 1241)
LEVEL 1 RT WING GEAR W/W CORRODED AT CANTED BULKHEAD RBL 2 STA 1241. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02. PAINT TOUCH UP PER MM 51-24-00.
Part: SKIN — CORRODED (LT HORIZ STAB)
LEVEL 1 LT STAB PANEL 334PBL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SPAR STRAP — CRACKED (WS 485)
LT WING UPPER SURFACE FRONT SPAR UPPER STRAP CRACKED AT WS 485. REPAIRED PER BOEING SRM 51-40-15.
Part: SKIN — CORRODED (LT HORIZ STAB)
LEVEL 1 LT STAB PANEL 334FBL SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (RT HORIZ STAB)
LEVEL 1 RT STAB PANEL 344KBR SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.
Part: BEAM — CORRODED (BS 1250)
LEVEL 1 RT WING GEAR W/W CORRODED AT UPPER FACE OF HORIZ BEAM STA 1250 AT A/CONDITION DUCT FEED THROUGH. CORROSION REMOVED PER BOEING SRM 51-10-01 AND REPROTECTED PER BOEING SRM 51-10-02. PAINT TOUCH UP PER MM 51-24-00.
Part: SEAT TRACK — CRACKED (BS 1100)
ZONE C STA 1100, RBL R75 SEAT TRACK FOUND CRACKED. REPAIRED PER BOEING SRM 53-10-95.
Part: SUPPORT — CORRODED (BS 1350)
LEVEL 1 FX BS 1305 LBL 16 RBL 16 KEEL BEAM BOX LWR ACCESS PANEL SUPPORT BEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: FITTING — CORRODED (BS 470-490)
LEVEL 1 CORROSION, R1 DOOR LOWER GATE BS 470 TO 490, WL 204. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 1341)
LEVEL 1 FX BS 1341 LBL 16 RBL 16 KEEL BEAM LWR ACCESS PNL SUPPORT BEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1271-1341)
LEVEL 1 FX BS 1271 TO 1341 RBL 16 KEEL BEAM BOX LWR ACCESS PNL SUPPORT CHANNEL FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: KEEL BEAM — CORRODED (BS 1260-1261)
LEVEL 1 FX BS 1260 TO 1261 RBL R9 KEEL BEAM BOX EXT LWR CHORD LWR SURFACE FOUND CORRODED. CORROSION REMOVED PER BOEING SRM 51-10-01, AND REPROTECTED PER SRM 53-10-02.
Part: SUPPORT — CORRODED (BS 1271-1273)
LEVEL 1 FX BS 1271 TO 1273 RBL 16 TO LBL 16 KEEL BEAM BOX LWR ACCESS PANEL SUPPORT CHANNEL FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: ANGLE — CORRODED (BS 1295)
LEVEL 1 FX BS 1295 LBL 9 RBL 9 KEEL BEAM BOX EXT LWR LATERAL 'T' SHAPED ANGLE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1305)
LEVEL 1 FX BS 1305 LBL 16 RBL 16 KEEL BEAM BOX LWR ACCESS PANEL SUPPORT BEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND SRM 51-10-02.
Part: WEB — CORRODED (BS 1350)
LEVEL 1 RIGHT WLG W/W AT STN 1350 UPP CHORD ATT WEB UPP SURFACE FOUND CORRODED FROM RBL 25 TO 100 APPROX. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02. PAINT TOUCH UP PER MM 51-24-00.
Part: BULKHEAD ANGLE — CRACKED (BS 1480)
AFT CARGO STA 1480 BULKHEAD ATT ANGLE FOUND CRACKED AT RBL 38, LOCATED BETWEEN NR 5 AND NR 6 HORIZ STIFFENER COUNT FROM TOP. REPLACED SUPPORT WEB AND ANGLE PER BOEING SRM 51-10-01 AND INSTALLED PER SRM 51-30-02.
Part: SUPPORT — CORRODED (BS 1261)
LEVEL 1 FX BS 1261 LBL 9 RBL 9 KEEL BEAM LWR ACCESS PANEL SUPPORT BEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CORRODED (BS 1283)
LEVEL 1 FX BS 1283 LBL 17 RBL 17 KEEL BEAM BOX LWR ACCESS PANEL SUPPORT BEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: FITTING — CORRODED (AFT FUSELAGE)
LEVEL 1 TAIL POST ADAPTOR FITTING MOUNTING FACE SLIGHT SURFACE CORROSION REVEALED, AREA AROUND TAIL JACK. CORROSION REMOVED PER BOEING SRM 51-10-01 AND REPROTECTED PER SRM 51-10-02. PAINT TOUCH UP PER MM 51-24-11.
Part: LONGERON — CORRODED (BS 1900)
LEVEL 1 CORROSION, STR 51R FOUND AT STA 1900. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 271-1273)
LEVEL 1 FX BS 1271 TO 1273 RBL 16 LBL 16 KEEL BEAM BOX LWR ACCESS PNL SUPPORT CHANNEL FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: BULKHEAD ANGLE — CRACKED (BS 1480)
AFT CARGO STA 1480 BULKHEAD ATT ANGLE FOUND CRACKED AT LBL 38, LOCATED BETWEEN NR 5 AND NR 6 HORI STIFFENER COUNT FROM TOP. REPLACED SUPPORT WEB AND ANGLE PER BOEING SRM 51-10-01 AND INSTALLED PER SRM 51-30-02.
Part: FLOORBEAM — DEFORMED (BS 1900)
AFT CARGO FLOORBEAM UPPER CHORD DEFORMED AT STA 1900 LBL 23. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-02.
Part: ANGLE — CRACKED (L3 DOORWAY)
M/D-L3 DOOR S/W LOWER SUPPORT ANGLE CRACKED AT MID PORTION. REPAIRED PER BOEING SRM 51-40-03.
Part: SKIN — DENTED (AFT FUSELAGE)
AFT FUSELAGE DENT MARK 10 FWD OF TAIL JACK. SMOOTHED OUT DENT PER BOEING SRM 51-10-01 AND REPROTECTED PER SRM 51-10-02. PAINT TOUCH UP PER MM 51-24-11.
Part: STRUT — CHAFED (RT MLG)
RIGHT WLG SHOCK STRUT INNER CYLINDER YOKE ADJACENT AFT BRAKE EQUALIZER ROD AREA FOUND CHAFING MARK AS RED MARKED. REWORKED IN CONJUNCTION WITH BOEING FAX PAO-HKG-97-0008RE.
Part: ANGLE — CRACKED (BS 1480)
BULKHEAD ATT ANGLE FOUND CRACKED AT BS 1480, LBL L38. SUPPORT WEB AND ANGLE REPLACED PER BOEING SRM 51-10-01 AND INSTALLED PER BOEING SRM 51-30-02.
Part: ANGLE — CRACKED (BS 1480)
BULKHEAD ATT ANGLE FOUND CRACKED AT BS 1480, RBL R38. SUPPORT WEB AND ANGLE REPLACED PER BOEING SRM 51-10-01 AND INSTALLED PER BOEING SRM 51-30-02.
Part: SUPPORT — CORRODED (BS 1283)
LEVEL 1 FX BS 1283 LBL 17 RBL 17 KEEL BEAM BOX LWR ACCESS PNL SUPPORT BEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND SRM 51-10-02.
Part: FAIRING — DAMAGED (RT HORIZ STAB)
RT STAB LOWER AIR GATE FAIRING L/E DAMAGED. REPAIRED PER BOEING SRM 51-40-1. PAINT TOUCH UP PER MM 51-24-11.
Part: LONGERON — CORRODED (BS 1820-1860)
LEVEL 1 CORROSION, STR 48L FOUND AT STA 1840 TO 1860. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: LONGERON — CORRODED (BS 1860-1880)
LEVEL 1 CORROSION, STR 47R FOUND AT STA 1860 TO 1880. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: LONGERON — CORRODED (BS 1820-1840)
LEVEL 1 CORROSION, STR 51L FOUND AT 1820 TO 1840. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BULKHEAD ANGLE — CORRODED (BS 1480)
LEVEL 1 CORROSION, STA 1480 BULKHEAD NR 6 STIFFENER AT ANGLE AT LBL 38. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BULKHEAD — CORRODED (BS 1480)
LEVEL 1 CORROSION, STA 1480 BULKHEAD NR 6 HORI STIFFENER SURFACE AT RBL 13 TO 55. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BULKHEAD — CORRODED (BS 1480)
LEVEL 1 CORROSION, STA 1480 BULKHEAD NR 4 HORI STIFFENER SURFACE AT LBL 100 TO RBL 100. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: LONGERON — CORRODED (BS 1860-1900)
LEVEL 1 CORROSION, STR 51L FOUND AT STA 1860 TO 1900. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 1913)
LEVEL 1 CORROSION, FLOOR SUPPORT SURFACE AT STA 1913 AND LBL 25 TO 45. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: LONGERON — CORRODED (BS 1820-1830)
LEVEL 1 CORROSION, STR 44L FOUND AT STA 1820 TO 1830. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 460)
LEVEL 1 CORROSION, BS 460 RBL 47 TO 64 FLOOR SUPPORT UPPER AND LOWER FACE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 460-480)
LEVEL 1 CORROSION, BS 460 TO 480 RLB 28 TO 34 CURVE SHAPE FLOOR SUPPORT FLANGE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: LONGERON — CORRODED (BS 1820-1840)
LEVEL 1 CORROSION, STR 51R FOUND AT STA 1820 TO 1840. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BULKHEAD — CORRODED (BS 1480)
LEVEL 1 CORROSION, STA 1480 BULKHEAD NR 2 HORI STIFFENER SURFACE AT LBL 100 TO RBL 110. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: LONGERON — CORRODED (BS 1810-1850)
LEVEL 1 CORROSION, STR 49R FOUND AT STA 1810 TO 1850. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: FAIRING — DAMAGED (LT HORIZ STAB)
LT STAB AIR GATE FAIRING L/E DAMAGED. REPAIRED PER BOEING SRM 51-40-15, PAINTED PER MM 51-24-11.
Part: WEB — CORRODED (BS 1350)
LEVEL 1 LEFT WLG W/W AT STN 1350 UPP CHORD ATT WEB UPP SURFACE CORROSION REVEAL FROM LBL 25 TO 100 APPROX. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02. PAINT TOUCH UP PER MM 51-24-11.
Part: SKIN — DELAMINATED (L3 DOORWAY)
M/D L3 DOOR CUTOUT SKIN SHIM DELAMINATED AT AFT LWR CORNER AREA. CORNER REVEAL ASSY REINSTALLED WITH FASTENERS PER BOEING SRM 51-30-02.
Part: BULKHEAD — CORRODED (BS 1480)
LEVEL 1 CORROSION, STA 1480 BULKHEAD NR 3 HORI STIFFENER SURFACE AT LBL 100 TO RBL 105. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 1271-1341)
LEVEL 1 FX BS 1271 TO 1341 LBL 16 KEEL BEAM BOX LWR ACCESS PANEL SUPPORT CHANNEL FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: LONGERON — CORRODED (BS 1910-1920)
LEVEL 1 CORROSION, STR 47R FOUND AT STA 1910 TO 1920. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: WEB — CRACKED (L2 DOORWAY)
M/D L2 DOOR T/T CENTER PORTION CUTOUT RETAINER FOUND CRACKED. REPAIRED PER BOEING SRM 51-40-02.
Part: BULKHEAD SKIN — DELAMINATED (BS 1241)
LEFT WLG STN 1241 CANTED BULKHEAD FOUND SKIN DELAMINATED AT LBL 90. REPAIRED PER BOEING SRM 51-40-15, PAINTED PER MM 51-24-1.
Part: KEEL BEAM — CORRODED (BS 1300-1305)
LEVEL 1 CORROSION, BS 1300 TO 1305 KEEL BEAM BOX LWR WEB LWR SURFACE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CORRODED (BS 1261)
LEVEL 1 FX BS 1261 LBL 9 RBL 9 KEEL BEAM LWR ACCESS PANEL SUPPORT BEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: LONGERON — CORRODED (BS 1880-1920)
LEVEL 1 CORROSION, STR 48L FOUND AT STA 1880 TO 1920. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: FAIRING — DEFORMED (VERT STAB)
VERTICAL L/E FAIRING 321A T/E DEFORMED. REPAIRED PER BOEING SRM 51-40-01.
Part: FLOORBEAM — CORRODED (BS 1100)
LEVEL 1 CORROSION, ZONE C STA 1100 RBL 101 FLOORBEAM. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND 51-24-11.
Part: FLOORBEAM — CORRODED (BS 520)
LEVEL 1 CORROSION, BS 520 RBL 9 TO 47 LONGIT, FLOORBEAM UPPER CHORD. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BRACKET — CORRODED (WASTE TANK)
LEVEL 1 U/D BS 455 RBL 28 TO 31 WASTE TANK SUPPORT BRACKET CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: LONGERON — CORRODED (BS 1820-1840)
LEVEL 1 CORROSION, STR 47L FOUND AT STA 1820 TO 1840. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BRACKET — CORRODED (BS 1250-1262)
LEVEL 2 - FX - BS 1250- BS 1262 LBL 9 KEEL BEAM LWR ACCESS PANEL SUPPORT BRACKED FOUND CORRODED. REPLACED CORRODED BRACKET PER BOEING SRM 51-10-01.
Part: ANGLE — CORRODED (BS 1295)
LEVEL 1 FX BS 1295 LBL 9 RBL 9 KEEL BEAM BOX EXT LWR LATERAL 'T' SHAPED ANGLE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: BULKHEAD ANGLE — CORRODED (BS 1480)
LEVEL 1 CORROSION, STA 1480 BULKHEAD NR 3 HORI STIFFENER AT ANGLE AT LBL 30. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: FAIRING — CRACKED (VERT STAB)
VERTICAL FIN L/E FAIRING 321A T/E DEFORMED. REFORMED FAIRING AND CRACK CHECK PER BOEING SRM 51-40-01 AND NOT MM 51-00-00.
Part: SUPPORT — CRACKED (BS 492)
U/D - BS 492 RBL 33 CURVE SHAPE FLR SUPPORT FLANGE CRACKED. REPAIRED FLR SUPPORT PER BOEING SRM 51-40-03 SVC TAG NR FF 008352, FF008254.
Part: LONGERON — CORRODED (BS 1860-1880)
LEVEL 1 CORROSION, STR 50L FOUND AT STA 1860 TO 1880. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: ANGLE — CRACKED (L3 DOOR)
M/D L3 DOOR S/W LOWER SUPPORT ANGLE CRACKED AT MID PORTION. REPAIRED ANGLE PER BOEING SRM 51-40-03.
Part: SKIN — DELAMINATED (L3 DOOR)
M/D L3 DOOR CUTOUT SKIN SHIM DELAMINATED AT AFT LWR CORNER AREA. REINSTALLED CORNER REVEAL ASSY WITH FASTENERS PER BOEING SRM 51-30-02.
Part: FAIRING — DAMAGED (RT HORIZ STAB)
RT STAB LWR AIR GATE FAIRING L/E DAMAGED. REPAIRED PER BOEING SRM 51-40-15, PAINTED PER MM 51-24-11.
Part: FITTING — CORRODED (R2 DOOR)
LEVEL 1 - R2 DOOR UPPER HINGE ARM LOWER BEARING PLATE FOUND CORRODED. CORROSION REMOVED PER BOEING SRM 51-10-01, 53-10-01, 51-10-02, MM 51-24-11, 51-24-13.
Part: WEB — CORRODED (BS 1350)
LEVEL 1 LEFT WLG W/W AT STN 1350 UPP CHORD ATT WEB UPP SURFACE CORROSION REVEAL FROM LBL 25 TO 100 APPROX. CORROSION REMOVED PER BOEING SRM 51-10-01 AND REPROTECTED PER SRM 51-10-02. PAINT TOUCH UP PER MM 51-24-11.
Part: FLOORBEAM — CRACKED (FUSELAGE)
CRACKED FLOORBEAM UPPER CHORD. REPAIRED PER BOEING SRM 51-40-04.
Part: SKIN — CORRODED (R3 DOORWAY)
LEVEL 1 CORROSION, R3 DOOR CUTOUT LOWER HINGE AREA. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: KEEL BEAM — CORRODED (BS 1260-1261)
LEVEL 1 CORROSION, BS 1260 TO 1261 RBL 9 KEEL BEAM BOX EXT LWR CHORD LWR SURFACE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BULKHEAD — CORRODED (BS 1480)
LEVEL 1 CORROSION, STA 1480 BULKHEAD NR 5 HORI STIFFENER SURFACE AT LBL 55 TO RBL 100. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: BRACKET — CRACKED (WASTE TANK)
U/D BS 447 RBL 43 WASTE TANK SUPPORT BRACKET CRACKED. REPAIRED BRACKET PER BOEING SRM 51-10-01.
Part: FLOORBEAM — CORRODED (BS 1100)
LEVEL 1 ZONE-C STATION 1100 RBL 101 FLOORBEAM FOUND CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02, PAINT TOUCH UP PER MM 51-24-11.
Part: FAIRING — DENTED (LT HORIZ STAB)
LT STAB L/E FAIRING 331 OUTBD END DENT MARK FOUND. FAIRING REFORMED PER BOEING SRM 51-40-01.
Part: SUPPORT — CORRODED (BS 462)
LEVEL 1 CORROSION, BS 462 RBL 33 WASTE TANK SUPPORT DOME NUT AREA. CLEANED CORROSION PER BOEING SRM 53-10-01.
Part: FITTING — CORRODED (BS 1265)
LEVEL 1 CORROSION, R2 DOOR CUTOUT FWD LOWER REVEAL BS 1265, STR R26. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SKIN — DENTED (AFT FUSELAGE)
AFT FUSELAGE DENT MARK 10 FWD OF TAIL JACK. DENT SMOOTHED OUT PER BOEING SRM 51-10-01 AND REPROTECTED PER SRM 51-10-02. PAINTED PER MM 51-24-11.
Part: WEB — CRACKED (L4 DOORWAY)
M/D L4 DOOR FWD CUTOUT WEB BELOW NR 4 STOP FITTING FROM TOP FOUND CRACKED. TRIMMED OFF AS PER BOEING SRM 51-10-01 AND REPROTECTED AS PER BOEING SRM 51-10-02.
Part: FAIRING — CRACKED (LT HORIZ STAB)
CRACKED LT STAB L/E FAIRING 331CL DENT APPX 70 FROM OUTBD END. REFORMED PER BOEING SRM 51-40-01, REF 858928.
Part: FAIRING — DAMAGED (LT HORIZ STAB)
LT STAB AIR GATE FAIRING L/E DAMAGED. REPAIRED PER BOEING SRM 51-40-15. PAINT TOUCH UP PER MM 51-24-11.
Part: FAIRING — DELAMINATED (LT HORIZ STAB)
LT STAB L/E FAIRING 3310L DENT APPROX 70 FROM OUTBOARD END. REFORMED PER BOEING SRM 51-40-01 REFER CWS NR 858928.
Part: BULKHEAD SKIN — DELAMINATED (BS 1241)
LEFT WLG STN 1241 CANTED BULKHEAD FOUND SKIN DELAMINATED AT LBL 90 APPROX. REPAIRED PER BOEING SRM 51-40-15. PAINT TOUCH UP PER MM 51-24-11.
Part: LONGERON — CORRODED (BS 1830-1870)
LEVEL 1 CORROSION, STR 48R FOUND AT STA 1830 TO 1870. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: FAIRING — DELAMINATED (LT HORIZ STAB)
LT STAB L/E FAIRING 331 AT OUTBOARD END DENT MARK FOUND. REFORMED FAIRING PER BOEING SRM 51-40-01 REF CWS NR 858929.
Part: BULKHEAD — CORRODED (BS 1480)
LEVEL 1 CORROSION, STA 1480 BULKHEAD AT STIFFENER NR 6 AT RBL 55 TO 80. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: ANGLE — CORRODED (BS 1920)
LEVEL 2 BULK CARGO FLOORBEAM UPPER CHORD UNDERSIDE ATT ANGLE FOUND CORRODED AT STA 1920 AND RBL 40 TO 45. CORROSION REMOVED PER BOEING SRM 51-10-01.
Part: SUPPORT — CORRODED (BS 2000-2040)
LEVEL 1 - BULK CARGO - FLR SUPPORT CORRODED AT STA 2000-2040 AND REL 50. REMOVED CORROSION PER BOEING SRM 57-10-01, 51-10-02, 53-10-01 AND MM 11-24-11.
Part: SKIN — CRACKED (BS 820-840)
BS 820 TO 840 S12L FUSELAGE SKIN LAP JOINT TOP ROW FASTENER HOLES FOUND (2 EA) CRACKED. REPAIRED PATCH PER BOEING SRM 53-30-03 REF SRWS 913378.
Part: CLIP — CRACKED (BS 2120)
STR CLIP CRACKED AT BS 2120, STR L46. SLIGHTLY TRIMMED OFF AND REPROTECTED PER BOEING SRM 51-10-02.
Part: SKIN — DELAMINATED (BS 2220-2230)
FX - BS 2220-2230 STR 24R- STR 25R SKIN FOUND DENT MARK. SMOOTHED OUT DENTED SKIN REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: HINGE — CORRODED (CARGO DOOR)
LEVEL 1 FX AFT CARGO DOOR HINGE FOUND RUSTED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND SRM 51-10-02.
Part: SKIN — DELAMINATED (BS 740-760)
FX BS 740 TO 760 STR 26L TO 27L SKIN FOUND DENT MARKS. SKIN SMOOTHED OUT AS PER BOEING SRM 51-10-01 REPROTECTED PER BOEING SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 1920)
LEVEL 1 BULK CARGO FLOOR SUPPORT CORRODED AT STA 1920 AND RBL 45. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02. PAINT TOUCH UP PER MM 51-24-11.
Part: DOOR LOWER GATE — CORRODED (R5 DOOR)
LEVEL 1 CORROSION ON R5 DOOR LOWER GATE INSERT AREA. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: BULKHEAD — CORRODED (BS 1480)
LEVEL 1 CORROSION, STA 1480 BULKHEAD AT STIFFENER NR 5 FOUND AT LBL 55 TO 92. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: COWL — DEBONDED (NR 4 ENGINE)
NR 4 NOSE COWL FILLER IS DEBONDED AT 9 O'CLOCK POSITION. REPAIRED FILLER IAW BOEING SRM 51-40-06 REF CWS NR 834268.
Part: SUPPORT — CORRODED (BS 2030-2050)
LEVEL 1 CORROSION FLOOR SUPPORT AT BS 2030 TO 2050 AT BL 0. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: SUPPORT — CRACKED (BS 1980)
FLOOR SUPPORT FOUND CRACKED AT BS 1980, RBL 52. REPAIRED BS 1970 TO 1990 RBL 52, PER BOEING SRM 51-40-03, REF NRC NR 5852.
Part: SUPPORT — CORRODED (BS 2070-2105)
LEVEL 1 CORROSION FLOOR SUPPORT BS 2075 TO 2105 RBL 8. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: SUPPORT — CRACKED (BS 2060)
FLOOR SUPPORT CRACKED AT BS 2060, LBL 30. REPAIRED BS 2050 TO 2085, LBL 30, PER BOEING SRM 51-40-03.
Part: SUPPORT — CORRODED (BS 2000-2040)
LEVEL 1 CORROSION FLOOR SUPPORT BS 2000 TO 2040 RBL 50. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: SUPPORT — CORRODED (BS 1920)
LEVEL 1 BULK CARGO FLOORBEAM UPPER CHORD UNDERSIDE ATT ANGLE FOUND CORRODED AT STA 1920 AND RBL 40 TO 45. CORROSION REMOVED PER BOEING SRM 51-10-01.
Part: SKIN — CRACKED (BS 820-860)
BS 820-860 812R FUSELAGE SKIN CAP JOINT TOP ROW FASTENER HOLES FOUND 8 CRACKED. REPAIRED SKIN REF NRC 7150 EMBODIED.
Part: SUPPORT — CORRODED (BS 2040-2050)
LEVEL 1 CORROSION FLOOR SUPPORT AT BS 2040 TO 2050 LBL 8. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: SUPPORT — CORRODED (BS 1930)
LEVEL 1 CORROSION FLOOR SUPPORT BS 1930 LBL 30. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: SKIN — DELAMINATED (PAX DOOR)
M/D L5 PAX DOOR EXT SKIN ON FWD LWR CORNER FOUND DEFORMED. SKIN DRESSED OUT AS PER BOEING SRM 51-10-01 AND REPROTECTED PER BOEING SRM 51-10-02.
Part: SUPPORT — CORRODED (BS 2020)
LEVEL 1 CORROSION FLOOR SUPPORT AT BS 2020 LBL 8 TO LBL 0. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-0 AND TREATED PER 51-10-02, 51-24-11.
Part: SUPPORT — CRACKED (BS 1960-2000)
FLOOR SUPPORT FOUND CRACKED AT BS 1960 TO 2000, RBL 23. REPLACED AT BS 1920 TO 2010 RBL 23 AS PER BOEING SRM 51-10-01, REF NRC NR 5394.
Part: SKIN — DENTED (BS 1980-2000)
FX - BS 1980-2000 STR 14R - STR 15R SKIN FOUND DENT MARK. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01, 51-10-02.
Part: FLOORBEAM — SHEARED RIVETS (BS 2040)
RIVETS (2 EA) SHEARED AT FLOORBEAM UPPER CHORD AT STA 2040, LBL 15. REPLACED PER BOEING SRM 51-30-02.
Part: SUPPORT — CORRODED (BS 1920)
LEVEL 1 CORROSION, FLOOR SUPPORT CORROSION AT STA 1920 & LBL 38. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.
Part: SUPPORT — CRACKED (BS 2060)
FLOOR SUPPORT CRACKED AT BS 2060, LBL 38. REPAIRED BS 2050 TO 2090, LBL 38. PER BOEING SRM 51-40-03.
Part: SUPPORT — CORRODED (BS 2060)
LEVEL 1 CORROSION FLOOR SUPPORT BS 2060 AT BL 0. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: SUPPORT — CRACKED (BS 1980)
FLOOR SUPPORT FOUND CRACKED AT BS 1980, R52. REPAIRED BS 1970 TO 1990 RBL 52, PER BOEING SRM 51-40-03.
Part: SUPPORT — CRACKED (BS 1960)
FLOOR SUPPORT FOUND CRACKED AT STA 1960, RBL 15 ATT ANGLE RIVETS SHEARED. REPAIRED PER BOEING SRM 51-40-03.
Part: SKIN — DELAMINATED (BS 480-500)
FX BS 480 TO 500 STR 22L TO 23L SKIN FOUND DENT MARK. SKIN REFORMED PER BOEING SRM 51-40-01 AND REPROTECTED PER BOEING SRM 51-10-02.
Part: FLOORBEAM — MISSING RIVETS (BS 2080)
RIVETS (4 EA) MISSING AT FLOORBEAM UPPER CHORD AT STA 2080 AND RBL 44. REPLACED PER BOEING SRM 51-30-02.
Part: SEAL PLATE — CRACKED (NR 1 ENGINE)
NR 1 ENG 8TH STAGE PNEUMATIC DUCT SWIVAL JOINT SEAL PLATE IS CRACKED AT WELD SEAL AREA LOCATED JUST ABOVE OIL TANK. CHECKED AREA REPAIRED PER REF TAG S/N DY0508, REF CWS NR 858535.
Part: SUPPORT — CORRODED (BS 1920)
LEVEL 1 CORROSION FLOOR SUPPORT BS 1920 AT RBL 8. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01 AND TREATED PER 51-10-02, 51-24-11.
Part: PANEL — CORRODED (WS 1056)
CORROSION RT WING UPPER SURFACE AFT OF L/E GLASS PANEL AT WS 1056 BULGED UP. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01, 51-10-02.
Part: PANEL — CORRODED (WS 862)
LEVEL 1 RHW UPPER SURFACE AFT OF L/E F/GLASS PANEL AT WS 862 BLUGED UP. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01, 51-10-02.
Part: SKIN — DENTED (BS 2000)
FX BS 2000, STR 48 TO 49 SKIN FOUND DENT MARK. DRESSED OUT AND REPROTECTED PER BOEING SRM 51-10-02.
Part: SKIN — DENTED (BS 1700-1740)
FX BS 1700 TO 1740 STR 39R TO 40R SKIN FOUND DENT MARK. PRESSED OUT AND REPROTECTED PER BOEING SRM 51-10-02.
Part: SUPPORT — CRACKED (BS 1940-2000)
FLOOR PNL SUPPORT FOUND CRACKED AT BS 1940 TO 2000, RLB 23. REPLACED AT BS 1920 TO 2010 PER BOEING SRM 51-10-01.
Part: SKIN — DENTED (BS 1740-1760)
FX BS 1740 TO 1760 STR 31R TO 32R SKIN FOUND DENT MARK. DRESSED OUT AND REPROTECTED PER BOEING SRM 51-10-02.
Part: DOOR — DENTED (APU COMPT)
RT APU ACCESS DOOR SEVERAL DENT MARKS. PRESSED OUT DENT MARKS PER BOEING SRM 51-10-01 AND REPROTECTED PER SRM 51-10-02. CRACK CHECK CARRIED OUT. PAINT TOUCH UP PER MM 51-24-11.
Part: SKIN — DENTED (BS 500-520)
SKIN FOUND DENT MARK AT BS 500 TO 520, STR R44 TO R45. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 1820-1860)
FX BS 1820 TO 1860 STR 40L TO 42L SKIN FOUND DENT MARKS. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DELAMINATED (BS 620-700)
SKIN FOUND DENT MARKS AT BS 620 TO 700, STR L40 TO 42. SKIN SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 2340-2360)
FX-BS 2340 TO 2360 STR 50R TO 51R SKIN DENT. DRESSED OUT SKIN AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: COWL — CORRODED (NR 2 ENGINE)
LEVEL 1 - NR 2 ENG NOSE COWL EXTERNAL PANEL (BTN 12 TO 9 O/C) IS BULGED AT L/E AND T/E (6 PLACES) PLUS FILIFORM CORROSION FOUND ON SCREW ATTACH AREA. REMOVED CORROSION AND REPAIRED PER BOEING SRM 51-10-01, 51-10-02 AND 51-40-06 PART 2 REF CWS NR 863,840, AND 858780.
Part: TR SLEEVE — DELAMINATED (NR 2 ENGINE)
DELAMINATION NR 2 ENG T/R SLEEVE EXTERNAL SKIN AT 8 O'CLOCK POSITION. NEW ENGINE S/N 695755.
Part: SUPPORT — CRACKED (BS 1980)
FLOOR PNL SUPPORT FOUND CRACKED AT BS 1980, RBL 8. REPAIRED PER BOEING SRM 51-40-03.
Part: SKIN — DENTED (BS 720-740)
SKIN FOUND DENT MARK AT BS 720 TO 740, STR R39 TO R40. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DELAMINATED (BS 420-440)
FX BS 420 TO 440 STR 39L TO 40L SKIN FOUND DENT MARK. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DAMAGED (LT ELEVATOR)
LY I/B ELEV I/B EDGE DAMAGED AT REAR CORNER. REPAIRED PER BOEING SRM 51-40-15. PAINT TOUCH UP PER MM 51-24-11.
Part: SUPPORT — CRACKED (BS 1980-2000)
FLOOR PNL SUPPORT FOUND CRACKED AT BS 1980 TO 2000, LBL 0. REPAIRED PER BOEING SRM 51-40-03.
Part: SKIN — DENTED (BS 520-540)
SKIN FOUND DENT MARK AT BS 520 TO 540, STR R45 TO R46. FX SKIN SMOOTHED OUT AND REPROTECTED PER SRM 51-10-01, 51-10-02.
Part: PANEL — CORRODED (WS 1380)
LEVEL 1 RHW UPPER SURFACE AFT OF L/E F/GLASS PNL AT WS 1380 BLUGED UP, (LOCATION AFT OF NR 24 VC FLAP POSITION). CORROSION REMOVED AND REPORTECTED PER SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 2120-2140)
FX BS 2120 TO 2140 STR 41R TO 44R SKIN FOUND DENT MARKS. SMOOTHED SKIN AND REPROTECTED PER BOEING SRM 51-10-01 AND SRM 51-10-02.
Part: SKIN — DENTED (CARGO DOOR)
FWD CARGO DOOR EXT SKIN FOUND DENT MARK 2 PLACES. SMOOTHED OUT SKIN AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DELAMINATED (BS 1960-1980)
FX BS 1960 TO 1980 STR 43R TO 46R SKIN FOUND DENT MARK. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CRACKED (BS 1975-2040)
FLOOR PNL SUPPORT FOUND CRACKED AT BS 1975 TO 2040, RLB 30. REPAIRED AT BS 1940 TO 1990 AND 2040 RBL 30 PER BOEING SRM 51-40-03.
Part: SKIN — DELAMINATED (BS 360-400)
SKIN FOUND DENT MARKS AT BS 360 TO 400, STR L26 TO 29. SMOOTHED OUT AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.
Part: SKIN — DELAMINATED (BS 480-520)
SKIN DELAMINATED AT BS 480 TO 520, STR R37 TO R40. SKIN SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND SRM 51-10-02.
Part: SKIN — DENTED (BS 720-740)
SKIN FOUND DENT MARK AT BS 720 TO 740, STR R26 TO R27. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DELAMINATED (BS 620)
SKIN FOUND DENTED AT BS 620, STR L37 TO L38. SKIN SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 1915-1920)
FX BS 1915 TO 1920 STR 41L TO 42L SKIN FOUND DENT MARK. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: TR SLEEVE — DENTED (NR 2 ENGINE)
NR 2 ENG FAN T/R SLEEVE EXTERNAL SURFACE IS DENTED AT T/E AREA AT 10 O'CLOCK POSITION. NEW ENGINE S/N 695755.
Part: SKIN — CRACKED (PAX DOOR)
M/D L1 PAX DOOR INNER SKIN CRACK AT WINDOW CUTOUT AFT UPPER CORNER. REPAIRED PATCH PER BOEING SRM 51-40-02.
Part: SKIN — DENTED (BS 540-560)
SKIN DENT MARK FOUND IN SEVERAL PLACES BS 540 TO 560, STR R37 TO R41. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — CORRODED (NR 8 SPOILER)
LEVEL 1 RHW NR 8 SPOILER PNL TOP SURFACE SLIGHTLY SURFACE CORROSION FOUND. REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SLIN — CRACKED (LT ELEVATOR)
LT O/B ELEV I/B LWR EDGE CRACKED AS MARKED. REPAIRED PER BOEING SRM 51-40-15. PAINT TOUCH UP PER MM 51-24-11.
Part: SKIN — DENTED (BS 1960-1970)
FX BS 1960 TO 1970 STR 39L TO 40L SKIN FOUND DENT MARK. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 1950-1960)
FX BS 195 TO 1960 STR 42L TO 43L SKIN FOUND DENT MARK. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 1760-1780)
FX BS 1760 TO 1780 STR 30R TO 32R SKIN FOUND DENT MARK. SMOOTHED OUT AND REPORTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: WEB — CORRODED (L1 DOOR)
LEVEL 1 CORROSION L1 PAX DOOR HORIZONTAL WEB TOP BETWEEN DOOR OUTER/INNER SKIN AT STRINGER 23. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02, AND 51-24-11.
Part: SKIN — DENTED (BS 1860-1880)
BS 1860 TO 1880 STR R48 TO 49 SKIN FOUND DENT MARKS. DRESSED OUT AND REPROTECTED PER BOEING SRM 51-10-02.
Part: SKIN — DELAMINATED (BS 1800-1820)
BS 1800 TO 1820, STR L48 TO 49 SKIN FOUND DENT MARK. DRESSED OUT AND REPROTECTED PER BOEING SRM 51-10-02.
Part: SUPPORT — CRACKED (BS 2000)
FLOOR PNL SUPPORT FOUND CRACKED AT BS 2000, LBL 38. REPAIRED PER BOEING SRM 51-40-03.
Part: SKIN — DELAMINATED (BS 520-540)
SKIN FOUND DENT MARK AT BS 520 TO 540, STR L30 TO L31. SKIN SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DELAMINATED (BS 420-440)
SKIN FOUND DENT MARK AT BS 420 TO 440, STR L39 TO L40. SKIN SMOOTHED OUT AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 500-520)
SKIN FOUND DENT MARK BS 500 TO 520, STR R39 TO R40. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: TR SLEEVE — DELAMINATED (NR 2 ENGINE)
NR 2 ENG T/R SLEEVE EXTERNAL SURFACE HAS SEVERAL DENTS AND SCRATCHES. T/E SLIGHTLY SPLIT AT 4 O'CLOCK POSITION. NEW ENGINE S/N P695755.
Part: SKIN — SCRATCHED (BS 1880)
FX BS 1880 STR 42R SKIN FOUND SCRATCH MARK. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: STRUT — RUSTED (RT MLG)
LEVEL 1 RT BODY GEAR-OLEO RUSTED. REMOVED RUST PER BOEING SRM 51-10-01 AND REPROTECTED PER BOEING 51-10-02. PAINTED PER MM 51-24-00.
Part: SKIN — DENTED (BS 2060-2080)
FX BS 2060 TO 2080 STR 35R TO 36R SKIN FOUND DENTS. SMOOTHED SKIN AND REPROTECTED PER BOEING SRM 51-10-01 AND SRM 51-10-02.
Part: PANEL — DELAMINATED (RT WING)
RHW UPPER SURFACE T/E FIXED F/GLASS PNL AT FWD OF NR 12 SPOILER POSITION PREVIOUSLY REPAIRED AREA DELAMINATED. REPAIRED PER BOEING SRM 51-40-15.
Part: SKIN — DELAMINATED (BS 670-680)
BS 670 TO 680, STR R28 TO 29 SKIN FOUND DENT MARK. SKIN SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: MOUNT — DELAMINATED (NR 1 ENGINE)
NR 1 ENG AFT LWR MOUNT AND TAUGENTIAL LINK UPPER SURFACE ARE CHAFED AT SEVERAL PLACED AT RHS. BLENDED OUT AFFECTED ARE IAW BOEING SRM 51-10-01 AND CHAFE MARK IS WITHIN MM 71-21-00, REF CWS NR 854155.
Part: SKIN — CRACKED (RT LE FLAP)
RHW NR 17 VC FLAP FOLDING NOSE O/B PORTION CRACKED AND DEFORMED. REPAIRED NOSE FAIRING PER BOEING SRM 57-50-03. REMOVAL/INSTALLATION PER MM 27-81-02 DWP C/N 012 RAISED.
Part: SKIN — DENTED (BS 540-580)
SKIN FOUND DENT MARK AT BS 540 TO 580, STR L37 TO L38. SMOOTHED OUT AND REPROTECTED AS PER BOEING SRM 51-10-01 AND SRM 51-10-02.
Part: SKIN — DENTED (BS 670-700)
SKIN DENT MARK FOUND IN SEVERAL PLACES BS 670 TO 700, STR R32 TO R38. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 2120-2140)
FX BS 2120 TO 2140 STR 40L TO 41L SKIN FOUND DENT MARK. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 2000-2020)
FX BS 200 TO 2020 STR 44L TO 45L SKIN FOUND DENT MARK. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 1780-1800)
FX BS 1780 TO 1800 STR 40L TO 41L SKIN FOUND DENT MARK. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: PANEL — DELAMINATED (NR 11 SPOILER)
RHW - NR 11 SPOILER PANEL DELAMINATED AT O/B FWD PORTION. RHW NR 11 SPOILER PANEL HOT BOND REPAIRED PER BOEING SRM 51-40-06, SPOILER PANEL REMOVAL/INSTALLATION PER MM 27-61-02.
Part: SKIN — DEFORMED (NLG DOOR)
NLG RT FWD DOOR LWR EDGE DEFORMED-APPOX 25 INCH FWD OF AFT CORNER. REFORMED PER BOEING SRM 51-40-01.
Part: STRUT — CORRODED (RT MLG)
LEVEL 1 RT BODY GEAR TRUCK BEAM RUST BELOW INNER CYLINDER. REMOVED PER BOEING SRM 51-10-01 AND REPROTECTED PER SRM 51-10-02. PAINT TOUCH UP PER MM 51-24-00.
Part: SKIN — CORRODED (WS 1056)
LEVEL 1 RHW UPPER SURFACE AFT OF L/E F/GLASS PNL AT WS 1056 BLUGED UP, LOCATION AFT OF NR 20 VC FLAP. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: WEB — CORRODED (CARGO DOOR)
LEVEL 1 AFT CARGO DOOR LWR WEB SURFACE CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — CRACKED (L1 PAX DOOR)
M/D L1 PAX DOOR INNER SKIN FWD MID ACCESS PANEL CRACKED. REPAIRED PANEL PER BOEING SRM 51-40-02.
Part: PANEL — DELAMINATED (RT WING)
RHW-UPPER SURFACE FWD OF O/B AIL I/B PORTIONS T/E FIXED PNL SURFACE TORN REVEALED. REPAIRED PER BOEING SRM 51-40-15.
Part: SUPPORT — CRACKED (BS 1980-2000)
FLOOR PNL SUPPORT FOUND CRACKED AT BS 1980 TO 2000, LBL L8. REPAIRED PER BOEING SRM 51-40-03.
Part: SKIN — DENTED (BS 2000-2020)
FX BS 200 TO 2020 STR 41R TO 42R SKI FOUND DENT MARK. SMOOTHED SKIN OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND SRM 51-10-02.
Part: PANEL — CORRODED (WS 914)
LEVEL 1, RHW UPPER SURFACE AFT OF L/E F/GLASS PANEL AT WS 914 BLUGED UP (LOCATION AT AFT OF NR 19 VC FLAP POSITION). CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — SCRATCHED (BS 1920-1941)
FX BS 1920 TO 1941 STR 30R TO 32R SKIN FOUND SCRATCH MARKS. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND SRM 51-10-02.
Part: SKIN — DENTED (BS 420-460)
BS 420 TO 460, STR R38 TO R41 SKIN FOUND DENT MARKS. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DELAMINATED (BS 660-680)
SKIN FOUND DENT MARKS AT BS 660 TO 680 STR L35 TO L38. SKIN SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 1840-1900)
FX BS 1840 TO 1900 STR 36L TO 40L SKIN FOUND DENT MARKS. SKIN REFORMED PER BOEING SRM 51-40-01 AND REPROTECTED PER SRM 51-10-02.
Part: SKIN — DENTED (BS 680-720)
SKIN FOUND DENT MARK AT BS 680 TO 720, STR R41 TO R42. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 680-720)
SKIN FOUND DENT MARK AT BS 68 TO 720, STR R35 TO R36. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SKIN — DENTED (BS 680-720)
SKIN FOUND DENT MARKS AT BS 680 TO 720, STR L40 TO L42. SMOOTHED OUT AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: SUPPORT — CRACKED (BS 1940)
FLOOR PANEL SUPPORT FOUND CRACKED AT BS 1940, LBL 15. REPLACED PER BOEING SRM 51-10-01.
Part: SUPPORT — CRACKED (BS 2000-2040)
FLOOR PNL SUPPORT FOUND CRACKED AT BS 2000 TO 2040, LBL 23. REPAIRED PER BOEING SRM 51-40-03.
Part: FLOOR PANEL — PUNCTURED (BS 680)
M/D BS 680 LBL 5 FLOOR PNL FOUND PUNCH HOLE. REPAIRED FILLER PER BOEING SRM 51-40-07.
Part: PANEL — TORN (LT WING)
LHW FWD OF NR 6 SPOILER I/B AREA (3 EA) UPPER T/E ACCESS PANELS SURFACE TORN. REPAIRED PER BOEING SRM 51-40-15.
Part: DOOR — DENTED (LT MLG)
LT BODY GEAR I/B STRUT DOOR REAR EDGE LWR CORNER DENT MARK FOUND. REPAIRED CORNER PER BOEING SRM 51-40-03 AND PAINTED PER MM 51-24-11.
Part: FLOOR PANEL — CRACKED (BS 1640)
M/D BS 1640 RBL 5 FLOOR PNL FOUND PUNCH HOLE. REPAIRED FILLER PER BOEING SRM 51-40-07.
Part: DOOR — DENTED (LT MLG)
LT BODY GEAR O/B STRUT DOOR OUTER FACE DENT. SMOOTHED OUT PER BOEING SRM 51-10-02.
Part: SKIN — MISSING RIVETS (L5 DOORWAY)
M/D R5 DOOR CUTOUT FWD LOWER AREA FOUND NON-STANDARD FASTENERS. REPLACED RIVETS PER BOEING SRM 51-30-02.
Part: PANEL — DELAMINATED (LT WING)
LHW FWD OF NR 6 SPOILER O/B AREA UPPER T/E ACCESS PANEL I/B AREA DELAMINATED. REPAIRED PER BOEING SRM 51-40-13.
Part: SKIN — DENTED (LT MLG DOOR)
LT BODY GEAR, O/B STRUT DOOR OUTER FACE DENT MARK. SMOOTHED OUT DENT MARKS PER BOEING SRM 51-10-02.
Part: RIVETS — SHEARED (LT WING)
LHW WING TIP ANTENNA AREA UPPER SURFACE SHEAR RIVETS. REPLACED RIVETS PER BOEING SRM 51-30-02.
Part: SKIN — CORRODED (LWR FUSELAGE)
CORRODED NR 2 VHF COMM ANT BELLY AREA. REINSTALLED AND FUNCTIONAL CHECKED NORMAL, REF MM 23-21-00.
Part: HINGE PANEL — DELAMINATED (NR 3 SPOILER)
LHW- NR 3 SPOILER HINGE PANEL MID AREA TORN. REPAIRED AREA FIBERGLASS PER BOEING SRM 51-40-15.
Part: FAIRING — DELAMINATED (LT WING)
LHW STATIC DISCHARGER FAIRING FWD EDGE TORN. REPAIRED PER BOEING SRM 51-40-15.
Part: WING TIP — DELAMINATED (LT WING)
LHW WING TIP UPPER SURFACE TORN FWD O/B OF THE MOST O/B STATIC DISCHARGER. REPAIRED PER BOEING SRM 51-40-15.
Part: FASTENERS — FAILED (RT WING)
RHW UPPER SKIN FRONT SPAR TO L/E PANEL ATTACH PLATE FOUND SHEARED RIVETS BETWEEN NR 17 AND NR 18 VC FLAP. REPLACED PER BOEING SRM 51-30-02.
Part: ACCESS PANEL — TORN (LT WING)
LHW NR 4 FWD UPPER T/E ACCESS PANEL O/B FWD AREA SLIGHTLY TORN (COUNT FROM WING ROOT). REPAIRED PER BOEING SRM 51-40-15.
Part: FLOOR PANEL — CRACKED (BS 1370)
M/D BS 1370 RBL 5 FLR PNL FOUND PUNCH HOLE. REPLACED AND REINSTALLED PER SV TAG NR 2042207.
Part: PANEL — DELAMINATED (LT WING)
LHW NR 2 FWD UPPER T/E ACCESS PANEL DELAMINATED (COUNT FROM WING ROOT). REPAIRED PER BOEING SRM 51-40-15.
Part: PANEL — DELAMINATED (LT WING)
LHW THE MOST I/B UPPER T/E ACCESS PANEL SOME LOCATIONS DELAMINATED. REPAIRED PER BOEING SRM 51-40-15.
Part: PANEL — TORN (LT WING)
LHW NR 2 FWD UPPER T/E ACCESS PANEL O/B EDGE AFT AREA TORN (COUNT FROM WING ROOT). REPAIRED PER BOEING SRM 51-40-15.
Part: PANEL — CORRODED (LT WING)
LEVEL 1 LHW NR 6 AFT UPPER TOP T/E PANEL I/B EDGE SLIGHTLY CORRODED (COUNT FROM WING ROOT). CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: PANEL — TORN (LT WING)
LHW NR 3 SPOILER HINGE PANEL MID AREA AND O/B AREA TORN. REPAIRED PER BOEING SRM 51-40-15.
Part: PANEL — CORRODED (LT WING)
LEVEL 1 LHW FWD OF NR 6 SPOILER HINGE PANEL I/B AREA SLIGHTLY CORRODED. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02.
Part: FASTENERS — FAILED (RT WING)
LEVEL 1 RHW UPPER SURFACE FRONT SPAR TO L/E PANEL ATTACH PLATE FOUND RIVET HEAD SHEARED AND CORRODED ADJACENT TO WING ROOT AREA. REPLACED PER BOEING SRM 51-30-02.
Part: FASTENER — FAILED (RT WING)
RHW UPPER SURFACE FRONT SPAR TO L/E PANEL ATTACH RIVET SHEARED AT O/B OF NR 15 KRUEGER FLAP AREA. REPLACED PER BOEING SRM 51-30-02.
Part: PANEL — DELAMINATED (LT WING)
DELAMINATION LT WING FWD OF O/B AILERON T/E FIXED PANEL. REPAIRED PER BOEING SRM 51-40-15.
Part: PANEL — CORRODED (LT WING)
LHW THE MOST I/B FWD UPPER T/E ACCESS PANEL O/B FWD CORNER BULGED. REPAIRED PER BOEING SRM 51-40-15.
Part: PANEL — TORN (LT WING)
LHW FWD OF NR 5 SPOILER HINGE PANEL O/B AREA UPPER T/E ACCESS PANEL PUNCHED AND SURFACE TORN. REPAIRED PER BOEING SRM 51-40-15.
Part: PANEL — DELAMINATED (LT WING)
LHW FWD OF I/B AILERON, T/E FIXED PANEL DELAMINATED. REPAIRED PER BOEING SRM 51-40-15.
Part: HYD LINE — WRONG LENGTH (NR 1 HYD SYST)
NR 1 HYDRAULIC SYSTEM DECREASED ON CLIMBOUT. TURNED ADP OFF, NO HELP. DEPRESSURIZED EDP HYDRAULIC LOSS, STOPPED AT 2 GALLONS. FOUND BROKEN PRESSURE MODULE AT EDP PRESSURE PORT. FOUND PRESSURE LINE TO MODULE TO BE WRONG LENGTH, REQUIRED EXCESSIVE PRELOAD TO CONNECT LINE. REPLACED LINE WITH 65B01512-1141 LINE. REPLACED HYDRAULIC MODULE P/N 36370-4 PER MAINTENANCE MANUAL 29-11-23 AND 20-11-05. CHECKED CLEARANCES PER SB 747-54A2159. LEAK CHECKED PER 29-11-00 PAGE 601.
Part: PRESS MODULE — CRACKED (NR 1 HYD SYST)
ON TAXI IN, LOST ALL HYDRAULIC FLUID FROM NR 1 SYSTEM. FOUND CRACKED ENGINE DRIVEN PUMP PRESSURE MODULE. REPLACED PER BOEING MAINTENANCE MANUAL 29-11-23.
Part: ENGINE — FAILED (NR 3)
NR 3 ENGINE AUDIBLE SURGE AND SHUT DOWN, EGT 960 FOR 1 SEC. RETURNED TO MIA. FOUND METAL IN 3.5 BLEED INDICATING ENGINE FAILURE. ENGINE REPLACED PER BOEING MAINTENANCE MANUAL USING POLAR AIR WORK CARD M 7100-002.
Part: MODULE — CRACKED (NR 1 ENGINE)
NR 1 ENGINE DRIVEN PUMP PRESSURE MODULE LEAKING. FOUND CRACKED MODULE, REPLACED PER BOEING MAINTENANCE MANUAL 29-11-23, LEAK CHECK OK.
Part: CONNECTOR — DIRTY (RT AILERON)
RIGHT OUTBOARD AILERON FAILED TO UNLOCK WITH FLAPS EXTENDED ON TAXI OUT FOR DEPARTURE. CLEANED CANNON PLUG ON RIGHT HAND AILERON LOCK OUT ACTUATOR.
Part: CONNECTOR — DIRTY (RT AILERON)
RIGHT OUTBOARD AILERON LOCK ACTUATOR FAILED TO OPERATE DURING TAXI. CLEANED CANNON PLUG AT ACTUATOR, OPERATIONAL CHECK OK PER BOEING MAINTENANCE MANUAL 27-11-00.
Part: TR UNIT — FAILED (NR 3 ENGINE)
NR 3 ENGINE FAN THRUST REVERSE DRIVE UNIT FAILED TEST REQUIRED BY AD 95-16-02. REPLACED DRIVE UNIT PER BAC MM 78-38-01.
Part: SKIN — CORRODED (LT NR 4 SPOILER)
LEVEL 1 CORROSION NR 4 SPOILER LEADING EDGE SURFACE. REPAIRED PER BOEING SRM 51-10-01.
Part: PANEL — CORRODED (FUSELAGE)
LEVEL 1 CORROSION PANEL 191X. REPAIRED PER BOEING SRM 51-10-01.
Part: COWL — CRACKED (NR 4 ENGINE)
CRACK NR 4 ENGINE CORE COWL INBOARD SIDE. REPAIRED PER BOEING SRM 51-40-02.
Part: FRAME — CRACKED (NR 2 PYLON)
CRACKED FRAME ON NR 2 PYLON AT STA 195. REPAIRED PER BAC SRM 54-10-03, PAGE 2B.
Part: PANEL — CRACKED (LT WING)
CRACKED LEFT WING PANEL LOCATED OUTBOARD OF INBOARD AILERON. REPAIRED PER BOEING SRM 51-40-09.
Part: FITTING — CRACKED (LT TE FOREFLAP)
CRACKED ATTACH FITTING FOR INBOARD FOREFLAP TRACK SUPPORT. REPLACED FITTING PER BAC MM 27-50-00.
Part: BRACKET — BROKEN (NR 1 ENGINE)
BROKEN SUPPORT BRACKET FOR ENGINE BLEED AIR DUCT NR 1 ENGINE. REPLACED BRACKET PER BOEING MAINTENANCE MANUAL 75-22-01.
Part: PANEL — CORRODED (FUSELAGE)
LEVEL 1 CORROSION PANELS 191QL AND 192QR. REPAIRED PER BOEING SRM 51-10-01.
Part: SKIN — CORRODED (LT NR 6 SPOILER)
LEVEL 1 CORROSION LEFT WING NR 6 GROUND SPOILER ON PREVIOUS REPAIR. REPAIRED PER BOEING SRM 51-10-01, 51-10-02 AND 51-21-11.
Part: BRACKET — CRACKED (NR 2 ENG COWL)
CRACKED SUPPORT BRACKET ON NR 2 ENGINE CORE COWL. REPAIRED PER BAC MM 72-01-101B AND BAC SRM 51-30-02.
Part: DOOR — DISBONDED (LT MLG)
DISBONDED PANEL LEFT WING LANDING GEAR FIXED DOOR. REPAIRED PER BOEING SRM 51-40-06.
Part: CASCADE VANE — DAMAGED (NR 2 ENGINE)
DAMAGED CASCADE VANE ON NR 2 ENGINE FAN REVERSE SLEEVE. REPAIRED PER BAC MM 78-31-07.
Part: PANEL — CORRODED (FUSELAGE)
LEVEL 1 CORROSION ON PANEL 191S. REPAIRED PER BOEING SRM 51-10-02.
Part: SKIN — CRACKED (BS 205)
DENT WITH CRACK IN FUSELAGE SKIN BS 205 BL 0. REPAIRED PER BOEING SRM 53-30-03.
Part: SKIN — PUNCTURED (LT TE FOREFLAP)
LEFT OUTBOARD FOREFLAP LEADING EDGE PUNCTURED. REPAIRED PER BAC SRM 51-40-09.
Part: SKIN — DELAMINATED (LT TE FOREFLAP)
DELAMINATION ON LEFT WING OUTBOARD FOREFLAP LEADING EDGE. REPAIRED PER BAC SRM 51-49-09.
1996
Part: DOOR — BENT (FWD CARGO)
GROUND DAMAGE FORWARD CARGO DOOR BENT UP BY CARGO LOADER AT LOWER AFT CORNER APPROXIMATELY 8 TO 10 INCH LENGTH. INSTALLED OUTSIDE SKIN DOUBLER AS PER BOEING SRM 51-40-03 AND PRESS CHECKED PER BOEING M/M 21-00-00.
Part: ENGINE — OVER TEMP (NR 1)
ABORTED TAKEOFF AND RETURNED TO RAMP DUE TO ENGINE NR 1 EXCEEDING MAX EGT LIMITS WHEN APPLYING TAKEOFF THRUST. EGT REACHED 976 DEGREES FOR APPROXIMATELY 5 SECONDS. PERFORMED OVERTEMP INSPECTION REQUIRED BY 71-00-00 AREA C. BORESCOPE PER 72-00-00, NO DEFECTS NOTED, 80 HOUR LIMIT ENGINE CHANGED 12/17/96. SUSPECT 8TH STAGE CHECK VALVE OR HIGH STAGE VALVE FAILURE CAUSING EXCESSIVE BLEED AIR DURING TAKEOFF.
Part: SKIN — PUNCTURED (BS 160)
FRAME WEB, INNER AND OUTER CHORD AT BS 160 WERE FOUND DAMAGED BETWEEN STRINGER S36L AND S42AL. REPAIRED PER POLAR AIR CARGO MA 5330-13:01 AND 5310-19:01.
Part: SKIN — CRACKED (CARGO DOOR)
SEVEN INCH CRACK AT LOWER FORWARD SKIN ON THE REAR LOWER LOBE CARGO DOOR. REPAIRED PER BAC SRM 52-00-03 FIG 4.
Part: SKIN — DENTED (BS 540)
DENT IN SKIN AT STATION 540 BETWEEN LAP SEAM S39R AND STRINGER S38R. EDDY CURRENT CHECK CONFIRMED NO CRACK. REPAIRED PER BAC SRM 51-40-01.
Part: SKIN — CRACKED (CARGO DR CUTOUT)
CRACK BY FORWARD CARGO DOOR CUTOUT LOWER FORWARD CORNER. BLENDED OUT IN OUTER SKIN AS PER BOEING SRM 51-30-01 FIG 1 AND CLEANED AND PAIRNET PER BOEING SRM 51-21-04 EDDY CURRENT OUTER SKIN PER NDT MANUAL PART 6 53-10-25. ACCOMPLISHED PER POLAR AIR CARG0 MA 5330-11-01.
Part: LADDER STEP — CRACKED (UPPER DECK)
CRACK ON 4TH STEP OF UPPER DECK LADDER. REPAIRED PER BAC SRM 51-40-03.
Part: BRACKET — BROKEN (LT FUEL PANEL)
LEFT WING FUEL PANEL HOLD OPEN BRACKET BROKEN. REPAIRED PER SRM 51-10-01.
Part: SKIN — DAMAGED (RUDDER)
HOLE FOUND ON PRE-DELIVERY CK ON LEFT OUTER LOWER MID SKIN OF UPPER RUDDER. REPAIRED PER BAC SRM 51-40-15 AND 51-40-11.
Part: SKIN — CORRODED (BS 2484)
BULGE IN FUSELAGE SKIN AT BS 2484 S46L. REMOVED FASTENERS AT THE AREA OF THE BULGE, INSPECTED FOR CORROSION AND NO CORROSION FOUND. REINSTALLED FASTENERS PER BOEING SRM 51-30-02.
Part: SEAL DEPRESSOR — TORN (AFT CARGO DOOR)
TORN AND BENT SEAL DEPRESSOR AFT CARGO DOOR. REMOVED AND REPLACED SEAL DEPRESSOR PER BOEING SRM 51-10-01.
Part: SEAL DEPRESSOR — TORN (CARGO DOOR)
TORN SEAL DEPRESSOR FORWARD CARGO DOOR AFT EDGE. REPLACED PER BOEING SRM 51-40-01.
Part: PANEL — DAMAGED (LT WING LE)
THREE DAMAGED LEADING EDGE FIBERGLASS PANELS ON LEFT WING. REPAIRED PANELS PER BAC SRM 51-40-15 AND 51-40-11.
Part: BRACKET — CRACKED (NR 4 ENGINE COWL)
CRACKED BRACKET AT NR 4 ENGINE NOSE COWL. FABRICATED AND INSTALLED NEW BRACKET PER BAC SRM 51-10-01.
Part: COWLING — CRACKED (NR 2 ENGINE)
CRACKED UPPER FORWARD CORNER ON NR 2 ENGINE INBOARD COWL. FABRICATED REPAIR AND INSTALLED PER BAC SRM 51-10-02 AND 51-30-02.
Part: BUSHING — MIGRATED (LT TE FLAP)
MIGRATED BUSHING ON FORE FLAP SUPPORT FITTING OF LEFT INBOARD FLAP OUTBOARD TRACK. REPLACED BUSHING FASTENERS.
Part: FAIRING PLATE — TORN (NR 2 ENGINE)
BLOCKER DOOR FAIRING PLATE TEARING UPWARD THROUGH SCREWS OF NR 2 ENGINE FAN REVERSE SLEEVE IN AFT AREA AT 6:30 POSITION. REMOVED AND REPLACED FAIRING PLATE PER BAC SRM 51-10-01 AND 51-30-02.
Part: ANGLE — TORN (NR 3 ENGINE)
NR 3 ENGINE INBOARD COWL INNER ANGLE TORN AT LATCH. REPAIRED COWL PER BAC SRM 51-10-02 AND 51-10-01.
Part: BUSHING — MIGRATED (TE FLAP FITTING)
BUSHING MIGRATED AT RIGHT INBOARD FOREFLAP TRACK ATTACH FITTING. FOUND FASTENERS AT FAULT AND REPLACED BUSHING FASTENERS PER BAC MM 27-51-02.
Part: SKIN — BUCKLED (HORIZ STAB)
BUCKLED SKIN ON LEFT HORIZONAL STABLIZER UPPER TRAILING EDGE. REPAIRED SKIN PER BAC SRM 51-40-09.
Part: SKIN — DELAMINATED (RT VERT STAB)
ROUGH REPAIL LIFTED OUT, DELAMINATED ON RIGHT VERTICAL STABLIZER LOWER SKIN. REPAIRED AREA PER BAC SRM 51-40-06.
Part: SKIN — DELAMINATED (ELEVATOR)
DELAMINATED SKIN ON LEFT INBOARD ELEVATOR TRAILING EDGE INBOARD MID. REPAIRED WITH FIBERGLASS OVERLAY PER BAC SRM 51-41-00.
Part: DOOR — CORROSION (RT MLG)
LIGHT SURFACE CORROSION ON WHEEL WELL DOOR OF RIGHT BODY GEAR. REMOVED CORROSION PER BAC SRM 51-10-52.
Part: SKIN — PUNCTURED (LT MLG STRUT DR)
PUNCTURED SKIN ON LEFT BODY GEAR STRUT DOOR TRAILING EDGE. ROUTED DAMAGED AREA PER BAC SRM 51-10-01.
Part: DOOR — CRACKED (LT MLG)
CRACKED WEB ON AFT END OF LEFT WING GEAR STRUT DOOR. REPAIRED PER BAC SRM 51-10-1 AND 51-30-02.
Part: SKIN — CRACKED (APU DOOR)
SKIN CRACKED ON LEADING EDGE OF APU BATTERY ACCESS DOOR. FABRICATED REPAIR PER BAC SRM 51-40-02 AND INSTALLED PER BAC SRM 51-30-02.
Part: RADOME — DAMAGED (FWD FUSELAGE)
THREE HOLES IN A/C RADOME. MADE FIBERGLASS REPAIR PER BAC SRM 53-30-03, 53-50-03 AND 51-24-11.
Part: BRACKET — BROKEN (MAIN CARGO DECK)
BROKEN SUPPORT BRACKET AT RIGHT SIDE MAIN DECK CARGO SAFETY NET. REPLACED BRACKET, FABRICATED PER BAC SRM 51-10-01 AND 51-30-02.
Part: DUCT — CRACKED (NR 1 ACM)
DUCT CRACKED AT NR 1 AIR CYCLE MACHINE. REMOVED AND REPLACED DUCT PER BAC MM 21-50-03.
Part: FAIRING — PULLED RIVETS (LT HORIZ STAB)
RIVET HEADS SUNK INTO UPPER FIXED FAIRING MID SECTION ON LEFT HORIZONAL STABLIZER. MADE FIBERGLASS REPAIR PER BAC SRM 51-40-09.
Part: RIVET — SHEARED (RT MLG)
SHEARED RIVETS ON AFT OUTBOARD CORNER OF RIGHT BODY GEAR. REPLACED DAMAGED RIVETS PER BAC SRM 51-30-02.
Part: FAIRING — BROKEN (BS 920)
BROKEN DRAIN HOLE FAIRING AT BODY FAIRING STATION 920. REPAIRED BODY FAIRING DRAIN HOLE FAIRING PER BAC 53-30-03.
Part: DRAIN LINE — CRACKED (NR 3 SEPARATOR)
CRACKED DRAIN LINE AT NR 3 PACK WATER SEPARATOR. REPLACED DAMAGED LINE WITH NEW LINE AND INSTALLED PER BAC MM 21-51-00.
Part: B-NUT — LOOSE (NR 4 PYLON)
NR 4 HYDRAULIC SYSTEM LOSS OF FLUID. DEPRESSURIZED ENGINE DRIVEN PUMP. FOUND LOOSE B-NUT ON ENGINE DRIVEN PUMP SUPPLY LINE. LEAK CHECK OK PER MAINTENANCE MANUAL 29-00-00.
Part: HYD LINE — LOOSE (NR 4 PYLON)
NR 4 HYDRAULIC SYSTEM LOW QUANTITY LIGHT CAME ON AFTER TAKEOFF. DEPRESSURIZED ADP AND EDP QUANTITY STABILIZED AT 1.6 GALLONS. AFTER SYSTEM USED FOR LANDING QUANTITY RAISED TO 4.0 GALLONS THEN DROPPED TO 3 GALLONS AFTER LANDING. TIGHTENED LOOSE B-NUT ON SUPPLY LINE AT TOP OF PYLON, LEAK CHECK OK PER BOEING MAINTENANCE MANUAL 29-11-00.
Part: DOUBLER — CRACKED (NR 4 PYLON)
CRACKED DOUBLER ON NR 4 PYLON LEFT SIDE AFT OF REAR MOUNT AREA. REMOVED DOUBLER, FABRICATED, AND INSTALLLED NEW DOUBLER PER BOEING SRM 54-10-03.
Part: DUCT — CRACKED (NR 4 PYLON)
CRACKED PNEUMATIC DUCT NR 4 PYLON BY T-CONNECTION FOR PRESSURE ANTICIPATOR ASSEMBLY. REMOVED AND REPLACED DUCT PER BOEING MAINTENANCE MANUAL 36-11-01.
Part: SKIN — CRACKED (RT MLG DOOR)
RIGHT HAND BODY GEAR DOOR INNER SKIN CRACKED UNDER ATTACH ROD FITTING SUPPORT FRAME. REMOVED DAMAGED SECTION OF SKIN, INSTALLED DOUBLER REPAIR ON INNER FRAME, INSTALLED DOUBLER ON DOOR INNER SKIN IAW SRM 51-40-02.
Part: PANEL — DAMAGED (RT WING LE)
FOUND RIGHT WING TOP LEADING EDGE AT NR 19 VARIABLE CAMBER FLAP WITH PREVIOUS COMPOSITE REPAIR CHIPPING AND ERODED. APPLIED NEW FIBERGLASS REPAIR IAW SRM 51-40-15.
Part: PANEL — DAMAGED (LT ELEVATOR)
FOUND LEFT OUTBOARD ELEVATOR PANEL DAMAGED. REPAIRED PER SRM 51-40-04.
Part: PANEL — DELAMINATED (HORIZ STAB)
FOUND PREVIOUS REPAIR ON UPPER SURFACE LEFT HORIZONTAL STABILIZER TRAILING EDGE PANEL DELAMINATED. REPAIRED IAW SRM 51-40-06.
Part: NOSE COWL — CRACKED (NR 3 ENGINE)
FOUND NR 3 ENGINE NOSE COWL DENTED AND CRACKED AT THE 8 O'CLOCK POSITION. POTTED DENT, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-40-06.
Part: PANEL — DELAMINATED (FUSELAGE)
FOUND PANEL DELAMINATED AFT OF NR 2 PACK HEAT EXCHANGER. REMOVED DELAMINATED SKIN, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 51-40-15.
Part: PANEL — DAMAGED (RT WING LE)
FOUND RIGHT WING TOP LEADING EDGE PANEL AT NR 18 VCF WITH PREVIOUS COMPOSITE REPAIR MISSING TOP SURFACE, EXPOSING CORE MATERIAL. REPAIRED LEADING EDGE PANEL WITH FIBERGLASS OVERLAYS IAW SRM 51-30-02.
Part: PANEL — DELAMINATED (FUSELAGE)
FOUND PANEL DELAMINATED AFT OF NR 3 PACK HEAT EXCHANGER. REMOVED DELAMINATED SKIN, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 51-40-15.
Part: CORE COWL — CRACKED (NR 1 ENGINE)
FOUND OLD REPAIR CRACKED AND BROKEN ON NR 1 ENGINE OUTBOARD CORE COWL, AFT TOP END. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW REPAIR IAW SRM 51-30-02.
Part: TURBINE EXH — CRACKED (NR 3 ENGINE)
NR 3 ENGINE 'R' AND 'S' RAILS CRACKED IN PREVIOUS WELDED AREAS AT 12 O'CLOCK POSITION. THE 'S' FLANGE CLEVIS PIN HAS PINHOLE CRACK, THE 'R' FLANGE 12 O'CLOCK RACETRACK SLOT RADIAL CRACK TO RAIL. INSPECTED TURBINE EXHAUST CASE AT 1,000 HR INTERVALS FOLLOWING DISCOVERY OF INITIAL CRACK INDICATION TO ENSURE ABOVE LIMITS HAVE NOT BEEN EXCEEDED.
Part: FLANGE — CRACKED (NR 2 CORE COWL)
FOUND NR 2 ENGINE INBOARD CORE COWL MATING FLANGE ON T/R TRAILING EDGE CRACKED AND WORN. REMOVED AND REPLACED FLANGE IAW SRM 51-10-01.
Part: TE TIP — CRACKED (NR 2 PYLON)
FOUND NR 2 ENGINE OUTBOARD PYLON TRAILING EDGE TIP HAD FASTENER MISSING AND CRACKED END. REMOVED PART, WELDED ON TRAVELER, INSTALLED PART IAW SRM 51-30-02.
Part: DOOR — DAMAGED (RT AC BAY)
FOUND HOLE IN HONEYCOMB PANEL ON INTERIOR SURFACE OF LOWER FUSELAGE RIGHT HAND AIR CONDITIONING BAY DOOR, THIRD ONE AFT. REPAIRED DOOR IAW SRM 51-40-15 AND SRM 51-40-09.
Part: COWL — DELAMINATED (NR 4 ENGINE)
FOUND NR 4 ENGINE OUTBOARD FAN COWL DELAMINATED AT 2 O'CLOCK POSITION. REMOVED AND REPLACED OUTBOARD FAN COWL IAW MM 71-11-04.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
FOUND CREW SLIDE DOOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY ASSY AND RELAMPED IAW MM 33-51-00, OPS CHECK NORMAL.
Part: PANEL — MISSING (WS 1116)
UPPER WING PANEL DEPARTED IN FLIGHT, CONTINUED WITHOUT ANY DIFFICULTIES. MISSING PANEL LOCATION, INBOARD OF LEADING EDGE STA 1116, APPROX 3 FT BY 4 FT. ALL FASTENERS STILL INSTALLED. TEMPORARY PANEL FABRICATED FOR FERRY FLIGHT TO NEW YORK. PANEL REPLACED IN NEW YORK IAW SRM 51-30-02.
Part: SKIN — CRACKED (LT TE FLAP)
FOUND CRACK IN LOWER EDGE ON INBOARD EDGE, AFT T/E FLAP LEFT WING. REPAIRED SAME IAW SRM 51-40-09.
Part: FRAME — CRACKED (NR 2 PYLON)
FOUND CRACKED FRAME AND IMPROPERLY INSTALLED REPAIR DOUBLER ON LEFT HAND SIDE SKIN UPPER MOST OVAL HOLE. OLD REPAIR REMOVED, NEW DOUBLER MANUFACTURED FROM STAINLESS STEEL AND INSTALLED IAW SRM 54-12-02.
Part: PANEL — DELAMINATED (HORIZ STAB)
FOUND DELAMINATED PANELS 334DB, 334HB, 334KB ON LEFT HORIZONTAL STABILIZER. REPAIRED SAME IAW SRM 51-40-06.
Part: FAIRING — CRACKED (LT MLG DOOR)
FOUND LT WLG STRUT DOOR FAIRING CRACKED ON FWD AND AFT CORNERS. REPAIRED SAME IAW SRM 51-40-09.
Part: SKIN — DELAMINATED (LT WING)
FOUND DELAMINATED AREAS ON LEFT WING L/E UPPER SKIN BEHIND INBOARD SIDE OF L/E FLAP NR 8 AND NR 10. REPAIRED SAME IAW SRM 51-40-09.
Part: PANEL — DELAMINATED (LT WING)
FOUND DELAMINATED AREAS ON LEFT WING UPPER SKIN AT T/E BETWEEN SPOILER NR 4 AND INBOARD AILERON AND ON TRIANGLE PANEL INBOARD TO GATE FITTING. REPAIRED IAW SRM 51-40-09.
Part: COWL — CRACKED (NR 3 ENGINE)
FOUND LOWER AFT CORNER OF NR 3 LT FAN COWL CRACKED, NR 3 RT FAN COWL CRACKED AT OLD REPAIR. REPAIRED IAW SRM 51-40-06.
Part: BRACKET — CRACKED (LT WING GEAR)
FOUND CRACKED BRACKET IN LT WLG DOOR CUTOUT ON LG SUPPORT BEAM. FABRICATED AND INSTALLED NEW BRACKED IAW SRM 51-30-02.
Part: SKIN — CORRODED (WING CTR SECT)
FOUND LEVEL 1 CORROSION ON SKIN ABOVE LOWER CHORD OF FRONT SPAR IN WING CENTER SECTION DRY BAY, BS 1000 LBL 33. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-1.
Part: SKIN — CORRODED (WING)
FOUND LEVEL 1 CORROSION ON CEILING SKIN OF WING CENTER SECTION DRY BAY, BETWEEN FRONT SPAR AND S-28C BETWEEN RBL TO LBL 128. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: RIB — CRACKED (NR 4 PYLON)
FOUND CRACK IN NR 4 PYLON INTERIOR CAVITY RIB NS 163. DEFECTIVE AREA REMOVED AND REPAIRED IAW SRM 54-12-02.
Part: SKIN — CHAFED (NR 2 PYLON)
FOUND RT INTERIOR SKIN LOWER EDGE CHAFED ON NR 2 PYLON, NS 222. PATCHED AND RIVETED IAW SRM 54-12-02.
Part: PANEL — CORRODED (BS 760-780)
FOUND LEVEL 1 CORROSION AROUND FASTENERS ON LAV SERVICE PANEL, LOWER FUSELAGE BETWEEN BS 760 TO 780. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. INSTALLED NEW FASTENERS/RIVETS.
Part: SUPPORT — CORRODED (BS 900)
FOUND LEVEL 1 CORROSION AND CRACKED AIR LOCKS ON FAIRING SUPPORT, LOWER FUSELAGE AT BS 900 BETWEEN BL 0 AND LBL 50. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF 53-10-01. INSTALLED NEW AIR LOCKS IAW SRM 57-30-02.
Part: SKIN — CORRODED (WS 1280-1485)
FOUND LEVEL 1 CORROSION ON LEFT WING LOWER SURFACE AROUND FUEL TANK ACCESS BETWEEN WS 1280 TO 1485. REMOVED CORROSION IAW SRM 51-10-01, VERIFIED WITHIN LIMITS OF SRM 57-10-01.
Part: BEAM — CORRODED (LT WING GEAR)
FOUND LEVEL 1 CORROSION ON LT WING L/G BEAM AFT SIDE STA 1350. CORROSION REMOVED IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SUPPORT — CORRODED (BS 840)
FOUND LEVEL 1 CORROSION ON FAIRING SUPPORT LOWER FUSELAGE AT BS 840 RIGHT SIDE NEAR STR 37. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: PANEL — CRACKED (LT LE FLAP)
FOUND CRACK ON LEADING EDGE FIBERGLASS PANEL ON LEADING EDGE FLAPS 6, 7, 10, 11. REPAIRED IAW SRM 51-40-09.
Part: PANEL — DELAMINATED (VERT STAB)
FOUND LEFT SIDE PANEL NR 324AL ON VERTICAL STABILIZER DELAMINATED. REPAIRED IAW SRM 51-40-06.
Part: PANEL — DELAMINATED (RT WING)
FOUND DELAMINATION ON RT WING LEADING EDGE FIBERGLASS PANEL TOP OF WING, NEAR NR 18 AND NR 19 LEADING EDGE. REPAIRED IAW SRM 51-40-09.
Part: SKIN — CORRODED (WS 1084)
FOUND LEVEL 1 CORROSION ON LEFT WING UPPER SURFACE BETWEEN MID AND REAR SPARS AROUND WS 1084. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: BEAM — CORRODED (LT WING GEAR)
FOUND LEVEL 1 CORROSION ON UPPER CHORD OF LT WING L/G BEAM STA 1350. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-30-01.
Part: BRACKET — CRACKED (NR 2 ENGINE)
FOUND SKIN SEPARATION WITH SMALL CRACK IN ENGINE FAN COWL TOP BRACKED AFT MOUNT FITTING GROOVE ON NR 2 ENGINE. INSTALLED NEW SKIN IAW SRM 51-30-02.
Part: SPAR CHORD — CORRODED (WING)
FOUND LEVEL 1 CORROSION ON FRONT SPAR UPPER CHORD IN WING CENTER SECTION DRY BAY BS 1000 BETWEEN LBL TO RBL 120. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SKIN — CORRODED (BS 2200)
FOUND LEVEL 1 CORROSION AND SKIN SWELLING ON LOWER FUSELAGE NEAR BS 2200 STR 33. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SKIN — CORRODED (BS 1000)
FOUND LEVEL 1 CORROSION ON SKIN ON LOWER CHORD OF FRONT SPAR IN WING CENTER SECTION AT ACCESS TO DRY BAY, BS 1000 APPROX RBL 98. CORROSION REMOVED IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SKIN — CRACKED (NR 4 PYLON)
FOUND CRACK IN SKIN FRONT SPAR NS 128.5 AT NR 4 PYLON. REPAIRED IAW SRM 54-12-02.
Part: ELEVATOR — CRACKED (LEFT)
FOUND INBOARD AFT CORNER OF LEFT HAND INBOARD ELEVATOR CRACKED. REPAIRED IAW SRM 51-40-09.
Part: PANEL — CRACKED (RT OUTBD AILERON)
FOUND CRACKED PANEL BETWEEN TWO INBOARD BALANCE WEIGHTS OF RT OUTBOARD AILERON. REPAIRED IAW SRM 51-40-09.
Part: PANEL — CRACKED (LT WING)
FOUND FIBERGLASS PANEL ON LOWER LEFT WING NEAR NR 3 CANOE CRACKED. REPAIRED IAW SRM 51-40-09.
Part: SKIN — DELAMINATED (BS 1475-1540)
FOUND DELAMINATED AREA AND HOLES ON RT UPPER FUSELAGE AT OVERWING FAIRINGS, BS 1475 TO 1540. REPAIRED SAME IAW SRM 51-40-09.
Part: FAIRING — DELAMINATED (BS 1475-1540)
FOUND DELAMINATED AREAS AND HOLES ON FUSELAGE WING BODY FAIRINGS, BS 1475 TO 1540. REPAIRED IAW SRM 51-40-09.
Part: SKIN — CRACKED (NR 2 PYLON)
FOUND LEFT HAND SIDE SKIN NS 180 LOWER CORNER CRACKED ON INTERIOR SIDE. NEW STRAP FIRE SHIELD MANUFACTURED AND INSTALLED IAW SRM 54-12-02.
Part: FRAME — CRACKED (NR 2 PYLON)
FOUND RIGHT SIDE FORWARD CORNER ON SLOT SEAL INST FRAME CRACKED. CRACK REMOVED, PATCH FABRICATED FROM 301 1/2 HARD STAINLESS STEEL AND INSTALLED IAW SRM 54-12-02.
Part: SKIN — DELAMINATED (RT HORIZ STAB)
FOUND DELAMINATED AREA ON RIGHT STABILIZER UPPER SURFACE AHEAD OF OUTBOARD ELEVATOR AND BEHIND REAR SPAR. REPAIRED IAW SRM 51-40-06.
Part: PANEL — CORRODED (BS 1000)
FOUND LEVEL 1 CORROSION ON FAIRING SUPPORT AND PANEL ON LOWER FUSELAGE BS 1000 BETWEEN BL 0 AND RBL 25. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: PANEL — PUNCTURED (RT WING)
FOUND HOLE ON INBOARD SURFACE OF LOWER FIXED PANEL, RT WING T/E CAVITY. REPAIRED IAW SRM 51-40-09.
Part: STRINGER — CORRODED (WING CTR SECT)
FOUND LEVEL 1 CORROSION ON HORIZONTAL STRINGERS IN CEILING OF WING CENTER SECTION DRY BAY, BETWEEN S-23C AND S-29C BETWEEN RBL TO LBL 128. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: PANEL — DELAMINATED (RT WING)
FOUND DELAMINATED PANEL ON RT WING UPPER SURFACE NEAR NR 2 SPEED BRAKE. REPAIRED SAME IAW SRM 51-40-09.
Part: COWL — CRACKED (NR 1 ENGINE)
FOUND CRACK IN OLD REPAIR OF NR 1 RT FAN COWL. REPAIRED IAW SRM 51-40-06.
Part: PANEL — DELAMINATED (RT WING)
FOUND DELAMINATED TOP PANEL ON RIGHT WING FORWARD OF NR 8 SPOILER. REPAIRED IAW SRM 51-40-09.
Part: COWL — CHAFED (NR 4 ENGINE)
FOUND UPPER EDGE CHAFED ON 4R ENGINE SIDE COWL. FABRICATED STRAP AND REPAIRED IAW SRM 51-40-02.
Part: ACCESS DOOR — CRACKED (NLG)
FOUND NOSE LANDING GEAR SERVICE INTERPHONE ACCESS DOOR CRACKED. REPAIRED SAME IAW SRM 51-40-09.
Part: STRAP — CRACKED (NR 3 PYLON)
FOUND CRACKED STRAP ON BOTH SIDES OF NR 3 SKIRT FORWARD EDGE. REPAIRED IAW SRM 54-12-02.
Part: SPAR CHORD — CORRODED (WING CTR SECT)
FOUND LEVEL 1 CORROSION AROUND RIVET ON LOWER CHORD OF FRONT SPAR IN WING CENTER SECTION DRY BAY, BS 1000 LBL 57. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SKIN — DELAMINATED (WS 807)
FOUND DELAMINATED AREA OVER UPPER WING LEADING EDGE SURFACE ON RT WING APPROX WS 807. REPAIRED SAME IAW SRM 51-40-09.
Part: VANE — CRACKED (NR 4 ENG)
FOUND CRACK ON NR 4 ENGINE CASCADE VANE. CRACK TREATED IAW SRM 51-10-02.
Part: FAIRINGS — DELAMINATED (BS 1475-1540)
FOUND DELAMINATED AREAS AND HOLES LT UPPER FUSELAGE AT OVERWING FAIRING, BS 1475 TO 1540.
Part: SUPPORT — CORRODED (BS 860)
FOUND LEVEL 1 CORROSION ON FAIRING SUPPORT LOWER FUSELAGE, BS 860 BETWEEN LBL 40 AND RBL 25. CORROSION REMOVED IAW SRM 51-10-01, FOUND WITHIN LIMITS OF 53-10-01.
Part: FLAP — CRACKED (NR 6/7)
FOUND CRACK ON LOWER EDGE OF LEADING EDGE FLAPS 6 AND 7. REPAIRED IAW SRM 51-40-09.
Part: FRAME — CRACKED (BS 2200)
FOUND FRAME LOWER CHORD STA 2200 STR 44 RT SIDE CRACKED. REINFORCED AND REPAIRED SAME IAW SRM 53-10-04.
Part: PANEL — DELAMINATED (RT HORIZ STAB)
FOUND RT STABILIZER PANELS 344HB, 344QB, 344JB DELAMINATED. REPAIRED IAW SRM 51-40-06.
Part: EYE BOLTS — CORRODED (CCA ASSY)
FOUND ALL EYE BOLTS ON PUSH-PULL RODS ON CCA PROGRAMMER CORRODED, RT W/G WHEEL WELL. REMOVED CORROSION IAW SRM 53-10-01, PAINTED IAW CP 20-40-00.
Part: TIP — DELAMINATED (RT WING)
FOUND PANEL DELAMINATED ON RT WING TIP UPPER SURFACE. REPAIRED SAME IAW SRM 51-40-06.
Part: SKIN — CORRODED (WS 585/807)
FOUND LEVEL 1 CORROSION ON LEFT WING UPPER SURFACE ABOVE THE CENTER WING SPAR AROUND WS 585.62 AND WS 807. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SKIN — CRACKED (RT LE FLAP)
FOUND TOP EDGE CRACKED ON LEADING EDGE FLAPS 19, 23 AND 25 RT WING. REPAIRED IAW SRM 51-40-09.
Part: SKIN — CORRODED (WS 1392)
FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE WING CENTER SPAR AROUND WS 1392. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SKIN — CORRODED (WS 586.62)
FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE AROUND WING CENTER SPAR AT WS 586.62. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: HINGE — CORRODED (CARGO DOOR)
FOUND LEVEL ONE CORROSION ON AFT CARGO DOOR UPPER HINGE CONNECTING TO FUS SKIN BS 1820 TO 1960. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: HINGE — CORRODED (CARGO DOOR)
FOUND LEVEL ONE CORROSION ON FWD DOOR UPPER HINGE CONNECTING TO FUS SKIN BS 560 TO 660. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SKIN — CORRODED (WS 862-1000)
FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE REAR SPAR BETWEEN WS 862 AND 1000. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SKIN — CORRODED (WS 1308/1336)
FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE REAR SPAR BETWEEN WS 1308 AND 1336. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: DOOR SILL — CRACKED (CARGO DOOR)
FOUND CRACK IN MAIN DECK SIDE CARGO DOOR SILL AT LOWER AFT END. REPAIRED CRACK IAW SRM 51-40-02.
Part: SKIN — CORRODED (WS 323.82)
FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE BETWEEN STR 26 AND WING CENTER SPAR NEAR WING ROOT, WS 323.82. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: PANEL — LOOSE (BS 1780)
FOUND BENT AND LOOSE RIVETS ON AFT CARGO DOOR SWITCH ACCESS PANEL, BS 1780 STR 35 TO 36. FABRICATED AND INSTALLED NEW PANELS AND FASTENERS IAW SRM 51-30-02.
Part: SKIN — CORRODED (WS 1336/1364)
FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE WING FRONT SPAR BETWEEN STA WS 1336 AND 1364. CORROSION REMOVED IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SKIN — CORRODED (WS 917-1140)
FOUND LEVEL ONE CORROSION ON LEFT LOWER WING SURFACE AT FUEL TANK ACCESS BETWEEN WS 917 AND 1140. REMOVED CORROSION IAW SRM 51-10-01, TREATED IAW SRM 51-10-02.
Part: SKIN — CORRODED (FS 1840-1880)
FOUND LEVEL ONE CORROSION ON LEFT LOWER FUSELAGE BETWEEN BS 1840 AND 1880, STR 49. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SKIN — CORRODED (WS 1516-1548)
FOUND LEVEL ONE CORROSION ON RIGHT WING LOWER SURFACE NEAR FUEL TANK ACCESS BETWEEN WS 1548.20 AND 1516.60. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
Part: SKIN — CORRODED (WS 917-1364)
FOUND LEVEL ONE CORROSION ON RIGHT WING LOWER SURFACE AROUND WING FUEL TANK ACCESS BETWEEN WS 917 AND 1364. REMOVED CORROSION IAW SRM 51-10-01, TREATED AREA IAW SRM 51-10-02.
Part: SKIN — CORRODED (WS 642-669.5)
FOUND LEVEL ONE CORROSION ON LEFT WING LOWER SURFACE AROUND FUEL TANK ACCESS BETWEEN WS 642 AND 669.50. REMOVED CORROSION IAW SRM 51-10-01, TREATED AREA IAW SRM 51-10-02.
Part: LE FLAP — BENT (LT WING)
FOUND LEADING EDGE FLAP NR 10 OUTBOARD CORNER FOLDED AND BENT. REPAIRED IAW SRM 57-50-03 AND INSTALLED PER SRM 51-30-02.
Part: ANGLE — BROKEN (BS 840)
FOUND BROKEN ANGLE AT CONNECTING POINT TO CEILING SUPPORT CHANNEL BS 840 NEAR LBL 33. FABRICATED NEW ANGLE IAW SRM 53-10-21 AND INSTALLED IAW SRM 51-30-02.
Part: SKIN — CORRODED (WS 469.82)
FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE REAR SPAR AT WS 469.82. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01.
1995
Part: FAN BLADES — FOD (NR 1/2/3 ENGINES)
DISCOVERED FAN BLADE DAMAGE NUMBERS 1, 2 AND 3 ENGINES, DUE TO ICE INGESTION. BLENDED BLADES TO FLYBACK LIMITS AT EWE AND AT JFK REPLACED COMPLETE SET OF FAN BLADES ON NR 2 ENGINE. BLENDED AND REPLACED MATCHED SETS NR 1 AND NR 3 ENGINE IAW MM 72-31-02.
Part: SEAT TRACK — CRACKED (FO SEAT)
FOUND FIRST OFFICER'S AFT INBOARD SEAT TRACK CRACKED AT FORWARD END. REPLACED SEAT TRACK IAW MM 25-11-01, OPS CHECK OK.
Part: A-12 CARD — INOPERATIVE (LOGIC MODULE)
DURING LANDING APPROACH WITH FLAPS AT 25 DEGREES AND GEAR DOWN, WARNING HORN SOUNDED AND COULD NOT SILENCE WARNING HORN. FOUND A-12 CARD IN PRIMARY LANDING GEAR LOGIC MODULE INOP. REPLACED A-12 CARD IAW MM 32-61-14, OPS CHECKS GOOD.
Part: SWITCH MODULE — FAILED (CONTROL STAND)
AFTER ENGINE START, TAXI AND DURING FLIGHT ENGINEER CHECK, SHUT OFF NR 4 ENGINE FUEL BOOST PUMPS AND ENGINE SHUTDOWN. REPLACED START LEVER CONTROL STAND SWITCH MODULE PER MAINTENANCE MANUAL 76-11-02.
Part: DUCT — FAILED (LT WING)
ON PUSH-BACK, LT WING OVERHEAT LIGHT AND FORWARD CARGO OVERHEAT LIGHT CAME ON. REPLACED FAILED DUCT BETWEEN NR 1 AND NR 2 PYLON.
Part: SKIN — CRACKED (NR 4 PYLON)
SKIN CRACK AT NR 4 PYLON, FORWARD ACCESS DOOR CUTOUT 1.75 INCH LONG, TERMINATES AT FASTENER. REPAIRED PER BOEING SRM 54-30-03 FIG 17B.
Part: STRINGER — CRACKED (BS 480)
ON WALK AROUND FOUND POPPED FASTENERS AT BS 480, STRINGERS 44 AND 47. ALSO, FOUND CRACKED STRINGER AND CORROSION. REPAIRED PER BOEING SRM 53-30-03.
Part: TIRE — BLOWN (NR 9)
NR 9 TIRE CAME APART OUT OF SEL. REPLACED NR 9 AND NR 10 TIRES, REPLACED BROKEN BODY GEAR CONNECTING ROD, TESTED ANTI-SKID SYSTEM, AND PERFORMED BLOWN TIRE INSPECTION.
Part: TIRE — BLOWN (RT BODY GEAR)
AFTER TAKEOFF OUT OF KHV, TOWER REPORTED RUBBER ON RUNWAY. ON LANDING IN ANC FOUND NR 9 AND NR 10 TIRES BLOWN. DAMAGE TO BODY GEAR DOOR LINKAGE, GEAR DOOR HANDLE, SEVERAL CONDUITS, HYDRAULIC LINES, PRESSURE WEB STIFFENERS. INVESTIGATING CAUSE OF FAILURES WILL UPDATE.
Part: TIRE — BLOWN (RT BODY GEAR)
DURING TAKEOFF, SLIGHT SHUDDER FELT SUSPECTED TIRE DAMAGE, CONTINUED TAKEOFF. ON LANDING IN NAN FOUND NR 9 AND NR 10 TIRES BLOWN ALONG WITH MINOR DAMAGE TO RT INBOARD BODY GEAR SHOCK STRUT DOOR. ALSO, FOUND NR 12 WHEEL DAMAGED. REMOVED AND REPLACED NR 9, 10 AND 12 WHEEL AND TIRE ASSEMBLIES. PERFORMED INTERIM REPAIR ON GEAR DOOR.
Part: HYD UNION — CRACKED (NR 1 PYLON)
FLT 9601 - MIA-ASU - AIRCRAFT EXPERIENCED RAPID LOSS OF FLUID FROM HYDRAULIC SYSTEM 1. DEPRESSURIZED ENGINE DRIVEN PUMP. DIVERTED TO CCS. GEAR EXTENSION AND LANDING NORMAL. FOUND UNION FITTING CRACKED INTERIOR OF THE PYLON AT BULKHEAD MID PYLON. REPLACED FITTING, LEAK CHECK OK. (W)
Part: SKIN — DEBONDED (LT TE FLAP)
LEFT INBOARD MID FLAP, P/N 65B0202527, LOWER SURFACE, INBOARD SURFACE NEAR INBOARD TRACK, LEADING EDGE PANEL HAS DEBONDED INBOARD EDGE. REPAIRED IAW BOEING SRM 51-40-15. TOTAL CYCLES 18,248.
Part: SKIN — DELAMINATED (LT T/E PANEL)
LEFT WING TRAILING EDGE PANEL OUTBOARD OF FLIGHT SPOILER P/N 65B0817173, DELAMINATED (FORWARD EDGE AND OUTBOARD REAR). REPAIRED IAW BOEING SRM 51-40-14. TOTAL CYCLES 18,248.
Part: SKIN — DELAMINATED (RT WING)
DELAMINATION (4 INCHES BY 6 INCHES) RIGHT WING PANEL JUST BELOW R3 DOOR. REPAIRED IAW BOEING SRM 51-40-09. TOTAL CYCLES 18,248.
Part: SKIN — DEBONDED (LT TE FLAP)
INBOARD LEFT MID FLAP, P/N 65B0202527, OVER 2ND ATTACH ARM OF THE AFT TRAILING EDGE FLAP HAS 2 INCH DEBONDED AREA. REPAIRED IAW BOEING SRM 51-40-15. TOTAL CYCLES 18,248.
Part: LE SKIN FLAP — GOUGED (RT TE FLAP)
GOUGED LEADING EDGE RIGHT WING OUTBOARD FORE FLAP P/N 65B019014, 28.5 INCHES FROM OUTBOARD EDGE. REPAIRED IAW SRM 51-40-09 TABLE 1. TOTAL CYCLES 18,248.
Part: SKIN — CRACKED (LT INBD AILERON)
LOWER SURFACE LEFT INBOARD AILERON, P/N 65B001173, 5 INCH AREA CRACKED TO HONEYCOMB. REPAIRED IAW BOEING SRM 51-40-09 TABLE 1. TOTAL CYCLES 18,248.
Part: SKIN — DELAMINATED (LT TE FLAP)
LEFT INBOARD FORE FLAP, P/N 65B89011601, LOWER SURFACE AFT OF CARRIAGE ATTACH BRACKET HAS 25 INCH AREA OF DELAMINATION. REPAIRED IAW BOEING SRM 51-40-06. TOTAL CYCLES 18,248.
Part: SKIN — DELAMINATED (LT AILERON)
DELAMINATION LEFT INBOARD AILERON, P/N 65B001173, INBOARD CORNER UPPER AND LOWER SURFACE HAS 12 INCH AREA OF DELAMINATION. REPAIRED AILERON IAW SRM 51-40-15 TABLE 1. TOTAL CYCLES 18,248.
Part: SKIN — DELAMINATED (TE FLAP)
DELAMINATION (3 INCHES BY 5 INCHES) BOTTOM SIDE AIRCRAFT LEFT INBOARD TRAILING EDGE FLAP P/N 65B020707 APPROXIMATELY 4 INCHES FROM INBOARD END. REPAIRED IAW BOEING SRM 51-40-06.
Part: SKIN — DELAMINATED (RT TE FLAP)
DELAMINATION TOPSIDE RIGHT OUTBOARD MID FLAP TRAILING EDGE P/N 65B0192538, 72 INCHES FROM OUTBOARD END (1 INCH BY 5 INCHES). REPAIRED IAW BOEING SRM 51-40-15.
Part: SKIN — DELAMINATED (TE MID FLAP)
DELAMINATION LEFT INBOARD FLAP P/N 65B620701 LOWER SURFACE DELAMINATED AT INBOARD TRAILING EDGE. REPAIRED PER BOEING SRM 51-40-15.
Part: SKIN — DELAMINATION (NR 3 SPOILER)
DELAMINATION NR 3 FLIGHT SPOILER P/N 65B0225043 UPPER AND LOWER SURFACES. TWO LARGE AREAS INBOARD EDGE. THE COMPLETE LENGTH ON OUTBOARD TRAILING EDGE APPROXIMATELY 15 SQUARE INCHES. REPLACED SPOILER ASSEMBLY IAW BOEING MM 27-61-02.
Part: SKIN — DELAMINATED (NR 1 SPOILER)
LEFT WING TRAILING EDGE PANEL OUTBOARD OF NR 1 SPOILER, P/N 65B0817173, LOWER CORNER DELAMINATED AND WORN TO HONEYCOMB (2 INCH BY 3 INCH AREA). REPAIRED IAW WITH BOEING SRM 51-40-06. TOTAL CYCLES 18,248.
Part: SKIN — DELAMINATED (RT TE FLAP)
GOUGE IN TOP SIDE OF THE RIGHT OUTBOARD AFT FLAP P/N 65B019002 15 INCHES FROM OUTBOARD END. REPLACED BOLT CAUSING DAMAGE. REPAIRED GOUGE IAW BOEING SRM 51-40-6.
Part: PANEL — DELAMINATED (WING)
DELAMINATIONPANEL 193C AFT OF LEFT BODY GEAR. REPAIRED EPR BOEING SRM 51-40-9.
Part: SKIN — DELAMINATED (RT TE MID FLAP)
AREA 5 INCHES BY 3 INCHES DELAMINATED, TOPSIDE RIGHT WING INBOARD MID FLAP (P/N 65B0262528) 8 INCHES FROM INBOARD EDGE AND 26 INCHES FROM AFT EDGE. REPAIRED IAW BOEING SRM 51-40-9.
Part: SKIN — DELAMINATED (LT TE FLAP)
LEFT INBOARD MID FLAP P/N 65B0202527 INBOARD LOWER SURFACE NEAR END DELAMINATED. REPAIRED PER BOEING SRM 51-40-09 TABLE 1 AND 51-40-15.
Part: SKIN — DELAMINATED (LT TE FLAP)
CRACKED AND DELAMINATED AREA LEFT OUTBOARD MID FLAP P/N 65B0192537 LOWER SURFACE AT THE THIRD TRAILING EDGE FLAP ATTACHMENT. REPAIRED IAW BOEING SRM 51-40-14.
Part: SKIN — DAMAGED (RT TE FLAP)
FOUR AREAS OF DAMAGE RIGHT WING INBOARD AFT FLAP P/N 65B0207020, TWO DEEP GOUGES, ONE IS AFT OF THE NR 3 EXTEND/RETRACT ARM AND THE OTHER ONE IS 34 INCHES FROM THE NR 2 EXTENSION/RETRACTION ARM. TWO AREAS OF DELAMINATION, ONE 6 INCHES FROM TRAILING EDGE OUTBOARD AT THE NR 2 EXTEND/RETRACT ARM. THE OTHER 14 INCHES FROM THE TRAILING EDGE OUTBOARD AT THE NR 2 EXTEND/RETRACT ARM. REPLACED AFT FLAP ASSEMBLY IAW BOEING MM 27-51-03. TOTAL CYCLES 18248.
Part: SKIN — CRACKED (TE MID FLAP)
LEFT INBOARD MID FLAP P/N 65B0202527 LOWER SURFACE BETWEEN INBOARD AND OUTBOARD CARRIAGE FORWARD SECTION HAS 3 INCH BY 3 INCH CRACKED AND DELAMINATED AREA. REPAIRED IAW BOEING SRM 51-40-15 TO 51-40-9 TABLE 1.
Part: SKIN — DELAMINATED (TE MID FLAP)
SKIN DELAMINATION RIGHT WING INBOARD MID FLAP P/N 65B0202527 TRAILING EDGE AT NR 2 ACTUATION ARM. REPAIRED IAW BOEING SRM 51-40-15.
Part: O/B MIDFLAP SKIN — WORN (LT TE FLAP)
HONEYCOMB SHOWING (LIGHT SHOWS THROUGH) LEFT OUTBOARD MID FLAP P/N 65B0192537, UPPER AND LOWER SURFACE APPROXIMATELY 1 INCH BY 1 INCH AREA. REPAIRED IAW SRM 51-40-06.
Part: SKIN — CHAFED (TE FORE FLAP)
DEEP CHAFED AREA LEFT INBOARD FORE FLAP P/N 65B39011601 LOWER INBOARD SURFACE 4 INCHES BY 1 INCH. REPAIRED IAW WITH BOEING SRM 51-40-15.
Part: SKIN — WORN (TE FLAP)
WEAR DAMAGE AT OUTBOARD LEFT TRAILING EDGE FLAP P/N 65B019001. REPAIRED IAW BOEING SRM 51-40-15 TO 51-40-09 TABLE 1.
Part: SKIN — DELAMINATED (TE MID FLAP)
DELAMINATED SKIN BOTTOM SIDE RIGHT OUTBOARD MID FLAP P/N 65B0192538, 50 INCHES OUTBOARD OF THE INBOARD JACK SCREW. REPAIRED AREA IAW BOEING SRM 51-40-09.
Part: SKIN — WORN (LT TE FLAPS)
THREE DEEP CHAFED AND WORN AREAS UPPER LEADING EDGE SURFACE LEFT OUTBOARD FORE FLAP P/N 65B019013. REPAIRED IAW BOEING SRM 51-40-09 AND 51-40-15.
Part: SKIN — DELAMINATED (LT TE FLAP)
DELAMINATED FIBERGLASS STRIP LOWER SURFACE AT LEFT OUTBOARD TRAILING EDGE FLAP P/N 65B019001. REPAIRED FLAP IAW BOEING SRM 51-40-15.
Part: SKIN — DELAMINATED (TE MID FLAP)
DELAMINATION ON LOWER SURFACE AT THE LEFT INBOARD FLAP FORE FLAP P/N 65B39011601, OUTBOARD AT THE OUTBOARD CARRIAGE. REPAIRED IAW BOEING SRM 51-40-1 TO 51-40-09 TABLE 1.
Part: SKIN — DELAMINATED (LT TE FLAP)
DELAMINATION AT LEFT INBOARD TRAILING EDGE FLAP P/N 65B020707 INBOARD SECTION CENTER PANEL LOWER SURFACE. REPAIRED DELAMINATION IAW BOEING SRM 51-40-15.
Part: SKIN — DELAMINATED (LT AILERON)
LEFT OUTBOARD AILERON P/N 65B001171 UPPER SURFACE SMALL AREA AT DELAMINATION AREA 1.5 INCH BY 1.5 INCH. REPAIRED IAW BOEING SRM 51-40-06.
Part: UNION — LOOSE NUT (NR 1 PYLON)
AIRCRAFT LEFT ORD WITH 10.5 GALLONS HYDRAULIC FLUID, UPON ARRIVAL AT JFK HYDRAULIC QUANTITY FOR SYSTEM 1 6.5 GALLONS. TIGHTENED B-NUT AT CHECK VALVE IN PYLON REF IPC 29-11-03-01 FIG 335. LEAK CHECK OK. (W)
Part: WIRE — FAULTY (GEAR EXT)
EN ROUTE TO ORD, AIRCRAFT EXPERIENCED LOSS OF NR 1 SYSTEM HYDRAULIC QUANTITY. ON APPROACH TRIED TO LOWER FLAPS AND GEAR USING ALTERNATE SYSTEM. RT BODY GEARS WOULD NOT LOWER AND INBOARD FLAPS WOULD NOT EXTEND. REVERTED TO HYDRAULIC MODE. OPERATION OF GEAR AND FLAPS WAS NORMAL. ON POST FLIGHT INSPECTION, FOUND HYDRAULIC FLUID LEAKING FROM NR 1 PYLON. OPERATION CHECK OF ALTERNATE FLAP FOUND ELECTRIC DRIVE MOTOR FAILED. CHECK OF ALTERNATE GEAR EXTENSION SYSTEM INDICATES WIRING PROBLEM. SECURED B-NUT ON HYD RETURN LINE UNION IN WING TO UPPER PYLON DISC BOX. TIGHTENED B-NUT AT CHECK VALVE IN PYLON RED IPC 29-11-03-01 FIG 335. LEAK CHECK OK. (W)
Part: MOTOR — FAILED (INBOARD T/E FLAP)
EN ROUTE TO ORD, AIRCRAFT EXPERIENCED LOSS OF NR 1 SYSTEM HYDRAULIC QUANTITY. ON APPROACH TRIED TO LOWER FLAPS AND GEAR USING ALTERNATE SYSTEM. RT BODY GEARS WOULD NOT LOWER AND INBOARD FLAPS WOULD NOT EXTEND. REVERTED TO HYDRAULIC MODE. OPERATION OF GEAR AND FLAPS WAS NORMAL. ON POST FLIGHT INSPECTION, FOUND HYDRAULIC FLUID LEAKING FROM NR 1 PYLON. OPERATION CHECK OF ALTERNATE FLAP FOUND ELECTRIC DRIVE MOTOR FAILED. CHECK OF ALTERNATE GEAR EXTENSION SYSTEM INDICATES WIRING PROBLEM. SECURED B-NUT ON HYDRAULIC RETURN LINE UNION IN WIG TO UPPER PYLON DISC BOX. TIGHTENED B-NUT AT CHECK VALVE IN PYLON REF IPC 29-11-03-01 FIG 335. LEAK CHECK OK. (W)
Part: B-NUT — LOOSE (NR 1 HYD)
EN ROUTE TO ORD, AIRCRAFT EXPERIENCED LOSS OF NR 1 SYSTEM HYDRAULIC QUANTITY. ON APPROACH TRIED TO LOWER FLAPS AND GEAR USING ALTERNATE SYSTEM. RT BODY GEARS WOULD NOT LOWER AND INBOARD FLAPS WOULD NOT EXTEND. REVERTED TO HYDRAULIC MODE. OPERATION OF GEAR AND FLAPS WAS NORMAL. ON POST FLIGHT INSPECTION, FOUND HYDRAULIC FLUID LEAKING FROM NR 1 PYLON. OPERATION CHECK OF ALTERNATE FLAP FOUND ELECTRIC DRIVE MOTOR FAILED. CHECK OF ALTERNATE GEAR EXTENSION SYSTEM INDICATES WIRING PROBLEM. SECURED B-NUT ON HYD RETURN LINE UNION IN WING TO UPPER PYLON DISC BOX. TIGHTENED B-NUT AT CHECK VALVE IN PYLON REF IPC 29-11-03-01 FIG 335. LEAK CHECK OK. (W)
Part: PANEL — CRACKED (LT WING SPOILER)
TOP LEFT WING, FIBERGLASS PANEL FWD OF NR 6 SPOILER LEADING EDGE IS CRACKED MARKED. SANDED AREA, CLEANED AND REPAIRED PE SRM 51-40-09. AIRCRAFT RELEASED FOR SERVICE. (W)
Part: FOREFLAP — DELAMINATION (LT INBD FOREFLAP)
LEFT INBOARD FOREFLAP, LEADING EDGE OF OUTBOARD SECTION HAS OVERLAY MISSING FROM PREVIOUS REPAIR AND HAS APPROXIMATELY 4 DELAMINATION. REMOVED FOREFLAP LEADING EDGE. REPAIRS ACCOMPLISHED PER SRM 51-40-09. REINSTALLED LEADING EDGE OF FOREFLAP. AIRCRAFT RELEASED FOR SERVICE. (W)
Part: PANEL — DELAMINATION (LT WING L/E FLAP)
TOP LEFT WING, PREVIOUS REPAIR OF HONEYCOMB UPPER SKIN ABOVE NR 6 LEADING EDGE FLAP COMING APART, MARKED. REMOVED OLD REPAIR, POTTED CORE AND OVERLAYED AREA. REPAIR ACCOMPLISHED PER SRM 51-40-09. AIRCRAFT RELEASED FOR SERVICE. (W)
Part: BLADES — FAILURE (NR 3 ENGINE)
EN ROUTE SYD TO HKG, WHILE RETARDING ENGINES IN CRUISE, NR 4 ENGINE FLAMED OUT, COULD NOT RESTART UNTIL DESCENT TO FL 210. IN KHG, INSPECTED ENGINE PER MM 71-00-00, NO DAMAGE FOUND, AIRCRAFT DISPATCHED. ON CLIMB-OUT FROM HKG, AT FL 164, NR 4 ENGINE STALLED, EGT WENT TO 960 DEGREES WITH VIBRATION. ENGINE SHUT DOWN USING ALTERNATE PROCEDURES. AIRCRAFT RETURNED TO HKG. POST FLIGHT INSPECTION REVEALED METAL IN TAIL PIPE. ENGINE CHANGE CALLED. ADDITIONAL INFORMATION WILL BE SENT WHEN AVAILABLE. AFTER ENGINE CHANGE, AIRCRAFT RELEASED FOR SERVICE.
Part: TIRES — DISINTEGRATED (NR 11/12 MLG)
ON LANDING AT ANC, NR 11 AND 12 MLG TIRES BLEW. KHV TOWER REPORTED THAT AIRCRAFT LEFT RUBBER ON RUNWAY ON TAKEOFF. POST FLIGHT INSPECTION REVEALED DAMAGE TO RT ADF PANEL AND RT. BODY LANDING GEAR STRUT DOOR ROD. MAINTENANCE REPLACED NR 11 AND 12 WHEEL ASSEMBLIES, REPLACED STRUT DOOR ROD AND PERFORMED SPECIAL INSPECTION PER MM 5-51-34. FUSELAGE FAIRING PANELS WERE REPAIRED PER SRM 51-40-03. ADF PANEL HAD INTERIM REPAIR PER SRM UNTIL REPLACEMENT OF RT ADF PANEL HAD INTERIM REPAIR PER SRM UNTIL REPLACEMENT OF RT ADF PANEL ON 4-11-95. AIRCRAFT RELEASED FOR SERVICE.