N17773

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

FUSELAGE SKIN AT BS 720D-740 BETWEEN S25-27 RT MISREPAIRED. REPAIRED ON FASI WO 21180, NR 104209.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 67,453 hrs · 44,951 cycles

FUSELAGE SKIN MISREPAIRED AT BS 418 BETWEEN S15-18R. REPAIRED ON FASI WO 21180, NR 104095.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

SKIN AT BS 720C+16.5 - 720D+7.5 BETWEEN STR 27R-28R MISREPAIRED. REPAIRED ON FASI WO 21180, NR 104230.

Part: SKIN — CORRODED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

SKIN BS 676 BETWEEN S21-22R CORRODED AROUND EDGES OF REPAIR. REPAIRED ON FASI WO 21180, NR 104160.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

FUSELAGE SKIN MISREPAIRED AT BS 332 S19R LAPJOINT. REPAIRED ON FASI WO 21180, NR104091.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

FUSELAGE SKIN MISREPAIRED AT BS 412.5 S19R LAPJOINT. REPAIRED ON FASI WO 21180, NR104092.

Part: SKIN — CORRODED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

BS 419 - 533 S19R LAP JOINT CORRODED. REPAIRED ON FASI WO 21180, NR 104151.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

FUSELAGE SKIN AT BS 356 S23R MISREPAIRED. REPAIRED ON FASI WO 21180, NR 104108.

Part: SKIN — DENTED (ZONE 200) · airframe 67,453 hrs · 44,951 cycles

SKIN BS 690 ABOVE S4R DENTED. REPAIRED ON FASI WO 21180, NR 104195.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

FUSELAGE SKIN AT BS 990, C-2 DOOR CUTOUT AFT EDGE MISREPAIRED. REPAIRED ON FASI WO 21180, NR 104099.

Part: SKIN — DAMAGED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

UPON REMOVAL OF EXTERNAL DOUBLER AT BS 665 S21R FOUND DAMAGED. REPAIRED ON FASI WO 21180, NR 104205.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 67,453 hrs · 44,951 cycles

FUSELAGE SKIN, STA 254.5 BETWEEN S9-11L MISREPAIRED. REPAIRED ON FASI WO 21180, NR 104097.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 67,453 hrs · 44,951 cycles

BS 375 S12R, LOWER INTERCOSTAL CRACKED. REPAIRED ON FASI WO 21180, NR 104200.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 67,453 hrs · 44,951 cycles

BS 375 S12R, UPPER INTERCOSTAL CRACKED. REPAIRED ON FASI WO 21180, NR 104199.

Part: SKIN — BULGED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

S-19R, STA 694 SKIN HAS A BULGE (POSSIBLE CORROSION). REPAIRED ON FASI WO 21180, NR 104148.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

FUSELAGE SKIN, BS 431 BETWEEN S21-23L MISREPAIRED. REPAIRED ON FASI WO 21180, NR 104143.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 67,453 hrs · 44,951 cycles

FUSELAGE SKIN STA 395.5 AT S22R MISREPAIRED. REPAIRED ON FASI WO 104115, NR 104115.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SURFACE COROSSION ON CHORD AT STA.1183 LEFT SIDE. REPAIRED ON NR# 8745 FASI W/O# 20172.

Part: PAN — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

LEFT AFT FLOOR PAN CORRODED STA 1183-1146. REPAIRED ON NR 8792 FASI W/O 20172.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK CORRODED STA 1070-1030 RBL 45. REPAIRED ON NR 8712 FASI W/O 20172.

Part: FRAME — CRACKED (ZONE 200) · airframe 67,248 hrs · 44,827 cycles

FRAME CRACKED AT STA 312 BETWEEN S13-14R. REPAIRED ON NR 8911 FASI W/O 20172.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK PITTING STA. 880-910 RBL 24. REPAIRED ON NR 8724 FASI W/O 20172.

Part: FRAME — CRACKED (ZONE 200) · airframe 67,248 hrs · 44,827 cycles

FRAME CRACKED AT STA 328 BETWEEN S13-14R. REPAIRED ON NR 8912 W/O 20172.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK 2 HOLES DRILLED IN TRACK STA 1120 LBL 24. REPAIRED ON NR 8790 FASI W/O 20172.

Part: SEAT TRACK — DAMAGED (BS 1110) · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK 2 HOLES DRILLED IN TRACK STA 1110 LBL 45. REPAIRED ON NR 8791 FASI W/O 20172.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK PITTING STA. 990 RBL24. REPAIRED ON NR 8716 FASI W/O 20172.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK PITTING STA 876 LBL 24. REPAIRED ON NR 8769 FASI W/O 20172.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 67,248 hrs · 44,827 cycles

STA 360 FLOORBEAM FASTENER HOLE ELONGATED RBL.55. REPAIRED ON NR 8861 FASI W/O 20172.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK CORRODED STA. 360 RBL.55. REPAIRED ON NR 8708 FASI W/O 20172.

Part: SKIN — DELAMINATED (NR 9 SPOILER) · airframe 67,248 hrs · 44,827 cycles

RIGHT WING NR 9 SPOILER UPPER SURFACE DELAMINATED. REPAIRED ON NR 8312 FASI W/O 20172.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK PITTING STA. 480-460 RBL.24. REPAIRED ON NR 8741 FASI W/O 20172.

Part: SEAT TRACK — CORRODED (BS 540-580) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK PITTING STA. 540-580 RBL.45. REPAIRED ON NR 8739 FASI W/O 20172.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK PITTING STA. 970 LBL.45. REPAIRED ON NR 8786 FASI W/O 20172.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK STA. 360 RBL 20 CORRODED. REPAIRED ON NR 8707 FASI W/O 20172.

Part: SEAT TRACK — DAMAGED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK STA. 720-740 LBL24 DAMAGED. REPAIRED ON NR 8764 FASI W/O 20172

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK PITTING STA. 1030-1110 LBL.24. REPAIRED ON NR 8788 FSAI W/O 20172

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK PITTING STA. 760-848 LBL.24. REPAIRED ON NR 8768 W/O 20172.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

MAIN CABIN FLOORBEAM AT STA 1130 LBL 24 IS CORRODED. REPAIRED ON NR 8871 W/O 20172

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,248 hrs · 44,827 cycles

SEAT TRACK PITTING STA. 680-700 LBL 45.

Part: BUSS TIE — OVERHEATED (NR2 GENERATOR)

FLT 421 - BED - PRIOR TO DEPARTURE FLIGHT CREW NOTED SMOKE ON FLIGHT DECK. FOUND SUSPECT EVIDENCE OF NR 2 BUS TIE BREAKER OVERHEAT WITH SUBSEQUENT DAMAGE TO ELECTRICAL SHELF. REMOVED AND REPLACED ELECTRICAL SHELF AND NR 2 BUS TIE BREAKER. NR 2 BUS TIE BREAKER, VOLTAGE REGULATOR, AND BUS PROTECTION PANEL REPLACED AS PRECAUTION DUE TO SMOKE RESIDUE FROM FAILED BUS TIE BREAKER. (M)

Part: WIRE — SHORTED (CABIN)

INSPECTION FOUND EMERGENCY PATH LIGHTS INOPERATIVE AT DOORS AND OVERWING EXITS AND AFT SECTION OF LIGHTS WAS DIM. SEVERAL WIRES WERE FOUND SHORTED. THE WIRING WAS REPAIRED IAW WIRING DIAGRAM 33-51, OPERATIONAL CHECKS WERE GOOD IAW MM 33-50.

Part: SUPPORT — CRACKED (BS 1183)

INSPECTION FOUND A 1.2 INCH CRACK IN VERTICAL SUPPORT AT STA 1183, RBL 50. THE CRACK WAS STOP DRILLED, TWO ANGLES WERE FABRICATED AND INSTALLED IAW ECRA 5310-03748.

Part: ANGLE — CRACKED (BS 1183)

INSPECTION FOUND A 1.5 INCH CRACK IN ANGLE AT STA 1183 BETWEEN STRINGER 18R AND 19R, RBL 45. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.

Part: BOTTLE PIN — CORRODED (LT WING/FUS)

INSPECTION FOUND LT FORWARD WING TO FUSELAGE BOTTLE PIN BLEEDING RUST AT SEALANT AREA. THE BOTTLE PIN WAS REMOVED AND REPLACED IAW MM 57-41-1.

Part: RIB — CRACKED (RT TE MIDFLAP)

INSPECTION FOUND A 2 INCH CRACK IN RT WING INBOARD FLAP OUTBOARD CABLE ATTACH RIB (MIDFLAP). THE MIDFLAP WAS REMOVED AND REPLACED IAW WORK CARD 07-5750-1-4703.

Part: STRINGER — CRACKED (VERT STAB)

INSPECTION FOUND A 1.5 INCH CRACK IN STRINGERS 6L, 8L, AND 9L AT VERTICAL STABILIZER NR 9 RIB. THE CRACKED AREAS WERE CUT OUT IAW SRM 55-30-04. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 55-30-04 AND 51-10-2.

Part: SHEAR TIE — CORRODED (BS 500)

INSPECTION FOUND SHEAR TIE CORRODED AT STA 500, STRINGER 28R. THE CORRODED AREA WAS CUT OUT, A SHEAR TIE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION FOUND A .375 INCH CRACK AT O/B RIB WHERE LT WING NR 4 SLAT ACTUATOR FORWARD ROD END ATTACHES INSIDE SLAT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.

Part: STRINGER — CRACKED (VERT STAB)

INSPECTION FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER NR 7 RIB LT NR 9 STRINGER. THE CRACKED AREA WAS REMOVED IAW SRM 55-30-2. A STRINGER SECTION WAS FABRICATED AND INSTALLED IAW SRM 55-30-4.

Part: SKIN — DELAMINATED (RT TE AFT FLAP)

INSPECTION FOUND RT I/B AFT FLAP DELAMINATED AT 15 INCHES O/B OF I/B END AT UPPER SURFACE. THE AFT FLAP WAS REMOVED, REPAIRED AND REINSTALLED IAW WORK CARD 07-5750-1-2802.

Part: SKIN — DELAMINATED (LT TE FOREFLAP)

INSPECTION FOUND LT I/B FOREFLAP UPPER SKIN INBOARD END DELAMINATED. THE FOREFLAP WAS REMOVED, REPAIRED AND REINSTALLED IAW WORK CARD 07-5750-1-2801.

Part: SKIN — CRACKED (BS 500)

INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 500 STRINGER 28R. THE CRACKED AREA WAS CUT OUT, STRINGER SPLICE AND SKIN DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.

Part: BULKHEAD WEB — CRACKED (BS 1183)

INSPECTION FOUND A 1.5 INCH CRACK IN PRESSURE WEB SKIN AT STA 1183 BULKHEAD, RT SIDE, WL 188. THE CRACKED AREA WAS CUT OUT, DOUBLERS WERE FABRICATED AND INSTALLED IAW EA 553A0022.

Part: SKIN — CORRODED (BS 720)

INSPECTION FOUND FUSELAGE SKIN AND STRINGER CORRODED AT STA 720, STRINGER 28L. THE CORRODED AREA OF SKIN AND STRINGER WERE CUT OUT IAW SRM 53-30-3 AND 53-10-3. SKIN AND STRINGER SECTIONS WERE FABRICATED AND INSTALLED IAW SRM 53-30.

Part: SUPPORT — CORRODED (BS 640)

INSPECTION FOUND FLOOR SUPPORT CORRODED IN FORWARD CARGO COMPARTMENT AT STA 640, STRINGER 27L. THE CORRODED AREA WAS CUT OUT, REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, FIGURE 3 AND 51-10-2.

Part: SKIN — CORRODED (BS 680)

INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 680, STRINGER 27R TO 28R. THE CORRODED AREA WAS CUT OUT, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-3.

Part: FLOORBEAM — CORRODED (BS 1110)

INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT FS 1110, RBL 30. THE CORRODED AREA WAS CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, PAGE 18 AND 19.

Part: FLOORBEAM — CORRODED (BS 344)

INSPECTION FOUND FORWARD ENTRANCE WAY FLOORBEAM CORRODED AT STA 344, LBL 29 TO 60. THE CORRODED AREA WAS CUT OUT, A T-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.

Part: SEAT TRACK — CORRODED (BS 344,1025)

INSPECTION FOUND RT SEAT TRACK CORRODED AT STA 1025, RBL 54 AND LT SEAT TRACK WAS CORRODED BETWEEN STA 344 AND 360, LBL 44.

Part: STRINGER — CRACKED (BS 720)

INSPECTION FOUND A 1.5 INCH CRACK IN STRINGER 15L AT STA 720B. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-32. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-6, AND 53-10-3.

Part: SEAT TRACK — CORRODED (BS 380-1135)

INSPECTION FOUND SEAT TRACKS CORRODED AT STA 1110 TO 1135, RBL 24 AND AT STA 380 TO 420, RBL 27. THE CORRODED SEAT TRACKS WERE REMOVED AND NEW SECTIONS OF SEAT TRACK WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, 51-10-2, AND 51-40-5.

Part: BEAM — CRACKED (LT WING)

INSPECTION FOUND A .25 INCH CRACK IN LT WING TRAILING EDGE FLAP CORE AREA J BEAM JUST FORWARD OF NR 7 SPOILER CASTING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5750-02914, 51-10-2, AND 51-30-2.

Part: SUPPORT — CRACKED (BS 848-1130)

INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM SUPPORT BRACE AT STA 848, BL 0 AND A 2 INCH CRACK WAS FOUND IN SUPPORT BRACE AT STA 1110 TO 1130, LBL 36. THE SUPPORTS WERE REMOVED IAW SRM 51-10-1. NEW SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-6, AND 51-40-5.

Part: BRACE — CORRODED (BS 1070-1130)

INSPECTION FOUND FLOORBEAM SUPPORT BRACE AT STA 1070 TO 1110, RBL 64 AND AT STA 1130, RBL 16 CORRODED. THE SUPPORT BRACES WERE REMOVED IAW SRM 51-30-21. NEW SUPPORT BRACES WERE FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-30-2, 51-10-1, AND 51-10-6.

Part: PANEL — CRACKED (NLG WW)

INSPECTION FOUND A 1 INCH CRACK IN TOP RT NOSE WHEEL WELL PANEL. THE CRACKED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.

Part: STRAP — CRACKED (LT WING)

INSPECTION FOUND A 9/16 CRACK IN STRAP AT LT WING LOWER TRAILING EDGE AT OUTBOARD SIDE OF NR 3 FLAP TRACK MOUNT PAD AFT OF FALSE SPAR AREA. THE CRACKED AREA WAS REMOVED IAW SRM 51-10-1. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-40-4.

Part: PANEL — CRACKED (BS 290)

INSPECTION FOUND A .5 CRACK AT FASTENER HOLE OF NLG WHEEL WELL TOP CENTER PANEL, STA 290, LBL 2. THE CRACKED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.

Part: BRACES — CRACKED (BS 720-990)

INSPECTION FOUND FLOORBEAM SUPPORT BRACES CRACKED BETWEEN STA 950A-950B, BL 0, STA 970-990, BL 0, AND STA 720-720A, BL 0. THE CRACKS WERE 1-2.5 LONG. NEW SUPPORT BRACES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-40-4, AND 51-30-2.

Part: FITTING — CRACKED (BS 940)

INSPECTION FOUND A 2.5 INCH CRACK IN FITTING AT STA 940, STRINGER 18A. A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: FUEL NOZZLE — STREAKING (NR 1 ENGINE)

THE NR 1 ENGINE POPPED AND EGT WENT TO 600 DEGREES WHILE CLIMBING THROUGH 18000 FEET AFTER TAKEOFF FROM IAH. THE ENGINE VIBRATED AND WAS SHUTDOWN. THE N2 DROPPED TO 70 PERCENT BEFORE THROTTLE WAS PULLED TO IDLE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE PRIMARY CAUSE OF FAILURE WAS DUE TO TWO STREAKING FUEL NOZZLES WHICH CAUSED FIRST STAGE NGV'S TO HAVE COMPLETE BURN THROUGH, RESULTING IN FAILURE OF ONE HPT BLADE AND SUBSEQUENT DOWNSTREAM DAMAGE TO LPT.

Part: STRINGER — CRACKED (BS 720)

INSPECTION FOUND TWO 1 INCH CRACKS IN STRINGER 26L AT STA 720E TO 720F. THE CRACKED SECTION OF STRINGER WAS CUT OUT. A NEW STRINGER SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3.

Part: FRAME — CRACKED (BS 480)

INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO COMPARTMENT CIRCUMFERENTIAL FRAME AT BS 480 BETWEEN STRINGER 25R AND 26R. A FRAME SPLICE WAS INSTALLED AND FLOOR SUPPORT SPLICE WERE INSTALLED IAW SRM 53-10-4 AND 51-30-2.

Part: FITTING — CRACKED (LT MLG)

INSPECTION FOUND A .75 INCH CRACK IN LT MLG UPLOCK SUPPORT FITTING. A NEW FITTING WAS INSTALLED IAW SRM 51-10-1.

Part: SUPPORT — CORRODED (BS 340)

INSPECTION FOUND FORWARD LAV FLOOR SUPPORT CORRODED AT STA 340, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-1.

Part: STRINGER — CRACKED (WS 629)

INSPECTION FOUND A .75 INCH CRACK IN RT WING UPPER STRINGER AT WS 629.0 CUTOUT NR 7616. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5762-01050.

Part: SUPPORT — CORRODED (BS 420)

INSPECTION FOUND MAIN CABIN FLOOR PANEL SUPPORT CORRODED AT STA 420, RBL 10 TO 62. THE FLOOR SUPPORT WAS REMOVED, A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.

Part: STRINGER — CRACKED (WS 656.5)

INSPECTION FOUND A .75 INCH CRACK IN LT WING UPPER STRINGER WHERE IT ATTACHES TO RIB AT WS 656.50 TANK CUTOUT NR 7217. THE CRACKED SECTION WAS REMOVE, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2.

Part: STRINGER — CRACKED (WS 686.5)

INSPECTION FOUND A .75 INCH CRACK IN RT WING UPPER STRINGER AT CUTOUT NR 7618, WS 686.5. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW EA 5762-01050.

Part: FLOORBEAM — CORRODED (BS 400)

INSPECTION FOUND FLOORBEAM CORRODED AT STA 400, RBL 30. THE CORRODED AREA WAS CUT OUT, A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.

Part: ANGLE — CORRODED (BS 380)

INSPECTION FOUND FLOORBEAM UPPER CHORD ANGLE CORRODED AT BS 380, RBL 12. THE CORRODED AREA WAS REMOVED, A SUPPORT CHANNEL STRAP AND UPPER CHORD WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.

Part: SKIN — CRACKED (RT TE FOREFLAP)

INSPECTION FOUND A 2 INCH CRACK IN UNDERSIDE LEADING EDGE OF RT OUTBOARD FOREFLAP. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-50.

Part: FRAME — CORRODED (BS 600)

INSPECTION FOUND END OF FRAME CORRODED IN FORWARD CARGO COMPARTMENT AT STA 600, STRINGER 27R. REPAIRED IAW SRM 53-10-4.

Part: FLAP — DISBONDED (RT TE MIDFLAP)

INSPECTION FOUND THE RT OUTBOARD MIDFLAP OUTBOARD TRAILING EDGE DISBONDED. THE DISBONDED AREA WAS REMOVED, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-6.

Part: SKIN — CRACKED (LT TE MIDFLAP)

INSPECTION FOUND A 1.5 CRACK IN SKIN OF LT WING INBOARD MIDFLAP INBOARD SPINDLE CUTOUT NR 8443. THE CRACKED AREA WAS REMOVED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.

Part: CEILING PANEL — CRACKED (BS 273)

INSPECTION FOUND A .75 INCH CRACK AT FASTENER OF NLG WHEEL WELL CEILING PANEL FORWARD OF STA 273, LBL 14. A REPAIR WAS INSTALLED IAW SRM 51-40-2.

Part: PANEL — CRACKED (NLG WW)

INSPECTION FOUND THREE CRACKS AT FASTENERS OF NLG WHEEL WELL CEILING PANEL AT BS 286, BL 0. THE CRACKS WERE .5 TO 1 INCH LONG. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.

Part: SKIN — CORRODED (BS 560-590)

INSPECTION FOUND FORWARD CARGO SKIN CORRODED AT STA 560 TO 580, STRINGER 28R. THE CORROSION WAS REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, PAGE 8.

Part: INTERCOSTAL — CORRODED (BS 580-600)

INSPECTION FOUND INTERCOSTAL CORRODED IN FORWARD CARGO COMPARTMENT AT STA 580 TO 600, STRINGER 26L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.

Part: WEB — CRACKED (BS 1263)

INSPECTION FOUND A 1.5 INCH CRACK IN RT AFT STAIR TORQUE BOX WEB AT STA 1263 BELOW ACTUATOR FITTING. THE WEB WAS REMOVED AND A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-30-0 AND 51-30-2.

Part: ANGLE — CRACKED (NR 12 SPOILER)

INSPECTION FOUND A 2 INCH CRACK IN NR 12 SPOILER OUTBOARD SPAR ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1.

Part: FRAME — CORRODED (BS 540)

INSPECTION FOUND BOTTOM OF FRAME CORRODED IN FORWARD CARGO COMPARTMENT AT STA 540, STRINGER 28L TO 26R. THE FRAME WAS REPAIRED IAW SRM 53-10-4.

Part: SUPPORT — CORRODED (BS 315-340)

INSPECTION FOUND FORWARD LAV FLOOR SUPPORT CORRODED AT STA 315 TO 340, RBL 35. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-1.

Part: SUPPORT — CORRODED (BS 320-340)

INSPECTION FOUND FORWARD LAV FLOOR SUPPORT CORRODED AT STA 320 TO 340, RBL 15. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2.

Part: BRACKET — CRACKED (NR 2 LE FLAP ACT)

INSPECTION FOUND A 1 INCH CRACK AT INBOARD AND OUTBOARD ENDS OF NR 2 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.

Part: ANGLE — CRACKED (RT MLG WW)

INSPECTION FOUND A 2 INCH CRACK IN RT WHEEL WELL ANGLE FORWARD OF APU LOAD CONTROL VALVE DUCT AT KEEL BEAM. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.

Part: SKIN — CRACKED (RT TE FLAP)

INSPECTION FOUND A 3 INCH CRACK IN LOWER LEADING EDGE OF RT INBOARD TRAILING EDGE FLAP SKIN. A DOUBLER WAS FABRICATED AND INSTALLED IAW 57-40-4.

Part: ANGLE — CRACKED (RT MLG WW)

INSPECTION FOUND A 1 INCH CRACK IN RT WHEEL WELL ANGLE BELOW LOAD CONTROL VALVE. THE ANGLE WAS REMOVED, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.

Part: WEDGE — DISBONDED (LT TE FLAP)

INSPECTION FOUND LT WING TRAILING EDGE INBOARD AFT FLAP DISBONDED IN FIVE AREAS. LOWER SURFACE: 15-20 AND 54-69 FROM INBOARD EDGE. UPPER SURFACE: 73-80, 112-116, AND 142-146 FROM INBOARD EDGE. THE FLAP WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-51-2.

Part: TRACK — CRACKED (NR 4 TE FLAP)

INSPECTION FOUND A .75 INCH CRACK IN OUTBOARD SIDE OF NR 4 FLAP TRACK TO MAIN LANDING GEAR BEAM ATTACH BOLT AREA. THE FLAP TRACK WAS REMOVED AND REPLACED IAW SRM 57-10-0 AND MM 27-51-0.

Part: SKIN — DENTED (BS 350)

INSPECTION FOUND A DENT IN LT FUSELAGE SKIN JUST BELOW AND AFT OF FORWARD ENTRANCE DOOR AREA AT STA 350 BETWEEN STRINGER 17L AND 18L. THE DENTED AREA WAS CUT OUT, A FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-30-3, FIGURE 1.

Part: ANGLE — CRACKED (NR 7 LE SLAT)

INSPECTION FOUND A 1.5 INCH CRACK IN RADIUS OF ANGLE AT INBOARD UPSTOP BLOCK ON NR 7 LEADING EDGE SLAT. THE CRACKED ANGLE WAS REMOVED AND NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2.

Part: SKIN — DEBONDED (RT WING)

INSPECTION FOUND UPPER AND LOWER SKIN OF RT WING LOWER FIXED PANEL DEBONDING FORWARD OF WHEEL WELL DOOR RELEASE HANDLE. THE PANEL WAS REMOVED, REPAIRED IAW SRM 51-40-05 AND REINSTALLED.

Part: ANGLE — CRACKED (NR 8 LE SLAT)

INSPECTION FOUND A 1.5 INCH CRACK IN RADIUS OF ANGLE AT OUTBOARD UPSTOP BLOCK ON NR 8 LEADING EDGE SLAT. A 1.5 INCH CRACK WAS ALSO FOUND IN RADIUS OF ANGLE AT INBOARD UPSTOP BLOCK ON NR 8 LEADING EDGE SLAT. THE CRACKED AREAS WERE CUT OUT, REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-10-4.

Part: CIRCUMFERENTIAL — CORRODED (BS 950)

INSPECTION FOUND CIRCUMFERENTIAL CORRODED IN AFT CARGO COMPARTMENT AT STA 950A, STRINGER 30R. THE CORRODED TEE WAS REMOVED, A NEW TEE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.

Part: BATTERY — DISCHARGED (AFT ENTRY)

INSPECTION FOUND EMERGENCY LIGHT AT AFT ENTRY INOPERATIVE. THE BATTERY PACK WAS CHARGED AND REINSTALLED.

Part: SKIN — CRACKED (RT WING LE)

INSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE SKIN AT AFT END OF OUTBOARD HOOK CUTOUT FOR NR 6 SLAT. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 57-30-4.

Part: DUCT — BLOWN (FUEL HT VLV)

THE NR 3 ENGINE FIRE WARNING BELL AND LIGHT ACTIVATED SHORTLY AFTER TAKEOFF FROM IAH WITH ENGINE AT CLIMB POWER. THE THROTTLE WAS RETARDED AND THE FIRE WARNING CEASED. WHEN THE NR 3 THROTTLE WAS ADVANCED TO CLIMB POWER THE FIRE WARNING BELL AND LIGHT ACTIVATED AGAIN. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE FUEL HEAT VALVE DUCT FLANGE BLOWN. THE DUCT WAS REMOVED AND REPLACED. THE NR 3 ENGINE WAS RUN AND NO LEAKS WERE OBSERVED.

Part: HYD PUMP — LEAKING (NR 1 ENGINE)

FLT NR 0693 - EWR - THE 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO AFTER TAKEOFF FROM EWR. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 1 HYDRAULIC PUMP WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (W)

Part: SKIN — CRACKED (LT WING)

GSO - INSPECTION FOUND A .9 INCH CRACK IN LEFT WING FIXED LEADING EDGE SKIN AT TOP OF CENTER OF CUTOUT FOR OUTBOARD TRACK ON NR 3 SLAT. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5762-01020. (W)

Part: SHEAR TIE — CRACKED (FS 400)

GSO - INSPECTION FOUND A 1 INCH CRACK IN SHEAR TIE AT STATION 400 BETWEEN STRINGERS 27-28L. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2. (W)

Part: WEB — CRACKED (WS 139)

GSO - INSPECTION FOUND RIGHT WING CENTER INBOARD OF STATION 139 WITH CRACKS IN WEBBING AROUND FASTENER HOLES. THE CRACKS WERE .8 INCH IN LENGTH. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-6. (W)

Part: FLOORBOARD — CRACKED (FS 940)

GSO - INSPECTION FOUND A 1.5 INCH CRACK AT MLG PRESSURE FLOOR, STATION 940R. THE CRACK WAS APPROXIMATELY 12 INCHES INBOARD OF OUTSIDE EDGE OF THE FLOOR. THE CRACKED FLOORBOARDS WERE REMOVED AND REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. (W)

Part: ANGLE — CRACKED (FS 1183)

GSO - INSPECTION FOUND A .5 INCH CRACK IN AFT ENTRY DOOR SILL ANGLE AT STATION 1183 (BELOW FLOOR) ON BOTH SIDES, RBL 15 AND LBL 15. THE DOOR SILL ANGLE WAS REMOVED, A NEW DOOR SILL ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. (W)

Part: RIB — CORRODED (NR 3 LE SLAT)

GSO - INSPECTION FOUND THE OUTBOARD RIB/WEB AND BOLT HOLE BUSHINGS CORRODED AT NR 3 LEADING EDGE SLAT OUTBOARD TRACK TO SLAT ATTACH POINT. THE CORROSION WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-30-3 AND 51-30-2. (W)

Part: INTERCOSTAL — CRACKED (NR 6 SLAT)

GSO - INSPECTION FOUND THE NR 6 SLAT INTERIOR WITH A CRACK IN EACH OF TWO INTERCOSTALS AT INBOARD SLAT TRACK ATTACH FITTING. THE CRACKS WERE 1.2 INCHES LONG. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-50-3. (W)

Part: INTERCOSTAL — CRACKED (NR 2 SLAT TRACK)

GSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT SLAT TRACK ATTACH FITTING AREA OF NR 2 SLAT INBOARD SLAT TRACK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-3 AND 51-30-02. (W)

Part: RIB — CRACKED (WS 738)

GSO - INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF RT RIB LOWER FORWARD ATTACH HOLE AT WS 738. THE CRACK WAS STOP DRILLED. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-10-5. (W)