N675UP
Registered owner: WHEELS UP PARTNERS LLC, NY (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
Maintenance disclosures
BRAKE FAILURE WHILE TAXI TO TAKEOFF. COMPLETED FULL ANTISKID BRAKE TEST PRIOR TO FAIL. SIC CHECKED HIS BRAKES SUCCESSFULLY AND RETURNED CONTROLS, FELT LIKE BRAKE TEST. USED EMERGENCY TO STOP BEFORE RUNWAY BUT CROSSED LINE.
INSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 613. REPAIRED LT WING BEADED DOUBLER XOS 610-616 IAW SRM 57-40-02, REPAIR 15, FIG 203.
EMERGENCY LIGHT OVER THE FLT DECK STAIRS INOP (LOW BATTERY). REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-51-00, OPS NORMAL.
NR 3 ENG N2 REACH 112 PERCENT DURING DEPARTURE. THRUST REVERSE LEVERS IDLE AND N2 WAS 10 PERCENT OR HIGHER THAN OTHER ENGS. NR 3 ENG SHUTDOWN AND RETURNED TO FIELD. DUMPED FUEL AND DECLARED EMERGENCY. ATB, INTERCHANGED ENG NR 2 AND 3 N2 INDS. ENG GRND RUN UP PERFORMED BY FLT CREW. AT IDLE PWR ENG NR 2 N2 IND WAS READING APPROX 1.5 PERCENT HIGHER THAN ENG NR 3 WITH AN INCREASE OF RPM. ENG NR 2 INDICATION DIFFERENCE BECAME GREATER 10 PERCENT TLA DIFFERENCE BECAME GREATER. 10 PERCENT TLA DIFFERENCE APPROX 4 PERCENT BOTH N1 MATCHED INDICATION ENG NR 2 HIGHER ENG NR 3 N2 INDS RETURNED TO POS M306224.
NLG RT SIDE WEB FOUND CRACKED AT STA 300 WL 150. CRACK LENGTH 0.25 IN. NLG W/W RHS SIDE WEB REPAIRED AT BS 300 WL 150 AREA AS PER SRM 53-10-04 FIG 116.
FLOORBEAM AT STA 1800 HAS ELONGATED HOLES. A/C OOS AND WILL REQUIRE MX FERRY (9127) TO SAT. INSTALLED FREEZE PLUG AT STA 1800 LBL 99 IN FLOORBEAM IAW SA SK 675-800542.
INSPECTION TYPE:N/A EMERGENCY LIGHT CONTROL SWITCH INTERMITTENT FOR EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL MODULE AS PER MM 33-51-09, OPS CHECKS OK.
BS 1080 TO BS 1100 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100" BY 1" BY 5" EXCEED SRM LIMIT. ALL REPAIR PARTS AND NEW STRINGER SEGMENT INSTALLED AS PER RS R-53-41-35252 AND ENGINEERING FILE NUMBER : 747-53-20221.
BS 1560 - 1580 AFT RHS WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.040" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPLICE ANGLE INSTALLED AS PER SRM 51-40-04 FIG 3. STRINGER SEGMENT AND SPLICE ANGLE REWORKED REFER COMPONENT WORK PROCESS CARD SEQUENCE NR HE70522-1, -2, -3 FOR DETAILS.
BS 1560 TO 1580 AFT LT WINDOW FORGING REMOVED FOUND STR CORROSION. CORROSION BLEND OUT 0.040 INCH BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPLICE ANGLE INSTALLED AS PER RS R-53-61-35239 AND ENGINEERING FILE NUMBER : 747-53-20222.
BS 980 - 1000 AFTER LT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.060" BY 1" BY 3" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPLICE ANGLE INSTALLED AS PER RS R-53-41-35234 AND ENGINEERING FILE NUMBER : 747-53-20213.
INSPECTION TYPE:C M/D BS 1580 TO BS 1600 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.100 X 1 X 10 EXCEED SRM LIMIT. STRINGER SEGMENT AND SPLICE ANGLE REWORKED REFER COMPONENT WORK PROCESS CARD SEQUENCE NR HE70480-1, -2, -3 FOR DETAILS.
INSPECTION TYPE:C BS 1560 TO BS 1580 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.060 X 1 X 7 INCH, EXCEED SRM LIMIT. FLAP PEEN CARRIED OUT AS PER SRM 51-10-07 AND SOPM 20-10-03, STRINGER SEGMENT AND SPLICE ANGLE REWORKED REFER COMPONENT WORK PROCESS CARD SEQUENCE NR HE70480 -1, -2, -3 FOR DETAILS.
BS 1020 TO 1040 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100 BY 1 BY 10 INCHES EXCEED SRM LIMIT. ALL REPAIR PARTS AND NEW STRINGER SEGMENT INSTALLED AS PER RS R-53-41-35252 AND ENGINEERING FILE NUMBER : 747-53-20221.
BS 1220 TO 1240 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.080" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT, SPLICE ANGLE AND REPAIR STRAP INSTALLED AS PER RS R-53-41-35245 AND ENGINEERING FILE NUMBER : 747-53-20220.
BS 1438 TO 1460 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT, REPAIR STRAP AND SPICE ANGLE INSTALLED AS PER RS R-53-41-35248 AND ENGINEERING FILE NUMBER : 747-53-20223.
INSPECTION TYPE:C, CORROSION INDICATOR REVEALED ON FUSELAGE UPPER SKIN AT BS 1820 TO BS 1825 STR 46L. CORROSION BLEND OUT 0.035 X 2 X 2 INCHES EXCEED SRM LIMIT. OVER LAPPING SKIN REPLACED AS PER SRM 53-30-03 FIG 17 AND REPAIR DOUBLER AND FILLER INSTALLED AS PER SRM 53-30-03 FIG 17.
INSPECTION TYPE:C RT WING BS 1241 UPPER REAR SPAR SIDE-TO-BODY KICK FITTING AREA FOUND CRACK AT TERMINAL FITTING NR 2 HOLE. HOLE REPAIRED AS PER SB 747-57A2314.
BS 940, S25L FRAME I/B CHORD FOUND CRACK. M/D BS 940 FRAME AT S-25L, FRAME REPAIRED PER RS R-53-22-35244 AND EO B747-5310-21670-A.
INSPECTION TYPE:C - BS 1160 - 1220 RBL 97 SEAT TRACK I/B FLANGE FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 2 INCH. SEAT TRACK CUT OFF AT BS 1070 RBL 98 AS PER SRM 51-10-01. REPROTECTED AS PER SRM 51-10-02. SEAT TRACK REPAIR PARTS FABRICATED PER SRM 53-10-05 FIG 34.
INSPECTION TYPE:C - BS 520 - 540 LBL 46 SEAT TRACK CORRODED AS MARKED. U/D BS 520 - 560 LBL 46 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 6. CORROSION BLEND OUT 0.060 X 1 X 1 INCHES EXCEED SRM LIMIT.
INSPECTION TYPE:C U/D - BS 480 LBL 46 SEAT TRACK CORRODED AS MARKED. U/D BS 480 - 500 LBL 46 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 6. CORROSION BLEND OUT 0.050 X 1 X 2 INCHES EXCEED SRM LIMIT.
INSPECTION TYPE:C - FLOORBEAM BS 340 LBL 11 - 39 UPPER CHORD CORRODED. REPAIR PARTS FABRICATED AS PER SRM 53-10-07 FIG 23. CORROSION BLEND OUT 0.050 X 2 X 2 INCHES EXCEED SRM LIMIT.
INSPECTION TYPE:C - R3 DOOR LOWER WEB CRACKED AT LOWER GATE PUSH ROD CUTOUT. LOWER WEB REPAIRED AS PER SRM 51-40-02 FIG 1.
BS 480 - 500 RBL 66 SEAT TRACK CORRODED AS MARKED. SEAT TRACK PART FABRICATED AS PER SRM 51-10-01 PG 9. CORROSION BLEND OUT 0.050 X 2 X 2 INCHES EXCEED SRM LIMIT.
STA 1170 TO 1250, BTN L11 AND R11 FLR METAL PNL SKIN FOUND CORR. METAL FLOOR PANEL REPAIRED AS PER RS R53-20-35251 AND EO B747-5320- 21675-A AND THIS METAL PANEL NEED REPLACEMENT WITHIN 18 MONTHS OR 1000 CYCLES WHICHEVER OCCURS FIRST. CORROSION BLEND OUT DEPTH 0.040 INCH WIDTH 2 INCHES LENGTH 5 INCH OUT OF SRM 53-10-01 FIG 1 LIMIT.
INSPECTION TYPE:C - BS 1000 LBL 33 O/B SEAT TRACK FLANGE CORRODED. M/D BS 990 - 1000 LBL 33 SEAT TRACK REPAIR PARTS FABRICATED AS PER SRM 53-10-05 FIG 1A. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM LIMIT.
STA 1020 TO 1110, BTN L11" AND R11" FLR METAL PNL SKIN FOUND CORROSION. FLOOR PANEL REPAIRED AS PER RS R53-20-35251 AND EO B747-5320-21675-A AND THIS METAL PANEL NEED REPLACEMENT WITHIN 18 MONTHS OR 1000 CYCLES WHICHEVER OCCURS FIRST. CORROSION BLEND OUT DEPTH 0.004" WIDTH 1" LENGTH 4" WITHIN SRM 53-20-01 FIG 1 LIMITS.
INSPECTION TYPE:C M/D - BS 1180 RBL 97 I/B SEAT TRACK SUPPORT FOUND CORRODED. CORROSION BLEND OUT 0.050 X 1 X 1 INCH, EXCEED SRM LIMIT. SEAT TRACK REPAIR PARTS FABRICATED PER SRM 53-10-05 FIG 34.
INSPECTION TYPE:C M/D - STR END BS 739 S-8L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-21-35238 AND ENGINEERING FILE NUMBER 747-53-20206.
INSPECTION TYPE:C - BS 960, S8R, FRAME FOUND CRACK. FRAME REPAIRED PER SRM 53-10-04 FIG 54.
INSPECTION TYPE:C, RIGHT WING UPPER REAR SPAR SIDE-OF-BODY SPLICE PLATE FITTING CRACK FOUND AT HOLE NR 5 RUNNING FWD APPROX 0.060 INCH AND AFT APPROX .125 INCH. PLS REFER ATTACH FIG. HOLE REPAIRED AS PER S/B 747-57A2314.
INSPECTION TYPE:C - FRAME BS 760 STR CUTOUT CRACKED AT S-6L AND S-7L. M/D BS 760 BETWEEN STR 6L AND STR 7L FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.
INSPECTION TYPE:C - BS 740, BETWEEN S7 - 8R, FRAME FOUND CRACK. M/D BS 740 BETWEEN STR 7R AND STR 8R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.
INSPECTION TYPE:C - BS 760, BETWEEN STR 5 - 8R, FRAME FOUND CRACK. M/D BS 760 BETWEEN STR 5R AND STR 8R FRAME REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 54.
INSPECTION TYPE:C - BS 640, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.
INSPECTION TYPE:C U/D - BS 620, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.
INSPECTION TYPE:C, FWD CARGO COMPT - SUPPORT FRAME WEB SURFACE FOUND CRACKED AT STA 880 BETWEEN STRINGER 37L TO STRINGER 38L. SUPPORT FRAME REPAIRED PER SRM 53-10-04 FIG 52.
INSPECTION TYPE:C U/D - BS 680, S9R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.
INSPECTION TYPE:C - STRINGER END BS 990 S-9L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.
INSPECTION TYPE:C - STRINGER END BS 990 S-7L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.
INSPECTION TYPE:C - BS 736 - 738, S23R STRINGER END FOUND CRACK. M/D BS 736 TO BS 738 S-23R STRINGER END REPAIRED AS PER RS 53-61-35230 AND ENGINEERING FILE NUMBER 747-53-20204.
INSPECTION TYPE:C U/D - BS 560, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.
BS 1482 - 1485, STR 13R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER RS 53-41-35250 AND ENGINEERING FILE NUMBER 747-53-20214.
BS 1480 - 1485, S6L, STRINGER END FOUND CRACKED. STRINGER REPAIRED PER RS R53-41-35249 AND ENGINEERING FILE NUMBER 747-53-20215.
INSPECTION TYPE:C - BS 736 - 738, S8R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.
INSPECTION TYPE:C - BS 1080 RBL 99 BELOW FLOOR STIFFENER FOUND CRACKED. M/D BS 1080 RBL 99 BELOW FLOOR STIFFENER REPLACED IAW SRM 51-10-01 PAGE 9.
INSPECTION TYPE: C, RIGHT WING STA 1241 UPPER REAR SPAR SIDE - OF - BODY SPLICE PLATE AREA FOUND HOLE NR 3 CRACKED AT WING UPPER SKIN AND INTERNAL SPLICE FITTING APPROX 0.040 INCH REFER ATTACHED SKETCH. HOLE REPAIRED AS PER SB 747-57A2314.
INSPECTION TYPE:C M/D - BS 1220 RBL 118 BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. WEB REPAIR PER SRM 51-40-02 FIG 1.
BS 1060 STR 5R, STRINGER TIE CLIP FOUND CRACKED. M/D BS 1060 STR 5R, STRINGER TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9.
STR END BS 1485 S-8L CRACKED. STRINGER REPAIRED PER RS 53-1-35249 AND ENGINEERING FILE NUMBER 747-53-20215.
BS 1460 - 1480 S8R STRINGER END FOUND CRACKED. STRINGER REPAIRED PER RS R53-41-35249 AND ENGINEERING FILE NUMBER 747-53-20215.
INSPECTION TYPE:C - BS 1040 STR 1R, STRINGER TIE CLIP FOUND CRACKED. M/D BS 1040 STR 1R, STRINGER TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9.
INSPECTION TYPE:C M/D - BS 1500 RBL 38 FLOORBEAM FOUND CORRODED. FLOORBEAM REPAIR PARTS FABRICATED PER SRM 51-40-04 FIG 1. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM LIMIT.
BS 1480 - 1500 S8R STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER HX RS R-53-41-35249 AND ENGINEERING FILE NUMBER: 747-53-20215.
INSPECTION TYPE:C M/D - BS 660, BET S25 - 26R, FRAME I/B CHORD O/B FACE FOUND CRACK. FRAME I/B CHORD REPLACED PER SRM 51-10-01 PG 9.
INSPECTION TYPE :C, STR BS 1120 S-7L CRACKED, M/D BS 1120 STR 7L STRINGER. REPAIRED CARRIED OUT IAW SRM 53-10-03 FIG 4.
INSPECTION TYPE:C - STA 1482 LBL 99 SEAT TRACK FLANGE CORROSION. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.050 INCH BY 1 INCH BY 1 INCH. CORROSION BLEND OUT EXCEED SRM 53-10-01 FIG 1 LIMITS, REPAIR REFER TO SRM 53-10-05 FIG 1A.
INSPECTION TYPE: C, FWD CARGO COMPT SUPPORT FRAME SHEAR TIE FOUND CRACKED AT STA 780 STR 33 TO STR 34. SHEAR TIE REPAIRED PER SRM 53-10-04 FIG 4.
INSPECTION TYPE:C M/D - BS 742 - 744 STR 23R, STRINGER END FOUND CRACK. M/D BS 742 TO BS 744 S-23R STRINGER END REPAIRED AS PER RS : 53-61-35230 AND ENGINEERING FILE NUMBER 747-53-20204.
INSPECTION TYPE:C M/D - BS 1040 S9R STRINGER TIE CLIP FOUND CRACKED. STRINGER CLIP REPLACED PER SRM 51-10-01 PG 9.
INSPECTION TYPE:C - BS 1480 - 1500 RBL 11 SEAT TRACK O/B FLANGE FOUND CORRODED. SEAT TRACK REPAIR PARTS FABRICATED PER SRM 53-10-05 FIG 14. CORROSION BLEND OUT 0.040 X 1 X 3 INCHES EXCEED SRM LIMIT.
INSPECTION TYPE:C M/D - BS 1040 S3R STRINGER TIE CLIP FOUND CRACKED. STRINGER CLIP REPLACED PER SRM 51-10-01 PG 9.
INSPECTION TYPE:C - BS 620 S15L FRAME TIE CLIP FOUND CRACK. TIE CLIP REPLACED PER SRM 51-10-01 PG 9.
INSPECTION TYPE:C - BS 1040 S2R STRINGER TIE CLIP FOUND CRACKED. M/D BS 1040 STR 2R STRINGER TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9.
STR END BS 1003 S-3L CRACKED. STRINGER REPAIRED PER RS R-53-41-35231 AND ENGINEERING FILE NUMBER 747-53-20216.
STR END BS 1476 S-6L CRACKED. CRACKED STRINGER REPAIRED PER RS R53-41-35242 AND ENGINEERING FILE NUMBER : 747-53-20217.
INSPECTION TYPE:C, FWD CARGO COMPT - SUPPORT FRAME UPPER CHORD LOWER ATTACH ANGLE SURFACE FOUND CORROSION AT STA 700 LBL 38. ANGLE REPLACED AS PER SRM 51-10-01 PG 9. CORROSION BLEND OUT 0.040 X 1 X 2 INCH.
INSPECTION TYPE:C, RT WING UPPER REAR SPAR SIDE OF BODY SPLICE NR 11 FASTENER HOLE CRACKED AT UPPER SKIN LAYER APPROX 0.060 INCH RUNNING AFT. HOLE REPAIRED AS PER SB 747-57A2314.
INSPECTION TYPE:C, AFT CARGO COMPT RT STA 1660 - 1680 STRINGER 30 WEB SUPPORT BOTTOM SURFACE CORROSION AS MARK. CORROSION BLEND OUT 0.030 X 2 X 2 INCHES EXCEED SRM LIMIT. WEB SUPPORT AND TIE CLIP REPLACED AS PER SRM 51-10-01.
INSPECTION TYPE:C - LEFT BS 2658 STR 13 FOUND CRACKED. STRINGER REPLACED AS PER SRM 50-10-01.
INSPECTION TYPE:C - BS 1000 TO 1020 S10R STRINGER END FOUND CRACKED. M/D BS 1000 TO BS 1030 STR 10R STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 4.
INSPECTION TYPE:C, LOWER FUSELAGE LT INTERNAL NOSE L/G WHEEL WELL VERTICAL BEAM HORIZONTAL STIFFENER ATTACH CLIP FOUND CRACKED AT STA 300 WL 150. STIFFENER ATTACH CLIP REPLACED PER SRM 51-10-01 PG 9.
INSPECTION TYPE:C M/D - STR END BS 1476 S-15L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-41-35226 AND ENGINEERING FILE NUMBER 747-53-20202.
INSPECTION TYPE:C - BS 1160 S15L STRINGER TIE CLIP FOUND CRACKED. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.
FRAME BS 1540 INNER FLANGE CRACKED BTN S-25L / S-26L. INNER FRAME REPAIRED PER RS R-53-62-35241 AND EO B747-5310-21656-A.
BS 940, STR 25L, FRAME FOUND CRACK. M/D BS 940 FRAME AT S-25L REPAIRED AS PER RS R-53-22-35244 AND EO B747-5310-21670-A.
BS 1476 - 1478 STR 13R STRINGER END FOUND CRACK. STRINGER REPAIRED PER RS 53-41-35250 AND ENGINEERING FILE NUMBER 747-53-20214.
FRAME BS 1600 INNER FLANGE CRACKED BTN S-25 / S-26L. INNER FLANGE REPAIRED PER RS R53-62-35240 AND EO B747-5310-21668-A.
FRAME BS 1416 INNER FLANGE CRACKED AT S-22L. M/D FRAME INNER FLANGE REPAIRED AT BS 1416 S-22L AS PER RS : R-53-42-35233 AND ENGINEERING FILE NUMBER : 747-53-20219.
BS 980, STR 26R FRAME I/B CHORD FOUND DEEP CHAFING MARK. FRAME I/B CHORD REPAIRED PER RS 53-62-35225 AND EO B747-5310-21667-A.
INSPECTION TYPE:C M/D - BS 1372, BETWEEN STR 22 - 23R, FRAME I/B CHORD O/B FACE FOUND CRACK. M/D FRAME I/B CHORD REPAIRED AT BS 1372 BETWEEN S-22R AND S-23R AS PER RS 53-62-35246 AND ENGINEERING FILE NUMBER 747-53-20208.
INSPECTION TYPE:C - FRAME BS 1372 INNER FLANGE CRACKED AT S-22L. INNER FRAME REPAIRED PER RS 53-42-35235 AND ENGINEERING FILE NUMBER 747-53-20205.
INSPECTION TYPE:C - STR END BS 1484 S-17L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-41-35227 AND ENGINEERING FILE NUMBER 747-53-20203.
INSPECTION TYPE:C M/D - FRAME BS 1438 SHEAR TIE CRACKED BTN S-23L/S-24L. M/D BS 1438 BETWEEN STR 23L/STR 24L FRAME SHEAR TIE REPAIR CARRIED OUT IAW SRM 53-10-04 FIG 4.
INSPECTION TYPE:C, LEFT WING UPPER REAR SPAR OF BODY SPLICE FOUND CRACK AT NR 8 HOLE UPPER SPLICE FITTING RUNNING AFT. BOLT HOLE REWORK AS PER S/B 747-57A2314.
INSPECTION TYPE:C, LT WING UPPER REAR SPAR SIDE OF BODY SPLICE FOUND CRACK AT NR 1 HOLE AT SPAR CHORD (REFER FIGURE FOR DETAILS ). HOLE REPAIRED AS PER S/B 747-57A2314.
INSPECTION TYPE:C, LT WING UPPER REAR SPAR SIDE OF BODY SPLICE FOUND CORROSION CRACK AT HOLE NR 4 AT INTERNAL SPLICE FITTING (REFER FIGURE FOR DETAILS ). HOLE REPAIRED AS PER SB 747-57A2317.
FRAME BS 1394 INNER FLANGE CRACKED AT S-22L. M/D FRAME AT BS 1394 S-22L INNER FLANGE REPAIRED PER RS R-53-42-35229 AND ENGINEERING FILE NUMBER : 747-53-20218.
BS 1560, STR 26R, FRAME I/B CHORD FOUND CRACK. FRAME REPAIRED PER RS R-53-62-35243 AND EO B747-5310-21669-A.
INSPECTION TYPE:C M/D - BS 1640 LT STR 3L TIE CLIP FOUND CRACKED. M/D BS 1640 STR 3L TIE CLIP REPLACED IAW SRM 51-10-01 PAGE 9.
INSPECTION TYPE:C - BS 1680 LT S-L8 STRINGER FOUND CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 4.
INSPECTION TYPE:C - BS 1540 LT, 11L STRINGER FOUND CRACKED. M/D BS 1540 CTR 11L STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 4.
INSPECTION TYPE:C, NR 4 NACELLE STRUT REAR MOUNT BULKHEAD FWD OUTBOARD FRAME WEB FOUND CRACKED (REFER ATTACH SKETCH FOR LOCATION). REAR ENG MOUNT BULKHEAD FRAME REPAIRED PER RS R54-53-35228 AND ENGINEERING FILE NUMBER 747-54-20050.
INSPECTION TYPE:C, RT WING NR 23 O/B ARM I/B RIB O/B FACE -D- POINT AREA SUSPECT CRACK. RIB REPAIRED AS PER RS R-57-41-35223 AND EO B747-5740-21619-A.
INSPECTION TYPE:C, LEFT BLG WHEEL WELL AFT BULKHEAD STA 1480 APU DUCT PASSING HOLE CUTOUT SUSPECT CRACKED AT 10:30 POSITION AS MARKED. LEFT BS 1480 BULKHEAD WEB APU DUCT CUTOUT REPAIR CARRIED OUT AS PER EO B747-5310-C APPENDIX B FIG 4 AND DWG 144U2602.
INSPECTION TYPE: SPV, SEAT TRACK SUPPORTS HAVE ELONGATED MOUNTS HOLES AT STA 1920, 1940, LBL 98.58. REMOVED 2EA DAMAGED SUPPORT ANGLES. FABBED ANGLE 69B04527 PER DWG STA 1920 ATTACH ANGLE CRACKED. FABBED AND INSTALLED REPAIR PER SRM 51-40-03. NDT VERIFIED DAMAGE REMOVAL. INSTALLED ALL REPAIRED AND/OR REM. PARTS REF SRM 51-10-02, 51-30-02, 51-40-03.
INSPECTION TYPE: SPV, FLOORBEAM 65B38092, STA 1840 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD HOLE 0.330 IN, AFT HOLE 0.390 IN. REAMED HOLES TO 0.389 AND 0.432. FABRICATED AND INSTALLED FREEZE PLUGS PER EO. REPLACED 65B38120-1 FITTING DUE TO OVERSIZED HOLES. FAB & INSTALLED 69B04576-5 & 69B04576-7 FITTINGS DUE TO EXCESSIVE GOUGES FOUND DURING DISASSMBLY.
INSPECTION TYPE: SPV, FLOORBEAM 65B38095 STA 1900, LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED FWD HOLE 0.350, AFT HOLE 0.390. REMOVED AFT ATTACH ANGLE, REAMED BEAM HOLES FWD 0.389, AFT 0.432 PER EO. FAB & INSTALLED 2EA FREEZE PLUGS PER SKETCH & SRM 51-10-08. FWD ATTACH FITTING 69B04576-7 GOUGED BEYOND LIMITS. FAB & INSTALLED -7 PER DWG AND SK AFT FTG 69B04576-5. FAB & INSTALLED PER DWG & SK, C/W SAA SK675-619.
INSPECTION TYPE: SPV, FLOORBEAM 65B38093, STA 1860 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED. FWD HOLE 0.350, AFT HOLE 0.410. REMOVED AFT TRACK ATTACH ANGLE. REAMED BEAM HOLES TO 0.389 & 0.432 PER EO. FAB & INSTALLED FREEZE PLUGS PER SKETCH AND SRM 51-10-08. REAMED TRACK ATTACH FITTING O/B HOLES TO 0.341 & 0.400 PER EO. FAB & INSTALLED 1EA 69B04297-1 & 69B04576-7 PER EO C/W SK675-916.
INSPECTION TYPE: SPV, FLOORBEAM 65B38094 STA 1880, LBL 98.58 SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD HOLE 0.340, AFT HOLE 0.380. REMOVED AFT ATTACH ANGLE, REAMED HOLES IN BEAM TO 0.389 PER EO. FAB & INSTALLED FREEZE PLUGS PER SKETCH. REAMED OVERSIZED TRACK ATTACH FITTING HOLES TO 0.375 IN. FAB AND INSTALLED 1 EA 69B04297-3 & 1 EA 69B04576-5 PER EO TO C/W SAA SK675-916.
INSPECTION TYPE: SPV, FLOORBEAM 65B38096 STA 1920 LBL 98.58, SEAT TRACK ATTACH HOLES FOUND OVERSIZED, FWD & AFT HOLES 0.380. REAMED BEAM HOLES TO; FWD 0.389, AFT 0.432 PER EO. FAB & INSTALLED FREEZE PLUGS PER SKETCH & SRM 51-10-08. FAB FWD FITTING 69B04238 & AFT FITTING 65B38747. INSTALLED FITTING PER EO C/W SK675-916.
INSPECTION TYPE: SPV, MAIN DECK SEAT TRACK REMOVED ALONG LBL 98.58 FROM STA 1840-1920. TRIMMED OUT DAMAGED SEAT TRACK & FABBED REPLACEMENT SECTION REF SRM 53-10-05 FIG 1A, DETAIL II. FABRICATED SPLICE FITTING 69B02537-15 PER DWG. FABRICATED 69B04238-1,-3 FITTINGS PER DWG'S, INSTALLED ALL PARTS PER SRM 53-10-05 FIG 1A DETAIL II, 51-10-2 & EO B747-5310-21190.
MAIN CARGO DECK CEILING EMERGENCY LIGHT FWD OF L1 DOOR HAS ONE BULB INOPERATIVE AND VERY DIM. REMOVED AND REPLACED MAIN CARGO DECK CEILING EMERGENCY LIGHT JUST FWD OF L1 DOOR IAW MM 33-51-07. OPS CKS NORMAL.
INSPECTION TYPE: C-FX, STA 500, S38L SUPPORT FRAME FOUND CRACK AS MARKED. FX STA 500 STR 38L SUPPORT FRAME REPAIRED AS PER RS R53-12-35040 AND EO B747-5310-18971-A.
INSPECTION TYPE: C FX - STA 240 LBL 28, M/D FLOOR SUPPORT BEAM WEB FOUND CRACKED AS MARKED. FX - STA 240 M/D FLOOR SUPPORT BEAM WEB REPAIRED IAW SRM 53-10-07 FIG 11 JUST BETWEEN LBL 18 INCHES TO LBL 38 INCHES.
INSPECTION TYPE:C FX - STA 255 S39L STRINGER SPLICE FOUND CRACKED. FX - STA 249 - STA 260 S39L STRINGER SPLICE REPLACED IAW SRM 51-10-01 P.8
INSPECTION TYPE:C RT BLG W/W PRESSURE DECK SKIN CORRODED AT FS 1391 - 1395 RBL 116-120 . FS 1385- FS 1395 PRESSURE DECK WEB REPAIRED IAW SRM 53-10-07 FIG 2.
INSPECTION TYPE:C RT BLG W/W PRESSURE DECK WEB CORRODED CRACK AT FS 1436-1438 RBL 112-114. PRESSURE WEB REPLACED IAW SRM 51-10-01 PG 8 DUE TO COR CRACK 1 INCH X 1 INCH AND THROUGH THE WHOLE THICKNESS EXCEEDED SRM 53-10-01 FIG 1 LIMITATION.
INSPECTION TYPE:C FX - FUSELAGE EXTERIOR SKIN CORROSION CRACKED AT RIVET HOLE AREA AT STA 2200, S40R - S42R AS MARKED. FX EXTERIOR SKIN REPAIRED AT BS 2200 STR 40R - STR 42R IAW SRM 53-30-03 FIG 1 DUE TO CORROSION CRACKED AREA TRIMMED 2.75 INCHES X 3 INCHES.
INSPECTION TYPE:C FX - LOWER FUSELAGE EXTERNAL SKIN FOUND BULGE - AT STA 2182 TO STA 2184 STRG 44R RT SIDE. FX STRINGER REPAIRED AT BS 2180 - 2210 STR 41R AS IAW SRM 53-10-03 FIG 1 AND FX EXTERNAL SKIN REPAIRED AT BS 2180 - 2184 STR 44R AS IAW SRM 53-30-03 FIG 47 DUE TO SKIN BLENDED OUT AREA 0.042 INCH X 2 INCH LENGTH X 1 WIDTH AND STRINGER CORROSION CRACK ABOUT .7500 INCH LONG WHICH ARE EXCEEDED SRM 53-30-01 FIG 1 AND 53-10-01 FIG 1 LIMITATION RESP.
INSPECTION TYPE: C, NR 2 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD, CRACK REVEALED AT O/B SIDE FWD FRAME WEB LOWER O/B EDGE AS MARKED. NR 2 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD FRAME WEB REPAIRED AS PER RS R54-53-35039 AND UPS ENGINEERING FILE NR 747-54-20037.
INSPECTION TYPE: C, NR 2 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD, CRACK REVEALED AT I/B SIDE AFT FRAME WEB LOWER EDGE AS MARKED. NR 2 NACELLE STRUT REAR ENGINE MOUNT BULKHEAD FRAME WEB REPAIRED AS PER RS R54-53-35039 AND ENGINEERING FILE NUMBER 747-54-20037.
INSPECTION TYPE:C FX - AIR CONDITIONING BAY PANEL SUPPORT LOWER SURFACE FLOATING NUT AREA FOUND SURFACE CORROSION AT STA 1220 TO STA 1235 RBL 57 I/B SIDE. PANEL SUPPORT REPAIRED AT FX BODY FAIRING SUPPORT LOWER BS 1220-1235 RBL 57 I/B SIDE AS IAW SRM 51-40-04 FIG 1.
ELECTRICAL FUMES IN COCKPIT. FOUND R-1 WINDOW WIRE HOT. WIRE AND POST SO HOT YOU COULD NOT TOUCH THEM. FOUND D404 TERMINAL ARCING AND IT HAD DAMAGED TERMINAL SO IT COULD NOT BE REPAIRED. REMOVED AND REPLACED WINDOW. LT WINDOW HEAT CONTROLLER REMOVED AND REPLACED PER MM 30/41/01. REMOVED AND REPLACED R-1 WINDOW IAW MM 56-11-1. OK FOR SERVICE,
DURING PREFLT INSPECTION 2 EMERGENCY LIGHTS ARE OUT ABOVE UPPER DECK EMERGENCY EXIT DOOR. REMOVED AND REPLACED BATTERY POWER UNIT (X327) PER WDM 33-51-01 & OPERATION CHECKED GOOD.
INSPECTION TYPE:PFLT UPPER DECK EMERGENCY EXIT DOOR HAS 1 LIGHT INOP. REMOVED PANEL, RELAMPED UPPER DECK CREW SERVICE DOOR AFT EMERGENCY LIGHT & INSTALLED & SECURED PANEL.
INSPECTION TYPE:N/A I/BOUND TO SDF MX FOUND UPPER DECK, AFT EMER LIGHT FWD LIGHT BULB IN OP. R/R LIGHT.
INSPECTION TYPE:N/A, ON CLIMBOUT GOT A BTB TRIP ON NR 2 WITH MOMENTARY FLASH OF FIRE WARNING HAD GCU LT ON GEN PARALLEL SHOWED MOMENTARY FLUX ON AC VOLT. RESET PWR AOM OPS NORMAL REMAINDER OF FLIGHT. NOTED TO MMOC INFM NR 2 BTB OK WITH APU PWR AND FIRE WARNING SYS TEST NORMAL. RAN ENG NR 2 FOR GCU OPR. CHECKED ALL OK BY FLT CREW.
INSPECTION TYPE:N/A LENS ASSY MISSING FROM EMERGENCY LIGHT AT STA 340 RT MAIN CARGO DECK. REPLACED MISSING LENS ASSY.
INSPECTION TYPE:N/A OVERHEAD EMERGENCY LIGHT STA 405 ONLY REMAINS ILLUMINATED FOR APPROX 5 SEC. REMOVED AND REPLACED LIGHT PACK ASSY, OPS NORMAL.
INSPECTION TYPE:N/A ENG NR 2 OIL TEMP CLIMBED INTO YELLOW RANGE THEN HIT RED RADIAL 8 MIN LATER. EXECUTED PRECAUTIONARY INFLIGHT SHUTDOWN AT 08H53Z. REMOVED AND REPLACED FUEL HEATER VALVE AND FUEL /OIL COOLER. ENG RUN AT EPR 1.18 FOR 32 MIN OIL TEMP 70 DEGREES C. ALL CHECKS OK.
INSPECTION TYPE:C AFT CARGO COMPT - AFTER BEAM UPPER CHORD REMOVED, BS 1820 S42L TO 43L FRAME FOUND HEAVY CORROSION. FRAME REPAIR AT AFT CARGO BS 1820 STR 42L-43L.
INSPECTION TYPE:C FWD CARGO COMPT - BS 960 RBL 25 TRACK FLANGE FOUND CORRODED AFTER END FITTING REMOVED. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-21 FIG 5.
INSPECTION TYPE:C M/D - BS 895 RBL 33 SEAT TRACK HEAVY CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.
INSPECTION TYPE:C M/D - BS 1935 LBL 98 SEAT TRACK CROWN FOUND CORROSION. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1.
INSPECTION TYPE:C RT BS 1480 HOLE 3 FOUND CRACK AT OUTER CHORD SPLICE FITTING. RT BS 1480 OUTER CHORD SPLICE FITTING 3 HOLE OVERSIZED TO DIA 0.625 AND CRACK FREE PER SB 747-53A2390 AND EO 5310-10732 REPAIR BUSHING INSTALLED AS PER SB 747-5A2390.
INSPECTION TYPE:C FUSELAGE - BODY FAIRING SUPPORT FRAME WEB CORRODED AT BS 1540 RBL 20. FAIRING SUPPORT WEB REPAIRED SRM 53-50-04 FIG 1.
INSPECTION TYPE:C EMP - BS 2360 APB AFT FACE AT 11 O/C POSITION RADIAL LAP FOUND 1 REPAIR WHICH CANNOT CATEGORIZED AS DETAIL I TO V REPAIR AS PER EO B747-5310-10823-I. THE EXISTING DOUBLER WAS REMOVED, AREA INSPECTED AND A FASTENER LOCATION WAS FOUND WITH A DENTED MARK ON AFT WEB AREA, REPAIRED AS PER HX RS R-53-83-34744, UPS EO B747-5310-16417-A.
INSPECTION TYPE:C AFT CARGO COMPT - BS 1577 RBL 25 TIE DOWN TRACK VERTICAL ATTACHMENT CORRODED. TIE DOWN TRACK REPLACED AT BS 1500 - BS 1590 RBL 25 AS PER SRM 51-10-01 PG 8.
INSPECTION TYPE:C M/D AFTER WINDOW FORGING REMOVED FOUND SURROUND FX SKIN CORRODED. REPAIR WINDOW FORGING ATT SKIN DOUBLER AT BS 2060-2080 STR 20L - STR 22L AS PER RS R53-61-34742.
INSPECTION TYPE:C M/D - AFTER WINDOW FORGING REMOVED FOUND SURROUND FX SKIN CORRODED. REPAIR SKIN AT BS 1960 - 1980 STR 20R - STR 22R AS PER RS R53-61-347 42.
INSPECTION TYPE:C M/D - AFTER WINDOW FORGING REMOVED FOUND SURROUND FX SKIN CORRODED. REPAIR SKIN AT BS 2120-2140 STR 20R - STR 22R AS PER RS R53-61-34742.
INSPECTION TYPE:C FWD CARGO COMPT BS 760 S40R FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.
INSPECTION TYPE:C AFT CARGO COMPT - BS 1880, LBL 30 FLOORBEAM CORROSION CRACKED. REPAIR FLOORBEAM PER SRM 51-40-04.
INSPECTION TYPE:C AFT CARGO COMPT - BS 1600 LBL 2 TO RBL 2 FLOORBEAM UPPER CHORD CHAFED. FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 2.
INSPECTION TYPE:C M/D - BS 2180 S25L FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.
INSPECTION TYPE:C M/D - BS 2270-7780 RBL 80 LONGITUDINAL FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT CHANNEL REPAIRED AS PER SRM 51-40-03 FIG 1.
INSPECTION TYPE:C AFT CARGO COMPT - BS 1880 S48L FLOORBEAM UPPER CHORD SUPPORT PAD CORRODED. FLOORBEAM UPPER CHORD SUPPORT PAD REPLACED AS PER SRM 51-10-01.
INSPECTION TYPE:C AFT CARGO - BS 1820 LBL 47 FLOORBEAM FOUND CORR CRACK AS MARK. FLOORBEAM REPAIR AT BS 1820 LBL 47 MOST O/B AS PER SRM 51-40-04.
INSPECTION TYPE:C M/D - BS 1940-1990 LBL 118 FLOOR SUPPORT FOUND CORROSION. FLOOR SUPPORT CHANNEL REPLACED AS PER SRM 51-10-01.
INSPECTION TYPE:C M/D - BS 2180 S-25L STRINGER FOUND CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.
INSPECTION TYPE:C M/D - BS 2140 S25L FRAME FOUND CRACK. FRAME REPAIRED AS PER SRM 51-40-03 FIG 02.
INSPECTION TYPE:C AFT CARGO COMPT - BS 1879-1880 S-48L FLOOR SUPPORT WEB CORRODED. REPLACED FLOOR SUPPORT WEB AS PER SRM 51-10-01.
INSPECTION TYPE:C M/D - BS 2120 S25L FRAME FOUND CRACK. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.
INSPECTION TYPE:C M/D - BS 2340- 2360 STRINGER S44R FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.
INSPECTION TYPE:C M/D - BS 2160 S25L FRAME FOUND CRACK. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.
INSPECTION TYPE:C RT BLG W/W BS 1394 O/B WEB UPPER O/B FILLET AREA FOUND CORROSION ADJACENT PRESSURE DECK AREA AS MARK. WEB REPAIRED AS PER 53-10-04 FIG 4.
INSPECTION TYPE:C RIGHT BS 1480 RIGHT WEB 23 HOLE FOUND CRACK AT BULKHEAD WEB SPLICE FITTING. PLS REFER SKETCH FOR DETAILS. RIGHT BS 1480 BULKHEAD WEB 23 HOLE OVERSIZED TO DIA 0.562 INCH AND REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 AND EO 747-510-10732.
INSPECTION TYPE:C RT BS 1480 BULKHEAD WEB 13 FASTENER HOLE CRACK REVEALED APPROX 0.030 INCH IN LENGTH FOR DETAIL. RT BS 1480 BULKHEAD WEB 13 HOLE OVERSIZED TO 0.500 INCH AND REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 AND EO747-5310-10732.
INSPECTION TYPE:C AFT CARGO - STRINGER END FOUND CRACKED AT BS 1740 STR 42R. AFT CARGO COMPT BS 1700 STR 43R REPAIRED PER HX RS 53-61-34732.
INSPECTION TYPE:C M/D - BS 1980-2020 LBL 11 SEAT TRACK O/B FLANGE FOUND CORROSION. TRACK REPLACED AS PER SRM 53-10-05 FIG 14.
INSPECTION TYPE:C M/D - L1 DOOR UPPER HINGE DOUBLER FOUND NON-STANDARD REPAIR. L1 DOOR UPPER HINGE CUTOUT SKIN REPAIRED PER S/B747-52-2144.
INSPECTION TYPE:C FWD CARGO COMPT BS 840 S39R STRINGER CORRODED (AROUND RIVET AREA). STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.
INSPECTION TYPE:C M/D - BS 2313 LBL 7 - RBL 15 HAT SECTION FOUND CORRODED. HAT SECTION REPLACED AS PER SRM 51-10-01.
INSPECTION TYPE:C LT BS 1480 HOLE 19 FOUND CRACKED AT BULKHEAD WEB PNL. LT BS 1480 BULKHEAD WEB 19 HOLE OVERSIZED TO 0.5500 INCH AND REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 AND EO 747-5310-10732.
INSPECTION TYPE:C RT BS 1480 HOLE 3 FOUND CRACKED AT LONGERON EXTENSION FITTING. RT BS 1480 LONGERON EXTENSION FITTING 3 HOLE OVERSIZED TO DIA 0.625 AND REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 AND EO 747-5310-10732.
INSPECTION TYPE:C AFT CARGO DOOR CLOSEOUT BEAM WEB CORRODED AT BS 1910 - 1915. AFT CARGO DOOR AFT LOWER WEB AT BS 1910 - 1905 REPAIRED AS PER SRM 51-40-02 FIG 1.
INSPECTION TYPE:C M/D - BS 1700-1720 S-8L STR FOUND CRACKED. BS 1710-1740 STR 8L REPAIRED AS PER SRM 53-10-03 FIG 4.
INSPECTION TYPE:C FX - RT SIDE TUNNEL STA 300 NOSE WHEEL WELL VERTICAL BEAM WEB ATTACH CHORD FOUND CRACKED AT LOWER AREA FWD FACE AS MARKED. FX RT SIDE TUNNEL STA 300 NOSE WHEEL WELL VERTICAL BEAM WEB ATTACH CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.
INSPECTION TYPE:C M/D - BS 980 RBL 65 FLOORBEAM FOUND CRACK. FLOORBEAM REPAIRED AS PER SRM 53-10-07 FIG 12.
INSPECTION TYPE:C M/D- BS 850 RBL 11 SEAT TRACK O/B FLANGE LOWER FACE CORRODED.
INSPECTION TYPE:C M/D - BS 770 LBL 33 SEAT TRACK FLANGE CORROSION CRACK. SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1.
INSPECTION TYPE:C M/D - BS 770 RBL 75 SEAT TRACK O/B FLANGE CORROSION FOUND. SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 1A.
INSPECTION TYPE:C M/D - UPPER LOBE CROWN STRINGER SPLICE FITTING CORROSION CRACKING FOUND AT BS 1737 S-2R. REPLACED STR SPLICE BS 1740 S2R AS PER SRM 51-10-01 PG 8.
INSPECTION TYPE:C M/D - BS 1920-1940, STR 22R WINDOW FORGING AREA FOUND CORROSION. REPAIRED STRINGER PER SRM 51-40-04 FIG 3.
INSPECTION TYPE:C FX - LT STA 1960 STR 26 SKIN ATT DOUBLER FOUND CRACKED. EXTERNAL DOUBLER REPAIRED AS PER RS R53-61-34730.
INSPECTION TYPE:C RT BS 1480 HOLE 2 FOUND CORROSION AT BULKHEAD CHORD. RT BS 1480 BULKHEAD CHORD 2 HOLE OVERSIZED TO 0.625 INCH AND CRACK FREE AS PER SB 747-53A2390 AND EO 747-5310-10732.
INSPECTION TYPE:C M/D - UPPER LOBE CROWN STRINGER END CRACKED AT BS 1955-1960 S-6R. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 6.
INSPECTION TYPE:C M/D - BS 1660-1680 RBL 11 SEAT TRACK LIP FOUND WORN. SEAT TRACK REPAIRED AT M/D BS 1600-1680 RBL 11 AS PER SRM 53-10-05 FIG 14.
INSPECTION TYPE:C M/D - BS 1700 LBL 70-73 FLOORBEAM LWR CHORD SPLICE FOUND CRACK. CRACKED SPLICE REPLACED AS PER SRM 51-10-01.
INSPECTION TYPE:C M/D - BS 1900-1920, BETWEEN S20R AND S22R WINDOW FORGING AREA FOUND CORROSION. STRINGER REPAIR AT BS 1900 - BS 1960 STR 20R AS PER SRM 51-40-04.
INSPECTION TYPE:C RT BS 1480 HOLE 22 FOUND CRACKED AT BULKHEAD WEB SPLICE PLATE. PLS REFER ATTACHED SKETCH FOR DETAILS. RT BS 1480 BULKHEAD WEB SPLICE PLATE 22 HOLE OVERSIZED TO 0.500 INCH AND REPAIR BUSHING INSTALLED AS PER SB 747-5A2390 AND EO 747-5310-10732.
INSPECTION TYPE:C M/D - BS 1600-1620 RBL 11 SEAT TRACK I/B FLANGE FOUND CORRODED. SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 4.
INSPECTION TYPE:C M/D - UPPER LOBE CROWN STRINGER END CRACKED AT BS 1955 - 1960 S-5R. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 6.
INSPECTION TYPE:C M/D - BS 1800-1820, STR 22R WINDOW FORGING AREA FOUND CORROSION. STRINGER REPAIR PER SRM 51-40-04.
INSPECTION TYPE:C RT BS 1480 HOLE 2 FOUND CRACKED AT FUSELAGE SKIN. RT BS 1480 FUSELAGE SKIN 2 HOLE OVERSIZED TO DIA 0.625 INCH AND CRACK FREE AS PER SB 747-53A2390 AND EO 747-5310-10732.
INSPECTION TYPE:C M/D - BS 760-780 RBL 10, TIE DOWN TRACK FLANGE FOUND CORROSION CRACK AS MARKED. TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 14.
INSPECTION TYPE:C BULK CARGO COMPT - BS 1960 S49R STRINGER FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 8. STRINGER SPLICE REPLACED AS PER SRM 51-10-01.
INSPECTION TYPE:C M/D - BS 1980-2000 S22L STRINGER FOUND CORROSION. REPAIRED AS PER SRM 51-10-01.
INSPECTION TYPE:C M/D - BS 2160-2180 STR S22L STRINGER FOUND CORROSION. REPAIRED AS PER SRM 51-40-04 FIG 3.
INSPECTION TYPE:C M/D - BS 2060-2080 S22L STRINGER FOUND CORROSION. REPAIRED AS PER SRM 51-10-02.
INSPECTION TYPE:C M/D - BS 1780, S17-24R, FRAME I/B CHORD SEVERAL SCRATCH MARK FOUND. SCRATCH MARK SMOOTHED OUT AS PER SRM. FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.
INSPECTION TYPE:C M/D - BS 240 RBL 30 SEAT TRACK CROWN FOUND CRACKED DUE HANDLING. SEAT TRACK REPLACED SRM 51-10-01.
INSPECTION TYPE:C FWD CARGO COMPT - BS 960 RBL 25 LOCK END FITTING CORROSION DAMAGE AT LOW FACE I/B. LOCK END FITTING REPLACED AS PER SRM 51-10-01 PG 8.
INSPECTION TYPE:C M/D - BS 960 LBL 97 SEAT TRACK CROWN CORRODED. SEAT TRACK REPAIRED AS PER SRM 53-10-05.
INSPECTION TYPE:C M/D - BS 2360-S-18R STRINGER FOUND CRACKED. STRINGER REPAIRED AS PER SRM 5-10-03 FIG 4.
INSPECTION TYPE:C FWD CARGO COMPT - BS 840 S-40R STRINGER FOUND CORROSION CRACKED. STRINGER REPAIR AT FWD CARGO BS 830 - 850 STR 40R AS PER SRM 53-10-03 FIG 1.
INSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD UPPER CORNER FOUND FASTENER HOLE CRACKED APPROX .125 INCH AT SKIN BS 1810 TO 1820, WL 190 TO 195. AFT CARGO DOOR FWD UPPER CUTOUT CORNER REPAIRED AS PER SRM 53-30-03 FIG 62.
INSPECTION TYPE:C FWD CARGO COMPT BS 760 RBL 55 FLOOR SUPPORT FOUND CORRODED. FLOOR SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.
INSPECTION TYPE:C FWD CARGO COMPT - S760 S-44R STRINGER FOUND CRACKED. BS 740-770 STR 44R STRINGER REPAIRED AS PER SRM 53-10-01 FIG 1.
INSPECTION TYPE:C M/D : L1 DOOR LOWER HINGE ARM CUTOUT CRACK FOUND. CUTOUT SKIN REPAIRED AS PER S/B747-52-2144.
INSPECTION TYPE:C FWD CARGO COMPT BS 800 S-43R STRINGER FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 01.
INSPECTION TYPE:C UPS CUSTOMER REQUEST NEED TO REEVALUATE PREVIOUS REPAIR - PATCH ON FUSELAGE APPROXIMATELY S36 WING TO BODY FAIRING PANEL RT FWD. EXISTING INTERNAL PATCH REPAIRED BY REPLACEMENT PER SRM 53-30-03 FIG 1 INTERNAL SHEER TIE REPAIRED AT BS 760 STR 37R TO S39R PER SRM 53-10-04 FIG 3.
INSPECTION TYPE:PFLT EMERGENCY EXIT SIGN OVER CREW SERVICE DOOR INOP. REMOVED AND REPLACED POWER SUPPLY MODULE M312 IAW B747 MM 33-51-04, OPS CHECK GOOD.
INSPECTION TYPE:PFLT EMERGENCY INST LIGHT INOP. AFTER TROUBLESHOOTING FOUND LIGHT BULBS BURNT OUT.
INSPECTION TYPE: PREFLT, R-1 WINDOW OUTER PANE CRACKED & SPIDER-WEBBED. INSTALLED WINDOW IN R1 POSITION IAW MM 56-10
INSPECTION TYPE:C, WINDOW BELT AT BS 540 - 560 LHS. SKIN DOUBLER BLENDED AND FOUND OUTSIDE LIMITS. EXTERNAL DOUBLER REPAIR CARRIED OUT IAW QUERY NOTE 40/2000 AMD IAW SRM 51-30-02.
INSPECTION TYPE:C, CRACKS PROPAGATING FORE AND AFT THROUGH 3 FASTENERS AT BS 320 - 340 O/B CHORD OF CREASE BEAM (STR 26R). REPAIR CARRIED OUT IAW SRM 51-40-02.
INSPECTION TYPE:C, MAIN DECK FUSELAGE FRAME WEB CRACKED AT CUTOUT FOR STRINGER AT BS 380 STR 24R. FRAME WEB REPAIRED IAW SRM 53-10-04.
INSPECTION TYPE:C, WINDOW BELT AT BS 740 - 780 LT SIDE. SKIN DOUBLER AT BS 740 - 760 AND 760 - 780 BLENDED AND FOUND OUTSIDE LIMITS. STRINGER 22 ALSO FOUND OUTSIDE LIMITS. REPAIRED IAW QUERY NOTR 37/2000.
INSPECTION TYPE:C, WINDOW BELT AT BS 660 - 700 LT SIDE. SKIN DOUBLER AT BS 660 - 700 AND 760 - 780 BLENDED AND FOUND OUTSIDE LIMITS. EXTERNAL SKIN DOUBLER REPAIR CARRIED OUT IAW QUERY NOTES 33/2000 AND 34/2000.
INSPECTION TYPE:C, WINDOW BELT AT BS 700 - 720 RT SIDE. SKIN DOUBLER BLENDED AND FOUND OUTSIDE LIMITS. EXTERNAL DOUBLER REPAIRED IAW QUERY NOTE 14/2000.
INSPECTION TYPE:C, CRACK FOUND IN FITTING AT BS 1000 RBL 11. REPAIRED IAW QUERY NOTE 57-2000.
INSPECTION TYPE:C, WINDOW BELT AT BS 540 - 560 LT SIDE STRINGER 20 BLENDED AND FOUND OUT SIDE LIMITS. STRINGER REPAIRED IAW QUERY NOTE 40/2000 AND 33/00 STRINGER REPAIRED AND EXTERNAL DOUBLER FITTED TO WINDOW BELT.
INSPECTION TYPE:C, DOOR 2L CRACK IN FWD LOWER CORNER VERTICAL FLANGE. REPAIR CARRIED OUT IAW SRM 52-10-02.
INSPECTION TYPE:C, DOOR 4L CRACK IN FWD LOWER CORNER VERTICAL FLANGE. REPAIR CARRIED OUT IAW SRM 52-10-02.
INSPECTION TYPE:C, DOOR 5R CRACK IN FWD LOWER CORNER VERTICAL FLANGE. REPAIRED IAW QUERY NOTE 66/2000.
INSPECTION TYPE:C, INSPECTION OF BATH FITTING IN NR 3 PYLON REVEALS CRACKS AT VERTICAL FASTENERS. BATH TUB FITTING REPLACED IAW SRM 51-30-02.
INSPECTION TYPE:C, WINDOW BELT AT BS 660 - 680 LHS WINDOW FORGING CRACKED AT TWO LOCATIONS. WINDOW FORGING REPLACED IAW SRM 31-30-02.
INSPECTION TYPE:C, DOOR 1L CRACK IN FWD LOWER CORNER VERTICAL FLANGE. REPAIR CARRIED OUT IAW SRM 52-10-02.
INSPECTION TYPE:C, DOOR 1R CRACK IN FWD LOWER CORNER VERTICAL FLANGE. REPAIR CARRIED OUT IAW SRM 52-10-02.
INSPECTION TYPE:C, DOOR 4R CRACK IN FWD LOWER CORNER VERTICAL FLANGE. REPAIR CARRIED OUT IAW SRM 52-10-02.
INSPECTION TYPE:C, AFT CARGO SUPPORT STRAP AT STR 40 APPROX BETWEEN BS 2060 - BS 2080 RHS CRACKED. NEW STRAP FABRICATED AND FITTED IAW SRM 51-20-01 AND SRM 51-30-02.
INSPECTION TYPE:C, BULK CARGO SUPPORT STRAP AT STR 40L APPROX BETWEEN BS 1960 - 1980 LHS CRACKED. NEW STRAP FABRICATED AND FITTED IAW SRM 51-20-01 AND SRM 51-30-02.
INSPECTION TYPE:C, REPLACE CRACKED BRACKET AT WS 590 BOTTOM CHORD LHS. BRACKET REPLACED IAW SRM 51-30-02.
INSPECTION TYPE:C, FWD CARGO SHEAR TIE BETWEEN UPPER MAIN DECK FLOOR STRUCTURE AT BS1000 BBL 33 IS CRACKED. SHEAR TIE REPLACED IAW Q/NOTE 56/2000 PER STANDARD SRM PROCEDURES.
INSPECTION TYPE:C, WINDOW BELT AT BS 600 - 620 RHS STRINGER 22 CORRODED BEYOND LIMITS. STRINGER REPAIR CARRIED OUT IAW QUERY NOTE 18/2000 AND SRM 51-30-02.
INSPECTION TYPE:C, WINDOW BELT AT BS 220 - 240 STRINGER 20 CORRODED OUTSIDE LIMITS. DAMAGED STRINGER SECTION REMOVED IAW SRM 51-30-02, STRINGER REPAIRED IAW QUERY NOTE 16/2000.
INSPECTION TYPE:C, WINDOW BELT AT BS 360 LHS STRINGER 22 CORRODED BEYOND LIMITS. DAMAGED SECTION OF STRINGER REMOVED IAW SRM 51-30-02, STRINGER REPAIRED IAW QUERY NOTE 14/2000.
INSPECTION TYPE:C, WINDOW BELT AT BS 380 - 400 LHS STRINGER CORRODED BEYOND LIMITS. STRINGER REPAIRED IAW QUERY NOTE 16/2000.
INSPECTION TYPE:C, MAIN DECK FLOORBEAM INTERCOSTAL CRACKED BS 420 - 440 LBL 56. INTERCOSTAL REPAIRED IAW SRM 51-40-02.
INSPECTION TYPE:C, CHANNEL CRACKED AT BS 580 AT FWD CARGO DOOR FWD HINGE FITTING. CHANNEL REPAIR IAW SRM 514003.
INSPECTION TYPE:C, DOOR 1R FWD FRAME LOWER HINGE CUTOUT A CRACK HAS BEEN STOP DRILLED BUT CRACK IS RUNNING BEYOND HOLE. REPAIRED IAW SRM 52-11-02.
INSPECTION TYPE:C, RT WING BULGING ON UPPER L/E RABBET STRAP AT WS 1415. CORROSION REMOVED, AREA EVALUATED AND FOUND WITHIN LIMITS PER SRM 51-10-01.
INSPECTION TYPE:C, FRAME WEB CRACKED AT STRINGER CUTOUT BS 66 STR 24L. REPAIR CARRIED OUT IAW Q/NOTE 44/00, SRM 53-10-04 FIG 35 DETAILS 1 AND 2.
INSPECTION TYPE:C, EXT FUS WING TO BODY FAIRING SUPPORT STRUCTURE BS 960, RBL 7 CORRODED. WING TO BODY SUPPORT STRUCTURE REPAIRED IAW Q/NOTE 48/00, SRM 53-50-04 FIG 1.
INSPECTION TYPE:C, CRACK IN BRACKET AT BS 440 LBL 30 BOTTOM OF CABIN FLOOR. NEW BRACKET FABRICATED AND FITTED IAW SRM 51-20-01 AND 51-30-01.
INSPECTION TYPE:C, FRAME WEB CRACKED AT STRINGER CUTOUT STA 600 STR 25L. THIS REPAIR IS INCORPORATED WITH REPAIR STR 24L BS 660. REF NRC 44336 030 AND MRR CONTROL NR UPS00434336.
INSPECTION TYPE:C FRAME WEB CRACKED AT STRINGER CUTOUT STA 640 STR 25L. REPAIR CARRIED OUT IAW Q/NOTE 43/00, SRM 53-10-04 FIG 35 DETAIL 2.
INSPECTION TYPE:C, FRAME WEB CRACKED AT STRINGER CUTOUT STA 560 STR 24L. REPAIR CARRIED OUT IAW Q/NOTE 42/00, SRM 53-10-04 FIG 35 DETAIL 3.
INSPECTION TYPE:C, FRAME WEB CRACKED AT STRINGER CUTOUTS STA 600 STR 24L/25L. REPAIR CARRIED OUT IAW Q/NOTE 45/00, SRM 53-10-04 FIG 35 DETAIL 1 AND 2.
INSPECTION TYPE:C, FRAME WEB CRACKED AT STRINGER CUTOUT STA 580 STR 24L. REPAIR CARRIED OUT IAW Q/NOTE 41/00 SRM 53-10-04 FIG 35 DETAIL 3.
INSPECTION TYPE:C, PYLON NR 4 CRACK FOUND IN HYD RES SUPPORT BRACKET. BRACKET REPLACED.
INSPECTION TYPE:C, MAIN DECK LT CLOSEOUT PANEL IS CRACKED AROUND TRIM AIR DUCTS ON CANTED PRESS BULKHEAD WHEEL WELL SIDE. CLOSE OUT PANEL REPLACED IAW EO B747-5310-2758-E.
INSPECTION TYPE:C, NR 1 PYLON DAMAGE TO PYLON SKIN LWR SHIRT AREA INBOARD OF REAR ENGINE MOUNT AND FWD OF ENGINE MOUNT. REPAIR CARRIED OUT IAW SRM 54-30-03 FIG 36.
INSPECTION TYPE:C, DOOR 4 L AFT FRAME LOWER CORNER IS CRACKED. DOOR REPAIRED IN SHOP IAW OHM 52-11-03.
INSPECTION TYPE:C, CORROSION ON UPPER DECK SEAT TRACK AT BS 660 - 672 LBL 30. SEAT TRACK REPLACED IAW SRM 51-30-02.
INSPECTION TYPE:C, UPPER DECK CORROSION ON UPPER DECK SEAT TRACK AT BS 560 - BS 620 LBL 48. NEW SECTION OF SEAT TRACK FITTED IAW SRM 51-30-02 FROM BS 550 - 630.
INSPECTION TYPE:C, PYLON NR 3 TT2 SENSOR SUPPORT BRACKET CRACKED. SUPPORT BRACKET REPLACED.
INSPECTION TYPE:C, UPPER DECK SURFACE CORROSION ON SEAT TRACK AT BS 544 LBL 48. NEW SECTION OF SEAT TRACK FITTED FROM BS 520 TO BS 550.
INSPECTION TYPE:C, EXT FUS WING TO BODY FAIRING SUPPORT STRUCTURE. SUPPORT CLIPS ATTACHED TO BELLY PANEL AT BS 860 CORRODED. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
INSPECTION TYPE:C, BRACKET CRACKED AT BS 400 RBL 18 AT E&E FLOOR LEVEL. NEW ANGLE FABRICATED AND FITTED IAW SRM 51-20-02 AND SRM 51-30-02.
INSPECTION TYPE:C, CORROSION ON STRINGER CLIP STA 540 STR 15L. STRINGER CLIP REPLACED IAW SRM 51-30-01.
INSPECTION TYPE:C, RIGHT WLG WW 1241 CANTED B/HEAD TO 1241 WEB UPPER CHORD HAS FOUR AREAS OF VISABLE CORROSION. CORROSION REMOVED AND FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, DOOR 2R AFT FRAME IS CRACKED APPROX 6 INCHES FROM BOTTOM. REPAIR ACCOMPLISHED IAW SRM 52-10-02.
INSPECTION TYPE:C, FRAME WEBS CRACKED AT BS 560, BS 580, BS 600, BS 660, STR 24L, ALSO BS 600, BS 640, BS 660 STR 25L. CRACKS STOP DRILLED IAW SRM 51-10-01.
INSPECTION TYPE:C, TEE PIECE CRACKED AT BS 400 BL 0 AT E&E FLOOR LEVEL. T-PIECE REPLACED IAW SRM 51-30-02.
INSPECTION TYPE:C, BRACKET CRACKED AT BS 400 LBL 20. BRACKET REPAIRED IAW SRM 51-40-04.
INSPECTION TYPE:C, RT WING T/E SPOILER SUPPORT BEAM IS CRACKED AT EXISTING REPAIR ON UPPER CHORD O/B OF I/B HINGE NR 7 SPOILER. REPAIR CARRIED OUT IAW Q/NOT 68/00 NEW SPLICE ANGLES FABRICATED AND FITTED.
INSPECTION TYPE:C, NOSE GEAR WHEEL WELL FWD BULKHEAD WEB STIFFENER CRACKED AT FLOORBEAM BS 265 LBL 22. NEW STIFFENER FABRICATED AND INSTALLED IAW SRM 51-30-02.
INSPECTION TYPE:C, DOOR 2L FWD FRAME BOTTOM LOWER CORNER IS CRACKED. REPAIRS CARRIED OUT IN SHOP IAW SRM 52-30-02.
INSPECTION TYPE:C, SUSPECT CRACK AT BS 320 RHS OF WHEEL WELL THIRD BRACKET UP. NEW BRACKET FABRICATED AND FITTED IAW SRM 51-20-01 & 51-30-02.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 280 - 300 LT. WINDOW FORGING REMOVED, CORROSION REMOVED FROM SKIN DOUBLER IAW SRM 53-10-01. CORROSION REMOVED FROM WINDOW FORGING IAW SRM 53-10-01. FORGING INSTALLED.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 360 - 380 LT. WINDOW FORGING REMOVED, CORROSION REMOVED FROM SKIN DOUBLER AND STR 20 AND 22 IAW 51-10-01. CORROSION REMOVED FROM WINDOW FORGING IAW 56-20-01. STRINGER 22 REPAIRED IAW QUERY NOTE 14/2000.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 380 - 400. WINDOW FORGING REMOVED, CORROSION REMOVED FROM SKIN DOUBLER AND STR 20 AND 22 IAW SRM 51-10-01. CORROSION REMOVED FROM WINDOW FORGING. STRINGER 22 REPAIRED IAW QUERY NOTE 16/2000. WINDOW FORGING INSTALLED.
INSPECTION TYPE:C LH WING . BULGE ON UPPER L/E RABBET STRAP AT WS 893 LIGHT CORROSION REMOVED IAW SRM 51-10-01. EVALUATED AND FOUND WITHIN LIMITS IAW 57-30-01. AREA FLAP PEENED IAW BAC 5730. AREA REPROTECTE D IAW 51-10-02. RIVETS INSTALLED IAW SRM 51-30-02
INSPECTION TYPE:C LH WING . BULGING ON UPPER L/E RABBET STRAP AT WS 550. LIGHT CORROSION REMOVED IAW SRM 51-10-01. EVALUATED AND FOUND WITHIN LIMITS IAW SRM 57-30-01. AREA FLAP PEENED IAW BAC 5730. AREA REPROT ECTED IAW 51-10-02. RIVETS INSTALLED IAW SRM 51-30-02.
INSPECTION TYPE:C, CRACK IN WEB AT BS 134 STR 26R. WEB REPAIRED IAW SRM 51-40-02 AND FITTED IAW SRM 51-30-02.
INSPECTION TYPE:C, SUSPECT CRACK AT BS 300 ON LHS OF WHEEL WELL 2ND BRACKET UP. NEW BRACKET FABRICATED AND FITTED IAW SRM 51-20-01 AND 51-30-02.
INSPECTION TYPE:C, CORROSION FOUND UNDER WINDOW FORGINGS AT BS 220 - 240 LT. WINDOW REMOVED, CORROSION REMOVED FROM DOUBLER IAW SRM 53-10-01. CORROSION REMOVED FROM WINDOW FORGING IAW 53-10-01. FORGING INSTALLED.
INSPECTION TYPE:C, FUSELAGE SKIN FOUND DAMAGED AROUND FASTENER AT BS 1940 BETWEEN STR 46 L AND 47L. DAMAGED EVALUATED AND FOUND TO BE WITHIN LIMITS PER SRM 51-30-01.
INSPECTION TYPE:C, CORROSION AND TOOL DAMAGE TO LWR SURFACE OF TOP CHORD AT BS 265 RBL 10 - 20. PLEASE INVESTIGATE CORROSION REMOVED IAW SRM 51-10-01 AND REPROTECTED IAW SRM 51-30-02.
INSPECTION TYPE:C, SUSPECT CRACK AT BS 280 RHS OF WHEEL WELL 3RD BRACKET UP. NEW BRACKET FABRICATED AND FITTED IAW SRM 51-20-02 & 51-30-02.
INSPECTION TYPE:C, LEFT WLG DOOR FWD HINGE CRACKED. NEW HINGE FITTED IAW MM 32-12-02.
INSPECTION TYPE:C, LEFT BLG WW STA 1416 PREVIOUS REPAIR FOUND CRACKED ON W/BODY SUPPORT FRAME. REPAIR CARRIED OUT IAW SRM 51-40-02.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 540 - 560 LT. CORROSION REMOVED IAW SRM 53-10-01 FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, LT WING WIDE SPREAD SURFACE CORROSION AROUND FASTENER HEADS ON UPPER IN SPAR SKIN. CORROSION REMOVED IAW SRM 51-10-01. AREA EVALUATED IAW SRM 57-30-01. AREA REPROTECTED IAW SRM 51-10-02.
INSPECTION TYPE:C LH WING. BULGE ON UPPER L/E RABBET STRAP AT WS 1374 LIGHT CORROSION REMOVED IAW SRM 51-10-01. EVALUATED AND FOUND WITHIN LIMITS. IAW 57-30-01. AREA FLAP PEENED IAW BAC 5730. AREA REPROTECT ED IAW SRM 51-10-02. RIVETS INSTALLED IAW SRM 51-30-02
INSPECTION TYPE:C, CORROSION FOUND ON SEAT TRACK AT BS 500 RBL 12. SEAT TRACK REPLACED IAW SRM 51-30-02.
INSPECTION TYPE:C, SEAT TRACK CORRODED AT BS 520 LBL 11. SEAT TRACK REPLACED IAW SRM 51-30-02.
INSPECTION TYPE:C, CORROSION FOUND ON SEAT TRACK AT BS 490 RBL 67. NEW SECTION OF TRACK FITTED IAW SRM 51-30-02.
INSPECTION TYPE:C, UPPER DECK LIGHT CORROSION ON UPPER DECK SEAT TRACK AT BS 544 LBL 48. NEW SECTION OF SEAT TRACK FITTED IAW SRM 51-30-02 FROM BS 520 TO BS 550.
INSPECTION TYPE:C, CORROSION FOUND ON RT HORIZONTAL STAB INTERIOR BETWEEN STA 114 AND 122 ON LOWER SURFACE OF REAR SPAR UPPER CHORD. REPAIR CARRIED OUT IAW Q/NOTE 65/00. AREA BLENDED OUT AND EVALUATED. OPEN HOLE HFEC AND DYE PENETRANT INSP ACCOMPLISHED. AREA REPROTECTED. SHIMS FABRICATED AND FITTED.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 640 TO 660 RT. CORROSION REMOVED IAW SRM, FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CENTER WING FRONT SPAR. LOWER CHORD CORRODED AT RBL 85, BS 1000. REPAIRS ACCOMPLISHED PER Q/NOTES 57/00 AND 57/00 SHEAR TIE P/N 69B14 267-6 AND FITTING P/N 69B14592-6 REPLACED.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 720 TO 740 LT. CORROSION REMOVED IAW SRM WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 560 TO 580 LT. CORROSION REMOVED FOUND TO BE WITHIN LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER WINDOW FORGING AT BS 220 - 240 LT. WINDOW FORGING REMOVED. CORROSION REMOVED FROM FORGING AND SKIN DOUBLER IAW SRM 56-20-01 AND 56-10-01. FORGING RE-INSTALLED.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 760 TO 780 RT. CORROSION REMOVED IAW SRM AND FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 740 TO 760 RT. CORROSION REMOVED IAW SRM AND FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 720 TO 740 RT. CORROSION REMOVED IAW SRM AND FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 700 TO 720 RT. CORROSION REMOVED IAW SRM 53-10-01 AND FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 680 TO 700 RT. CORROSION REMOVED IAW SRM AND FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 660 TO 680 RT. CORROSION REMOVED IAW SRM, FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 620 TO 640 RT. CORROSION REMOVED IAW SRM, FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 600 TO 620 RT. CORROSION REMOVED, FOUND OUTSIDE LIMITS REF MRR UPS00434380 FOR REP AIR DETAILS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 580 TO 600 RT. CORROSION REMOVED IAW SRM, FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 560 TO 580 RT. CORROSION REMOVED IAW SRM, FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 540 TO 560 RT. CORROSION REMOVED IAW SRM, FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 520 TO 540 RT. CORROSION REMOVED IAW SRM, FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 760 TO 780 LT. CORROSION REMOVED IAW SRM 53-10-02 AND FOUND INSIDE SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 740 TO 760 LT. CORROSION REMOVED IAW SRM 53-10-02 AND FOUND WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 700 TO 720 LT. CORROSION REMOVED IAW SRM 51-30-02, FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 680 TO 700 LT. CORROSION REMOVED IAW SRM 53-10-02 AND FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 660 TO 680 LT. WINDOW FORGING REMOVED IAW SRM 51-30-02. CORROSION REMOVED FROM SKIN DOUBLER AND STRINGERS IAW SRM 53-30-01. CORROSION REMOVED FROM WINDOW FORGING IAW SRM 56-20-01. CRACKS FOUND NEW FORGING INSTALLED IAW SRM 51-30-02 REF MRR UPS 00434379.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 640 TO 660 LT. CORROSION REMOVED, FOUND TO BE WITHIN SRM LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 620 TO 640 LT. CORROSION REMOVED, FOUND TO BE WITHIN LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 600 TO 620 LT. CORROSION REMOVED, FOUND TO BE WITHIN LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 580 TO 600 LT. CORROSION REMOVED, FOUND TO BE WITHIN LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 540 TO 560 LT. CORROSION REMOVED IAW SRM 51-10-01 AND FOUND INSIDE LIMITS.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 520 TO 540 LT. WINDOW FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED FROM SKIN DOUBLER AND STRINGERS 20 AND 22 IAW SRM 53-10-01, CORROSION REMOVED FROM WINDOW FORGING IAW SRM 56-20-01, WINDOW INSTALLED IAW SRM 51-30-01.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 380 TO 400 LT. WINDOW FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED FROM SKIN DOUBLER AND STR 20 AND 22 IAW SRM 53-10-01. CORROSION REMOVED FROM WINDOW FORGING IAW SRM 56-20-01, STRINGER REPAIRED IAW QUERY NOTE 16/2 000 REF MRR UPS 00434383, WINDOW INSTALLED IAW SRM 51-30-02.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 360 TO 380 LT. WINDOW FORGING REMOVED IAW SRM 51-30-02, CORROSION REMOVED FROM SKIN DOUBLER AND STR 20 AND 22 IAW SRM 53-10-01, CORROSION REMOVED FROM WINDOW FORGING IAW SRM 56-20-01. STRINGER REPAIRED IAW QUERY NOTE 14/200 0, WINDOW INSTALLED REF MRR UPS00434381.
INSPECTION TYPE:C, CORROSION FOUND UNDER MAIN DECK WINDOW FORGING AT BS 280 TO BS 300 LT. WINDOW FORGING REMOVED IAW SRM 51-30-02. CORROSION REMOVED FROM SKIN DOUBLER IAW SRM 51-10-01. CORROSION REMOVED FROM WINDOW FORGING IAW 5-20-01. FORGING INSTALLED IAW 51-30-02. STRINGER REPAIRED IAW QUERY NOTE 17/2000, REF MRR UPS00434381.
INSPECTION TYPE:C, RIGHT WING L/E CRACK ON L/E RIB BOLT HOLE AT OLES 1206.05. REPAIR CARRIED OUT IAW QUERY NOTE 61/2000.
INSPECTION TYPE:C, CORROSION FOUND ON UPPER DECK SEAT TRACK AT BS 544 LBL 48. NEW SECTION OF SEAT TRACK FITTED IAW SRM 51-30-02.
INSPECTION TYPE:C, RIGHT WING L/E CRACK ON L/E RIB BOLT HOLE AT OLES 1277.15. REPAIR CARRIED OUT IAW QUERY NOTE 61/2000.
INSPECTION TYPE:C, RIGHT WING L/E CRACK ON L/E RIB BOLT HOLE AT OLES 1318.65. REPAIR CARRIED OUT IAW QUERY NOTE 61/2000.
INSPECTION TYPE:C, RIGHT WING L/E CRACK ON L/E RIB BOLT HOLE AT OLES 1482.85. REPAIR CARRIED OUT IAW QUERY NOTE 61/2000.
INSPECTION TYPE:C, RIGHT WING L/E RIVETS LOOSE IN TORQUE TUBE O/B OF NR 1 L/E PDU RIGHT. L/E PDU RIGHT REMOVED MM 27-81-03. SERVICABLE TORQUE TUBE FITTED IAW MM 27-81-05. L/E PDU NR 1 RIGHT REFITTED IAW MM 27-81-03. FLAP GROUP RIGGED IAW MM 27-81-00.
INSPECTION TYPE:C, RT WING L/E CRACK ON L/E RIB BOLT HOLE AT OLES 1246.35. REPAIR CARRIED OUT IAW Q/NOTE 61/00.
INSPECTION TYPE:C, UPPER DECK SECTION OF FLOORBEAM CORRODED AT BS 420 RBL 6, 12 AND 45. SECTION OF FLOORBEAM CHORD REPLACED IAW SRM 51-30-02.
INSPECTION TYPE:C, CORROSION ON DOUBLER AT LT BS 1241 CANTED DECK BULKHEAD. REPAIR CARRIED OUT IAW Q/NOTE 60/00. NEW DOUBLER FABRICATED AND FITTED. MODIFICATION ACCOMPLISHED PER SB 53-2329 R2.
INSPECTION TYPE:C, FUSELAGE SKIN CRACKED JUST FWD OF LAV SERVICE DOOR, INTERIM EXTERNAL DOUBLER FITTED. ACCOMPLISH PERMANENT REPAIR THIS VISIT PER EO B747-5 330-12953A. PERMANENT REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 1.
INSPECTION TYPE:N/A, SMOKE ODOR IN FLIGHT DECK. DEACTIVATED L3 WINDOW CAPPING WINDOW THERMOSTAT WIRES PER MEL 30-11-3. INSTALLED PLACARD WINDOW HEAT THERMOSTAT INOP.
INSPECTION TYPE:N/A, PILOT REPORTED A ELETRICAL SMELL IN CABIN SUSPECTS THE COFFEE HOT CUP. *S/D* REMOVED AND REPLACED HOT CUP TIMER PER MM 25-30-00, OPS CHECKS GOOD.
INSPECTION TYPE:N/A, MAIN CARGO DECK EMERGENCY LIGHT IN CEILING AFT OF STAIRS INOP. REMOVED AND REPLACED LIGHT ON MAIN CARGO DECK AFT OF STAIRS PER B747 MM 33-51-07.
INSPECTION TYPE:N/A, UPPER DECK FWD COURIER SEAT EMERGENCY LIGHT DIM. REMOVED AND REPLACED UPPER DECK FWD COURIER EMERGENCY LIGHT ASSEMBLY PER 33-51-07.
PILOTS REPORT- NR 3 HYD QTY DROPPED TO APPROX 1.1 GAL 3 HOURS INTO FLIGHT FOUND HYD PRESS LINE IN PYLON CRACKED. REMOVED AND REPLACED NR 3 PYLON HYDRAULIC LINE, LEAK CHECKS OK PLACARD REMOVED.
INSPECTION TYPE:N/A, FLIGHT DECK EMERGENCY EVAC SLIDE INOP. GAS GENERATOR DEPLETED. INSTALLED NEW GAS GENERATOR. PLACARD REMOVED.
UPPER DECK AFT RT EMERGENCY LIGHT VERY DIM. REMOVED AND REPLACED LIGHT ASSY,
UPPER DECK AFT RT EMERG LIGHT VERY DIM. REMOVED AND REPLACED LIGHT ASSY, AISLE. OPS NORMAL.
FIRE WARNING BELL WOULD NOT RESET. RESEATED A2 FIREWARNING CARD.
INSPECTION TYPE:N/A, EMERGENCY LIGHT OVER EVALUATION SLIDE INOP. REMOVED AND REPLACED BATTERY ASSY, OPS CHECK GOOD.
NR 3 ENGINE COWL DAMAGED ON INBOARD SIDE PUNCTURED. PERFORMED TEMP REPAIR PER EO AND DEFERRED INCIDENT RS99-409 DEFFERAL D182831.
INSPECTION TYPE-N/A, CREW OXYGEN DROPPED FROM 1200 PSI AT PREFLIGHT TO 500 PSI AT TOP OF CLIMB. REMOVED AND REPLACED LOWER AND UPPER 02 BOTTLES, LEAK CHECKED GOOD. AIR TURNBACK.
INSPECTION TYPE-N/A, BLOCK TURNBACK DUE TO BURNING ODOR IN COCKPIT. FOUND A16 CARD IN MASTER DIM AND TEST ELECTRONIC CARD FILE FAULTED CAUSING ODOR IN FLIGHT COMPARTMENT.
INSPECTION TYPE-N/A, ALL 3 EMERGENCY WALNUT LIGHTS UNDER PANEL CENTER LEFT RIGHT INOP. REPAIRED BAD WIRE ON CENTER EMERG/FLOOD LIGHT ASSY, OPS CHECK GOOD PER W/D 33-13-11.
INSPECTION TYPE-N/A, EMERGENCY CEILING LIGHT MAIN DECK STA 300 INOP. REPLACED BATTERY PACK IN EMERGENCY LIGHT ASSY AT STA 350 RT, OPERATION CHECKS GOOD.
INSPECTION TYPE-A CHECK, EMERGENCY LIGHT ON MAIN DECK FAILED. REMOVED AND REPLACED BATTERY ASSY, OPS CHECKS OK.
FIRE WARNING INDICATION AND BELL, INTERMITTENT, SUSPECTED FROM LWR CARGO BUT CANNOT ISOLATE DUE TO RAPID ONSET AIR DIVERT TO MSP. REMOVED AND REPLACED FIRE WARNING CIRCUIT CARD A8 ON M825 PER MM 26-10-01 AND TESTED PER MM 26-16-00. GRD CHECKS NORMAL. PN ON OFF - 69B47519-3, NSN ON/OFF. PLEASE NOTE L/P 011538 ITEM 2 AND 3.
INSPECTION TYPE-N/A, R-4 ENTRY DOOR LOWER FWD CORNER SEPARATED FROM A/C. REMOVED AND REPLACED R4 ENTRY DOOR IAW MM 52-11-01.
INSPECTION TYPE-N/A, WHILE AT CRUISE ALT FL 350 FLT EXPERENCED MASTER WARNING CARGO FIRE AT ZONE NR 4. SILENCED BELL TO RESET SYSTEM AND RUN CHECK LIST. A/C HAD VARIOUS HAZ MATS IN POSITION NR 14L CLOSE ENOUGH TO NR 4 TO DECLARE EMERGENCY LANDING INTO CYWC ON FINAL INTO CYWC THE CARGO AND ZONE NR 4 WENT OUT, ONCE ON GROUND EMERG CREWS FOUND NO SMOKE OR FIRE. NO ACTION TAKEN AT THIS REPORT TIME.
INSPECTION TYPE-N/A, COCKPIT CEILING ESCAPE HATCH OUTSIDE LATCH WILL NOT STAY STOWED, BY OPERATING INTERIOR LATCH OUTSIDE HANDLE POPS UP. REF MM 52-21-00, CLEANED AND LUBED EXIT HATCH HANDLE AND INTERIOR MECHANISM, REMOVED BUFF FROM HANDLE GUIDE. OPERATED DOOR SEVERAL TIMES, NO DEFECTS NOTED.
INSPECTION TYPE:C, RT WING, WING GEAR WALKING BEAM FWD BEARING HOUSING SUPPORT FITTING UPPER OUTBD ATTACHMENT HOLE HAS 1 CRACK APPROX 1 INCH. REPLACED FITTING ACC KLM DFX 97-257 REV 3 APPROVED PER UPS EFN 747-57-0399.
INSPECTION TYPE:C LT WING WLG WALKING BEAM FWD BEARING HOUSING SUPPORT FITTING, OUTBD UPPER ATTACHMENT HOLE HAS 3 CRACKS, INBD LOWER HOLE HAS 1 CRACK WS (530). REPLACED FITTING ACC KLM DFX 97-257 REV 3 APPROVED PER UPS EFN 747-57-399.
INSPECTION TYPE-C, CORROSION FOUND ON LOWER EDGE OF AFT CARGO DOOR. SECTIONS OF INTERNAL SKIN REPLACED AND EXTERNAL DOUBLERS INSTALLED ACC SRM 53-30-03 FIG 1A FWD DOUBLER 66 X 17 X 0.160 AFT DOUBLER 27 X 16 X 0.160.
INSPECTION TYPE-N/A, FUSELAGE SKIN CRACKED AND PILLOWING IN TWO PLACES INBD OF RT OUTFLOW VALVE. REMOVED DAMAGE AS REQUIRED. FABRICATED DOUBLER ACCOMPLISHED. REPAIR PER SRM 53-30-02.
INSPECTION TYPE-N/A, UPPER DECK EMERGENCY SLIDE LT LIGHT INOP REQ A 381806 EMERGENCY BATT NOT STOCKED (P/N 60-1612-3), MUST ORDER NUMBER AS SHOWN NO ALT. REMOVED AND REPLACED UPPER DECK EMER SLIDE BATTERY PACK.
INSPECTION TYPE-N/A, UPPER DECK EMERGENCY DOOR SILL LIGHT INOP. RELAMPED AND CKS UPPER DECK EMERGENCY LIGHT NORMAL.
INSPECTION TYPE-N/A, RT I/B FLAP, MID FLAP O/B TRAILING EDGE SUPPORT AFT MOUNT AREA DELAMINATED AND CRACKED. REPAIRED TRAILING EDGE SUPPORT MT PER SRM 51-40-15.
INSPECTION TYPE-N/A, DURING CRUISE THE AFT CARGO FIRE LOWER LIGHT CAME ON INTERMITTENTLY FOR ABOUT A 5 MIN PERIOD OF TIME IT DID NOT COME ON AGAIN UNTIL OUR DESCENT INTO KIX AND WAS INTERMITTENT AGAIN. *S/D* REPLACED 4 SMOKE DETECTORS, OPS GOOD M128482 CLEARED PLACARD. REMOVED (P/N 2156-80) (S/N OFF 108) (S/N ON 112) (S/N OFF 114) (S/N ON 154) (S/N OFF 115) (S/N ON 117).
NR 4 ENG NACELLE TEMP GAUGE, IN TURBULANCE A LOOP TEMP INDICATOR MOVED FROM 0 TO 2 CAUSING FIRE DETECTION LIGHT ON PILOTS PANEL TO FLICKER ON/OFF. REMOVED AND REPLACED NR 4 ENG UPPER AFT SENSING ELEMENT PER MM 26-11-02. OPS CHECKED NORMAL PER 26-11-00 S/N ON 0195 SN OFF 0978 PN ON 472923, THIS CLEARS ITEM M 127189.
INSPECTION TYPE-N/A, AT CRUISE ALTITUDE FL330 NR 4 A-LOOP FIRE DETECTOR FAULT LIGHT ILLUMINATED. FIRE DETECTOR NACELLE TEMP INDICATOR WAS FLUXUATING FROM 0 TO FULL SCALE SELECTED B-LOOP AND FOLLOWED AOM PROCEDURE. RE-RACK ENGINE NR 4 A-LOOP CARDS, OPS CHECK NORMAL.
INSPECTION TYPE: C. FOUND CORROSION ON WEB PLATE AT BS 460 BETWEEN RBL 80 AT WL 308. REMOVED CORROSION ON WEB PLATE AT BS 460 BETWEEN RBL 42/80 ACC SRM 5 1-10-01. CORROSION NOT IN LIMITS ACC SRM 53-10-01. REPLACED WEB PLATE ACC SRM 51-30-02.
INSPECTION TYPE: C. RT BLG WHEELWELL - LOWER SKIN CORNER OF PRESSURE DECK, STA 1373 OUTBOARD SIDE OF WHEELWELL IS BROKEN OFF AND THERE ARE SIGNS OF CORROSION AT THAT SKIN. REMOVED CORROSION IAW SRM 51-10-01. CORROSION OUT OF LIMITS IAW SRM 51-10- 01. REPAIRED IAW SRM 53-10-01 PER DRAWING KLM DFX96-176, EFN 747-53-0787.
INSPECTION TYPE: C. MAIN DECK BS 400 BULKHEAD WEB CRACKED JUST BELOW LT STR 26, BS 400 LT BULKHEAD WEB CRACK REPAIRED IAW SRM 53-10-04, FIG 78.
INSPECTION TYPE CPCP, MAIN DECK FLOOR, STRUCTURE FITTING AT BS 2060 RBL 65 IS CRACKED, LENGTH OF CRACK IS 1.5 INCH. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING IAW SRM 51-30-02.
INSPECTION TYPE: C. SKATE ANGLE PYLON NR 1 RT HAS CRACKS AT THE TWO FIRST FASTENER HOLES. REPAIRED IAW KLM DFX 96-180 / EFN 747-54-0132.
INSPECTION TYPE: C. PYLON NR 3, FOUND VERTICAL FIRE WALL AT NAC STA 180 CRACKED AT LT TOP CORNER (CRACK IS 1.5 INCHES LONG). REPLACED FIRE WALL IAW SRM 51-30-02.
INSPECTION TYPE CPCP, MAIN DECK FLOOR STRUCTURE CORROSION AT FLOOR PANEL FASTENER HOLES IN FLOOR BEAM UPPER CHORD AT STA 2040 RBL 75 TO 98.58. REMOVED CORROSION UPPER CHORD BS 2040 BETWEEN RBL 75 TO 108 IAW SRM 51-10-01. UPPER CHORD OUT OF LIMITS IAW SRM 53-10-01. REPAIRED UPPER CHORD IAW SRM 53-10-07.
INSPECTION TYPE: C. MAIN DECK FLOOR STRUCTURE, FITTING AT STA 1960 RBL 57 IS CRACKED. LENGTH OF CRACK IS 1.5 INCHES. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING AT BS 1960 RBL 57 IAW SRM 51-30-02.
INSPECTION TYPE-C, RT WING FRONT SPAR WEB FOUND TWO CRACKS OUTSIDE OF SB747-57A2266. INSPECTION AREA REF NRC 710789, THE FIFTH HOLE 2MM, SEVENTH HOLE .5MM. REPAIRED TWO CRACKS ACC KLM DFX 96-0165 ISSUE 4 APPR ACC TO FAA FORM 2110-3 AND UPS EO B747-5720-8543-A.
INSPECTION TYPE-C, FOUND SIGNS OF TAIL STRIKE BETWEEN BS 2450 TO 2580 LOTS OF DEEP SCRATCHES AND DENTS. REPAIRED FUSELAGE IAW SRM 53-30-03.
INSPECTION TYPE: C. FOUND SEVERAL SPOTS OF CORROSION ON PRESS MAIN DECK AT RBL 57 BETWEEN STA 1625/1480. CORROSIVE SPOTS ARE OUT OF LIMITS. REPAIRED PRESS MAIN DECK AT RBL 57 BETWEEN BS 1265/1480 IAW SRM 53-10-07 FIG 2.
INSPECTION TYPE CPCP, MAIN DECK FLOOR BEAM UPPER CHORD CORRODED AT BS 1000 BETWEEN RBL 70 TO 100. REMOVED CORROSION IAW SRM 51-10-01, UPPER CHORD OUT OF LIMITS IAW SRM 53-10-01. REPAIRED UPPER CHORD AT BS 1000 FROM RBL 70 TO RBL 108 IAW SRM 53-10-07.
INSPECTION TYPE-C, RT WING FRONT SPAR FOUND DURING NDO INSPECTION OF SB 747-57A2266 CRACK IN FRONT SPAR WEB AT STIFFENER FS 655.75 FOURTH HOLE FROM UPPER SIDE 4MM. AFTER INSP ALSO FOUND CRACKS AT FIFTH AND SEVENTH HOLE 2MM, .05MM. REPAIRED FOURTH HOLE FROM UPPER SIDE ACC KLM DFX 96-165 ISSUE 4 APPR ACC TO FAA FORM 0110-3 AND UPS EO B747-5720-8543-A.
INSPECTION TYPE: C. FOUND ON PRESS MAIN DECK AT LBL 75 BETWEEN STA 1306 AND STA 1380, SEVERAL SPOTS CORRODED OUT OF LIMITS. REPAIRED PRESS MAIN DECK AT LBL 75 BETWEEN STA 1306 AND STA 1380 IAW SRM 53-10-07 FIG 2.
INSPECTION TYPE: C. MAIN DECK FLOORBEAM: FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 1580 RBL 69/88. CORROSION REMOVED ON UPPER CHORD BS 1580 RBL 69/88 IAW SRM 51-10-01. UPPER CHORD OUT OF LIMITS IAW SRM 53-10-01, REPAIRED UPPER CHORD BETWEEN RBL 69/88 IAW SRM 53-10-07.
INSPECTION TYPE: C. PRESS MAIN DECK FOUND CRACKED IN SKIN AT RBL 33 BETWEEN BS 1310 AND BS 1350. REPAIRED PRESS MAIN DECK AT RBL 33 BS 1310/1350 IAW SRM 53-10-07 FIG 2.
INSPECTION TYPE: C. FOUND AT MAIN PRESS DECK AT BS 1360 AT RBL 33 , CRACK. REPAIRED PRESS MAIN DECK AT 1360 AT RBL 33 IAW SRM 53-10-07 FIG 2.
INSPECTION TYPE: C. FOUND AT PRESS MAIN DECK WEB, CRACK AT RBL 33 AT BS 1270. REPAIRED PRESS MAIN DECK WEB AT BS 1270 AT RBL 33 IAW SRM 53-10-07 FIG 2.
INSPECTION TYPE: C. AT PRESS MAIN DECK AT BS 1265/1300 AT RBL 75, SEVERAL SPOTS CORROSION OUT OF LIMITS. REPAIRED PRESS MAIN DECK AT BS 1265 TO BS 1300 AT RBL 75 IAW SRM 53-1 0-07 FIG 2 AND IAW UPS EFN 747-53-0780.
INSPECTION TYPE: C. CRACK FOUND ON PRESS MAIN DECK AT BS 1370 AT RBL 75 . REPAIRED PRESS MAIN DECK WEB AT RBL 75 AT BS 1370 IAW SSRM 53-10-07 FIG 2.
INSPECTION TYPE: C. PYLON NR 1, WEAR DAMAGE IN PYLON LEADING EDGE SKIN LT NAC STA 211/216 AND WEAR DAAMAGE IN PYLON SKIN LT TOP SIDE NAC 220/225. REPAIRED LEADING EDGE SKIN IAW UPS EFN 747-54-0129, KLM 96-160. REPAIRED PYLON SKIN LT TOP SIDE IAW SRM 51-30-03, FIG 17A.
INSPECTION TYPE: CPCP. MAIN DECK FLOORBEAM UPPER CHORD CORRODED AT BS 860 BETWEEN RBL 65/110. CORROSION REMOVED IAW SRM 51-10-01. OUT OF LIMITS PER SRM 53-10-01. UPPER CHORD AT BS 860 RBL 65 TO RBL 110 REPAIRED IAW SRM 53-10-07.
INSPECTION TYPE: C. CRACK IN PYLON SKIN AT ACCESS PANEL CUTOUT LT NAC STA 208. REPAIRED SKIN IAW SRM 54-30-03, FIG 17B.
INSPECTION TYPE-C, PYLON NR 4 FOUND FRAME CRACKED AT NAC STA 160 LT. REPLACED RIB AND DOUBLER IAW SRM 51-30-02.
INSPECTION TYPE-C, BECAUSE OF OLD NOT ACCORDING SRM REPAIR, MOD DOUBLER MUST BE REPLACED BY NEW ENLARGED DOUBLER AT MED LT LOWER AFT CORNER. REPLACED DOUBLER IAW KLM DFX 96-155 ISSUE 4.
INSPECTION TYPE: C. FOUND LT SKIRT ANGLE CRACKED APPROXIMATELY 6 INCHES AFT OF LAST TRAILING EDGE DOOR HINGE. ALSO, 2 INCHES FORWARD ATTACHMENT HOLES WORN OUT. REPAIRED SKATE ANGLE IAW TO KLM DFX 96-171 ISSUE NR 3 AND IAW EFN 747-54-0131.
INSPECTION TYPE: C. MAIN DECK FLOOR BEAM UPPER CHORD CORRODED AT BS 680 BETWEEN 11 RT/LT. CORROSION REMOVED ON UPPER CHORD AT BS 680 BETWEEN 11 RT/LT. UPPER CHORD OUT OF LIMITS IAW SRM 53-10-01. REPAIRED UPPER CHORD AT BS 680 BETWEEN 11 RT/LT IAW SRM 51-40-04, FIG 1.
INSPECTION TYPE: C. PYLON NR 3, FOUND LT FORWARD FRAME OF BULKHEAD NAC STA 222 CRACKED AT TOP SIDE (CRACKS 2X RUNNING FROM AFT TOP FASTENER TO FRAME EDGE). PERFORMED REPAIR IAW KLM DFX 96-153 ISSUE NR 2 UPS EFN NR 747-54-0128.
INSPECTION TYPE: C. APU BATTERY ACCESS DOOR SKIN CRACKED AND DEFORMED. REWORKED SKIN PLATE OF APU ACCESS DOOR IAW SRM 51-10-01. SKIN PLATE AND FRAMES ARE NOT IN LIMITS IAW SRM 52-00-02. REPLACED APU ACCESS DOOR ACC SRM 51-30-02.
INSPECTION TYPE-C, RT WING LOWER CHORD CRACKED AT RT ILES 1117.00 INSIDE L/E AREA. REMOVED BROKEN OFF PIECE AND TRIMMED CHORD. REPAIR ANGLE PLACED, APPROVED UPS AMS 96-0172RE.
INSPECTION TYPE-C, RT WING T/E, FOUND FIBERGLASS PANEL BULGED AT WS 410. REMOVED AND INSTALLED PANEL IAW 51-30-02, BLEND OUT CORROSION AND INSPECT THE REWORKED AREA, SHOTPEEN, ALODINE AND REFINISH THE AREA, EDDY CURRENT FASTENER HOLES REPLACED FASTENERS, UPS AMS 96-0181.
INSPECTION TYPE N/A, LOWER CARGO FIRE WARNING CAME ON 4 TO 5 TIMES ON DESCENT.
INSPECTION TYPE-C, MAIN DECK FLOOR BEAM UPPER CHORD CORRODED AT BS 640 BETWEEN RBL 33, 98 UPPER CHORD AT BS 640 BETWEEN RBL 33, 98. REPLACED IAW SRM 53-10-07 FIG 12 AND UPS EFN 747-53-0778, KLM DFX 96-150.
MAINTENANCE REPORTED, CABIN DOOR EMERGENCY LIGHT INOP. CLEANED CONTACTS, OPS CHECK OK.
CREW REPORTED WHILE CRUISING AT 35,000 FEET BETWEEN EWR AND SDF, HAD A MAIN CARGO DECK FIRE WARNING. COULD NOT DETECT ANY FIRE OR SMOKE VISUALLY, UPS EMERGENCY PROCEDURES WERE USED. MADE EMERGENCY DESCENT INTO PIT. FIRE TRUCKS MET THE AIRCRAFT. FIRE TEAM CAME ON BOARD, NO FIRE WAS FOUND. DEFERRED DETECTOR, RETURNED TO SDF.
MAINTENANCE REPORTED, UD RT EMERGENCY LT OUT. INSTALLED SERVICABLE EMERGENCY LIGHT ASSEMBLY IN UPPER DECK MM 33-50, (P/N 51356B37), OFF (S/N 291-1571), ON (S/N 104-029).
WHILE ON GROUND, MAINTENANCE FOUND RIGHT INBOARD MIDFLAP RIGHT HAND TRAILING EDGE CORNER HAS CRACK. ACCOMPLISHED COMPOSITE REPAIR REF SRM 51-40-09.
SUPPLEMENTAL MRR - PILOT REPORTED, ENGINE MAIN DECK CARGO FIRE AND SMOKE LIGHT NR 3 ILLUMINATED, WHILE AT FL 390. INITIATED UPS EMER PROCEDURE. WITH PACKS OFF AND A/C COMPLETELY PRESSURIZED AND PASSING THROUGH 10,000 FT, LIGHT EXTINGUISHED. NO SMOKE OR FIRE WAS EVER VISIBLE TO CREW. REPLACED BOTH 3A AND 3B SMOKE DETECTORS. ALSO, REPLACED AMPLIFIER AS PRECAUTIONARY, OPS CK GOOD PER MM 26-14-00.
WHILE ON GROUND, MAINTENANCE FOUND 1 EMER LIGHT BURNED OUT, AFT O/H ABOVE FLT RECORDER. RELAMPED AS REQ'D, OPS CK GOOD.
WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND FORWARD LOWER CARGO COMPARTMENT CRACK IN UPPER CHORD STA 720 RBL 1. REPAIRED IAW E.O. 747-53-0717.
WHILE IN AMSTERDAM FOR C-CHECK MAINTENANCE, FOUND CORROSION ON STRING 45 AT STA 2160, 30 RBL. REPAIRED IAW SRM 51-10-07, 53-10-07, 53-10-03.
WHILE IN AMSTERDAM FOR C-CHECK MAINTENANCE, FOUND RT WING UPPER T-CHORD CRACKED ON FWD SIDE WS 440. REPAIRED IAW EO 747-57-0257.
WHILE IN AMSTERDAM FOR C-CHECK MAINTENANCE, FOUND CORROSION ON SEAT TRACK STA 510, RBL 58. REPLACED TRACK IAW SRM 53-10-5.
WHILE IN AMSTERDAM FOR C-CHECK MAINTENANCE, FOUND CRACK IN FRAME AT STA 360 LT BETWEEN STR 25 AND 26. REPAIRED IAW 747-53-0066.