N929UP
Registered owner: BOEING CO, WA (owner ≠ operator)
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.
163 reports on file, 1995-04-05 – 2003-01-20.
Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 54,888 hrs · 39,648 cycles
INSPECTION TYPE:SP CRACK FOUND ON FUSELAGE ABOVE # 1 ENGINE STATION 1183 STRINGER 4L-8L REMOVED PREVIOUS REPAIR DOUBLER AND DAMAGED AREA I.A.W. SRM.53-30-3 FIG. 26 & 24, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER I.A.W. SRM. 53-30-3 FIG. 26 & 24 AT STA. 1183 BETWEEN STRINGER 4L TO 8L
Earlier reports · 1995–2001 · 162 reports
2001
Part: LIGHT — WILL NOT TEST (COCKPIT DOOR)
INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT AT COCKPIT DOOR WILL NOT TEST. R&R LIGHT ASSY WITH NEW BATTERIES, OPS CHECK K PER MM 33-50-01.
Part: LIGHT — DEFECTIVE (COCKPIT)
INSPECTION TYPE:IN COCKPIT EMERGENCY LIGHT ILLUMINATED DURING FLIGHT THEN FELL OUT OF ITS CONTAINER. UNABLE TO REINSTALL. REINSTALLED EMERGENCY EXIT LIGHT ASSY TEST OK LENS SECURED.
Part: GIRT BAR — INOPERATIVE (ESCAPE SLIDE)
INSPECTION TYPE: PREFLT, ESCAPE SLIDE GIRT BAR STOW HOOKS DO NOT HOLD BAR IN PLACE WHEN SLIDE IS DISENGAGED. REMOVED MAIN ENTRY DOOR SLIDE COVER FOR REPAIR. INSTALLED MAIN ENTRY DOOR EVACUATION SLIDE AND COVER IAW B727 MM 25-60-03.
Part: SLIDE — OUT OF POSITION (DOOR)
INSPECTION TYPE IN ESCAPE SLIDE FELL OUT. RE-PACKED EMERGENCY ESCAPE SLIDE.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS FOUND INOP, PRE-FLT. FOUND BATTERIES WEAK, INSTALLED NEW BATTERIES. OPS CKS NORMAL.
Part: LIGHT — MALFUNCTIONED (COCKPIT)
INSPECTION TYPE:IN, COCKPIT DOOR EMERGENCY LIGHT VERY DIM. OPS CHECK COCKPIT EMERGENCY LIGHTS WITH BOTH THE SWITCH AT THE ASSY AND THE EMERGENCY LIGHT ARM/DISARM ON THE P4. NO DEFECTS NOTED.
Part: LIGHT — INOPERATIVE (CABIN)
INSPECTION TYPE:IN, NEITHER EMERGENCY ENT LIGHT WORKING. RESET SWITCH, OPS CHECK IAW MM 33-50-01. OPS CHECK NORMAL.
Part: ANGLE — CRACKED (FWD LAVATORY)
INSPECTION TYPE:C CK FWD LAV FLOOR INTERCOSTAL ANGLE HAS 2 CRACKS AT STA 320 RIGHT SIDE 20 INCHES FROM RIGHT HAND WALL. INSTALLED DOUBLER REPAIR, ACCOMPLISHED IN ACCORDANCE WITH SRM 51-40-2. REPLACED UPPER ANGLE IN ACCORDANCE WITH SRM 52-30-2.
2000
Part: STRUCTURE — CRACKED (RT WING)
INSPECTION TYPE:C CK RIGHT WING L/E CAVITY AT STA 330.6, EXISTING REPAIR ANGLE IS CRACKED. REMOVED AND REPLACED REPAIR ANGLE IN ACCORDANCE WITH SRM 51-30-2.
Part: LIGHT — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULBS, OPS OK. A/C OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT ABOVE CABIN ENTRANCE DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD.
Part: FLOOR PAN — CRACKED (BS 910)
CRACK AT RT MLG FLOOR PAN STA 910. TRANSFERRED TO DMI D185355 AIRCRAFT TO FERRY TO MIA FOR REPAIR.
Part: WEB — CRACKED (MLG WW)
CRACK AT RT MLG WEB BS STA 910. TRANSFER TO DMI D185355 AC TO FERRY TO MIA FOR REPAIR. ALL FERRY FLIGHT PROCEDURES HAVE BEEN ACCOMPLISHED AND A/C IS IN SAFE OPERATING CONDITION FOR FERRY.
Part: SKIN — DELAMINATED (NLG DOOR)
NLG RT FIXED STRUT DOOR DELAMINATED AT LEADING EDGE. AREA OF DELAMINATION APROX .375 SQ INCH ON LEADING EDGE OF DOOR. REPAIRED PER SRM 51-40-09 PG 25 ITEM TRANSFERRED TO DMI LOG D185351.
1999
Part: FLAP TRACK — CRACKED (LT TE FLAP)
INSPECTION TYPE:N/A LH INBD FLAP OUTBD TRACK CRACKED ***MRR FILED AS OPEN***
Part: SUPPORT — CORRODED (AILERON LOCKOUT)
INSPECTION TYPE:C CORROSION UNDER AFT AILERON LOCKOUT GEARBOX ATTACH BOLT (NUTSIDE) ON L/W O/B AILERON LOCKOUT FITTING. REPLACED AILERON LOCKOUT FITTING (SUPPORT) PER ER NR 99-5678.
Part: SEAT TRACK — CORRODED (BS 590-605)
INSPECTION TYPE:C, SEAT TRACK FROM BS 590 TO 605 RBL 25 WL 208 HAS CORROSION IN CHANNEL. AFTER THE CORROSION REMOVAL PROCESS, FOUND THE AREA TO GO BEYOND ALLOWABLE LIMITS.
Part: SKIN — CORRODED (BS 687)
INSPECTION TYPE:C, CORROSION (C53-113-01.01-01) ON SKIN BS 687 TO 694 LBL 25 JUST ABOVE STR 26 LT SIDE. AFTER REMOVAL OF CORROSION, FOUND THE SKIN TO GO BEYOND ALLOWABLE DAMAGE. REMOVED DAMAGED SECTION. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER ALL DONE IAW SRM 51-10-6, 53-10-1, 51-10-2 AND 51-30-2, SRM 53-30-3.
Part: SKIN — CRACKED (BS 243.7)
INSPECTION TYPE:C, CRACK INDICATED NOTED AROUND 2 FASTENER HEADS AT LT BS 243.7, WL 198.5 AND WL 200. AREAS MARKED IN RED. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED WORK DONE IAW SRM 53-30-3, SRM 51-30-02 AND MM 51-20-151.
Part: SKIN — CRACKED (BS 243.7)
INSPECTION TYPE:C, CRACK INDICATION NOTED AT BS 243.7 WL 229 AROUND FASTENER HEAD MARKED IN RED (RIGHT HAND SIDE. REMOVED DAMAGE, FABRICATED DOUBLER AND INSTALLED WORK DONE IAW SRM 53-30-03, 51-30-02 AND MM 51-20-151.
Part: SKIN — CRACKED (BS 235.8)
INSPECTION TYPE:C CRACK INDICATION NOTED AROUND TWO FASTENER HEADS AT RT BS 235.8 WL 228 AND 229, MARKED IN RED. CUT OUT DAMAGE FABRICATED FILLER AND DOUBLER AND INSTALLED. WORK DONE IAW 53-30-03, 51-10-2, AND 51-30-2
Part: CHORD — CORROSION (BS 349)
INSPECTION TYPE:C, CORROSION (C53-111-03.00-01) ON NOSE MID CHORD BS 349, LBL 15, WL 169. REMOVED CHORD, INSTALLED NEW CHORD. REPLACED WEB WITH FABRICATED WEB, WORK DONE IAW SRM 51-30-2, 53-10-2.
Part: FRAME — CRACKED (BS 930)
BS 930 FRAME INBOARD AND OUTBOARD FLANGE CRACKED, FROM STRINGER 18A TO MAIN LANDING GEAR PRESSURE DECK. REPLACED BS930 FITTING, RIGHT SIDE IN ACCORDANCE WITH BOEING DRAWING 65-16336.
1998
Part: LIGHT — INOPERATIVE (COCKPIT)
INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT ABOVE STAIR TO COCKPIT INOP (UPPER DECK). REMOVED AND REPLACED COCKPIT STAIR EMERGENCY LIGHT, OPS CHECK GOOD (P/N 51356B37) ON, (S/N 18149) ON, (S/N 33648) OFF.
Part: BATTERY — DISCHARGED (CABIN)
INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS LIGHTS, COCKPIT FWD ENTRY DOOR INOP. REMOVED AND REPLACED BOTH SETS OF BATTERIES OUT OF THE EMERGENCY EXIT LIGHT UNITS PER MM 25-60-00, OPS CHECK NORMAL AT THIS TIME.
1996
Part: SLAT ACTUATOR — INOPERATIVE (NR 2 SLAT)
INSPECTION TYPE-N/A, NR 2 SLAT WOULD NOT RETRACT AFTER T/O. COMPLETED AOM PROCEDURES, DUMPED FUEL AND RETURNED TO OAK. REPLACED NR 2 SLAT ACT AS PER MM 27-81-32, SLAT OPS CHKS NORMAL ON GROUND (P/N 141095-9-2) (S/N 3997L) OFF, (S/N 01405BDJLMN) ON.
Part: BATTERIES — DISCHARGED (CABIN)
INSPECTION TYPE N/A, EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES.
Part: BATTERIES — DISCHARGED (CABIN)
INSPECTION TYPE N/A EMERGENCY LIGHT INOP. REPLACED BATTERIES.
Part: FRAME — CRACKED (BS 870)
INSPECTION TYPE SI, RT 870 FORGING SPLICE AT STR 9 HAS 5 CRACKED HOLES AND ONE 2 TO 3 INCH CRACK IN RADIUS OF AFT FLANGE. REPAIRED BS 870 FORGING BY REMOVING DAMAGED SECTION AND SPLICING A NEW SECTION IN PLACE IAW B727-5310-3057 AND B727-5310-8080A.
Part: FRAME — CRACKED (BS 870)
INSPECTION TYPE SI, LT 870 FORGING STR 9 HAS ONE CRACKED HOLE AND CRACK IN RADIUS ON FWD FLANGE. INSTALLED EXTERNAL DOUBLERS AND REPAIRED IAW EO B727-5310-3057E AND EO B727-5310-8080A.
Part: FLOOR — CORRODED (BS 209-231)
INSPECTION TYPE SI, CORROSION ON FLOOR STA 209 TO 231 LBL 6 TO 18 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED FLOOR PANEL PER SRM 51-40-2, 51-10-2 MM 51-20-151, SRM 51-30-02.
Part: FLOOR BEAM — CORRODED (BS 640)
INSPECTION TYPE SI, CORROSION AT NUTPLATES IN FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE STA 640 WL 207.5 LBL 38 AREAS MARKED. FOUND FLOOR BEAM AT BS 640 LBL 38 TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FLOOR BEAM AT BS 640 LBL 38 PER UPS EO 727-53-1780.
Part: FLOOR BEAM — CORRODED (BS 680)
INSPECTION TYPE SI, CORROSION ON FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE AT NUTCLIP HOLES STA 680 WL 207.5 LBL 5, 29, 33, 35 RBL 4, 37, 59, 60, AREAS MARKED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED PER EO 96-2363.
Part: FLOOR BEAM — CORRODED (BS 1110)
INSPECTION TYPE SI, DOUBLE HOLES IN LOWER FLANGE OF THE 1110 FLOOR BEAM LBL 19 RBL 45 WL 201. DURING REMOVAL OF CEILING SUPPORT FOUND FLOOR BEAM TO BE CORRODED OUT OF LIMITS PER SRM 53-10-01. REPAIRED PER EO 96-2357.
Part: FRAME — CORRODED (BS 304)
INSPECTION TYPE SI, FOUND CORROSION ON FRAME AT BS 304 WL 175 LBL 44. CLEANED AND REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER EO 96-2371.
Part: EXPANSON LINK — CORRODED (BS 850-870)
INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 850 TO 870 LBL 45 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPLACED EXPANSION LINK PER SRM 51-10-1, 51-30-5, 51-30-8, 51-30-2, 51-20-4.
Part: EXPANSION LINK — CORRODED (BS 740-760)
INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 740 TO 760 LBL 25 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED EXPANSION LINK PER SRM 51-10-1, 51-30-2.
Part: SUPPORT — CORRODED (BS 304)
INSPECTION TYPE SI, CORROSION ON COCKPIT ENTRY SUPPORT STA 304 WL 208 LBL 4,9 RBL 3,8 AREA MARKED. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, FARICATED REPLACEMENT SUPPORT PER SRM 51-20-1, 51-30-8 AND 51-30-5. REPLACED FLOOR SUPPORT AT BS 304 LBL 15 PER SRM 51-30-2.
Part: STIFFENER — CORRODED (BS 740-760)
INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 740 TO 760 RBL 25 WL 208 IN CENTER CHANNEL AT FWD END. FOUND EXPANSION LINK TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED EXPANSION LINK AT BS 740 TO 760 RBL 25 WL 208 PER SRM 51-10-1, 51-30-4, 51-30-8, 51-10-6, 51-10-2.
Part: WEB — CORRODED (BS 480)
INSPECTION TYPE SI, CRACK ON FLOOR WEB STA 480 WL 208 LBL 55 AREA MARKED. WHILE WORKING CRACK FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-10-1. REPAIRED PER SRM 51-40-2, 51-10-2 AND M/M 51-21-151.
Part: CHANNEL — CORRODED (BS 850)
INSPECTION TYPE SI, CORROSION ON INTERCOSTAL STA 850 LBL 45 TO 65 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-1.
Part: FRAME — CORRODED (BS 351)
INSPECTION TYPE SI, CORROSION ON BS 351 WEB AT RBL 37 AND 47, WL 168 BELOW DOGHOUSE FLOOR. REMOVED DAMAGED WEB SECTION AND INSTALLED NEW SECTION IAW SRM 51-40-2. ALSO, REPLACED CORRODED SHEAR TIE AT STR 24R DUE TO CORROSION OUT OF LIMITS.
Part: TRACK — CORRODED (NR 4 LE FLAP)
INSPECTION TYPE SI, NR 4 SLAT TRACKS, BOTH HAVE CORROSION ON FWD ENDS AND BOTH SIDES. REMOVED AND REPLACED SLAT TRACKS IAW OHM 57-51-61.
Part: LINK — CORRODED (BS 740-760)
INSPECTION TYPE SI, CORROSION ON EXPANSION LINK IN CENTER CHANNEL STA 740 TO 760 BL 0 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED EXPANSION LINK IAW 51-10-2, 51-10-6, 51-30-2, 51-30-4 AND 51-30-8.
Part: BULLNOSE — CORRODED (NR 3 LE FLAP)
INSPECTION TYPE SI, BULLNOSE CENTER HINGE LOWER ATTACH POINT ON NR 3 K-FLAP IS CORRODED UNDER BOLT HEAD. REMOVED AND REPLACED NR 3 K-FLAP IAW MM 27-81-01.
Part: KEEL BEAM — CRACKED (BS 870)
INSPECTION TYPE SI, APU SIDE WEBS ARE CRACKED AT BS 870, LBL 5.5 AND RBL 5.5 WL 156. CUTOUT DAMAGE AND REPAIRED KEEL BEAM IAW UPS IAW EO B727-5330-1995-B AND BOEING DRAWING 65-88832.
Part: CHANNEL — CORRODED (BS 300-342)
INSPECTION TYPE SI, CORROSION ON HAT CHANNEL FROM BS 300 TO 342, RBL 12, WL 208. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-30-2, 53-10-1, 51-40-4.
Part: STIFFENER — CORRODED (BS 351)
INSPECTION TYPE SI, CORROSION ON DOGHOUSE FLOOR SUPPORT AT BS 351, RBL 20 AND RBL 30, WL 170. REMOVED AND REPLACED STIFFENER/FLOOR SUPPORT IAW SRM 51-30-2, 53-10-1, 51-30-5.
Part: RIB — CRACKED (NR 8 LE FLAP)
INSPECTION TYPE SI, NR 8 SLAT I/B TRACK SUPPORT STRUCTURE O/B RIB IS CRACKED IN 2 PLACES. REMOVED AND REPLACED NR 8 SLAT I/B TRACK SUPPORT FITTINGS AND WEBS PER SRM 51-30-2.
Part: CREASE BEAM — CORRODED (BS 1176)
INSPECTION TYPE SI, CORRROSION ON STA 1176 CREASE BEAM FROM LBL 25 TO 55 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. REMOVED CREASE BEAM CHORD AND REPLACED PER SRM 51-30-2.
Part: SPAR — CORRODED (RT WING)
INSPECTION TYPE SI, CORROSION R/W UPPER REAR SPAR CHORD AT WBL 86 JUST ABOVE NR 3 ENGINE FUEL SHUTOFF VALVE. REPAIRED UPPER REAR SPAR CHORD IAW SB 727-57-0145, SRM 57-10-6 AND BOEING DRAWING 65-C19647.
Part: FRAME — CORRODED (BS 312)
INSPECTION TYPE SI, CORROSION ON FRAME CHORD STA 312, RBL 43, WL 178. REMOVED AND REPLACED CHORD IAW SRM 53-10-1, 51-40-3, 51-30-2.
Part: INTERCOSTAL — CORRODED (BS 219.8-227)
INSPECTION TYPE SI, CORROSION ON BOTTOM OF INTERCOSTAL STA 219.8 TO STA 227 LBL 42 WL 227. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-10-2, 51-30-2, 51-20-4.
Part: FLOOR SUPPORT — CORRODED (BS 315)
INSPECTION TYPE SI, CORROSION ON LAV FLOOR SUPPORT STA 315 WL 208 RBL 17, 20, 24, 27, 30, 39 AREAS MARKED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-1, 51-30-2, 53-10-1, 51-30-5.
Part: ANGLE — CRACKED (BS 365)
INSPECTION TYPE SI, GOUGE AND CRACK ON BARRIER NET SUPPORT ANGLES AT STA 365 STR 7 AND 8 LT. REMOVED AND REPLACED BARRIER SUPPORT ANGLES AND CHANNEL IAW SRM 51-30-2, 51-10-2, 51-10-1.
Part: SUPPORT — CORRODED (BS 294-303)
INSPECTION TYPE SI, CORROSION ON FLOOR SUPPORT STA 294 TO 303 LBL 13 TO 15 WL 208 ON BOTTOM OF SUPPORT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-02, 51-20-4, 53-10-1.
Part: FITTING — CORRODED (RT AILERON)
INSPECTION TYPE SI, R/W O/B AILERON O/B WING SIDE HINGE FITTING IS CORRODED. FOUND R/W O/B AILERON O/B WING SIDE HINGE FITTING OUT OF LIMITS PER SRM 57-40-00. REMOVED AND REPLACED R/W O/B AILERON O/B WING SIDE HINGE FITTING PER SRM 51-30-02.
Part: FLOOR BEAM — CORRODED (BS 600)
INSPECTION TYPE SI, CORROSION IN NUTPLATE HOLES ON FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE STA 600 WL 207.5 RBL 47 TO 63 AREAS MARKED. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-01, REPAIRED FLOOR BEAM AT BS 600 RBL 47 TO 63 PER UPS 727-53-1769.
Part: HINGE FITTING — CORRODED (RT AILERON TAB)
INSPECTION TYPE SI, R/W O/B AILERON TAB SIDE HINGE FITTINGS ARE CORRODED. FOUND HINGE FITTINGS TO BE OUT OF LIMITS PER SRM 57-40-00. REMOVED AND REPLACED R/W O/B AILERON TAB HINGE FITTINGS PER MM 27-10-41.
Part: HINGE FTG — CORRODED (LT AILERON)
INSPECTION TYPE SI, L/W O/B AILERON O/B CENTER HINGE SUPPORT FITTING IS CORRODED. REMOVED CORRODED HINGE FITTING, DRILLED NEW FITTING AND INSTALLED IAW SRM 51-30-02.
Part: SEAT TRACK — CORRODED (BS 520)
INSPECTION TYPE SI, CORROSION ON SEAT TRACK AT BS 520 RBL 15 WL 150. REMOVED AND REPLACED SEAT TRACK FROM 480 TO 530 RBL 15 WL 15 IAW SRM 53-10-05.
Part: INTERCOSTAL — CORRODED (BS 313-327)
INSPECTION TYPE SI, CORROSION ON FLOOR SUPPORT INTERCOSTAL STA 313 TO 327 WL 208 RBL 47 AREA MARKED. FOUND SUPPORT OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5 AND 51-30-2.
Part: STRINGER TIE — CORRODED (BS 360)
INSPECTION TYPE SI, FOUND CORROSION ON FRAME AT STA 360, WL 50, LBL 25 TO RBL 25 AND STRINGER TIE AT RT STR NR 22, STA 360. CORROSION REMOVAL WAS BEYOND LIMITS ON STRINGER TIE AT STR 22R. REPLACED STR TIE PER 53-10-02, 53-10-03, 51-10-06, MM 51-20-151.
Part: BULKHEAD ANGLE — CORRODED (BS 480)
INSPECTION TYPE SI, CORROSION ON BULKHEAD ANGLE AT BS 480, WL 155, LBL 12, RBL 12. REMOVED AND REPLACED ANGLE IAW 51-30-02, 51-10-05 AND MM 51-20-151.
Part: FLOOR BEAM — CORRODED (BS 344)
INSPECTION TYPE SI, CORROSION ON FLOOR BEAM STA 344, WL 208 HAS NUMEROUS AREAS OF CORROSION FROM LBL 60 TO RBL 20. REMOVED AND REPLACED UPPER CHORD OF FLOOR BEAM IAW SRM 53-10-08.
Part: FLOOR SUPPORT — CORRODED (BS 480)
INSPECTION TYPE SI, CORROSION ON FLOOR SUPPORT AT BS 480 WL 155 LBL 9. REMOVED DAMAGED SECTON OF FLOOR SUPPORT AND SPLICED A REPLACEMENT SECTION IN IAW SRM 53-10-5 AND 51-30-2.
Part: STRINGER — CORRODED (BS 351.2-360)
INSPECTION TYPE SI, FOUND CORROSION ON STRINGER 22 RT BETWEEN STA 351.2 AND STA 360. CORROSION REMOVAL WAS OUT OF LIMITS PER SRM 53-10-01. REMOVED DAMAGED SECTION OF STRINGER, LOCATED AND DRILLED STRINGER REPAIR PARTS, INSTALLED PER SRM 53-10-03, 51-30-02, 51-20-04, MM 51-20-151.
Part: CARGO PUCK — CORRODED (BS 700)
INSPECTION TYPE SI, CORROSION ON CARGO PUCK STA 700, WL 208, LBL 57. REMOVED AND REPLACED CARGO TIE DOWN FITTING IAW SRM 51-30-02 AND 51-10-01.
Part: ANGLE — CORRODED (BS 870)
INSPECTION TYPE SI, CORROSION AT BS 870 VERTICAL SUPPPORT AND TIE ANGLE LBL 12 WL 199 LEFT MLG WHEEL WELL. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED SUPPORT AND TIE ANGLE IAW SRM 53-30-02, 51-40-04, MM 51-20-31, 51-30-00.
Part: STIFFENER — CORRODED (BS 344)
INSPECTION TYPE SI, CORROSION ON HORIZONTAL STIFFENER AT BS 344, LBL 12 WL 183. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-2, 51-10-5 AND 51-10-01.
Part: CARGO PUCK — CORRODED (BS 720)
INSPECTION TYPE SI, CORROSION ON CARGO PUCK STA 720, WL 208, LBL 57. REMOVED AND REPLACED CARGO TIE DOWN FITTING IAW SRM 51-30-02 AND 51-10-01.
Part: CARGO PUCK — CORRODED (BS 460)
INSPECTION TYPE SI, CORROSION ON CARGO PUCK STA 460, WL 208, LBL 40. REMOVED AND REPLACED CARGO TIE DOWN FITTING IAW SRM 51-30-02 AND 51-10-01.
Part: CARGO PUCK — CORRODED (BS 580)
INSPECTION TYPE SI, CORROSION ON CARGO PUCK STA 580, WL 208, LBL 40 AREA MARKED. REMOVED AND REPLACED CARGO PUCK IAW SRM 51-30-02 AND 51-10-01.
Part: INTERCOSTAL — CORRODED (BS 327-343)
INSPECTION TYPE SI, CORROSION ON FLOORBOARD SUPPORT INTERCOSTAL STA 327 TO 343, WL 208 LBL 30, AREAS MARKED. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-10-6. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-02.
Part: INTERCOSTAL — CORRODED (BS 257-277)
INSPECTION TYPE SI, CORROSION ON FLOOR SUPPORT STA 257 TO 277 LBL 13 TO 15 WL 208. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-20-04 AND 51-30-02.
Part: HAT CHANNEL — CORRODED (BS 1140)
INSPECTION TYPE SI, CORROSION ON HAT CHANNEL STA 1140 LBL 35 TO 55 WL 208. REPLACED HAT CHANNEL PER SRM 51-30-2, 51-10-2.
Part: SEAT TRACK — CORRODED (BS 1090-1130)
INSPECTION TYPE SI, CORROSION ON SEAT TRACK TOP AND BOTTOM OF FLANGES STA 1090 TO 1130 LBL 55 WL 208. FOUND CORROSION OUT OF LIMITS PER SRM 53-10-01, REMOVED AND REPLACED SEAT TRACK IAW SRM 51-10-2, 51-30-02 AND 51-30-05.
Part: SUPPORT — CORRODED (LT HORIZ STAB)
INSPECTION TYPE SI, LT HORIZONTAL STABILIZER SIDE RUB PAD IS PILLOWING. REMOVED RUB PLATE FROM SUPPORT AND FOUND CORROSION TO BE OUT OF LIMITS PER SRM 55-50-01. INSTALLED NEW RUB PLATE AND SUPPORT PER SRM 51-30-02 MATERIAL LOSS WAS 100 PERCENT OF SUPPORT.
Part: FITTING — CORRODED (NR 7 SPOILER)
INSPECTION TYPE SI, NR 7 SPOILER CENTER SUPPORT FITTING IS CORRODED. REMOVED AND REPLACED NR 7 SPOILER CENTER SUPPORT FITTING IAW MM 27-62-81.
Part: WEB — CORRODED (BS 259)
INSPECTION TYPE SI, CORROSION ON WEB STA 259 LBL 46 TO 49 WL 208 TO 222. FOUND CORROSION OUT OF LIMITS PER SRM 51-10-6. REMOVED AND REPLACED WEB IAW SRM 51-40-2, 51-30-2, 51-20-04 AND 51-10-02.
Part: ANGLE — CORRODED (BS 300-342)
INSPECTION TYPE SI, CORROSION ON VARIOUS ARES OF L-ANGLE BETWEEN BS 300 TO 342, RBL 58 TO 61, WL 208. FOUND AREAS OF CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, REMOVED AND REPLACED L-ANGLE IAW SRM 51-40-3.
Part: SUPPORT — CORRODED (RT HORIZ STAB)
INSPECTION TYPE SI, RT HORIZONTAL STABILIZER SIDE RIB PAD IS PILLOWING. REMOVED RUB PLATE FROM SUPPORT AND FOUND CORROSION TO BE OUT OF LIMITS PER SRM 55-50-01. INSTALLED NEW RUB PLATE AND SUPPORT PER SRM 51-30-02, MATERIAL LOSS WAS 1OO PERCENT OF SUPPORT.
Part: KEEL BEAM — CORRODED (BS 762-772)
INSPECTION TYPE SI, CORROSION ON KEEL BEAM OF ELECTRICAL GROUND WIRES BS 762 TO 772, LBL 7 WL 155. FOUND CORROSION OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED CHORD IAW SRM 51-40-4, REINSTALLED GROUND POST AND WIRES IAW WPM 20-20-00.
Part: HINGE FTTNG — CORRODED (LT INBD AILERON)
INSPECTION TYPE SI, L/W I/B AILERON TAB HAS ALL THREE HINGE FITTINGS CORRODED ON THE AILERON SIDE. REMOVED CORRODED HINGE FITTINGS, INSTALLED NEW HINGE FITTINGS IAW SRM 51-30-2, MM 27-10-11.
Part: FLOORBEAM — CORRODED (BS 328)
INSPECTION TYPE SI, CORROSION ON FLOORBEAM AT STA 328, WL 208, LBL 35, 31. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-10-8.
Part: WEB — CORRODED (BS 257)
INSPECTION TYPE SI, CORROSION ON WEB STA 257 RBL 46 WL 208 TO 229. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, FABRICATED NEW WEB IAW SRM 51-10-2, ALODINED AND PRIMED IAW MM 51-20-31 AND INSTALLED PER SRM 51-30-2.
Part: FLOORBEAM — CORRODED (BS 420)
INSPECTION TYPE SI, CORROSION ON FLOORBEAM STA 420 WL 206 IN NUTCLIP HOLES LBL 46 TO 60, LBL 24, RBL 24 AREAS MARKED. FOUND CORROSION OUT OF LIMITS FOR SRM 53-10-1, FABRICATED REPAIR PARTS PER SRM 53-10-8 AND INSTALLED REPAIR PARTS PER SRM 53-10-8.
Part: SKIN — CORRODED (LT ELEVATOR)
INSPECTION TYPE SI, LEFT ELEVATOR 2ND FROM O/B STATIC WICK BASE IS LOOSE. FOUND CORRODED SKIN UNDER BASE AND REPAIRED IAW SRM 55-20-01.
Part: SKIN — CORRODED (BS 553)
INSPECTION TYPE SI, CORROSION ON INTERNAL SKIN STA 553 LBL 6 WL 306. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3 AND 53-30-2.
Part: FAIL-SAFE STRAP — CORROSION (BS 351)
INSPECTION TYPE SI, CORROSION ON TOP OF FAIL-SAFE STRAP STA 351, WL 178, RBL 14 TO 20. REMOVED AND REPLACED FAIL-SAFE STRAP IAW SRM 51-30-2.
Part: WEB — CORRODED (BS 1135)
INSPECTION TYPE SI, FOUND CORROSION ON WEB AT STA 1135 LBL 62 WL 208. REMOVED CORROSION 10 BY 3 UP TO .027 ON .063 ORIGINAL THICKNESS OUT OF LIMITS, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-30-2.
Part: BULKHEAD BRACKET — CORRODED (BS 745)
INSPECTION TYPE SI, CORROSION AT EXPANSION LINK LBL 7 BS 745 WL 165 ON DELTA BEAM BOX. REMOVED AND REPLACED EXPANSION LINK FORK ASSM, BULKHEAD BRACKET AND BUSHING IAW SRM 51-30-2.
Part: INTERCOSTAL — CORRODED (BS 211)
INSPECTION TYPE SI, CORROSION ON INTERCOSTAL BETWEEN BS 211 AND 219 WL 174 RBL 27. REMOVED FAB'D AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-30-2 AND 53-10-1.
Part: FLOORBOARD SUPRT — CORRODED (BS 649/658)
INSPECTION TYPE SI, CORROSION ON FLOORBOARD SUPPORT HAT CHANNEL STA 649 AND STA 658 WL 207.5 RBL BOTTOM SIDE OF NUT CLIP HOLES. MECHANICALLY REMOVED CORROSION, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1, REPLACED CHANNEL STA 620 TO 680 IAW SRM 51-30-02, 51-30 -5, 51-30-3, 51-10-2 AND MM 51-20-151.
Part: STRINGER — CORRODED (BS 330-400)
INSPECTION TYPE SI, CORROSION ON STRINGER 1 STA 330 TO 400. MECHANICALLY REMOVED CORROSION, REWORK AREA AT STR 1 STA 380 TO 400 DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 1 IAW 53-10-3.
Part: FLOORBEAM — CORRODED (BS 312)
INSPECTION TYPE SI, CORROSION ON FLOORBEAM STA 312 WL 208 LBL 19, 20 LBL 40. CORROSION MECHANICALLY REMOVED FROM STA 312 FLOORBEAM LBL 19, 20, 40, REWORK AT LBL 19 DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FLOORBEAM AT LBL 19 STA 19 STA 312 IAW SRM 53-10-8 FIG 7.
Part: UPLOCK SUPPORT — CORRODED (BS 870-880)
INSPECTION TYPE SI, CORROSION ON LEFT MLG UPLOCK SUPPORT STRUCUTRE BS 872 TO 880 LBL 66 TO 70 WL 189 TO 192 ON HORIZONTAL WEB, VERTICAL WEB AND SUPPORT WEB L-ANGLE AND AT BS 889 ON WEB AND FLANGE. REMOVED CORROSION, REWORK ON WEB SUPPORT ANGLE DEEMED OUT OF LIMITS, ONLY REPLACED L-ANGLE IAW SRM 53-10-1, 53-10-2, 51-30-2, 51-30-5 MM 51-20-21, 51-20-31.
Part: T-STIFFENER — CORRODED (BS 740)
INSPECTION TYPE SI, CORROSION ON HORIZONTAL T-STIFFENER ON AFT SIDE OF BS 740 WEB BL 0 WL 160. CORROSION MECHANICALLY REMOVED REWORK DEEMED TO BE OUT OF LIMITS IAW SRM 53-10-01. REPLACED STIFFENER IAW SRM 51-10-1, 51-30-2 AND 51-30-5.
Part: CORNER REVEAL — CORRODED (GALLEY DOOR)
INSPECTION TYPE SI, CORROSION ON MID GALLEY DOOR FWD UPPER CORNER REVEAL CORRODED. REMOVED OLD FWD UPPER REVEAL CLAMPED NEW PART IN PLACE, BACK DRILLED THROUGH EXITING FASTENER HOLES AND INSTALLED PART IAW SRM 57-30-02.
Part: EXPANSION LINK — CORRODED (BS 848-870)
INSPECTION TYPE SI, FOUND CORRODED EXPANSION LINK STA 848 TO 870 RBL 45 WL 208 AND SUPPORT FITTING AT 870. REMOVED CORRODED EXPANSION LINK AND SUPPORT FITTING AND REPLACED WITH NEW PARTS IAW SRM 51-30-5, 51-21-1, 51-30-2.
Part: UPPER TAB — CRACKED (LT AILERON)
INSPECTION TYPE SI, S-13 UPPER TAB IS CRACKED AT LWS 656. REPAIRED S-13 AT LWS 656 IAW UPS EO B727-5710-0314F.
Part: SEAT TRACK WELL — CORRODED (BS 540-610)
INSPECTION TYPE SI, CORROSION AND MECHANICAL DAMAGE IN SEAT TRACK WELL STA 540 TO 610 RBL 45 WL 208. CORROSION AND MECHANICAL DAMAGE OUT OF LIMITS IAW SRM 53-10-1 SEAT TRACK WILL BE REPLACED ON UPS NRC 567976.
Part: SEAT TRACK WELL — CORRODED (BS 680-695)
INSPECTION TYPE SI, CORROSION AND MECHANICAL DAMAGE IN SEAT TRACK WELL RBL 45 680 TO 695 WL 208. CORROSION AND MECHANICAL DAMAGE OUT OF LIMITS IAW SRM 53-10-01, SEAT TRACK WILL BE REPLACED ON UPS NRC 567976.
Part: BONDING JUMPER — CORRODED (NR 4 LE FLAP)
INSPECTION TYPE SI, NR 4 K-FLAP IS CORRODED AT I/B BONDING JUMPER ATTACH POINT ON RIB. REMOVED CORROSION, REMOVED .085 FROM .170 1 BY 1 AREA OUT OF LIMITS. REMOVED CORRODED AREA, FABRICATED REPAIR PARTS AND INSTALLED RELOCATED JUMPER WIRE TO ANOTHER ATTACH POINT, ALL WORK DONE IAW SRM 57-50-01 AND 51-30-02.
Part: CASTING — CORRODED (RT EMER EXIT)
INSPECTION TYPE SI, CORROSION ON RT HAND OVERWING EXIT, HANDLE SEAL CASTING. REMOVED CORRODED CASTING, RECEIVED NEW DRILLED UP PART, SEALED AND INSTALLED ON DOOR IAW SRM 51-30-2.
Part: FLOOR — CRACKED (BS 296)
INSPECTION TYPE SI, CRACKED FLOOR AT HYLOCK BS 296, RBL 21, WL 208. REMOVED HYLOCK NDI LOCATED AND MARKED FOR STOP DRILLING NOTED. CRACK INDICATION STOP DRILLED CRACKS FOUND CRACKS TO BE CONTAINED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW 51-10-02 SRM 51-30-2, SRM 51-20-4.
Part: SHEAR TIE — CRACKED (BS 328)
INSPECTION TYPE SI, CRACKED SHEAR TIE AT BS 328 RBL 62 WL 191. REPAIRED BS 328 FRAME SHEAR TIE AT RBL 62 WL 191 IAW SRM 53-10-4, 51-30-2, 51-10-2 AND MM 51-20-151.
Part: TRUNNION FITTING — CORRODED (NLG)
INSPECTION TYPE SI, CORROSION ON LT AND RT NLG TRUNNION FITTING BORES. MACHINED LT AND RT TRUNNION ATTACH POINTS TO REMOVE CORROSION, FABRICATED NEW OVER SIZE BUSHINGS AND INSTALLED IAW SRM 53-40-01 AND BOEING DWG 65-7676.
Part: STRINGER — CORRODED (BS 428.5)
INSPECTION TYPE SI, FOUND STR 22L TO BE CORRODED AT BS 428.5. REMOVED CORROSION, SPLICE SECTION AT BS 440, CUT DAMAGED STRINGER, FOUND STR 22L AT BS 412 TO BE CORRODED BEYOND LIMITS AS WELL. CUT STRINGER AT BS 407, FABRICATED REPAIR PARTS AND INSTALLED NEW STRINGER AND REPAIR PARTS IN A/C PER SRM 51-30-02, SRM 53-10-02, 53-10-3.
Part: SHEAR TIE — CRACKED (BS 277)
INSPECTION TYPE SI, CRACKED SHEAR TIE AT BS 277 LBL 59 WL 194. REPAIRED FRAME SHEAR TIE AT STA 277 LBL 59 WL 194 IAW SRM 53-10-04 AND 53-30-02.
Part: MOP SILL — CRACKED (BS 294-300)
INSPECTION TYPE SI, MOP SILL IS CRACKED STA 294 TO 300 LBL 53 WL 208. REMOVED CRACKED MOP SILL AND REPLACED WITH NEW IAW SRM 51-30-02 SRM 51-30-05, SRM 51-10-01, SRM 51-20-04.
Part: SKIN — CORRODED (BS 1120-1130)
INSPECTION TYPE SI, CORROSION BS 1120 TO 1130 BTWN STR 19R AND 20R INTERIOR FUSELAGE SKIN BTWN SKIN DOUBLER AND SKIN AT LAP JOINT, ONE RIVET HAS BUCKTAIL POPPED OFF. REMOVED FASTENERS BS 1108 TO 1142 COMMON TO STR 20R AND SKIN LAP FOR ACCESS, FOUND DOUBLER TO BE CRACKED, INSTALLED SHORING FOUND TWO AREAS OF CORROSION ON TEAR STRAP, OUT OF LIMITS. SENT TO ENGINEERING RECEIVED RESPONSE AND REPAIRED PER EWO 96-2369 AND SRM 51-10-2 AND SRM 51-30-2.
Part: BALANCE PANEL — CORRODED (RT ELEVATOR)
INSPECTION TYPE SI, CORROSION RT NR 5 BALANCE PANEL AT MATING SURFACES OF BALANCE PANEL HINGE AND WEIGHT ASSM. REMOVED PANEL NR 5 BALANCE BAY, DRILLED OUT FASTENERS, REMOVED CORROSION FROM DOUBLER AND FOUND DOUBLER TO BE OUT OF LIMITS. FABRICATED NEW DOUBLER AND INSTALLED PANEL, BALANCE PANEL AND HINGE IN A/C PER MM 27-30-21, SRM 51-36-5 AND SRM 55-20-2.
Part: SEAT TRACK — CORRODED (BS 760-848)
INSPECTION TYPE SI, CORROSION AROUND NUTPLATES ON BOTTOM SIDE OF SEAT TRACK STA 760 TO 848 RBL 65 WL 208. REMOVED CORROSION OUT OF LIMITS, REMOVED SEAT TRACK, FABRICATED NEW AND INSTALLED IAW SRM 51-30-2, 53-10-2, 53-10-5.
Part: SEAT PEDESTAL — CORRODED (BS 226)
INSPECTION TYPE SI, CORROSION ON CAPTAINS SEAT PEDESTAL STA 226, LBL 13 TO 31, WL 208. REMOVED CORROSION WAS OUT OF LIMITS, REMOVED BAD CHANNEL RECEIVED NEW CHANNEL AND INSTALLED IAW SRM 51-30-2.
Part: SUPPORT FITTING — CORRODED (LT AILERON)
INSPECTION TYPE SI, L/W O/B AILERON, O/B SUPPORT FITTING ON WING IS PITTED AND CORRODED ON LOWER SURFACE AND AROUND BUSHINGS. REMOVED CORRODED PART, ORDERED NEW PART, RECEIVED DRILLED UP FITTING AND INSTALLED NEW FITTING IAW SRM 51-30-2, SRM 51-30-05.
Part: SEAT TRACK — CORRODED (BS 760-848)
INSPECTION TYPE SI, CORROSION ON TOP AND BOTTOM OF FLANGES ON SEAT TRACK STA 760 TO 848 LBL 45, WL 208. REMOVED CORROSION FOUND OUT OF LIMITS, REPLACED WITH FABRICATED ONE IAW SRM 53-10-01, SRM 51-30-02.
Part: SEAT TRACK — CORRODED (BS 700-730)
INSPECTION TYPE SI, CORROSION ON TOP OF SEAT TRACK AND INSIDE WALL STA 700 TO 730 RBL 62, WL 208. REMOVED CORROSION OUT OF LIMITS, FABRICATED NEW SEAT TRACK, REMOVED OLD SEAT TRACK, INSTALLED NEW SEAT TRACK PER SRM 51-30-2, 53-10-5.
Part: FLOOR — CORRODED (BS 460)
INSPECTION TYPE SI, CORROSION ON FLOOR WEB STA 460 WL 208, LBL 52 AREA MARKED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, CUT OUT DAMAGED AREA AND REPAIRED PER SRM 51-40-02.
Part: ACT SUPPORT WEB — CRACKED (NR 5 LE FLAP)
INSPECTION TYPE SI, NR 5 K-FLAP ACTUATOR O/B TRUNNION SUPPORT WEB IS CRACKED. REMOVED CRACKED SUPPORT WEB, FABRICATED NEW SUPPORT WEB AND INSTALLED ON A/C IAW SRM 51-30-2, SRM 51-10-2.
Part: WEB FINGER — CRACKED (BS 500)
INSPECTION TYPE SI, CRACKED WEB FINGER STA 500, LBL 7 WL 302. REMOVED DAMAGED SECTION OF WEB, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-30-02.
Part: ANGLE — CORRODED (BS 300)
INSPECTION TYPE SI, CORROSION IN RADIUS OF L-ANGLE AT BS 300, RBL 14 TO RBL 58 WL 208. ALSO, FOUND L-ANGLE TO BE CRACKED ALONG RADIUS. REMOVED AND REPLACED L-ANGLE WITH NEW IAW SRM 51-30-2.
Part: INTERCOSTAL — CORRODED (BS 313-327)
INSPECTION TYPE SI, CORROSION ON FLOORBOARD SUPPORT INTERCOSTAL STA 313 TO 327, WL 208, LBL 30 AREAS MARKED. CLEANED AND EVALUATED AREA 2.3 BY 14, OUT OF LIMITS WITH .040 REMOVED ON ORIG THICKNESS OF .078, ORDERED NEW PART RECEIVED AND INSTALLED IAW SRM 51-10-6, SRM 51-30-2.
Part: STRINGER TIE — CORRODED (BS 950)
INSPECTION TYPE SI, CORROSION ON STRINGER TIE STA 950 STR 1 WL 302. REMOVED CORROSION FROM STR TIE STA 950 STR 1 WL 302, REMOVED .035 FROM ORIGINAL .163 OUT OF LIMITS. REMOVED OLD STRINGER TIE AND INSTALLED NEW TIE IAW SRM 51-30-2.
Part: CENTERING CRANK — CRACKED (RUDDER)
INSPECTION TYPE SI, RUDDER AFT CONTROL CENTERING CRANK ASSM HOUSING IS CRACKED AT LEFT SPRING MOUNT FLANGE. REMOVED AND REPLACED RUDDER CENTERING MECHANISM IAW MM 27-20-91.
Part: RIB — CRACKED (NR 4 LE FLAP)
INSPECTION TYPE SI, 2ND AND 3RD RIB CRACKED ON NR 4 SLAT. REMOVED BOTH 2ND AND 3RD RIB FROM SLAT DRILLED UP NEW RIBS AND INSTALLED IN SLAT PER SRM 51-30-2.
Part: HAT CHANNEL — CORRODED (BS 342)
INSPECTION TYPE SI, CORROSION ON HAT CHANNEL AT BS 342 RBL 16 TO RBL 61, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED HAT CHANNEL, FABRICATED NEW HAT CHANNEL PER BOEING DWG 65-26173-3. INSTALLED NEW HAT CHANNEL, WORK DONE IAW SRM 51-30-2 SRM 53-10-1.
Part: STRINGER — CORRODED (BS 405)
INSPECTION TYPE SI, CORROSION ON RT STRINGER NR 7 STA 405. REMOVED CORROSION, 1 BY .025 BY .025 OF ORIGINAL .032 OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C AFTER TREATING AFFECTED AREA IAW SRM 51-10-6, 53-10-2 AND SRM 53-10-3.
Part: FLOOR BEAM — CORRODED (BS 760-850)
INSPECTION TYPE SI, CORROSION AROUND NUTPLATE ON FLANGE OF FLOOR BEAM STA 768 TO 858 RBL 45 WL 28. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-10-1, FABRICATED NEW PART AND INSTALLED IAW SRM 51-30-2.
Part: PULLEY FITTINGS — CORRODED (LT INBD AILERON)
INSPECTION TYPE SI, L/W I/B AILERON TURN AROUND PULLEY FITTING IS CORRODED ON LOWER SURFACE. REMOVED CORRODED FITTING WHICH WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-40, INSTALLED NEW FITTING IAW SRM 51-30-2, MM 27-10-00 MM 27-61-00.
Part: TAB HINGE FTG — CORRODED (RT AILERON)
INSPECTION TYPE SI, R/W I/B AILERON SIDE TAB HINGE FITTINGS ARE CORRODED. REMOVED CORRODED HINGE FITTINGS, LOCATED NEW ONES AND INSTALLED IAW SRM 51-30-2.
Part: TAB HINGE FTG — CORRODED (LT INBD AILERON)
INSPECTION TYPE SI, L/W I/B AILERON TAB HAS ALL THREE HINGE FITTINGS CORRODED, TAB SIDE. REMOVED L/W AILERON TAB I/B REMOVED FITTINGS AND INSTALLED NEW FITTINGS IAW SRM 51-30-2.
Part: MID SPAR — CORRODED (VERT STAB)
INSPECTION TYPE SI, CORROSION VERTICAL FIN MID SPAR CHORD IS CHAFED AND FRETTING AT ACCESS PANEL 9601. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C IAW SRM 51-30-2 AND EWO 96-2334.
Part: MID SPAR — CORRODED (VERT STAB)
INSPECTION TYPE SI, RT VERT FIN MID SPAR CHORD IS CHAFED AND FRETTING AT ACCESS PANEL 9602. REMOVED CORROSION FOUND OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C SRM 51-30-2 EWO 96-2333.
Part: HINGE FITTING — CORRODED (RT INBD AILERON)
INSPECTION TYPE SI, RT I/B AILERON CENTER WING SIDE HINGE FITTING IS CORRODED. REMOVED CORRODED CENTER HINGE FITTING, FOUND BEARING BLOCK TO HAVE BLOWN DUST SEAL. REPLACED WITH NEW BEARING BLOCK AND REPLACED HINGE FITTING IAW OHM 57-50-01.
Part: SPOILER MIXER — CORRODED (RT WHEEL WELL)
INSPECTION TYPE SI, CORROSION ON THE SPOILER MIXER INPUT QUADRANT. FOUND CORROSION TO BE OUT OF LIMITS SRM 57-40. REMOVED CORRODED SPOILER MIXER AND REPLACED WITH SERVICABLE UNIT MM 27-62-00, MM 27-61-31.
Part: CENTER HINGE — CORRODED (LE FLAP)
INSPECTION TYPE SI, BULLNOSE CENTER HINGE UPPER ATTACH POINT ON NR 3 K-FLAP B-CORRODED UNDER BOLT HEADS. REMOVED K-FLAP AND REPLACED WITH NEW K-FLAP.
Part: EXPANSION LINK — CORRODED (BS 748-760)
INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 740 TO 760 RBL 45 WL 208. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED CORRODED EXPANSION LINK AND REPLACED WITH NEW PART IAW OHM 20-41-05, 20-50-01, 20-50-03, 20-50-02.
Part: PANEL — CORRODED (NR 5 SPOILER)
INSPECTION TYPE SI, NR 5 SPOILER PANEL IS DELAMINATED AT THE CENTER HINGE FITTING UPPER SURFACE. REMOVED CENTER HINGE FITTING, REPLACED DELAMINATED AREA, FOUND CENTER HINGE FITTING TO BE CRACKED AND WILL REPLACE ON OTHER NRC, WORK DONE IAW SRM 57-50-06.
Part: DOWNSTOP FITTING — CORRODED (NR 14 SPOILER)
INSPECTION TYPE SI, NR 14 SPOILER O/B DOWNSTOP FITTING IS CORRODED. REMOVED AND REPLACED NR 14 SPOILER O/B DOWNSTOP FITTING IAW SRM 51-30-02.
Part: SKIN — DELAMINATED (NR 10 SPOILER)
INSPECTION TYPE SI, NR 10 SPOILER IS DELAMAMINATED AT THE CENTER HINGE UPPER SURFACE. REMOVED DELAMAMINATED AREA, REMOVED CENTER HINGE TO ACCESS AREA, IMPREGNATED GLASS CLOTH, SEALED REPAIR, REINSTALLED CENTER HINGE AND WORK DONE IAW SRM 51-40-06, MM 20-50-01, AND 51-30-2.
Part: BATTERIES — DISCHARGED (CABIN)
CREW LEFT EXIT LIGHTS ARMED, A/C SHUT DOWN BY OPERATIONS. REMOVED AND REPLACED BATTERIES.
1995
Part: EEL ASSY — MALFUNCTIONED (FLIGHT DECK)
MAINTENANCE REPORTED EMER EXIT LIGHT OVER FWD ENTRY DOOR, WHEN TURNED ON COMES ON BRIGHT FOR APPROX 45 SECONDS THEN GOES DIM. REPLACED LIGHT ASSY AND BATTERIES, OPS CHECK NORMAL.
Part: SILL — CORRODED (BS 580)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON MAIN CARGO DOOR SILL WEB, UNDER DOOR FITTING, STA 580. INSTALLED REPAIR PER USRM 51-40-2.
Part: FRAME — CORRODED (BS 1342)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT FRAME CHORD, STA 1342, RBL 20, WL 238. REPLACED PER UPS EO 727-5530-4601.
Part: SEAT TRACK — CORRODED (BS 760)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK LWR FLANGE OF CHORD, STA 760, LBL 45. INSTALLED REPAIR PER SRM 53-10-2, 51-30-2, 51-10-6, AND BOEING DRWNG 65-34144-13.
Part: SHEAR WEB — CORRODED (BS 1140-1145)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON TWO HOLES THROUGH LT SHEAR WEB AT BS 1140 TO 1145, LBL 30, AS SEEN FROM BELOW. INSTALLED REPAIR PER SRM 51-40-2 AND 51-30-2.
Part: SHEAR TIE — CRACKED (BS 1323)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON SHEAR TIE BS 1323, BETWEEN STRINGERS 17 AND 18L. REPLACED PER SRM 51-40-3 AND 53-10-2.
Part: CHORD — CORRODED (BS 1342)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE 1342 CHORD FWD SIDE. REPLACED PER UPS EO 727-5530-4601B.
Part: CHORD — CORRODED (BS 1342)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT O/B CHORD, STA 1342, LBL 30, WL 250. REPLACED PER UPS EO 727-5530-4601.
Part: CHORD — CORRODED (BS 1342)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON CENTER CHANNEL, STA 1342. REPLACED PER UPS EO 727-5530-4601B.
Part: FITTING — CORRODED (BS 760)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM TO SEAT TRACK SUPPORT FITTING, BS 760, LBL 48. REPLACED PER SRM 51-40-4 AND 51-30-2.
Part: FRAME — CORRODED (BS 1342)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT CHANNEL, AFT SIDE OF FRAME, STA 1342, WL 247, LBL 18. REPLACED PER UPS EO 727-5530-4601.
Part: CHANNEL — CORRODED (BS 1342)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT CHANNEL STA 1342, WL 247, RBL 18. REPLACED PER UPS EO 727-5530-4601.
Part: WEB — CRACKED (BS 1342)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON FIREWALL WEB AT BS 1342, LBL 24, WL 220. INSTALLED REPAIR PER SRM 51-40-2 AND 54-10-3.
Part: FRAME — CORRODED (BS 1342)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT FRAME CHORD, STA 1342, LBL 20, WL 238. REPLACED PER UPS EO 727-5530-4601.
Part: CHORD — CORRODED (BS 1342)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT O/B CHORD, STA 1342, RBL 30, WL 250. REPLACED PER UPS EO 727-5530-4601.
Part: FRAME — CORRODED (BS 1342)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT LWR FRAME CHORD STA 1342, RBL 24, WL 220. REPLACED PER UPS EO 727-5530-4601.
Part: RIB — CRACKED (BS 1365)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON O/B RIB STA 1365, LT SIDE. INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2.
Part: FLOORBEAM — CORRODED (BS 760)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR PANEL BEAM WEB, BS 760, LBL 48, BELOW FLOOR LEVEL AFT SIDE. INSTALLED REPAIR PER SRM 51-40-2.
Part: FRAME — CORRODED (BS 1342)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT LWR FRAME CHORD STA 1342, LBL 24, WL 220. REPLACED PER UPS EO 727-5530-4601.
Part: RIB — CRACKED (BS 1365)
WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON O/B RIB STA 1365, RT SIDE. INSTALLED REPAIR PER SRM 51-40-3 AND 1-30-2.