N68056

Part: PANEL — CRACKED (HORIZONTAL STAB) · airframe 63,674 hrs · 28,937 cycles

DURING NDT INSPECTION, FOUND 4 PANEL CRACKED, HORIZ STAB ZONE. REPLACED PANELS ON CENTER BOX STABILIZER AND LT STABILIZER IAW EA #8-5510-93812. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164297/N01297 AND IAW SB 55-16 FIG 5.

Part: DOOR FRAME — DAMAGED (BS 1305) · airframe 63,674 hrs · 28,937 cycles

MAIN CABIN FOUND NR 1EA CRACK ON WEB JAMB DOOR NR 3 AFT AT STA 1305 LONG 15 RT SIDE. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1, FAB PART IAW DETAIL PART TRAVELER F163495/N00495 AND IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1.

Part: SKIN — CRACKED (LT WING) · airframe 63,674 hrs · 28,937 cycles

LEFT WING UPPER SURFACE T/E FOUND 1EA CRACK ON HONEYCOMB PANEL AT XORS 299. REPAIRED PANEL IAW SRM 57-00-01 FIG 1 SHT 1 VOL 1 AND SRM 51-70-00 PARA 16 VOL 2, FABRICATED PART IAW DETAIL PART TRAVELER F163459/N00459 AND IAW SRM 57-00-01 AND 51-70-00 VOL 1-2.

Part: REPAIR — DAMAGED (FUSELAGE) · airframe 63,674 hrs · 28,937 cycles

FOUND EXTERNAL DOUBLER REPAIR AT RIGHT AIR CONDITIONING COMPT DOOR AT APPROX STA 515. INSTALLED REPAIR FILLERS, REPAIR STRAP, AND REPAIR ANGLE, AND REPAIR DOUBLER IAW SRM 52-10-00 FIG 2 AND SRM 53-00-01 FIG 4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164039/N01039 AND IAW SRM 52-10-00 FIG 2 AND SRM 53-00-01 FIG 4 AND EO 8-5100-7-5001P2.

Part: SKIN — CRACKED (TE FLAPS) · airframe 63,674 hrs · 28,937 cycles

LEFT WING O/B FLAP UPPER SKIN SURFACE STA XOF 575 FOUND CRACK 2 INCHES LONG BETWEEN INTERCOSTAL PLANE NR 1 AND NR 2. REMOVED AND REINSTALLED SECTION T/E IAW SRM 51-31-01 PAGE 36/41 VOL 2 AND REPAIRED SKIN DAMAGE IAW SRM 57-10-00 FIG 65 VOL 1. FABRICATED PARTS TRAVELER F163407/N00407 AND IAW SRM 57-10-00 FIG 65 VOL 1.

Part: SKIN — CRACKED (BS 595) · airframe 63,674 hrs · 28,937 cycles

LWR FUSELAGE EXT STRUCTURE FOUND 1EA CRACK 0.25 INCH LONG ON SKIN AT STA 595 BETWEEN LONG NR 48 LEFT AND LONG NR 47 LEFT NEAR CORNER OF EXHAUST. REMOVED RAM AIR EXHAUST IAW MM 21-55-02-4, PERFORMED PENETRANT INSP IAW MM 20-20-00. INSTALLED DOUBLERS IAW SRM 53-20-00 FIG 2 VOL 1. INSTALLED AND RIGGED RAM AIR IAW MM 21-55-02-4.

Part: REPAIR — UNKNOWN (LT WING TE FLAP) · airframe 63,674 hrs · 28,937 cycles

LEFT WING O/B FLAP T/E AREA FOUND AN EXTERNAL DOUBLER REPAIR BETWEEN WING STA XOF 563 AND XOF 575. REMOVED T/E IAW SRM 51-35-01 PAGE 1-13 VOL 2 AND DWG ARC1653, CUT AND REMOVED CRACKED SECTION AND REPAIRED IAW SRM 57-00-01 FIG 10 SHT 2 VOL 1 AND SRM 51-00-01 PAGE 124/125 VOL 1. REINSTALLED T/E IAW DWG ARC1653, FAB PARTS IAW DETAIL PARTS TRAVELER F164090/N01090 AND IAW SRM 57-10-00 FIG 85 VOL 1.

Part: WEB — CRACKED (BS 1256) · airframe 63,674 hrs · 28,937 cycles

UPPER CARGO AREA STA 1256 L15 LEFT SIDE FOUND WEB CRACK ON THE RADIUS ON L3 JAMB DOOR .5 INCH LONG. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163479/N00479 AND IAW SRM 53-50-00 FIG 19 VOL 1.

Part: BULKHEAD — CRACKED (MLG WW) · airframe 63,674 hrs · 28,937 cycles

CLG WHEEL WELL SPACE FOUND 4EA CRACKS FROM .5" INCH TO 2 INCHES LONG ON UPPER SIDE LEFT VERTICAL BULKHEAD FROM STA 1491 TO 1501 LEFT SIDE X 31. INSTALLED CABLE, PULLEY, ACCUMULATOR AND PIPES IAW MM 27-51-07-2 AND MM 27-51-09-2 AND MM 20-10-01-2 AND MM 29-12-01-4 AND IAW MM 29-00-00-2. LEAK TEST IAW MM 29-00-00-2. REINSTALLED SENSITY ELEMENT IAW MM 30-23-00-0.

Part: BOLT — MISINSTALLED (BULKHEAD) · airframe 63,674 hrs · 28,937 cycles

DISCREPANCY FUSELAGE STA 275 FWD PRESSURE BULKHEAD DURING VISUAL INSP IAW EA NR 8-5310-79443B P2 FOUND INSTALLED BOLT INSTEAD OF LOCK FASTENERS. REMOVED MECH ASSY STEERING IAW MM 20-50-02-2 ACCOMPLISHED EA NR8-5310-79443B. REINSTALLED MECH AND PERFORMED TEST IAW MM 20-20-02-2 AND MM 32-51-00-2.

Part: SKIN — CRACKED (TE FLAPS) · airframe 63,674 hrs · 28,937 cycles

RIGHT WING O/B FLAP T/E FROM STA XOF 458 TO XOF 467 FOUND 1EA CRACK 2 INCHES LONG ON UPPER SURFACE SKIN, 1EA CRACK ON INT CHANNEL REF SRM 57-52-01 PG 52, MANY RIVETS LOOSE ON UPPER AND LOWER SURFACE. CUT AND REMOVED T/E CHANNEL AND REPAIRED IAW SRM 57-20-00 FIG 10 SRM 51-35-01 PG 1-13 VOL 2, SRM 51-35-02 PG 3-9 VOL 2, SRM 57-00-01 FIG 10 SHT 2 VOL 1. REPAIRED SKIN IAW SRM 57-10-00 FIG 9 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F163398/N00398 AND IAW SRM 57-00-01 FIG 10 SHT 2 VOL 1.

Part: STRUCTURE — CRACKED (CARGO BAY) · airframe 63,674 hrs · 28,937 cycles

CTR CARGO COMPT CRACK 5 INCHES LONG ON FWD DOOR JAMB. REMOVED CRACKED SECTION IAW SRM 51-35-01 PG 1/13 VOL 2 AND SRM 51-33-01 PG 34/47 VOL 2. FABRICATED AND INSTALLED NEW PAN SECTION AND OLD SPLICE IAW SRM 52-00-01 FIG 7 VOL 1 IAW SRM 51-35-01 PG 1-13 VOL 2 AND SRM 51-33-01 PG 34/47 VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER F164602/N01602 AND IAW SRM 51-33-01 PG 34-47 VOL 2 AND SRM 51-35-01 PG 1-13 VOL 2.

Part: INTERCOSTAL — CRACKED (BS 1305) · airframe 63,674 hrs · 28,937 cycles

ON DOOR NR 3 RT FOUND NR 1EA CRACK 0.50 INCH LONG ON INTERCOSTAL SPLICE AT STA 1305 BETWEEN DOOR BEAM NR 5 AND NR 6 (REMOVED PART). BLENDED OUT DAMAGE PART IAW SRM 52-00-01 FIG 1A SHT 1 VOL 1 AND INSTALLED REPAIRED DOUBLER IAW SRM 52-00-01 FIG 7 SHT 1 VOL 1 STEP 3, FABRICATED PART IAW DETAIL PART TRAVELER F163387/N00387 AND IAW SRM 52-00-01 FIG 7 SHT 1 VOL 1.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 63,674 hrs · 28,937 cycles

ON DOOR NR 3 RT FOUND 1EA CRACK 0.50 INCH LONG ON INTERCOSTAL SPLICE AT STA 1256 BETWEEN DOOR BEAM NR 5 AND NR 6 (REMOVED PART). BLENDED OUT DAMAGE AREA IAW SRM 52-00-01 FIG 1A SHT 1 VOL 1 AND REPAIRED INSTALLED DOUBLER IAW SRM 52-00-01 FIG 7 SHT 1 VOL 1 STEP 3, FABRICATED PART IAW DETAIL PART TRAVELER F163386/N00386 AND IAW SRM 52-00-01 FIG 7 SHT 1 VOL 1.

Part: SKIN — DENTED (RT ELEVLATOR) · airframe 63,674 hrs · 28,937 cycles

RT ELEVATORS FOUND DEEP DENT ON SKIN AT STA XE 136 UPPER SURFACE. TRIMMED OUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163412/N00412 AND IAW SRM 55-10-00 FIG 8 VOL 1.

Part: BULKHEAD — CRACKED (BS 2163) · airframe 63,674 hrs · 28,937 cycles

AFT BODY BLKHD EXT STRUCTURE FOUND 1 CRACK 0.50" LONG ON HORIZONTAL LONGERON AT STA 2163.685 X37 LT SIDE. REPAIRED CRACKED STIFFENER IAW SRM 53-40-00 FIG 7 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163376/N00376 AND IAW SRM 53-40-00 FIG 7 VOL 1.

Part: RIB — CRACKED (WING) · airframe 63,674 hrs · 28,937 cycles

FUEL TANK NR 1 STA XORS 372 BELOW STR 12 UPPER RIB CHORD FOUND CRACKED. REPAIRED CRACK IAW SRM 57-20-00 FIG 38 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER NRC F163636/N00636 IAW SRM 57-20-00 FIG 38 VOL 1.

Part: CHANNEL — BROKEN (LT WING) · airframe 63,674 hrs · 28,937 cycles

LT WING L/E AT PYLON INTERSECTION ZONE 517 STA XDLE 315 FOUND CHANNEL BROKEN 1"1/2 LONG AND NUTPLATE MISSING ON THE AFT SECTION REF SRM 57-21-01 PAGE 18 ITEM 2. REMOVED SKIN IAW SRM 51-31-01 PAG 36/41 VOL 2 AND INTERCOSTAL IAW SRM 51-35-01 PAGE 1/13 VOL 2. TRIMMED OUT SECTION AND REPAIRED IAW SRM 57-00-01 FIG 10 SHT 1 VOL 1. REINSTALLED REMOVED PART IAW SRM 51-31-01 PAGE 36/41 AND SRM 51-35-01 PAGE 1/13 VOL 2. INSTALLED NUTPLATE IAW SRM 51-35-01 PAGE 1/13 VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER F163424/N00424 AND IAW SRM 57-00-01 FIG 10 SHT 1 VOL1.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 63,674 hrs · 28,937 cycles

RIGHT SIDE BELOW AND FWD OG R-2 DOOR FOUND EXT DOUBLER REPAIR BETWEEN STA 735 AND 755 AND LONGERONS 29 TO 31. REMOVED EXISTING REPAIR AND INSTALLED REPAIR IAW SRM 53-20-00 FIG 11 AND SRM 53-20-00 FIG 6 VOL 1.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 63,674 hrs · 28,937 cycles

RIGHT WING LOWER SURFACE OUTBOARD FLAP FOUND REPAIR AT TRAILING EDGE SECTION AT APPROX STA XOS 470. SCRAPED DOUBLER OF EXISTING EA REMOVED DAMAGED SECTION OF SKIN AND REPAIRED IAW SRM 57-10-00 FIG 7 SHT 3 VOL 1 FABRICATED PART IAW DETAIL PART TRAVELER F163850/N00850 AND IAW SRM 57-10-00 FIG 7 SHT 3 VOL 1.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 63,674 hrs · 28,937 cycles

RT WING OUTBOARD FLAP CRACK 1,5" LONG AND NR 20 FASTENERS U/S ON UPPER SKIN AT STA XOF 542. TRIMMED OUT CRACK AND REPAIRED IAW SRM 57-10-00 FIG 85 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163355/N00355 AND IAW SRM 57-10-00 FIG 85 VOL 1.

Part: SKIN — CRACKED (LT WING) · airframe 63,674 hrs · 28,937 cycles

FOUND LT WING L/E XOS 613 FOUND CRACK 1" LONG ON THE REFUEL DOOR VANE EXTERNAL SKIN. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 68 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163380/N00380.

Part: SKIN — CRACKED (RT WING) · airframe 63,674 hrs · 28,937 cycles

RT WING L/E FOUND CRACK 2" LONG ON EXT SKIN AT STA XORS 480. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 2-3 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163612/N00612 AND IAW SRM 57-10-00 FIG 68 SHT 2 VOL 1.

Part: HINGE — CRACKED (ACCESS PANEL) · airframe 63,674 hrs · 28,937 cycles

FOUND LT WING L/E XOS 792 FOUND ACCESS PANEL TEE/HINGE CRACK 1" LONG AND EXT SKIN LOWER SECTION CRACK 2" LONG. REPAIRED L/E SKIN IAW SRM 57-10-00 FIG 68 VOL 1 AND SRM 57-10-00 FIG 49 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F163378/N00378 AND IAW SRM 57-10-00 FIG 49 AND FIG 68 VOL 1.

Part: TANK — CRACKED (BS 1986-1997) · airframe 63,674 hrs · 28,937 cycles

AFT FUSELAGE WASTE TANK COMPT FOUND 1EA CRACK ON LONG 43, 3 INCHES LONG BETWEEN STA 1986 AND 1997 LT. REMOVED FRAME SPLICE AND ANGLES AND REINSTALLED PARTS IAW SRM 51-35-01 PAGE 1-13, DWG AJC7363, DWG NJC6074 AND SRM 51-33-01 PAGE 34-47 VOL 2. CUT LONGERONS AND INSTALLED NEW PART WITH SPLICE IAW SRM 53-10-00 FIG 1-2 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163237/N00237.

Part: SKIN — CRACKED (LT WING) · airframe 63,674 hrs · 28,937 cycles

LEFT WING EXTERNAL SKIN OF L/E SLAT TRACK NR 10 XOS 660 FOUND CRACK .5 INCH LONG ON THE SLAT TRACK HOLE ANGLE. INSTALLED EXTERNAL DOUBLER IAW SRM 57-10-00 FIG 68 VOL 1, FABRICATED PART IAW DETAIL PART TRAVELER F163379/N00379 AND IAW SRM 57-10-00 FIG 68 VOL 1.

Part: DOOR FRAME — CRACKED (BS 1256) · airframe 63,674 hrs · 28,937 cycles

MAIN CABIN FOUND 2 EA CRACKS 1 INCH LONG AND .50 INCH LONG ON WEB JAMB DOOR 3 FWD AT STA 1256 LONG 27 RT. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 1 VOL. FABRICATED PART IAW DETAIL PART TRAVELER F163498/N00498 AND IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1.

Part: BULKHEAD — CRACKED (BS 584) · airframe 63,674 hrs · 28,937 cycles

FOUND LT AIR CONDITIONING COMPT FOUND 1 CRACK 4" LONG ON SKIN OF BULKHEAD BETWEEN STA 584 AND STA 580 Z-46 BY 24. TRIMMED OUT CRACK AND INSTALLED FILLER AND 2 REPAIRED DOUBLERS IAW SRM 53-30-00 FIG 6 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164135/N01135 AND IAW SRM 53-30-00 FIG 6 SHT 2 VOL 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,674 hrs · 28,937 cycles

CAC LOWER LOBE BILGE FOUND 1EA CRACK, 3 INCHES LONG ON LT FRAME AT STA 1159 CLOSE TO PRESSURE PANEL FWD CENTER WING. REMOVED ATTACH ANGLE IAW SRM 51-33-01 PAR 6-10 VOL 2 REPAIRED FRAME IAW SRM 53-30- 00 FIG 7 VOL 1 REINSTALLED ATTACH ANGLE IAW SRM 51-33-01 PAR 6-10 VOL 2.

Part: DOUBLER — NONE (FUSELAGE) · airframe 63,674 hrs · 28,937 cycles

DISCREPANCY FOUND EXTERNAL DOUBLER BETWEEN STA 735 AND 755 AND LONGERONS 34 AND 35 LT SIDE, WHERE POTABLE WATER SERVICE PANEL USED TO BE LOCATED. PERFORMED INSPECTION ON REPAIR IAW SRM 53-20-00 FIG 6 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1.

Part: HINGE — CRACKED (LT WING) · airframe 63,674 hrs · 28,937 cycles

LT WING LEADING EDGE AT STA XOS 906 FOUND ACCESS PANEL TEE/HINGE CRACK .5 INCH LONG. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F163377/N00377 AND IAW SRM 57-10-00 FIG 49 VOL 1.

Part: FLANGE — CRACKED (BULKHEAD) · airframe 63,674 hrs · 28,937 cycles

CLG WHEEL WELL/SPACE: 1EA CRACK 1 INCH LONG ON DOUBLER FLANGE UPPER SIDE LT VERTICAL BULKHEAD FROM STA 1421 TO 1431 LT SIDE X 31. REMOVED DOUBLER IAW SRM 51-35-01 PG 1/13 VOL 2. CLEANED UP CRACK REPAIRED IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1 WITH FILLER AND REINSTALLED DOUBLER IAW SRM 51-35-01 PG 1/13 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F163443/N00443 AND IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1.

Part: REPAIR — UNKNOWN (BS 475) · airframe 63,674 hrs · 28,937 cycles

FWD AVIONICS COMPT AT STA 475 FOUND FRAME REPAIR AT X 60. NO ACTION TAKEN FRAME WILL BE REMOVED WITH NRC N00579.

Part: BULKHEAD — CRACKED (BS 575-569) · airframe 63,674 hrs · 28,937 cycles

RT AIR CONDITIONING COMPT FOUND 1 CRACK 2.50" LONG ON BULKHEAD BETWEEN STA 575 AND STA 569 Z-60 X-24. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164142/N001142 AND IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1.

Part: REPAIR — PROPER (BS 859) · airframe 63,674 hrs · 28,937 cycles

FWD OF FWD CARGO DOOR STA 859 BETWEEN STRINGERS 36 AND 37 ON THE RT SIDE THERE IS AN INTERNAL DOUBLER REPAIR. PERFORMED A INSPECTION OF REPAIR IAW EA#8-5330-93229 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO#8-5100-7-5001-P1 E3.

Part: DOOR FRAME — CRACKED (BS 1305) · airframe 63,674 hrs · 28,937 cycles

MAIN CABIN FOUND 2 CRACKS 1" LONG ALL ON WEB JAMB DOOR NR 3 AFT AT STA 1305 LONG 27 RT SIDE. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163497/N00497 AND IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1.

Part: BULKHEAD — CRACKED (BS 482-489) · airframe 63,674 hrs · 28,937 cycles

RT AIR CONDITIONING COMPT FOUND 1 CRACK 2 INCHES LONG ON BULKHEAD BETWEEN STA 482 AND STA 489 Z-60 X-24. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1, FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164141/N01141 AND IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1.

Part: ANGLE — CRACKED (BS 535) · airframe 63,674 hrs · 28,937 cycles

RIGHT AIR CONDITIONING COMPT FOUND 1 CRACK 1" LONG ON TEE ANGLE AT STA 535 Z-39 X-102. REPAIRED CRACK IAW SRM 53-00-01 FIG 9 SHT 7 VOL 1.

Part: REPAIR — PROPER (BS 401-470) · airframe 63,674 hrs · 28,937 cycles

FOUND EXTENSIVE DOUBLER REPAIR AROUND L-1 DOOR BETWEEN STA 401 AND 470.25 BOTTOM FWD AND AFT CORNERS ON FUSELAGE SKIN. PERFORMED A GVI OF EXISTING DOUBLER IAW FEDEX EA NR 8-5300-26224 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001.

Part: REPAIR — PROPER (BS 490-535) · airframe 63,674 hrs · 28,937 cycles

FOUND FLUSH DOUBLER REPAIR RT SIDE BETWEEN STA 490 AND 535 JUST ABOVE OF FWD NOSE LANDING GEAR ON AN AREA OF ABOUT 43'' BY 21''. PERFORMED A GVI OF REPAIRS IAW CONTINENTAL AIRLINES EC/RA NO 253C042 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO#8-5100-7-5001.

Part: REPAIR — PROPER (MLG DOOR) · airframe 63,674 hrs · 28,937 cycles

JUST ABOVE FWD NOSE LANDING GEAR DOOR BETWEEN STA 490 AND 555 LT SIDE, FOUND FLUSH DOUBLER OF APROX 62 X 25 INCH. PERFORMED A GVI OF REPAIRS IAW CONTINENTAL AIRLINES EC/RA 253C038, 253C039, 253C040, 253C042, 253C044 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001.

Part: DOOR FRAME — CRACKED (BS 1256) · airframe 63,674 hrs · 28,937 cycles

MAIN CABIN, FOUND 1 CRACK .25" LONG ON WEB JAMB DOOR NR 3 FWD AT STA 1256 LONG 15 RT. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163496/N00496 AND IAW SRM 53-50-00 FIG 19 VOL 1.

Part: REPAIR — UNDAMAGED (BS 505) · airframe 63,674 hrs · 28,937 cycles

BARON REPAIR, DOUBLER INSTALLED AT APPROX STA 505 RT SIDE BETWEEN LONG 39 AND 40. PERFORMED A GVI OF BARON DOUBLER IAW FEDEX EA NR 8-5320-38573B AND FEDEX EA NR 8-5320-35995A AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001.

Part: REPAIR — PROPER (BS 275) · airframe 63,674 hrs · 28,937 cycles

FOUND FWD PRESSURE BULKHEAD STA 275 LT HAND SIDE FOUND REPAIR DOUBLER BETWEEN X 13, X28 AND Z-14, Z-27.7 BEAMS. PERFORMED A GVI OF DOUBLER IAW CONTINENTAL AIRLINES EC/RA #253C037 AND FEDEX EA#8-5310-79443B AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO#8-5100-7-5001.

Part: REPAIR — UNDAMAGED (BULKHEAD) · airframe 63,674 hrs · 28,937 cycles

FOUND FLUSH DOUBLER REPAIR AT AFT PRESSURE BULKHEAD LOWER SECTION STA 2007 FROM X25 TO X-25 LONGERON 48L TO 48R. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND IN COMPLIANCE WITH SRM 53-40-00 PAG 9A.

Part: REPAIR — UNDAMAGED (BS 1139) · airframe 63,674 hrs · 28,937 cycles

FOUND EXTERNAL TRIPLE DOUBLER REPAIR AT STA 1139 BETWEEN LONGERON 47 AND 48 RT SIDE. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-20-00 FIG 6.

Part: REPAIR — UNDAMAGED (BS 1997-2013) · airframe 63,674 hrs · 28,937 cycles

FOUND EXTERNAL DOUBLER REPAIR BETWEEN STA 1997 AND 2013 LONGERONS 45 AND 41 LT SIDE AT THE AFT PRESSURE BULKHEAD FRAME AREA. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND IN COMPLIANCE WITH SRM 53-20-00 PAG 61.

Part: REPAIR — UNDAMAGED (FUSELAGE) · airframe 63,674 hrs · 28,937 cycles

FOUND EXTERNAL TRIPLE DOUBLER BETWEEN STA 1853 AND 1887 LONGERONS 36 AND 38 LT SIDE JUST AFT OF BULKHEAD CARGO DOOR. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-20-00 FIG 6.

Part: SKIN — UNKNOWN (BS 1601-1621) · airframe 63,674 hrs · 28,937 cycles

FOUND MAIN CABIN BETWEEN FUSELAGE STA 1601 AND 1621, STRINGERS 8 AND 9 RT SIDE FOUND A FLUSH REPAIR. PERFORMED A GVI OF EXISTING REPAIR IAW SRM 53-20-00 FIG 13 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001.

Part: REPAIR — UNDAMAGED (BS 625) · airframe 63,674 hrs · 28,937 cycles

FOUND SEAT TRACK PLUG REPAIR AT STA 625 X 27. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND REPAIR IN COMPLIANCE WITH SRM 53-70-00 FIG 2 PAG 9.

Part: DOOR FRAME — UNKNOWN (BS 1259) · airframe 63,674 hrs · 28,937 cycles

FOUND MAIN CABIN L-3 DOOR FWD DOOR JAMB STA 1259 FOUND DOUBLER REPAIR BETWEEN STRINGER 24 AND 27. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-50-00 FIG 19.

Part: REPAIR — UNDAMAGED (BS 595) · airframe 63,674 hrs · 28,937 cycles

AFT AIR CONDITIONING ACCESS DOOR, AFT TOP CORNER FOUND AN EXTERNAL TRIPLE DOUBLER REPAIR AT STA 595 LT SIDE. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND IN COMPLIANCE WITH SRM 53-50-00 PAG 19.

Part: REPAIR — UNDAMAGED (BS 2131) · airframe 63,674 hrs · 28,937 cycles

AFT FUSELAGE ABOVE HORIZONTAL STABILIZER LT SIDE STA Y2131 FOUND AN EXTERNAL DOUBLER REPAIR. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-00-01 FIG 4.

Part: REPAIR — UNDAMAGED (BS 839) · airframe 63,674 hrs · 28,937 cycles

FOUND SEAT TRACK SPLICE REPAIR AT STATION 839 X47.500 MAIN CABIN. PERFORMED A GVI OF EXISTING SPLICE IAW EO 8-5100-7-5001 CRITERIA, FOUND SPLICE IN COMPLIANCE WITH SRM 53-70-00 PAGE 3 FIG 1.

Part: DOUBLER — UNKNOWN (HORIZONTAL STAB) · airframe 63,674 hrs · 28,937 cycles

LOWER SURFACE OF HORIZONTAL STABILIZER CONSTANT SECTION AT FRONT SPAR LEFT SIDE BY REF PLANE YCH 137.6092, FOUND AN EXTERNAL DOUBLER REPAIR. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH SERVICE BULLETIN 55-16 FIG 13.

Part: TRIPLER — UNKNOWN (FUSELAGE) · airframe 63,674 hrs · 28,937 cycles

FOUND TRIPLE REPAIR AT STA 575 LONGERON 48 RT SIDE AT RAM AIR DUCT CORNER. PERFORMED A GVI ON EXISTING REPAIR DOUBLER IAW SRM 53-20-00 FIG 2. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO8-5100-7-5001.

Part: REPAIR — UNKNOWN (SEAT TRACK) · airframe 63,674 hrs · 28,937 cycles

MAIN CABIN STA 635 X27 FOUND STANDARD SEAT TRACK REPAIR. PERFORMED A GVI OF EXISTING REPAIR IAW EO8-5100-7-5001 CRITERIA FOUND REPAIR IN COMPLIANCE WITH SRM 53-70-00 FIG 2 SHT 1-2 VOL 1.

Part: DOUBLER — UNKNOWN (FLOORBEAM) · airframe 63,674 hrs · 28,937 cycles

CENTER CARGO COMPT, FLOOR SUPPORT BEAM FOUND A SPLICE DOUBLE REPAIR AT FUSELAGE STA 1701 BETWEEN X24 AND X48. PERFORMED A GVI OF EXISTING SPLICE IAW EO8-5100-7-5001 CRITERIA, FOUND SPLICE DOUBLER IN COMPLIANCE WITH SRM 53-60-01 PAGE 7.

Part: DOUBLER — UNKNOWN (HORIZONTAL STAB) · airframe 63,674 hrs · 28,937 cycles

LEFT L/E AT FRONT SPAR INBOARD AREA OF HORIZONTAL STABILIZER ON SKIN FOUND AN EXTERNAL DOUBLER REPAIR AT STAB STA XE35. PERFORMED A GVI OF EXISTING REPAIR IAW SRM 55-20-00 PG 45 FIG 9 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO8-5100-7-5001.

Part: PLUG — UNKNOWN (SEAT TRACK) · airframe 63,674 hrs · 28,937 cycles

SEAT TRACK PLUG REPAIR LOCATED AT STATION 1511 X75. PERFORMED A GVI OF EXISTING REPAIR IAW EO8-5100-7-5001 CRITERIA FOUND REPAIR IN COMPLIANCE WITH SRM 53-70-00 PAGE 11 FIG 62A VOL 1.

Part: DOUBLER — UNKNOWN (HORIZONTAL STAB) · airframe 63,674 hrs · 28,937 cycles

LEFT HAND HORIZONTAL STABILIZER UPPER SURFACE ON SKIN TRAILING EDGE, FOUND AN EXTERNAL DOUBLER REPAIR BETWEEN STATIONS XE84 AND XE109. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST AND FOUND IN COMPLIANCE WITH FEDEX EA8-5510-49668.

Part: PLUG — UNKNOWN (SEAT TRACK) · airframe 63,674 hrs · 28,937 cycles

SEAT TRACK PLUG REPAIR AT STA 969 X47. PERFORMED A GVI OF EXISTING REPAIR IAW EO8-5100-7-5001 CRITERIA FOUND REPAIR IN COMPLIANCE WITH SRM 53-70-00 PAGE 11 FIG 62A VOL 1.

Part: DOUBLER — UNKNOWN (TE FLAPS) · airframe 63,674 hrs · 28,937 cycles

FOUND EXTERNAL DOUBLER REPAIR AT LEFT WING INBOARD FLAP, INBOARD TRAILING EDGE AREA BETWEEN WING STATION XIF187 AND XIF189. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND IN COMPLIANCE WITH SRM 57-00-01 FIG 4 SHT 2 VOL 1.

Part: DOUBLER — UNKNOWN (HORIZONTAL STAB) · airframe 63,674 hrs · 28,937 cycles

EXTERNAL DOUBLER REPAIR FOUND ON RT HORIZONTAL STABILIZER UPPER SURFACE BETWEEN STA XE79 AND XE86. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH SERVICE BULLETIN 55-16 FIG 17.

Part: REPAIR — UNKNOWN (FLOORBEAM) · airframe 63,674 hrs · 28,937 cycles

CENTER CARGO COMPT FLOORBEAM SPLICE REPAIR AT STA 1701 RBL 36. PERFORMED A GVI OF EXISTING SPLICE IAW EO8-5100-7-5001 CRITERIA FOUND SPLICE DOUBLER IN COMPLIANCE WITH SRM 53-60-01 PAGE 7.

Part: DOUBLER — UNKNOWN (HORIZONTAL STAB) · airframe 63,674 hrs · 28,937 cycles

TRAILING EDGE LT HAND HORIZONTAL STABILIZER UPPER SURFACE ON SKIN THERE'S AN EXTERNAL DOUBLER REPAIR BETWEEN STAB STATIONS XE67 AND XE82. PERFORMED A GVI OF EXISTING DOUBLER IAW FEDEX EA8-5510-49668 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO8-5100-7-5001.

Part: DOUBLER — UNKNOWN (HORIZONTAL STAB) · airframe 63,674 hrs · 28,937 cycles

FOUND EXTERNAL DOUBLER REPAIR AT RT HORIZONTAL STABILIZER L/E ON FRONT SPAR INBOARD SECTION OF STAB STA XE35. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH SRM 55-20-00 FIG 9 SHT 1 VOL 1.

Part: DOUBLER — UNKNOWN (FLOORBEAM) · airframe 63,674 hrs · 28,937 cycles

AFT CARGO COMPT BILGE AREA, FLOOR SUPPORT BEAM FOUND A SPLICE DOUBLER REPAIR LBL 36 STA 1841. PERFORMED A GVI OF EXISTING SPLICE IAW EO8-5100-7-5001 CRITERIA, FOUND SPLICE DOUBLER REPAIR IN COMPLIANCE WITH SRM 53-60-01 PAGE 7.

Part: SKIN — DAMAGED (NR 1 SLAT) · airframe 63,674 hrs · 28,937 cycles

FOUND A SPLICE DOUBLER REPAIR AT RIGHT WING NR 1 SLAT LOWER SURFACE ON SLAT SKIN WING STATION XIS247 AT NR 3 SLAT TRACK AREA. PERFORMED A GVI OF EXISTING REPAIR IAW EO8-5100-7-5001 CRITERIA REQUEST AND FOUND IN COMPLIANCE WITH SRM 57-10-00 FIG 29.

Part: DOUBLER — UNKNOWN (ELEVATOR) · airframe 63,674 hrs · 28,937 cycles

LEFT HORIZONTAL STABILIZER INBOARD ELEVATOR LOWER SURFACE ON SKIN, FOUND AN INTERNAL DOUBLER REPAIR BETWEEN STAB STATIONS XE130 AND XE146. PERFORMED A GVI OF EXISTING REPAIR IAW EO8-5100-7-5001 CRITERIA REQUEST, FOUND DOUBLER IN COMPLIANCE WITH SRM 55-00-01 PG 9.

Part: DOUBLER — UNKNOWN (HORIZONTAL STAB) · airframe 63,674 hrs · 28,937 cycles

RT HORIZONTAL STABILIZER UPPER SURFACE FOUND EXTERNAL DOUBLER REPAIR ON SKIN BETWEEN STA XE58 AND XE70. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH SERVICE BULLETIN 55-16 FIG 18.

Part: DOUBLER — UNKNOWN (DOOR FRAME) · airframe 63,674 hrs · 28,937 cycles

MAIN CABIN L-3 DOOR AT FUSELAGE STA 1305 FOUND DOUBLER REPAIR AT AFT DOOR JAMB. PERFORMED A GVI ON EXISTING REPAIR IAW SRM 53-50-00 FIG 19. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO8-5100-7-5001.

Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 63,674 hrs · 28,937 cycles

AT FUSELAGE STA 392 RT SIDE FOUND INTERNAL DOUBLER REPAIR AT Z53 BEHIND CO-PILOT WINDOW. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA, FOUND DOUBLER IN COMPLIANCE WITH SRM 53-20-00 FIG 13 SHT 14.

Part: DOUBLER — UNKNOWN (NR 1 SLAT) · airframe 63,674 hrs · 28,937 cycles

FOUND EXTERNAL DOUBLER REPAIR AT LEFT WING NR 1 SLAT UPPER SURFACE L/E AREA BETWEEN WING STATIONS XIS129 TO XIS133. PERFORMED A GVI OF EXISTING REPAIR IAW SRM 57-10-00 FIG 84 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO8-5100-7-5001.

Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 63,674 hrs · 28,937 cycles

FOUND TRIPLE DOUBLER BOTTOM OF FUSELAGE BETWEEN STA 1019 AND 1059, AND STRINGERS 51 LT TO 51 RT ADF LOOP ANTENNA LOCATION. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA FOUND DOUBLER IN COMPLIANCE WITH SRM 53-20-00 FIG 7 PG 85.

Part: DOUBLER — UNKNOWN (HORIZONTAL STAB) · airframe 63,674 hrs · 28,937 cycles

FOUND EXTERNAL DOUBLER REPAIR AT LEFT HAND HORIZONTAL STABILIZER ON SKIN, TRAILING EDGE OF STAB BETWEEN STA XE48 AND XE60. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH DOUGLAS AIRCRAFT COMPANY SERVICE BULLETIN 55-16 FIG 10.

Part: DOUBLER — UNKNOWN (NR 1 SLAT) · airframe 63,674 hrs · 28,937 cycles

LEFT WING NR 1 SLAT L/E UPPER SURFACE FOUND A FLUSH DOUBLER REPAIR BETWEEN WING STATION XIS152 AND XIS157. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND IN COMPLIANCE WITH SRM 57-10-00 FIG 11.

Part: DOUBLER — UNKNOWN (AILERON) · airframe 63,674 hrs · 28,937 cycles

RIGHT WING LOWER SURFACE INBOARD AILERON FOUND AN EXTERNAL DOUBLER REPAIR BETWEEN WING STATIONS XIA316 TO XIA321. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST AND FOUND IN COMPLIANCE WITH SRM 57-00-01 FIG 4.

Part: DOUBLER — UNKNOWN (HORIZONTAL STAB) · airframe 63,674 hrs · 28,937 cycles

RT HAND HORIZONTAL STABILIZER LOWER SURFACE FOUND AN EXTERNAL DOUBLER REPAIR ON SKIN, BETWEEN HORIZONTAL STAB STATIONS XE75 AND XE86. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND DOUBLER IN COMPLIANCE WITH SERVICE BULLETIN 55-16 FIG 22.

Part: DOUBLER — UNKNOWN (SLAT TRACK) · airframe 63,674 hrs · 28,937 cycles

LT WING FOUND AN EXTERNAL DOUBLER REPAIR AT FIXED L/E LOWER SURFACE AT CUT OUT FOR SLAT TRACK LEFT SIDE STATION XOS 775. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND IN COMPLIANCE WITH SRM 57-10-00 PAGE 215.

Part: SKIN — DENTED (BS 295) · airframe 63,674 hrs · 28,937 cycles

LWR FUSELAGE EXT STRUCTURE FOUND DEEP DENT ON SKIN (2.25'' BY 1'' DEEP 0.11'') AT STA 295 BY 4 LT SIDE. REFORMED DENT AS PER SRM 53-20-00 FIG 13 VOL 1. INSTALLED FINGER DOUBLER AS PER SRM 53-20-00 FIG 13 VOL 1.

Part: SKIN — DENTED (BS 295-304) · airframe 63,674 hrs · 28,937 cycles

LWR FUSELAGE EXT STRUCTURE FOUND DEEP DENT ON SKIN (2'' BY 1'' DEEP 0.07'') BTWN STA 295 AND STA 304 BY 15 LT SIDE. REFORMED DENT AS PER SRM 53-20-00 FIG 13 SHT 14 VOL 1. INSTALLED FINGER DOUBLER AS PER SRM 53-20-00 FIG 13 SHT 14 VOL 1.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 63,674 hrs · 28,937 cycles

FOUND COCKPIT FLOOR SECTION STA 304 BY 13 CRACK ON MEMBRANE 2'' LONG RIF SRM 53-11-01 ITEM 1. REPAIRED CRACK ON MEMBRANE RIF SRM 53-11-01 ITEM 1 STA 304 BY 13.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 63,674 hrs · 28,937 cycles

COCKPIT FLOOR STRUCTURE FOUND 1 EA CRACK 2 INCHES LONG ON MEMBRANE STA 304 X-12 RT SIDE. REPAIRED CRACK ON MEMBRANE STA 304 X-12 RT SIDE RIF SRM53-11-01, ITEM 1.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 63,674 hrs · 28,937 cycles

COCKPIT FLOOR STRUCTURE FOUND 1 EA CRACK 2 INCHES LONG ON MEMBRANE STA 304 X-27 RT SIDE. REPAIRED CRACK ON MEMBRANE RIF 53-11-01 STA 304 X-27 RT SIDE.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 63,674 hrs · 28,937 cycles

COCKPIT FLOOR SECTION STA 313 CRACK ON MEMBRANE 1 INCH LONG RIF SRM 53-11-01, ITEM 1. REPAIRED MEMBRANE AT STA 313 RIF SRM53-11-01 FIG 4 SHT 2 VOL 1.

Part: CONDUIT — MISROUTED (LT MLG UPLOCK) · airframe 61,869 hrs · 28,062 cycles

WITH GEAR HANDLE UP THERE IS AN UNSAFE LEFT MAIN INDICATION ON BOTH PANELS. FOLLOWD QRH STEPS AND CYCLED GEAR LIGHTS REMAINED. RETURNED TO MEM. FOUND LT MLG UPLOCK SENSOR CONDUIT MIS-ROUTED BENEATH SENSOR LINK , WHICH PREVENTED THE SENSOR FROM MOVING IN RANGE OF THE TARGET. PROPERLY REROUTED CONDUIT ABOVE SENSOR LINK AS OUTLINED IN ILLUSTRATION IN DC-10 MM 32-61-03-2 FIGURE 202/SHEET 1. FOUND SENSOR TO TARGET GAP WITHIN LIMITS REF:MM 32-61032. SENSOR OPS CHECKED GOOD. REF:MM32-61-03-2. PRIMARY AND SECONDARY INDICATIONS NORMAL.

Part: WARNING LIGHT — MALFUNCTIONED (MLG) · airframe 61,869 hrs · 28,062 cycles

ON GEAR RETRACTION LT MAIN GEAR LIGHT STAYED RED ON FORWARD AND F/E'S GEAR INDICATION. RAN RED TABS, GEAR EXTEND NORMALLY. REPEAT WRITE UP, RETURNED TO MEM.

Part: SUPPORT — CORRODED (FLAP VANE) · airframe 61,808 hrs · 28,023 cycles

COMPLY WITH EA 8-5750-77428, WINGS - ARC1455 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-77428.

Part: VANE — CORRODED (FLAP VANE) · airframe 61,808 hrs · 28,023 cycles

COMPLY WITH EA 8-5750-77429 WINGS ARC1455-510 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-77429.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 61,808 hrs · 28,023 cycles

MAIN CARGO COMP SEAT TRACK HAS AREAS OF ELONGATED SCALLOPS FROM FS 1129-1530 LBL 8 AND IS CRACKED AT FS 1179 APPROX 4 INCHES LONG. NDT AT LBL 8 FS 1179 NO CRACK NOTED IAW NTSPM 06-10-01. BLENDED OUT DAMAGED AREAS AT LBL 8 FS 1129-1530 IAW SRM 53-70-00. STA 1129-1249 FOUND IN LIMITS IAW SRM 53-70-00. TREAT & PRIME AREA 1129-1249 IAW SRM 51-21-01, REINSTALLED FS 1129-1249 IAW SRM 51-34-01. FS 1249-1530 IS OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REPLACED FS 1249-1530 SEAT TRACK IAW SRM 51-31-01 AT MAE.

Part: BRACKET — CRACKED (RT WING) · airframe 61,808 hrs · 28,023 cycles

RIGHT WING T/E, HYD LINE SUPPORT IS BROKEN OFF SPOILER ACTUATOR NR 5. REMOVED AND FAB NEW BRACKET IAW DWJ ARK 0067 & DPS 3069 AND REINSTALLED NEW BRACKET IAW SRM 51-31-01 AT MAE.

Part: SKIN — GOUGED (LT WING) · airframe 61,808 hrs · 28,023 cycles

LEFT WING DROOPED LEADING EDGE O/B L/E HAS GOUGE. REPAIRED LEFT WING DROOPED L/E IAW SRM 57-00-01. GOUGE FOUND OUT OF LIMITS BY NTSPM 04-00-03 .070 BEFORE .045 AFTER. REMOVED & REPLACED BROKEN BRACKET ON O/B RIB IAW SRM 57-00-01, REMOVED AND REPLACED WORN BULB SEAL IAW DPS 3.579. DROOP L/E ON LEFT WING WAS REMOVED AND REINSTALLED ON DOCUMENT N01336. WORK DONE AT MAE.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 61,808 hrs · 28,023 cycles

VERTICAL STIFFENER FASTENER HOLES ELONGATED, UNDER DOOR SILL 115AZ INSIDE AVIONICS COMP. REMOVED VERTICAL STIFFENER & T-CLIPS. REC FROM FAB ON T4/429922. VERTICAL STIFFENER LOCATED & DRILLED. FAB 2 CLIPS FROM 60.8060.20MST000955 1 & 2 CLIP FROM 60.2781420MST0008469. LOCATED, DRILLED, TREATED, PRIMED & INSTALLED VERTICAL STIFFENER & 2 CLIPS IAW SRM 51-33-01 & DRG NCA6042 AT MAE.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 61,808 hrs · 28,023 cycles

NR 3 ENGINE LEFT T/R TRANSLATING SLEEVE, FWD LOWER SLIDER CRACKED. REMOVED CRACKED BRACKET IAW SRM 51-31-01 & 51-35-01. FAB NEW BRACKET IAW CF6-6 ENGINE MANUAL. INSTALLED IAW ENGINE MANUAL CF6-6 & SRM 51-31-01.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 61,808 hrs · 28,023 cycles

STA 1561 LGN 38R RT LWR UNDERWING FAIRING PANEL SUPPORT FRAME IS CRACKED. REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-35-01 AND SRM 51-31-01 AT MAE.

Part: ROLLER TRAY — DAMAGED (MAIN CARGO BAY) · airframe 61,808 hrs · 28,023 cycles

MAIN DECK BALL MAT AT STA 695-775 LBL 60-108 HAS DENT AND IS TORN. REPLACED BALL MAT IAW ANCRA MM 25-50-33 AT MAE.

Part: RUB STRIP — WORN (NR 2 COWLING) · airframe 61,808 hrs · 28,023 cycles

NR 2 ENGINE RIGHT CORE COWL FWD CHAFE STRIP IS WORN. REPLACED RUB STRIP IAW SRM 51-31-01AT MAE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,808 hrs · 28,023 cycles

AFT CARGO FLOOR SUPPORT BEAM IS CORRODED STA 1841 LBL 18 TO RBL 36. REPLACED SUPPORT BEAM IAW SRM 51-33-01 AND SRM 51-35-01 AT MAE.

Part: ROLLER TRAY — DAMAGED (MAIN CARGO BAY) · airframe 61,808 hrs · 28,023 cycles

MAIN DECK 2C BALL MAT HAS SEVERAL MISSING RETAINERS AND BALLS. REPLACED BALL MAT IAW ANCRA MM 25-50-33 AT MAE.

Part: SUPPORT BRACKET — CRACKED (L/E SLAT) · airframe 61,808 hrs · 28,023 cycles

RIGHT WING NR 3 SLAT TRACK LOWER FAIRING OUTBOARD SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-31-01 AND AMM 27-80-01-4 AT MAE.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 61,808 hrs · 28,023 cycles

LEFT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED AT XORS 714 INSIDE ACCESS 536AB. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE.

Part: SUPPORT — CORRODED (LT OB FLAP VANE) · airframe 61,808 hrs · 28,023 cycles

ARC1496 FLAP VANE SUPPORT CORROSION REWORK IAW EA 8-5750-77409. COMPLIED WITH EA 8-5750-77409 WINGS ARC1496 FLAP VANE SUPPORT CORROSION REWORK AT MAE.

Part: CLIP — CRACKED (LT WING) · airframe 61,808 hrs · 28,023 cycles

STA 1278 - STA 1441 LEFT WING OVERWING PANEL SUPPORT FRAME LOWER MOUNT CLIPS ARE CRACKED. REMOVED AND REPLACED CLIPS IAW SRM 51-31-01 AT MAE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,808 hrs · 28,023 cycles

AFT CARGO COMPT FLOOR SUPPORT IS CORRODED ON LOWER SURFACE STA 1781 LBL 27 TO LBL 42. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-31-01 AT MAE.

Part: SUPPORT FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 61,808 hrs · 28,023 cycles

LEFT O/B FLAP O/B HINGE REAR SPAR SUPPORT FITTING ATTACHED TO SPAR IS CORRODED IN AND AROUND BARREL NUT HOLE. REMOVED AND REPLACED SUPPORT FITTING IAW SRM 51-33-01, SRM 51-31-01 AND SRM 51-41-01 AT MAE.

Part: PAN — DELAMINATED (FWD LAVATORY) · airframe 61,808 hrs · 28,023 cycles

C/W EA 8-2540-77416 FWD LAV FLOOR PAN REPAIR. FWD LAV FLOOR PAN REPAIRED IAW EA 8-2540-77416 ON MAE TRAVLER T4/431252.

Part: FITTING — CORRODED (FLAP VANE) · airframe 61,808 hrs · 28,023 cycles

LEFT O/B FLAP NR 3 VANE FITTING FWD BOLT HOLE HAS CORROSION. AFT BOLT HOLE BUSHING IS CORRODED AND FITTING HAS NUMEROUS AREAS OF CORROSION. RECEIVED NEW NR 3 VANE FITTING TO BE INSTALLED ON WORK CARD E8-5750-7- 5000 PT 3 AT MAE.

Part: HINGE — CORRODED (T/E FLAP) · airframe 61,808 hrs · 28,023 cycles

COMPLY WITH EA 8-5740-77404 WINGS - LEFT INBOARD FLAP - AFT HINGE ASSY ARC2512 PIVOT BORE CORROSION. COMPLIED WITH EA 8-5740-77404 WINGS - LEFT INBOARD FLAP AFT HINGE ASSY ARC 2512 PIVOT BORE CORROSION AT MAE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 61,808 hrs · 28,023 cycles

RADIO ALTIMETER NR 1 & 2 AFT FUSELAGE STRUCTURE CORRODED. REMOVED AND REPLACED LT AND RT RADIO ALT DOUBLERS IAW SRM 51-31-01 AND SRM 51-35-01 AT MAE.

Part: CLIP — CRACKED (LT WING) · airframe 61,808 hrs · 28,023 cycles

LT WING VENT PIPE SUPPORT BRACKET BROKEN INSIDE 538AB. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 61,808 hrs · 28,023 cycles

MAIN DECK LT STA 1079 LONGERON 20 FRAME SUPPORT CRACKED. REMOVED AND REPLACED FRAME TEE SUPPORT IAW SRM 51-31-01 AND SRM 51-33-01 AT MAE.

Part: FLAP TRACK — WORN (T/E FLAP VANE) · airframe 61,808 hrs · 28,023 cycles

LEFT INBOARD FLAP VANE NR 2 TRACK HAS DEEP WEAR MARKS ON LOWER & UPPER SURFACE. REPLACED NR 2 LEFT I/B TRACK TO BE INSTALLED ON EO 8-5750-7-5002 AT MAE.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 61,808 hrs · 28,023 cycles

RIGHT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED IN 3 PLACES AT XORS 714 INSIDE ACCESS PANEL 636 AB. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE.

Part: CHANNEL — CRACKED (RT WING) · airframe 61,808 hrs · 28,023 cycles

RT WING VENT PIPE SUPPORT BRACKET CRACKED INSIDE 635 BT. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE.

Part: STRINGER CLIP — CRACKED (RT WING) · airframe 61,808 hrs · 28,023 cycles

RIGHT WING STRINGER TO RIB TIE CLIP CRACKED INSIDE 634 AT- S 37. REMOVED AND REPLACED CLIP IAW SRM 51-31-01 AND SRM 51-33-01 AT MAE.

Part: CHANNEL — CRACKED (RT WING) · airframe 61,808 hrs · 28,023 cycles

RT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED IN 2 PLACES AT XORS 738 INSIDE PANEL 636BB. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE.

Part: CLIP — BROKEN (CARGO BAY) · airframe 61,808 hrs · 28,023 cycles

CTR PIT ROLLER BRACKET BROKEN STA 1705 RBL 57. REMOVED AND REPLACED ROLLER AND CLIP IAW SRM 51-31-01AT MAE.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 61,808 hrs · 28,023 cycles

RT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED AND BROKEN AT XORS 683 INBOARD SIDE. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE.

Part: INTERCOSTAL — CRACKED (CARGO BAY) · airframe 61,808 hrs · 28,023 cycles

MAIN DECK L-1 DOOR AFT JAMB STRUCTURE 2ND ACCESS HOLE FROM THE FLOOR FRAME STRUCTURE CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-33-01 AT MAE.

Part: BRACKET — CORRODED (CARGO DOOR) · airframe 61,808 hrs · 28,023 cycles

FORWARD LWR CARGO DOOR LATCH SPOOL FITTING CORRODED AND SPOOL PITTED. REPLACED BRACKET AND SPOOL IAW MM 52-31-00-5 AT MAE.

Part: FLAP TRACK — WORN (T/E FLAP VANE) · airframe 61,808 hrs · 28,023 cycles

RIGHT O/B FLAP NR 3 VANE TRACK TOP PLATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 AT MAE.

Part: PLATE — GOUGED (CARGO DOOR) · airframe 61,808 hrs · 28,023 cycles

FWD LWR CARGO DOOR FWD JAMB CENTER ANTI-CHAFE PLATES GOUGED. REMOVED AND REPLACED ANTI-CHAFE PLATES IAW SRM 51-31-01AT MAE.

Part: STOP FITTING — WORN (T/E FLAP) · airframe 61,808 hrs · 28,023 cycles

RIGHT INBOARD FLAP STOP PAD FITTING FWD OF O/B HINGE FASTENER HOLES ELONGATED AND WORN. REPLACED ANTI FRICTION UPSTOP PAD IAW MM 20-50-02-2 AT MAE.

Part: FLAP TRACK — WORN (NR 2 FLAP VANE) · airframe 61,808 hrs · 28,023 cycles

RIGHT O/B FLAP NR 2 VANE TRACK TOP PLATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 AT MAE.

Part: GUARD — BROKEN (CARGO DOOR) · airframe 61,808 hrs · 28,023 cycles

FWD LWR CARGO DOOR VENT DOOR GRILL BENT GOUGED AND BROKEN. REMOVED AND REPLACED VENT DOOR GUARD IAW SRM 51-31-01 AT MAE.

Part: FLAP TRACK — GOUGED (T/E FLAP) · airframe 61,808 hrs · 28,023 cycles

RIGHT O/B FLAP NR 4 TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 AT MAE.

Part: FLAP TRACK — GOUGED (T/E FLAP) · airframe 61,808 hrs · 28,023 cycles

LEFT WING O/B FLAP NR 2 TRACK HAS GOUGE. REMOVED AND REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE.

Part: FLAP TRACK — GOUGED (NR 1 FLAP VANE) · airframe 61,808 hrs · 28,023 cycles

RIGHT O/B FLAP NR 1 VANE TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C E 8-5750-7-5000 PT 4 TA MAE.

Part: ROLLER TRAY — CORRODED (CARGO BAY) · airframe 61,808 hrs · 28,023 cycles

CENTER CARGO CENTER LINE ROLLER TRAY IS CORRODED STA 1621 AND STA 1681. REPLACED ROLLER TRAY IAW SRM 51-31-01 AT MAE.

Part: FLAP TRACK — GOUGED (T/E FLAP) · airframe 61,808 hrs · 28,023 cycles

LEFT WING O/B FLAP NR 4 TRACK HAS GOUGE. REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE.

Part: FLAP TRACK — WORN (T/E FLAP) · airframe 61,808 hrs · 28,023 cycles

LEFT WING O/B FLAP NR 3 TRACK TOP COATING IS WORN. REPLACED TRACK TO BE INSTALLED ON W/C 8-5750-7-5000 PT 3 AT MAE.

Part: PANEL — MISSING (THRUST REVERSER) · airframe 61,808 hrs · 28,023 cycles

NR 3 ENGINE TR UPPER AFT CLOSE OUT PANEL MISSING A SECTION. REMOVED AND REPLACED CLOSE OUT PANEL FABBED ON MAE TRAV 428784 AT MAE.

Part: DUCT — BROKEN (A/C BAY) · airframe 61,808 hrs · 28,023 cycles

COMPLY WITH EA 8-2150-77351 AIR/CONDITIONING NR 3 AC PACK EXHAUST DUCT REPAIR P/N ACM7019. REMOVED NR 3 AC PACK EXHAUST DUCT IAW MM 20-50-02-2 AND 21-62-09-2 EA 8-2150-77351. COMPLIED WITH ON MAE TRAVLER T4/428578. INSTALLED NR 3 AC PACK EXHAUST DUCT IAW MM 20-50-02-2 AND 21-62-09-2.

Part: BRACKET — CORRODED (LT WING) · airframe 61,808 hrs · 28,023 cycles

COMPLY WITH EA 8-5740-77350 WINGS - LEFT OUTBOARD FLAP-FWD CLEVIS BRACKET ASSY CORROSION REPAIR P/N ARC0538. REWORK OF BRACKET ASSY P/N ARC0538 ACCOMPLISHED PER EA 8-5740-77350.

Part: SUPPORT FITTING — CORRODED (T/E FLAP) · airframe 61,808 hrs · 28,023 cycles

COMPLY EA 85740-77347- LEFT OUTBOARD BRACE SUPPORT FITTING CORROSION REPAIR. COMPLIED WITH EA 8-5740-77347.

Part: CASE — GOUGED (NR 3 ENGINE) · airframe 61,808 hrs · 28,023 cycles

COMPLY WITH EA 8-7220-77402 ENGINE - GOUGES IN EXTERIOR OF NR 3 ENGINE AFT STATOR CASE. NO RESTRICTION NR 3 ENGINE AFT STATOR CASE HAS GOUGES, OK PER EA 8-7220-77402 IAW EA AFTER 50 FLIGHT CYCLES ACCOMPLISH AN INITIAL INSPECTION TO VERIFY THAT NO CRACKS EXIST UNDER 10X MAGNIFICATION. REPETITIVE INSPECTIONS WITHIN EVERY 200 FLIGHT CYCLES THEREAFTER, UNDER 10X MAGNIFICATION UNTIL TERMINATING ACTION AT NEXT ENGINE SHOP VISIT.

Part: HINGE FITTING — CORRODED (LT WING) · airframe 61,808 hrs · 28,023 cycles

COMPLY WITH EA 8-5740-77348 WINGS - LEFT OUTBOARD FLAP HINGE BRACKET CORROSION REPAIR P/N ARC0502-501. COMPLIED WITH EA 8-5740-77348 WINGS LEFT OUTBOARD FLAP INBOARD HINGE BRACKET CORROSION REPAIR P/N ARC0502-501.

Part: BRACKET — CORRODED (T/E FLAP) · airframe 61,808 hrs · 28,023 cycles

COMPLY WITH EA 8-5740-77349 WINGS - RIGHT I/B FLAP REWORK OF TRACK/DRIVE BRACKET P/N ARC2761. COMPLIED WITH EA 8-5740-77349- WINGS RIGHT I/B FLAP, REWORK OF TRACK / DRIVE BRACKET.

Part: CARGO TRACK — GOUGED (MAIN CARGO COMPT) · airframe 61,808 hrs · 28,023 cycles

MAIN CARGO COMPT CARGO TRACK HAS GOUGED AREAS FROM FS 1441-1501 RBL 27. REMOVED AND REPLACED CARGO TRACK IAW SRM 53-70-00 AT MAE.

Part: CARGO TRACK — ELONGATED (MAIN CARGO COMPT) · airframe 61,808 hrs · 28,023 cycles

MAIN CARGO COMPT CARGO TRACK HAS AREAS OF ELONGATED SCALLOPS FROM FS 999-1029 RBL 47. REMOVED AND REPLACED CARGO TRACK IAW SRM 53-70-00 FROM STA 989 TO 1009 AT MAE.

Part: CARGO TRACK — GOUGED (MAIN CARGO COMPT) · airframe 61,808 hrs · 28,023 cycles

MAIN CARGO COMPT CARGO TRACK HAS GOUGED AREAS FROM FS 899-919 LBL 47. REMOVED AND REPLACED CARGO TRACK AT FS 899-919 LBL 47 IAW SRM 51-31-01 AT MAE.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 61,808 hrs · 28,023 cycles

MAIN CARGO COMPT SEAT TRACK HAS AREAS OF ELONGATED SCALLOPS FROM F/S 1561-1651 RBL 8. REMOVED AND REPLACED SEAT TRACK AT FS 1561-1651 RBL-8 IAW SRM 51-31-01 & SRM 53-70-00 AT MAE.

Part: SUPPORT — CORRODED (RT FLAP VANE) · airframe 61,808 hrs · 28,023 cycles

RIGHT O/B FLAP VANE ASSY NR 4 VANE TRACK MOUNT AFT BOLT HOLE IS CORRODED. REPLACED SUPPORT ASSY TO BE INSTALLED AT MAE.

Part: FITTING — CORRODED (RT FLAP VANE) · airframe 61,808 hrs · 28,023 cycles

RIGHT O/B FLAP NR3 VANE FITTING FWD BOLT HOLE IS CORRODED. REPLACED NR 3 VANE FITTING TO BE INSTALLED ON EO 8-5750-7-5000 C PT 4 AT MAE.

Part: CAP ANGLE — CORRODED (BS 1761)

BELL FRAME CORRODED AT BS 1761. REMOVED BELL FRAME AND INSTALLED A NEW BELLFRAME AND SPLICE ANGLE DOUBLER PER SRM 53-40-00 FIG 1L.

Part: BLKHD STIFFENER — CRACKED (NR 2 ENGINE)

DISCREPANCY: NR 2 ENGINE NOSE COWL BLKHD STIFFENER ON D-DUCT WEB CRACKED AT 10 O'CLOCK POSITION. REFERENCE: FCD 08-55-005 SNRM 4225. CORRECTIVE ACTION: REMOVED STIFFENER, WELDED CRACK, AND RE-INSTALLED STIFFENER PER SRM 57-00-00.

Part: COWL STIFFENER — CRACKED (NR 2 ENGINE)

SNRM NR 4225, NR 2 ENGINE NOSE COWL BLKHD STIFFENER ON DUCT WEB CRACKED 10 O'CLOCK POS AS SEEN THROUGH PANEL 361 KL.

Part: FRAME — CORRODED (BS 1781)

STA 1781 LONGERONS 49 TO 52R BILGE SUMP FRAM/LONGERONS HAVE EXFOLIATION CORROSION AT AFT END OF CTR CARGO COMPARTMENT. *S/D* REMOVED AND REPLACED FRAME SECTION AND SPLICE PER SRM 53-30-00.