N509UA

Part: DOOR FRAME — DAMAGED (L2 DOOR) · airframe 75,639 hrs · 28,176 cycles

DOOR LEAK AT 2L, FOUND DOOR FRAME VERY ROUGH AT SEAL INTERFACE. FOUND LARGE GAPS IN SEAL AT LOWER GATE AREA. SMOOTHED & CONTOURED FRAME AREA, FILLED GAPS IN SEAL AT LOWER GATE.

Part: SEAL — LEAKING (L2 DOOR) · airframe 75,629 hrs · 28,172 cycles

DOOR 2L SEAL LEAKS UP TO ABOUT 10,000 FEET. SMOOTHED OUT PREVIOUS REM APPLICATION, PRESSURIZED CABIN IAW AMM NO AIR LEAKAGE DETECTED AROUND DR 2L.

Part: STRAP — CRACKED (FUSELAGE) · airframe 75,611 hrs · 28,163 cycles

FLOOR BEAM STABILIZER STRAP CRACKED BS 1399, LBL 45 IN AFT CARGO COMPARTMENT. R & R DAMAGED SECTION OF STABILIZER LBL 45 STRAP AT BS 1399 IAW REO-M0803 & UAL ECRA 5365-01081

Part: SKIN — CRACKED (R4 DOOR) · airframe 75,611 hrs · 28,163 cycles

DOOR 4R INNER SKIN CRACKED ADJACENT TO PULL ASSIST HANDLE. CUTOUT DAMAGE, HFEC VERIFIED DAMAGE, REMOVED IAW NDT PT 6, 51-00-19, NO DAMAGE NOTED. FABRICATED INNER SKIN DOUBLER & INSTALLED IAW ECRA 5200-01267. THIS IS A PERMANENT REPAIR.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 75,611 hrs · 28,163 cycles

DOOR 2L CUTOUT FRAME FLANGE STATION 690 HAS FOUR EACH HOLES ON INNER FLANGE, LOCATED NEAR UPPER LOCKING CAM. CUTOUT DAMAGED FASTENER HOLES & INSTALLED REPAIR DOUBLER & SPLICE PARTS IAW ECRA 5300-01 803.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 75,611 hrs · 28,163 cycles

MAIN CABIN FLOOR BEAM HAS A CRACK 1.5 INCHES LONG AT RADIUS OF THE UPPER CORD STATION 700, LBL 45.50. CUTOUT DAMAGE & INSTALLED REPAIR IAW ECRA5300-01807 NR 33108.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 75,611 hrs · 28,163 cycles

RT INBD SEAT TRACK HAS A BROKEN LUG. INSTALLED NEW SEAT TRACK SECTION & REPAIR ANGLES & STRAP REPAIR STATION 1180 - 1250, RBL 24 IAW SRM 53-00-52, FIG 201, NR 34227.

Part: SKIN — CRACKED (L4 DOOR) · airframe 75,611 hrs · 28,163 cycles

DOOR 4L INNER SKIN CRACKED AT LIGHTNING HOLE CTR AREA. TRIMMED OUT CRACK FROM INNER SKIN, FABRICATED REPAIR DOUBLER & SHIMS IAW ECRA 5200-01262, INSTALLED REPAIR NR 33994.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,611 hrs · 28,163 cycles

CORROSION ON FLOOR L ANGLE AT FASTENER HOLE STATION 1438, RBL 63. REMOVED CORROSION INSTALLED TWO EA 3 REPAIR SPLICES, TWO EA 5 REPAIR STRAPS & ONE EA REPAIR CHORD AT STATION 1438, RBL 63 IAW ECRA 5300-01416 N-R 230031.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,611 hrs · 28,163 cycles

CORROSION ON STRINGER SPLICE STATION 1465, STRINGER 28R. R & R STRINGER 28R SPLICE AT STATION 1465 IAW SRM 51-40-02, FIG 2, 3, 8, & 12 PN 146N3820, N-R 230031.

Part: FRAME — DAMAGED (CARGO DOOR) · airframe 75,611 hrs · 28,163 cycles

FWD CARGO DOOR HAS FIVE DENTS & GOUGES ON FRAME. INSTALLED NEW FRAME IAW SRM 51-40-02.

Part: FRAME — DENTED (FUSELAGE) · airframe 75,611 hrs · 28,163 cycles

BS 1480 FRAME IN AFT CARGO COMPARTMENT IS DENTED NEAR STRINGER 26L. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 REPAIR 5.

Part: FLOORBEAM — CRACKED (BS 680) · airframe 75,611 hrs · 28,163 cycles

MAIN CABIN FLOORBEAM HAS A CRACK ABOUT ONE INCH LONG AT RADIUS OF THE UPPER TEE BS 680 LBL 24.75. REPAIRED FLOORBEAM IAW ECRA 5310-05536.

Part: FLOORBEAM — SCRATCHED (BS 640) · airframe 75,611 hrs · 28,163 cycles

SCRATCHES ON TOP OF MAIN CABIN FLOORBEAM BS 640 FROM LBL 24.75 TO RBL 24.75. REPAIRED FLOORBEAM IAW ECRA 5310-05536 REPAIR 2 FIGURE 202.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 75,611 hrs · 28,163 cycles

DENTS TWO EACH BETWEEN BS 1554 & 1557 3.5 INCHES BELOW STRINGER 25LT. INSTALLED DOUBLER IAW SRM53-60-01 FIG 1 & 53-00-01 RPR 3 FIG 201.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 75,611 hrs · 28,163 cycles

DENTS TWO EACH BETWEEN BS 1554 & 1557 3.5 INCHES BELOW STRINGER 25LT. INSTALLED DOUBLER IAW SRM 53-60-01 FIG 1 & 53-00-01 RPR3 FIG 201.

Part: UNKNOWN — LEAKING (LAVATORY) · airframe 75,564 hrs · 28,145 cycles

AIRCRAFT CAME IN WITH NO WATER IN FWD LAVATORY. AFTER SERVICE, WATER COMING OUT OF FUSELAGE DRAIN ON LT SIDE OF NOSE GEAR. UPON INSPECTION OF ELECTRICAL COMPARTMENT, FOUND BLUE WATER & ICE REMNANTS IN SIDE RIBS ON LT SIDE OF NOSE GEAR BOX. ICE AND CLEAN BLUE WATER IN LT NOSE GEAR TUNNEL. REMOVED LAVATORY TANK COVER NO WATER IN LAVATORY OR AROUND TANK. FILLED TANK WITH CLEAN WATER NO LEAKS NOTED. FLUSHED TOILET NO LEAKS NOTED. FILLED & PARTIAL CONT OF AMIS ITEM 5642003. DRAINED LAVATORY THREE TIMES NO LEAKS NOTED IN FILL OR DRAIN LINES. ACCOMPLISHED ECRA 2011-01000 IN DEPTH CLEANUP & SECURED BLANKETS. OK FOR SERVICE DENMM 872 44.

Part: BATTERY — FAULTY (APU) · airframe 75,484 hrs · 28,115 cycles

APU NOT STARTING. REPEAT APU STARTING PROBLEM WITH NO INDICATED FAULTS NOTED. TROUBLE SHOOTING FOUND CHARGER & BATTERY AT FAULT. REPLACED APU BATTERY IAW MM 24-31-03 & REPLACED APU BATTERY CHARGER IAW MM 24-31-04. SYSTEM OPERATIONS CHECKED GOOD. APU STARTS MUCH FASTER & NO LONGER REQUIRES EXCESSIVE LONG RECHARGE.

Part: BUMPER — MISSING (FA SEAT) · airframe 75,266 hrs · 28,043 cycles

L2 DOOR FLIGHT ATTENDANT SEAT LOWER SEAT BUMPER ASSEMBLY IS MISSING.

Part: FCU — LEAKING (NR 2 ENGINE) · airframe 75,083 hrs · 27,973 cycles

NR 2 ENGINE FUEL CONTROL LEAKING AT NIPPLE TUBE BOSS FITTINGS. REPLACED FUEL CONTROL. 5 MINUTE IDLE RUN & WET MOTOR COMPLETE IAW MM.

Part: FUSE — FAILED (RT MLG W/W) · airframe 74,931 hrs · 27,916 cycles

MASSIVE HYD LEAK RT MLG WHEEL WELL AFTER ARRIVAL. HYD QTY DOWN TO 50 PERCENT. UPPER PART OF RT NORMAL ANTI SKID VALVE. FOUND HYD LEAK AT NORMAL ANTI-SKID HYD FUSE D. REPLACED FUSE IAW MM. LEAK CHECK AND OPS CHECK GOOD.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 74,479 hrs · 27,781 cycles

EMERGENCY LIGHT END CAP MISSING AT SEAT 6A & 1B. REPLACED END CAP.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 74,479 hrs · 27,781 cycles

EMERGENCY LIGHT END CAP NOT INSTALLED NEAR SEAT 40C. REPLACED MISSING END CAP.

Part: FAN — NOISY (LT RECIRCULATION) · airframe 74,445 hrs · 27,771 cycles

LEFT RECIRCULATION FAN HAD A LOUD BEARING NOISE WHILE RUNNING. SELECTED OFF AND NOISE DISSIPATED. REPLACED LT RECIRCULATION FAN.

Part: FILTER — WARNING MESSAGE (RT ENGINE FUEL) · airframe 73,525 hrs · 27,486 cycles

RIGHT ENGINE FUEL FILTER EICAS, RETURNED TO FIELD. REPLACED FUEL FILTER PER AMM. OPS & LEAK CHECKED GOOD. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,641 hrs · 27,198 cycles

EEL INOP IN BULLNOSE PAX SEAT 40D. RELAMPED EEL LIGHT AT 40D, OPS CHECKED GOOD PER AMM 33-51-00, PG 501. P-N 1317.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,641 hrs · 27,198 cycles

EEL AT RIGHT OVERWING EXIT INOP, FWD HATCH, AFT HATCH LIGHT, AFT HATCH BOTH HATCH LIGHTS. RELAMPED RIGHT OVERWING HATCH LIGHTS OPS CHECKED GOOD PER AMM. (P/N 1317).

Part: B-NUT — ODOR (HYD SYSTEM) · airframe 72,355 hrs · 27,097 cycles

STRONG ODOR FROM PACKS DURING CLIMB. RAN PACKS AT GATE WITH APU BLEED AND RECEIVED A HEAVY OIL ODOR IN COCKPIT AND FWD CABIN. BORESCOPED NR 1 ENGINE, FOUND OIL WETTING AND SMALL PUDDLE IN BOTTOM AREA. FOUND B-NUT ON HYDRAULIC LINE LOOSE, TIGHTEN B-NUT IAW SMP, NO LEAKS AT THIS TIME.

Part: SENSOR — DIRTY (L1 DOOR) · airframe 72,343 hrs · 27,093 cycles

1L DOOR SLIDE INOPERATIVE. CLEANED GIRT BAR SENSORS AND OPERATED ARMING OF DOOR 1L SLIDE ARM LIGHT OPERATES NORMALLY.

Part: UNKNOWN — ODOR · airframe 72,316 hrs · 27,084 cycles

VERY STRONG ODOR FROM PACKS AFTER TAKEOFF. REPLACED LT AND RT RECIRC FILTERS PRECAUTIONARY PER MM. SEE HISTORY OF ODOR PROBLEMS. UNABLE TO ISOLATE SOURCE. REQUESTED OUTBD CREW COMMENT TO ASSIST IN ISOLATING SOURCE. OPERATED BOTH PACKS ON THE GROUND WITH APU. NO ODORS PRESENT. RPL L PACK PLENUM.

Part: ENGINE — LEAKING (NR 1) · airframe 72,022 hrs · 26,983 cycles

ON ENGINE BLEED AIR, BOTH AIR CONDITIONERS OUTPUT VERY NASTY CONDITIONED AIR. BOROSCOPE INSPECTED NR 1 ENGINE 3RD STG BEARING FOUND OIL IN COMPRESSOR UPLOADED PIC TO RVI SITE. REPLACE ESN 726513 PER MM. REPLACED ESN 726513 WITH ESN 726621 IN POS 01 PER TOD AMM 71-00-02 CONFIG 2 PB400. DUE TO ODOR IN CABIN FROM NR 1 ENGINE, NEED TO ACP "PACK BURN" PER AMM. ENGINE BURNOUT PROCEDURE. ACCMP'D AMM. NO ODOR DETECTED IN CABIN. FOUND ENGINE NR 1 WITH OIL WETTING ON NR 3 AFT CARBON SEAL (ENG CHG RECORDED IN AMIS) ACCMP'D AMM 21-00-01-201. NO ODOR DETECTED.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 71,930 hrs · 26,951 cycles

EMERGENCY EXIT LIGHT AT FIRST CLASS CLOSET CAME OUT. SECURED EMERGENCY LIGHT, LIGHT DOES NOT ILLUMINATE DURING TEST. REPLACED FEEDER CABLE, OPS CHECKED GOOD.

Part: HANDLE — BROKEN (L2 DOOR) · airframe 71,885 hrs · 26,929 cycles

L2 DOOR, OUTSIDE HANDLE ONE SIDE WILL NOT COME UP. WHEN CLOSING FROM OUTSIDE, DOOR OPS OK FROM INSIDE. FOUND PARTS BROKEN. REMOVED HANDLE AND SHAFTS PER MM. REPLACED BROKEN PARTS PER ABOVE IPC 52-11-13-001B AND MM 52-11-13. OPS CHECKED GOOD.

Part: LIGHT — FAULTY (L4 DOOR) · airframe 71,823 hrs · 26,908 cycles

THE 4L WILL NOT ARM. RELAMPED "SLIDE" ARMING LIGHT. GIRT BAR ENGAGES. ALL FUNCTIONS OPERATE NORMAL.

Part: OVEN — FAULTY (GALLEY) · airframe 71,832 hrs · 26,910 cycles

CREW REPORTS BURNING SMELL FROM OVEN. LEFT OVEN FAN INOP. REPLACED FORWARD LEFT OVEN. OP TEST OKAY.

Part: SKIN — DENTED (BS 500) · airframe 71,818 hrs · 26,907 cycles

SKIN DENTED BS 500, BETWEEN S13 - 14L. FOUND OUT OF SRM LIMITS. CUT-OUT DAMAGE AND ACCOMPLISHED HFEC OF CUT-OUT. ACCOMPLISHED INSURANCE CUT AND NDT OF OPEN HOLES COMMON TO REPAIR. NO CRACKS. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FILLERS REPAIR REF EA PT57-53-023 AND ECRA 5330-04304.

Part: STRINGER — DENTED (BS 610, S16L) · airframe 71,818 hrs · 26,907 cycles

DENT ON FUSELAGE REPAIR AT FASTENER BS 610, STR 16L. REPAIRED STRINGER AT BS 640 STR 16L IAW ECRA 5330-04299 AND EA PT57-53-018.

Part: SKIN — DENTED (BS 610 S16L) · airframe 71,818 hrs · 26,907 cycles

DENT ON SKIN AT BS 610 S16L. REPAIRED SKIN IAW ECRA 5330-04299 AND EA PT57-53-018.

Part: SKIN — DAMAGED (BS 310 S23-24L) · airframe 71,818 hrs · 26,907 cycles

EXTERIOR FUSELAGE PREVIOUS BLENDED AREA OUT OF LIMITS BS 310 STR 23-24L. CUT-OUT DAMAGE AND ACCOMPLISHED HFEC REF NDTM 51-00-19 P6. NO CRACKS FOUND. FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 71,818 hrs · 26,907 cycles

CORROSION ON FLOORBEAM AT STA 365 RBL 1 TO RT CREASEBEAM. SUPPLEMENTAL DATA, REMOVED CORROSION AND FOUND OUT OF SRM LIMITS. CUT-OUT BS 365 UPPER CHORD FROM LBL 11.5 - RBL 70. ACCOMPLISHED HFEC OF ALL EXISTING FASTENER HOLES COMMON TO REPAIR. NO CRACKS FOUND. FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM UPPER CHORD, REPAIR ANGLES, REPAIR STRAPS AND REPAIR FILLERS AS REQUIRED REF PEMCO EA PT57-53-019 AND ECRA 5310-05566.

Part: FLOORBEAM — CORRODED (BS 325) · corrosion level 2 · airframe 71,818 hrs · 26,907 cycles

CORROSION ON FLOORBEAM TEE BS 325, RBL 40 - 61. REMOVED CORROSION AND FOUND OUT OF SRM LIMITS. CUT OUT FLOORBEAM UPPER FROM LBL 8 - RBL 70. ACCOMPLISHED HFEC OF FASTENER HOLES COMMON TO REPAIR. NO CRACKS FOUND. FABRICATED AND INSTALLED FLOORBEAM REPAIR CHORD, REPAIR ANGLES AND REPAIR STRAPS REF SRM 53-10-08 REPAIR NR 2.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 71,818 hrs · 26,907 cycles

CORROSION ON FLOORBEAM STA 1640, BL 0 - RBL 50. SUPPLEMENTAL DATA UPDATE, CORROSION ON FLOORBEAM AT STA 1640. REMOVED PER ECRA 5360-01218.

Part: ACTUATOR — FAULTY (MASK DOOR LATCH) · airframe 71,818 hrs · 26,907 cycles

OXYGEN MASK AT SEAT 3-E, F DID NOT DEPLOY. REMOVED AND REPLACED DOOR LATCH ACTUATOR IAW AMM, OPS CHECKED GOOD IAW 53-21 -00.

Part: SKIN — DENTED (BS 750) · airframe 71,818 hrs · 26,907 cycles

DENT IN SKIN ON LEFT SIDE OF ACFT AT BS 750 JUST AFT AND BELOW OF MID LAV SERVICE PANEL. DENT IS ABOUT 2 AND 1-2 INCHES IN DIAMETER BY 3-32 INCH DEEP. OPENED PIT, FOUND NO CRACKS OR PULLED RIVETS. HFEC AREA AND NO CRACKS FOUND. DENT IS WITHIN SRM 53-00-01 LIMITS. REPAIRED PER ECRA 5330-04295.

Part: SKIN — DENTED (BS 745-765) · airframe 71,818 hrs · 26,907 cycles

SKIN BETWEEN BS 745-765 AND BETWEEN S25-27L. REPAIRED IAW ECRA 5330-04295.

Part: SKIN — DAMAGED (BS 417) · airframe 71,818 hrs · 26,907 cycles

EXTERIOR FUSELAGE BLENDED AREA OUT OF LIMITS BS 417 ABOVE STR 22L. CUT OUT DAMAGE AREA IAW SRM 53-00-01. PERFORMED HFEC IAW NDT MANUAL PART 6 51-00-19. FABRICATED DOUBLER IAW SRM 53-00-01. MATCH DRILLED DOUBLER IAW SRM 53-40-05. INSTALLED DOUBLER IAW SRM 51-40-02 AND 53-00-01.

Part: PRESSURE DECK — CORRODED (BS 1680-1720) · corrosion level 2 · airframe 71,818 hrs · 26,907 cycles

CORROSION ON PRESSURE DECK PLATE STA 1680 - 1720, RBL 45. REMOVED CORROSION PER SRM 51-21-03. PERFORMED HFEC REF 757 NDT 51-00-19 PARTS 6 AND 7. FABRICATED REPAIR DOUBLER IAW ECRA 5330-04259 STEPS 11-14. INSTALLED REPAIR DOUBLER IAW ECRA 5330-04259 STEPS 17-19. RESTORED EXTERIOR FINISHES IAW ECRA 5330-04259 STEPS 16, 17, 20 AND 21.

Part: SKIN — DAMAGED (BS 417 S22L) · airframe 71,818 hrs · 26,907 cycles

EXTERIOR FUSELAGE PREVIOUS BLENDED AREA OUT OF LIMITS BS 417 ABOVE S22L. CUT OUT DAMAGE AREA IAW SRM 53-00-01. PERFORMED HFEC IAW NDT MANUAL PART 6 51-00- 19. FABRICATED DOUBLER IAW SRM 53-00-01. MATCH DRILLED DOUBLER IAW SRM 53-40-05.

Part: DECK PLATE — CORRODED (BS 1680-1720) · corrosion level 2 · airframe 71,818 hrs · 26,907 cycles

CORROSION ON PRESSURE DECK PLATE STA 1680 - 1720, RBL 45. REMOVED CORROSION PER SRM 51-21-03. PERFORMED HFEC REF 757 NDT 51-00-19 PARTS 6 AND 7. FABRICATED REPAIR DOUBLER IAW ECRA 5330-04259 STEPS 11-14. INSTALLED REPAIR DOUBLER IAW ECRA 5330-04259 STEPS 17-19. RESTORED EXTERIOR FINISHES IAW ECRA 5330-04259 STEPS 16, 17, 20 AND 21.

Part: SKIN — DAMAGED (BS 425 S23-24L) · airframe 71,818 hrs · 26,907 cycles

EXTERIOR FUSELAGE PREVIOUS BLENDED AREA OUT OF LIMITS BS 425 STR 23-24L. CUT OUT DAMAGE AREA PER SRM 53-00-01. PERFORMED HFEC PER NDT MANUAL PART 6 51-00-19. FABRICATED DOUBLER AND FILLER IAW SRM 53-00-01 DETAIL I. LOCATED AND DRILLED DOUBLER IAW SRM 51-40-05. INSTALLED DOUBLER IAW SRM 51-40-02 AND 53-00-01 REPAIR NR 7.

Part: SKIN — DAMAGED (BS 425) · airframe 71,818 hrs · 26,907 cycles

EXTERIOR FUSELAGE BLENDED AREA OUT OF LIMITS BS 425 STR 23-24L. CUT OUT DAMAGE AREA PER SRM 53-00-01. PERFORMED HFEC PER NDT MANUAL PART 6 51-00-19. FABRICATED DOUBLER AND FILLER IAW SRM 53-00-01 DETAIL I. LOCATED AND DRILLED DOUBLER IAW SRM 51-40-05. INSTALLED DOUBLER IAW SRM 51-40-02 AND 53-00-01 REPAIR NR 7.

Part: SKIN — DENTED (BS 500) · airframe 71,818 hrs · 26,907 cycles

A 2 FT DENT AFT OF L1 DOOR APPROX 5 WINDOWS BACK, APPROX BS 500 JUST ABOVE FLOOR LEVEL. ACCOMPLISHED NDT FOR CRACKS AND MATERIAL LOSS. NO CRACKS FOUND. MATERIAL LOSS WITHIN LIMITS OF SRM 53-00-01.

Part: PRESSURE DECK — CORRODED (BS 1681) · corrosion level 2 · airframe 71,818 hrs · 26,907 cycles

CORROSION ON PRESSURE DECK NUT PLATES BS 1681, RBL 5 - RBL 35. REMOVED CORROSION PER SRM AT STA 1680 RBL 31. REMAINING THICKNESS MEASURES .056-. 057, AREA FOUND TO BE OUT OF LIMITS PER SRM. FABRICATED REPAIR DOUBLER PER ECRA 5330-04259 STEPS 11-14. INSTALLED REPAIR DOUBLER PER ECRA 5330-04259 STEP 17-19. RESTORED EXTERIOR FINISH PER ECRA 5300-04259 STEPS 16-17 AND 20-21. TASK ACCOMPLISHED.

Part: DECK PLATE — CORRODED (BS 1681) · corrosion level 2 · airframe 71,818 hrs · 26,907 cycles

CORROSION ON PRESSURE DECK NUT PLATES BS 1681, RBL 5 - 35. REMOVED CORROSION PER SRM 51-21-03. REMAINING THICKNESS MEASURES .056-. 057. AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-51 DETAIL VI. FABRICATED REPAIR DOUBLER PER ECRA 5330-04259 STEPS 11-14. INSTALLED REPAIR DOUBLER PER ECRA 5330-04259 STEP 17-19. RESTORED EXTERIOR FINISH PER ECRA 5300-04259 STEPS 16-17 AND 20-21.

Part: SKIN — DAMAGED (BS 448-458 S22-2) · airframe 71,818 hrs · 26,907 cycles

EXTERIOR FUSELAGE PREVIOUS BLENDED AREA OUT OF LIMITS AT BS 448-458 S22-23L. CUT OUT DAMAGE AREA OUT IAW SRM 53-00-01. PERFORMED HFEC SURFACE AREA IAW NDT MANUAL PER PART 6 51-00-19. FABRICATED DOUBLER IAW SRM 53-00-01. DRILLED DOUBLER IAW SRM 51-40-05.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 71,818 hrs · 26,907 cycles

LEFT HORIZONTAL STABILIZER, UPPER SKIN PANEL BETWEEN FRONT SPAR AND AUX SPAR FROM FUSELAGE TO OTBD TIP HAS NUMEROUS DENTS APPROX 6 PER SQUARE FOOT. THERE WERE NO DEFECTS NOTED. SANDED, FILLED, SANDED, PRIMED AND PAINTED LT STAB UPPER SURFACE. ACCOMPLISHED EVA-81043, AND EVA-81044.

Part: SKIN — DAMAGED (BS 448-458) · airframe 71,818 hrs · 26,907 cycles

EXTERIOR FUSELAGE BLENDED AREA OUT OF LIMITS AT BS 448-458 STR 22-23L. CUTOUT DAMAGE AREA OUT IAW SRM 53-00-01. PERFORMED HFEC SURFACE AREA IAW NDT MAN UAL PER PART 6 51-00-19. FABRICATED DOUBLER IAW 53-00-01. DRILLED DOUBLER IAW SRM 51-40-05. INSTALLED DOUBLER IAW SRM 51-40-02.

Part: SKIN — DENTED (BS 1704 S15R) · airframe 71,818 hrs · 26,907 cycles

SKIN DENT BS 1704 AT STR 15R. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED SKIN, ACCOMPLISHED HFEC REF NDT PT6, 53-00-01, VERIFIED NO CRACKS. INSTALLED DOUBLER FILLER REPAIR PER 53-00-01 RPR 2, AND 51-40-02.

Part: STARTER — FAULTY (RT ENGINE) · airframe 71,504 hrs · 26,794 cycles

RIGHT ENGINE VERY SLOW TO START N2 ONLY REACHES 22-23 PERCENT TWO CONSECUTIVE LEGS SEPARATE IGNITES. REPLACED STARTER & STARTER VALVE. SERVICE ACCOMPLISHED, OK TO CONTINUE.

Part: WINDOW — CONTAMINATED (CABIN) · airframe 70,994 hrs · 26,621 cycles

WINDOW AT EMERGENCY EXIT 20F HAS CONDENSATION BETWEEN PANES OBSTRUCTING VIEW. REPLACED WINDOW ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,972 hrs · 26,613 cycles

FWD COAT CLOSET AND MID LAV EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT STRIPS.

Part: CONNECTOR — MISSING (EMERGENCY LIGHTS) · airframe 70,972 hrs · 26,613 cycles

FLOOR EMERGENCY LIGHTS FROM OVERWING EXITS AFT TO THE AFT LAV INOPERATIVE. FOUND CONNECTOR MISSING. INSTALLED CONNECTOR, OPS CHECKED NORMAL.

Part: FLAP — DENTED (RT WING) · airframe 70,570 hrs · 26,463 cycles

RIGHT O/B TRAILING EDGE FLAP DENTED OR PUNCTURED AT WBL 564 AND 4IN FROM T/E FLAP NEEDS TO BE REMOVED AND ROUTED TO SHOP FOR GRAPHITE REPAIR PER SM. INTERIM REPAIRED WITH TAPE. WITHIN LIMITS SRM. TO BE REPAIRED AT C CHECK. FLAP REPLACED.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 70,570 hrs · 26,463 cycles

RT TRAILING EDGE FLAP HAS PUNCTURE WBL 351 X 6.7\ FROM TRAILING EDGE. FLAP NEEDS TO GO TO SHOP FOR REPAIR. FOUND A 10"X10" DELAMINATION ON RT OUTBOARD FLAP LOWER SKIN ON INBOARD SIDE OF NR 3 CANOO 8" FROM BOTTOM & 37" FROM THE EDGE. PICTURES WILL BE POSTED ON THE RVI SITE. SERVICEABLE AFT FLAP INSTALLED ON SFOOV WU E8377H AT SMB PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,570 hrs · 26,463 cycles

RIGHT O/B TRAILING EDGE FLAP DENTED OR PUNCTURED AT WBL 433 AND 9.5IN FROM TRAILING EDGE FLAP NEEDS TO BE REMOVED AND ROUTED TO SHOP FOR REPAIR. FLAP NEEDS TO GO TO SHOP FOR REPAIR. FOUND A 10"X10" DELAMINATION ON RT OUTBOARD FLAP LOWER SKIN ON INBOARD SIDE OF NR 3 CANOO 8" FROM BOTTOM & 37" FROM THE EDGE. PICTURES WILL BE POSTED ON THE RVI SITE. SERVICEABLE AFT FLAP INSTALLED ON SFOOV WU E8377H AT SMB PER MM.

Part: SKIN — DENTED (TE FLAP) · airframe 70,570 hrs · 26,463 cycles

RIGHT O/B TRAILING EDGE FLAP DENTED OR PUNCTURED AT WBL 503.5 AND 8IN FROM T/E FLAP NEEDS TO GO TO SHOP FOR REPAIR. FOUND A 10"X10" DELAMINATION ON RT OUTBOARD FLAP LOWER SKIN ON INBOARD SIDE OF NR 3 CANOO 8" FROM BOTTOM & 37" FROM THE EDGE. PICTURES WILL BE POSTED ON THE RVI SITE. SERVICEABLE AFT FLAP INSTALLED ON SFOOV WU E8377H AT SMB PER MM.

Part: SKIN — DENTED (TE FLAP) · airframe 70,570 hrs · 26,463 cycles

RIGHT O/B TRAILING EDGE FLAP DENTED OR PUNCTURED AT WBL 406 AND 6.5IN FROM TRAILING EDGE. FLAP NEEDS TO BE REMOVED AND ROUTED TO SHOP FOR REPAIR. FLAP NEEDS TO GO TO SHOP FOR REPAIR. FOUND A 10"X10" DELAMINATION ON RT OUTBOARD FLAP LOWER SKIN ON INBOARD SIDE OF NR 3 CANOO 8" FROM BOTTOM & 37" FROM THE EDGE. PICTURES WILL BE POSTED ON THE RVI SITE. SERVICEABLE AFT FLAP INSTALLED ON SFOOV WU E8377H AT SMB PER MM.

Part: SKIN — DENTED (TE FLAP) · airframe 70,570 hrs · 26,463 cycles

RIGHT O/B TRAILING EDGE FLAP DENTED OR PUNCTURED AT WBL 541.5 AND 1.5 FROM T/E FLAP NEEDS TO GO TO SHOP FOR REPAIR. FOUND A 10"X10" DELAMINATION ON RT OUTBOARD FLAP LOWER SKIN ON INBOARD SIDE OF NR 3 CANOO 8" FROM BOTTOM & 37" FROM THE EDGE. PICTURES WILL BE POSTED ON THE RVI SITE. SERVICEABLE AFT FLAP INSTALLED ON SFOOV WU E8377H AT SMB PER MM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 70,570 hrs · 26,463 cycles

RT TRAILING EDGE FLAP HAS PUNCTURE WBL 349 X 9.5" FROM TRL EDGE. FLAP NEEDS TO GO TO SHOP FOR REPAIR. FOUND A 10"X10" DELAMINATION ON RT OUTBOARD FLAP LOWER SKIN ON INBOARD SIDE OF NR 3 CANOO 8" FROM BOTTOM & 37" FROM THE EDGE. PICTURES WILL BE POSTED ON THE RVI SITE. SERVICEABLE AFT FLAP INSTALLED.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 70,570 hrs · 26,463 cycles

RIGHT OTBD TRAILING EDGE FLAP HAS PUNCTURE WBL 364 X 9" FROM TRAILING EDGE. FLAP NEED TO GO TO SHOP FOR REPAIR. FLAP NEEDS TO GO TO SHOP FOR REPAIR. FOUND A 10"X10" DELAMINATION ON RT OUTBOARD FLAP LOWER SKIN ON INBOARD SIDE OF NR 3 CANOO 8" FROM BOTTOM & 37" FROM THE EDGE. PICTURES WILL BE POSTED ON THE RVI SITE. SERVICEABLE AFT FLAP INSTALLED ON SFOOV WU E8377H AT SMB PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,570 hrs · 26,463 cycles

RIGHT O/B TRAILING EDGE FLAP DENTED OR PUNCTURED AT WBL 547 AND 5IN FROM T/E FLAP NEEDS TO GO TO SHOP FOR REPAIR. FOUND A 10"X10" DELAMINATION ON RT OUTBOARD FLAP LOWER SKIN ON INBOARD SIDE OF NR 3 CANOO 8" FROM BOTTOM & 37" FROM THE EDGE. PICTURES WILL BE POSTED ON THE RVI SITE. SERVICEABLE AFT FLAP INSTALLED ON SFOOV WU E8377H AT SMB PER MM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 70,570 hrs · 26,463 cycles

RT OTBD TRAILING EDGE FLAP HAS PUNCTURE WBL 347 9" UP FROM TRAILLING EDGE. FLAP NEEDS TO BE ROUTED TO SHOP FOR FOR REPAIR. *SUPPLEMENTAL DATA UPDATE* FOUND A 10"X10" DELAMINATION ON RT OUTBOARD FLAP LOWER SKIN ON INBOARD SIDE OF #3 CANOO 8" FROM BOTTOM & 37" FROM THE EDGE. PICTURES WILL BE POSTED ON THE RVI SITE. SERVICEABLE AFT FLAP INSTALLED ON SFOOV WU E8377H AT SMB PER MM.

Part: SKIN — DENTED (TE FLAP) · airframe 70,570 hrs · 26,463 cycles

RIGHT O/B TRAILING EDGE FLAP DENTED OR PUNCTURED AT WBL 473 AND 4IN FROM TRAILING EDGE. FLAP NEEDS TO BE REMOVED AND ROUTED TO SHOP FOR REPAIR. FOUND A 10"X10" DELAMINATION ON RT OUTBOARD FLAP LOWER SKIN ON INBOARD SIDE OF NR 3 CANOO 8" FROM BOTTOM & 37" FROM THE EDGE. PICTURES WILL BE POSTED ON THE RVI SITE. SERVICEABLE AFT FLAP INSTALLED ON SFOOV WU E8377H AT SMB PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,514 hrs · 26,439 cycles

FOUND A 10"X10" DELAMINATION ON RT OUTBOARD FLAP LOWER SKIN ON INBOARD SIDE OF NR 3 CANOE 8" FROM BOTTOM & 37" FROM THE EDGE. INTERIM REPAIRED WITH TAPE. WITHIN LIMITS SRM. TO BE REPAIRED AT C CHECK. FLAP NEEDS TO BE RMV'D & ROUTED TO SHOP FOR GRAPHITE REPAIR PER SM. SERVICEABLE AFT FLAP INSTALLED. TEST FLIGHT GOOD FOR FLAP REPAIRS.

Part: SINK — UNKNOWN (LAVATORY) · airframe 70,019 hrs · 26,246 cycles

FWD GALLEY FLOODED WITH WATER. FOUND AN EXCESSIVE AMOUNT OF LIQUID DUMPED THRU FWD GALLEY TRASH SHOOT LEAKING DOWN THE SIDE OF TRASH CONTAINER. TRASH CAN LINER WAS NOT INSTALLED PROPERLY CAUSING FLUID TO LEAK ON THE SIDES OF THE TRASH CAN AND DOWN TO THE FLOOR LEVEL OF THE TRASH CAN COMPARTMENT. LAVATORY TOILET BOWL OVERFLOWING AT DR-2L AFT-CBN LAV. FWD AND MID LAVS OVERFLOWED ON TAKEOFF. MID LAV SINK DRAIN PLUGGED. FULL OF COFFEE GROUND AND WINE. FWD LAV SINK OK AND FWD TOILET OK 98909. SHOULD READ FWD LAV SINK OK, FWD AND MID TOILETS OK, ISSUE IS WITH MIDS LAV SINK. SHOULD READ FWD AND MID TOILETS OK. FWD LAV SINK OK. ISSUE IS WITH MID LAV SINK.

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 69,329 hrs · 25,985 cycles

HYDRAULIC LEAK NR 1 ENGINE. LOWER RIGHT REVERSER ACT LEAKS 10 DROPS PER CYCLE. NR 1 ENGINE ACT NEED REPLACEMENT PCN 152-9609 OK TO CONT 75 FLT. 18AUG ORD CQT- SHOULD READ 10 DROPS PER MIN. CLEANED ALL THREE RT ACTUATORS. CYCLED NR 1 ENG REVERSER 10 TIMES. NO ACTIVE LEAK NOTED.

Part: POWER CABLE — DISCONNECTED (CABIN) · airframe 69,208 hrs · 25,945 cycles

EMERGENCY FLOOR LIGHTING NEXT TO ROW 6 IS UNPLUGGED. RECONNECTED EEL PWR RIBBON & SECURED PLASTIC COVER AND END CAP. LIGHT STRIP CHECK'S GOOD.

Part: LAMP — INOPERATIVE (L1 DOOR SLIDE) · airframe 69,132 hrs · 25,918 cycles

DOOR 1L SLIDE LIGHT DOES NOT ILLUMINATE WHEN DOOR ARMED, 1L GIRT BAR VERIFIED ENGAGED. RELAMPED, LIGHT CHECKED GOOD.

Part: STRUCTURE — DAMAGED (SPOILER) · airframe 71,818 hrs · 26,907 cycles

NR 12 SPOILER HAS A HOLE. REPAIRED NR 12 SPOILER PER SRM 51-70-17.

Part: UNKNOWN — DAMAGED · airframe 69,116 hrs · 25,910 cycles

HAIL DAMAGE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 68,747 hrs · 25,779 cycles

MCP DISPLAY ISSUE, FLIGHT DIVERTED.

Part: WIRE — BURNED (GIRT BAR) · airframe 68,673 hrs · 25,742 cycles

DOOR2L SLIDE ARM LIGHT NOT ILLUMINATING WHEN DOOR IS ARMED. ON COMPLETION OF LM8651, FOUND BURNT WIRES ON FWD GIRT BAR PROXIMITY SWITCH. REPAIRED WIRE WITH ENVIRONMENT SPLICE. OPS CHECK SLIDE LIGHT GOOD.

Part: A/C PACK — NOISY (AC BAY) · airframe 67,534 hrs · 25,337 cycles

COCKPIT NOISE INFLIGHT. CREW INFLIGHT TROUBLESHOOTING FOUND THAT LT PACK WAS ALSO CAUSING PROBLEM, SEE DF842. CLEANED CTR AIR NOZZLE ASSY 23 AFT, ALL CLOGGED RESTRICTOR PLATES AND REPLACED RECIRC FAN FILTERS. FLT DECK NOISE 70 DB WITH LT FAN ON AND 72 WITH BOTH ON AND BOTH ENGINES RUNNING. RECIRC FAN IS LIKELY CULPRIT. STICKERED SWITCH PER MT 21-22-00 NOISE LEVEL WITHIN LIMITS.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 67,039 hrs · 25,147 cycles

END STOP PIECE THAT SECURES EMERGENCY LIGTH STRIP IS MISSING IN FIRST CLASS CABIN LEFT SIDE. CREW REPORTS THE MISSING PIECE WILL BE ON THE CENTER CONSOLE IN COCKPIT. REINSTALLED EMERGENCY LIGTH STRIP AND END PIECE.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 66,856 hrs · 25,083 cycles

CABIN FLOOR SOFT IN AISLE AT ROW 13. REMOVED PANEL IS IN CONTROL CTR 9 EA SCREWS ON AOG P1720. PANEL AOG'D H4896 1505 ETA INSTALLED NEW FLOOR PANEL.

Part: SKIN — DENTED (BS 418 S19-20L) · airframe 66,473 hrs · 24,941 cycles

EXT FUSELAGE AT BS 418, BETWEEN STR. 19 AND 20L IS DENTED. MAJOR REPAIR ACCOMPLISHED: FOUND DENT TO BE OUT OF LIMITS. REMOVED DAMAGED AREA ACCOMPLISHED HFEC FOR DAMAGE CUT-OUT AND FASTENER HOLES, NO CRACKS NOTED. FABRICATED AND INSTALLED A REPAIR DOUBLER AND FILLER. REPAIR NR 3 ACCOMPLISHED ON NON ROUTINE 2264N00104.

Part: SKIN — DENTED (BS 1473 S28-29R) · airframe 66,308 hrs · 24,874 cycles

DENT IN FUSELAGE ADJACENT TO AFT LOWER VHF ANTENNA. NOTE DEPTH, SIZE, ADJACENT STRUCTURE, RIVETS AND MARKINGS. DENT MEASURES 2.75 IN WIDE BY 5.5 IN LONG. DEPTH IS APPROX .062 AT STA 1473 BETWEEN S28R AND S29R. NO GOUGES, CRACKS OR LOOSE FASTENERS. LOCATED 7IN FROM CTR VHF ANT CUTOUT. ACP HFEC CK ON EXT SKIN OF INDICATED AREA=NO CRKS DETECTED. THIS ITEM IS TO BE RE-EVALUATED AT THE NEXT C-CHECK.

Part: SLIDE — FAULTY (OVERWING)

POROSITY ON SLIDE, FAILED AIR RETENTION TEST. SENT OT OEM FOR EVALUATION AND REPAIR OR INFLATABLE REPLACEMENT.

Part: FAN — FAULTY (RECIRCULATION) · airframe 65,184 hrs · 24,442 cycles

ODOR IN CABIN, RTFL. RT RECIRCULATION FAN SHOULD BE REPLACED. REPLACED RT RECIRCULATION FAN, OPS CHECKS OK. REPLACED RT CHECK VALVE LT, OK. REPLACED BOTH FILTERS. RT RECIRCULATION FAN AIR FILTER EXHIBITED SIGNS OF FAILURE WHEN REPLACED. CHECKED THE DUCTING AND MIX MANIFOLD. FOUND LT AIR CHECK VALVE INOP. REPLACED VALVE. RT CHECK VALVE OK.

Part: BLEED VALVE — FAULTY (RT ENGINE) · airframe 64,887 hrs · 24,322 cycles

RT ENG BLEED, FLIGHT DIVERTED. PNEUMATIC HEALTH CK ON NR 2 ENG ON THE FOLLOWING COMPONENTS IAW MM: HPC- HPSOV, PRC-PRSOV, FAMV. DURING ACCOMPLISHMENT OF HEALTH CK ON RT HI STAGE PILOT, SOLENOID FAILED TO CLOSE WHEN PINS 1181695 AND 6 WERE ENERGIZED. R & R NR 2 ENG HI-STAGE PILOT IAW MM. RE-ACCOMPLISHED HEALTH CK, TEST GOOD. ALSO DURING HEALTH CK OF FAMV VALVE FAILED REF PRESSURE (READING WAS 24 PSI). R & R FAMV ON NR 2 ENG IAW MM. RE-ACCOMPLISHED HEALTH CK ON NEW FAMV, TEST GOOD. RAN NR 2 ENG AND BLEED INDICATIONS AT IDLE WERE 18PSI AND BLEED TURNED OFF WHEN SWITCH SELECTED TO "OFF". FOUND ALL SENSE LINES SECURED AND NONE LEAKING.

Part: SEQUENCE VALVE — FAILED (NLG) · airframe 64,627 hrs · 24,224 cycles

NLG DID NOT EXTEND IN FLT. RAN ALT EXTEND CHECKLIST & GOT GREEN LIGHTS. NORMAL LANDING. REPLACED NLG SEQUENCE VALVE. AFTER REPLACEMENT OF SEQUENCE VALVE ACCOMPLISHED NOSE GEAR EXTENSION AND RETRACTION TEST NUMEROUS TIMES AND GEAR. OPS CHECKED NORMAL. NO LEAKS AT VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,695 hrs · 23,871 cycles

TWO (2) FOOT STRIP OF EMERGENCY EXIT LIGHTS OUT NEAR ROW 13C. REPLACED A STRIP OF EMERGENCY EXIT LIGHTS NEAR ROW 13C.

Part: MICROPHONE — INOPERATIVE (O2 MASK) · airframe 63,583 hrs · 23,826 cycles

F/O O2 MASK MICROPHONE INOPERATIVE. REPLACED F/O'S OXYGEN MASK, OPS CHECKS GOOD.

Part: CAP — LOOSE (CABIN) · airframe 63,362 hrs · 23,741 cycles

EMERGENCY EXIT LIGHTING AT ROW 6B NEEDS TO BE SECURED. SECURED END CAP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,328 hrs · 23,728 cycles

OVERWING EMERGENCY EXIT LIGHTS L810, L779 AND L780 DO NOT ILLUMINATE. REPLACED BATTERY PACK AT M10568, BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,119 hrs · 23,652 cycles

DOOR 2R SLIDE LIGHT INOPERATIVE. CREW RELAMPED BULBS, CHECKS OKAY.

Part: SLIDE — UNSERVICEABLE (DOOR 2R) · airframe 62,939 hrs · 23,579 cycles

UNABLE TO ARM DOOR 2R. REPLACED SLIDE PACK FOR DOOR 2R.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,886 hrs · 23,560 cycles

AFT FWD LAV JUST FWD OF DOOR EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,886 hrs · 23,560 cycles

MID LAV JUST FWD OF DOOR EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT STRIP.

Part: BATTERY — SMOKE (APU) · airframe 60,263 hrs · 22,540 cycles

SMOKE DETECTED IN AFT GALLEY BY OUTBD FA GATE. MECH IN COCKPIT TURNED OFF PWR TO AC. FOUND APU BATTERY SMOLDERED. REPLACED APU BATTERY & APU BATTERY CHARGER. ALL CHKS NORMAL.

Part: CONTROL PANEL — MALFUNCTIONED · airframe 60,171 hrs · 22,506 cycles

ON APPROACH NO LIGHTS ON RIGHT SIDE OF ANY SELECTED MCP BUTTONS AND FLIGHT DIR WOULD NOT CAPTU. *S/D* MCP FAILED. REPLACED MCP. ALL L-C-R AUTOFLIGHT LAND CAT III TESTS PASSED.

Part: GIRT BAR — CLOGGED (DOOR 1R) · airframe 59,205 hrs · 22,158 cycles

1R DOOR WILL NOT ARM. SUPPLEMENTAL DATA UPDATE CAUSE, DEBRIS UNDER GIRT BAR. REMOVED DEBRIS AND CLEANED SWITCHES, OPS CHECKS OK, ARMS/DISARMS NORMALLY.

Part: DOOR — OUT OF RIG (L2) · airframe 58,727 hrs · 21,988 cycles

DOOR 2 LEFT UNABLE TO ARM, FOUND DOOR OUT OF RIG. FOUND UPPER AND LOWER JAMB NUTS ON TORQ TUBE LOOSE. ON INSP FOUND TANG WASHER INSTALLED INCORRECTLY. LOWER GATE IS STRIKING DOOR THRESHOLD UPON DOOR CLOSURE. BY- 124277 :LOWER JAM NUT LOCK WASHER IS INSTALLED UPSIDE DOWN. LOCK WASHER IS NOW INEFFECTIVE AND WILL NOT SECURE LOWER JAM NUT. AS DOOR IS OPENED AND CLOSED LOWER JAM NUT WORKS LOOSE AND DOOR BEGINS TO SAG AGAIN. DOOR REMOVED FROM A/C AND RE-RIGGED, REWORKED JAMB WASHER. DOOR INSTALLED AND OPENS AND CLOSES PROPERLY.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 58,723 hrs · 21,987 cycles

EEL STRIP INOP IN FRONT OF MID AFT LAV. CAUSE, DAMAGED WIRING FROM UNKNOWN SOURCE. SPLICED WIRE ON EEL STRIP. OPS CHECKED OK.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,629 hrs · 21,953 cycles

FWD PIT, LEFT SIDE STA 660 BETWEEN STR 25 AND 26L, MAIN FRAME HAS DENT INTO RADIUS UPPER BEND. ACCOMPLISHED A MAJOR REPAIR AT ORD.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,629 hrs · 21,953 cycles

FORWARD PIT, LT SIDE, STA 580 BETWEEN STR 24L AND 25L, MAIN FRAME IS DENTED 3 PLACES, WITH ONE INTO FRAME UPPER RADIUS BEND. ACCOMPLISHED MAJOR REPAIR AT ORD.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 58,181 hrs · 21,792 cycles

LIGHTNING STRIKE AT STA 445, STRINGER 7L, IS BEYOND ALLOWABLE LIMITS. ACCOMPLISHED MAJOR REPAIR.

Part: CONNECTOR — BROKEN (CABIN) · airframe 57,898 hrs · 21,693 cycles

FOUND EEL LIGHT CONNECTOR BROKEN AT SEAT 13A. REPLACED EEL CONNECTOR STRIP- OPS CHECKED NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,762 hrs · 21,654 cycles

FLOOR EEL LIGHT INOP AT MID LAV. REPLACED MID LAV EEL STRIP, OPS CHECKED NORMALLY.

Part: O-RING — UNSERVICEABLE (SLIDE)

LOW BOTTLE PRESSURE. REPLACED O-RING

Part: SLIDE — READS LOW (R4 DOOR) · airframe 57,251 hrs · 21,462 cycles

FOUND DOOR 4R SLIDE PRESSURE IS LOW.

Part: SLIDE — FAULTY (R4 DOOR) · airframe 57,223 hrs · 21,451 cycles

FOUND DOOR 4R SLIDE DIFFICULT TO ARM.

Part: LIGHT — INOPERATIVE (R3 DOOR SLIDE) · airframe 57,223 hrs · 21,451 cycles

FOUND SLIDE ARM LIGHT NOT ON AT 3R.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,785 hrs · 21,289 cycles

FOUND DOOR 3L EXTERIOR EMERGENCY LIGHT INOP. REPLACED LAMP.

Part: TERMINAL BLOCK — BURNED · airframe 56,513 hrs · 21,185 cycles

FOUND BUNDY BLOCK BURNED AND DETERIORATED AT TB0158A POSITION 12. REF WDM76-11-11 PG 2A BETWEEN S37 L ENG FIRE SWITCH AND P36. DIODE IS LOCATED IN FWD E&E UNDER P8 CONTROL STAND, RIGHT SIDE, MOUNTED JUST BELOW FLOOR LEVEL ABOVE DOOR. 09-14-07 SUSPECT DAMAGED AISLE STANDBY LIGHTING RELAY. REPLACED DIODE BLOCK AT TB59 POS 12.

Part: OVEN — SPARKS (GALLEY) · airframe 55,988 hrs · 20,986 cycles

FIRST CLASS OVEN NR 107 ELECTRICAL SPARKS FROM BEHIND. TURNED OFF, NO MORE SPARKS. [06-20-07] NO DAMAGE TO AC WIRING NOTED, FOUND GUIDE PIN PUSHED INTO OVEN. REPLACED CONVECTION OVEN,

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,803 hrs · 20,921 cycles

RIGHT MAIN CABIN FLOOR STRUCTURE, EVIDENCE OF CORROSION BETWEEN FLOOR WEB AND SUPPORT ANGLE, BS 1681, RBL 34. MAJOR REPAIR ACCOMPLISHED: REMOVED ENTIRE LENGTH OF DAMAGED FLOORBEAM T-CAP. FABRICATED & INSTALLED REPLACEMENT CHORD.

Part: LEVER — STIFF (L1 DOOR) · airframe 55,803 hrs · 20,921 cycles

DOOR 1L DOES NOT ARM, LEVER IS STIFF. [SUP 06-06-07] GIRT BAR LIFT SPRING WAS JAMMED REPLACED LEFT DOOR GIRT BAR AND BAR LOCK AND REPLACED LEFT DOOR ASSIST BOTTLE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 55,801 hrs · 20,920 cycles

F-C EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED POWER INVERTER. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,801 hrs · 20,920 cycles

R-1 EXTERIOR EMERGENCY LIGHT IS INOP. [SUP 05-16-07] RELAMPED.

Part: SWITCH — DAMAGED (CABIN) · airframe 55,801 hrs · 20,920 cycles

EMERGENCY LIGHTS TEST SW S10295 BY L-4 DOOR HAS BROKEN TERMINALS. [SUP 06-06-07] REPLACED SWITCH.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 55,801 hrs · 20,920 cycles

R-2 DOOR FRAME IS CRACKED AT UPPER HINGE CUTOUT, .25 INCH LONG, FOUND AT THE 7 O'CLOCK POSITION. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA. FABRICATED & INSTALLED A CRES DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,801 hrs · 20,920 cycles

FWD PIT, LEFT SIDE, STA 580 BETWEEN STR 24L AND 25L, MAIN FRAME IS DENTED 3 PLACES, WITH ONE INTO FRAME UPPER RADIUS BEND. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE. COLD WORK HOLES & INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,801 hrs · 20,920 cycles

FWD PIT, LEFT SIDE STA 660 BETWEEN STR 25 AND 26L, MAIN FRAME HAS DENT INTO RADIUS UPPER BEND. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE. COLD WORKED HOLES & INSTALLED J-ANGLE REPAIR.

Part: WIRE — DAMAGED (CABIN) · airframe 55,801 hrs · 20,920 cycles

EEL BASE WIRE AT STA 1600 DAMAGED. REPLACED DAMAGED WIRE.

Part: LIGHT — BROKEN (CABIN) · airframe 55,801 hrs · 20,920 cycles

EEL LIGHT BAR BROKEN STA 740. REPLACED LIGHT BAR.

Part: STRUCTURE — CRACKED (L2 DOOR) · airframe 55,801 hrs · 20,920 cycles

DOOR 2L HAS HALF INCH CRACK AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. INSTALLED CRES DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,801 hrs · 20,920 cycles

AFT PIT STA 1540 LT AT STR 25L, FRAME IS DENTED ON INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE. INSURANCE CUT & INSTALLED "J" ANGLE REPAIR.

Part: CABLE — FROZEN (EVAC SLIDE) · airframe 55,801 hrs · 20,920 cycles

RT OVERWING SLIDE, MANUAL BACKUP CABLE IS FROZEN. [SUP 06-06-07] REPLACED CABLE, AND THE NON-FUNCTIONAL CABLE HAS BEEN THE ROOT CAUSE OF THE PROBLEM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,801 hrs · 20,920 cycles

MAIN CABIN STR 15L CRACKED STA 680. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED STRINGER. FABRICATED & INSTALLED NEW CHORD.

Part: BEAM — CRACKED (BS 680) · airframe 55,801 hrs · 20,920 cycles

MAIN CABIN STUB BEAM CRACKED STA 680 JUST ABOVE 10 INCH STR 13L. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED WEB. FABRICATED & INSTALLED NEW WEB.

Part: BEAM — CRACKED (BS 680 S13R) · airframe 55,801 hrs · 20,920 cycles

MAIN CABIN, STUB BEAM CRACKED STA 680, 10 INCH ABOVE STR 13R. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED WEB. FABRICATED & INSTALLED NEW WEB.

Part: BEAM — CRACKED (BS 680 S11R) · airframe 55,801 hrs · 20,920 cycles

MAIN CABIN, STUB BEAM CRACKED STA 680, 5 INCH BELOW STR 11R. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED WEB. FABRICATED & INSTALLED NEW WEB.

Part: GATE — DAMAGED (L-4 DOOR UPPER) · airframe 55,801 hrs · 20,920 cycles

L-4 DOOR UPPER GATE CORRODED AND CRACKED. [SUP 05-04-07] REPLACED UPPER GATE.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 55,801 hrs · 20,920 cycles

RT MAIN CABIN FLOORBEAM, UPPER CHORD HAS CORROSION BEYOND LIMITS, BS 1640, BETWEEN LBL10 TO RBL 87. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED CHORD. FABRICATED & INSTALLED NEW CHORD.

Part: BEAM — CRACKED (BS 680) · airframe 55,801 hrs · 20,920 cycles

MAIN CABIN STUB BEAM CRACKED STA 680, JUST BELOW 5 INCH STR 11L. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED WEB. FABRICATED & INSTALLED NEW WEB.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,801 hrs · 20,920 cycles

LEFT FUSELAGE SKIN HAS 2 EA DENTS WITHIN 1 INCH OF EACH OTHER STA 1510 ABOVE STR 17L. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE. INSURANCE CUT ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 55,801 hrs · 20,920 cycles

R-1 DOOR FWD FRAME AT LOWER HINGE CUTOUT IS CRACKED. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REMOVED CRACK FROM LOWER HINGE BY CUTTING -238 FRAME TO MAKE A -131 AND -237 SECTIONS PER BOEING AND UA ENGINEERING SPECIFICATIONS. ALODINED AND PRIMED AND REIDENTIFIED FRAME.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,801 hrs · 20,920 cycles

MAIN CABIN TEE CAP AT STA 324 IS CORRODED. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF T-CAP, MOST OUTBOARD 14 IN. RBL. FABRICATED PER UA ENGINEERING SPECIFICATIONS AND INSTALLED NEW REPAIR.

Part: CREASE BEAM — CORRODED (BS 1061) · airframe 55,801 hrs · 20,920 cycles

MAIN CABIN CREASE BEAM WEB HAS CORROSION STA 1061, LBL 7 0. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. INSTALLED DOUBLER REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 324-345) · airframe 55,801 hrs · 20,920 cycles

MAIN CABIN FLOOR SUPPORT STA 324 TO 345, RBL 60 HAS CORROSION. [SUP 05-04-07] MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW FLOOR SUPPORT.

Part: UNKNOWN — ODOR (CARGO BAY) · airframe 54,914 hrs · 20,598 cycles

FWD CARGO PIT HAS A STRONG ELECTRICAL ODOR. TROUBLESHOT TO RT RECIRC FAN. GOT INOP LIGHT AND ASSOCIATED HORN WHEN RT RECIRC FAN IS IN COMMAND.

Part: VALVE — LEAKING (SLIDE BOTTLE) · airframe 53,669 hrs · 20,116 cycles

LOW BOTTLE PRESSURE. BALL SEAT WAS LEAKING. REPLACED BALL SEAT.

Part: PROBE — BROKEN (LT ENGINE) · airframe 52,072 hrs · 19,548 cycles

DIVERTED TO DEN DUE TO LEFT ENGINE PROBE HEAT INDICATION PROBLEM, NON-ICING RESTRICTION. REPLACED P2-T2 PROBE PER MM 72-21-03 AND FAULT WAS REMOVED/INDICATOR EXTINGUISHED. ENGINE RUN AFTER PT REPLACEMENT WAS CLEAR. ITEM RESURFACED ON THE 02/01/2006, AND DEN REPLACED RELAYS K144 AND K10377 AS PRECAUTIONARY. EICAS CLEARED. NO ISSUES DURING RUN-UPS OR FURTHER FLIGHTS. PROBABLE CAUSE DUE TO WEAK RELAY AND/OR INTERMITTENT PROBE MALFUNCTION.

Part: PACKING — LEAKING (HYD SYSTEM) · airframe 50,197 hrs · 18,816 cycles

RETURNED TO FIELD DUE TO INDICATION OF LOSS OF HYDRAULIC FLUID. HYDRAULIC FLOW LIMITER PACKINGS WERE LEAKING AT THE UNIONS, THE PACKINGS WERE REPLACED. THE LEFT HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKED OK. AIRCRAFT WAS RETURNED TO SERVICE.

Part: GIRT BAR — DAMAGED (ESCAPE SLIDE)

SLIDE WOULD NOT ARM BY GIRT. INSPECTION SHOWS GIRT WAS OPERATIONAL. THE PACKBOARD CAME IN WITH MAJOR DAMAGE. GIRT WAS CHECKED FOR CORRECT POSITIONING AND LENGTH PER P-11886 PACKING MANUAL. SLIDE HAS NO RECENT HISTORY OF GIRT REPAIR. NO CAUSE FOR REPORTED DISCREPANT SLIDE ARMING WAS FOUND. SLIDE APPEARS TO HAVE BEEN DROPPED DURING HANDLING, CAUSING DAMAGE TO PACKBOARD CORNER. PACKBOARD WAS REPLACED AND SLIDE MADE SERVICEABLE.

Part: HYDRAULIC LINE — RUPTURED (HYDRAULIC SYS) · airframe 37,848 hrs · 14,262 cycles

AFTER TAKEOFF LOST LEFT HYDRAULIC SYSTEM. *S/D* LEFT DOWNLOCK ACTUATOR HOSE RUPTURED. REPLACED HOSE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

FLOORBEAM CORRODED STA 345, RBL 54. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED STRAP REPAIR.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

FWD CARGO DOOR LWR AFT EDGE FRAME IS CRACKED AT CORNER. REPLACED CORNER FRAME.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

FUSELAGE SKIN DENTED STA 1593-1596 BETWEEN STR 14R AND 15R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,917 cycles

AFT PIT FRAME HAS EXCESSIVE MATERIAL LOSS STA 1480 STR 27R. MAJOR REPAIR ACOMPLISHED. SPLICED REPAIR FRAME SECTION BETWEEN STR 22R TO 27R.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

FRAME DAMAGED AT STA 365 ADJACENT TO STR 17R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.INSTALLED FRAME DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

CABIN FLOORBEAM CORRODED STA 345 RBL 45 AROUND FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR STRAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

CABIN FLOORBEAM CORRODED STA 1640 RBL 10 TO CREASE BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP REPAIR PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

CABIN FLOORBEAM UPPER CHORD CORRODED STATION 365.25 BETWEEN BL 0 TO RBL 62. MAJOR REPAIR ACCOMPLISHED.INSTALLED T-CAP REPAIR PER SRM.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

CREASE BEAM DAMAGED INBOARD ANGLE RIGHT SIDE STA 1130-1133. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED DAMAGE SECTION OF CREASE BEAM USING SRM 51-70-12 TYPICAL EXTRUDED SECTION REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

FLOORBEAM CORRODED STA 1669-1673 RLB 40. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW FLOOR BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

FLOORBEAM STA 324.8 RBL 42 TO 49 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR ON T-CAP PER AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

FLOORBEAM CAP STA 310.5 RBL 44 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR ON T-CAP PER AMM.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

FUSELAGE SKIN DENTED LEFT SIDE AT FLOOR LINE BETWEEN STA 460 TO STA 492 STR 17L. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

FLOOR BEAM STA 324 BL 0 AND RBL 58 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED T-CAP REPAIR PER AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

CREASE BEAM WEB STA 1076 STR 17R HAS EXCESSIVE MATERIAL LOSS. REPLACED CREASE BEAM PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

MID CABIN FLOOR STRUCTURE SUPPORT ADJACENT TO DOOR 2R BS740 TO BS760 RBL 62 HAS EXCESSIVE MATERIAL LOSS. REPLACED ANGLES PER SRM.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

MID CABIN SUPPORT STRUCTURE ADJACENT TO DOOR 2R BS 740 TO BS 760 RBL 62 HAS EXCESSIVE MATERIAL LOSS. REMOVED AND REPLACED TWO ANGLES. MAJOR REPAIR ACCOMPLISHED.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

CREASE BEAM WEB STA 1076 STRINGER 17R HAS EXCESSIVE MATERIAL LOSS. REMOVED AND REPLACED AFFECTED CREASE BEAM WEB. MAJOR REPAIR ACCOMPLISHED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

CREASE BEAM WEB STA 1021 STR 17L HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

AFT CABIN FRAME BS 1681 STR 17R WL 208 IS EXFOLIATED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME PER SRM. INSTALLED DOUBLER ANGLE.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

FUSELAGE SKIN DENTED AT BS 650 JUST BELOW FLOORLINE STRINGER 17L. INSTALLED DOUBLER PER SRM.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 37,036 hrs · 13,970 cycles

NR 2 PYLON INBOARD SKIN ACCESS CUTOUT CRACKED. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

MID CABIN FLOORBEAM WEB STA 700 LBL 25 CRACKED. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLERS ON FLOORBEAM PER SRM.

Part: STRINGER — TOOL DAMAGE (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

AFT PIT RT SIDE STR 27 STA 1590 HAS TOOL DAMAGE. MAJOR REPAIR ACCOMPLISHED.INSTALLED STRINGER SPLICE PER SRM.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,036 hrs · 13,970 cycles

AFT PIT LT FRAME STA 1400 STR 28L TOP OF FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE PER MM.

Part: TUBE — LEAKING (SLIDE)

SLIDE FAILED AIR RETENTION TEST DURING SHOP VISIT. *S/D* POROSITY CAUSED SEAM LEAK. UNIT WAS SENT TO VENDOR FOR EVALUATION AND REPAIR.

Part: EXCITER — INOPERATIVE (APU)

APU START PROBLEM, PRESSURE GOES TO ZERO ON ENGINE START, APU INOP. *S/D* FAULTY IGNITION EXCITER. REPLACED IGNITION UNIT.

Part: MAIN TUBE — SEPARATION (SLIDE)

SLIDE REMOVED FOR SECOND TIME CONTROLLED OVERHAUL. A 3 INCH SEAM SEPARATION LOCATED ON THE RIGHT HAND MAIN TUBE APPROXIMATELY 1 FOOT FROM CROSS OVER TUBE. RETURNED UNIT TO ORIGINAL EQUIPMENT MANUFACTURER FOR REPAIR.

Part: LAMP — FAILED (CABIN)

EMERGENCY ESCAPE LIGHTING INOP AT OVERWING EXIT ROW 17 ABC. RELAMPED DEFECTIVE EMERGENCY ESCAPE LIGHT AT OVERWING EXIT ROW 17 ABC AND OPERATION CHECKS NORMAL.

Part: LEADER LINE — FAILED (AFT LAV)

FLOOR EMERGENCY ESCAPE LIGHTING INOP AFT LAVATORY AREA. REPLACED LEADER LINE FLOOR EMERGENCY ESCAPE LIGHTING AT AFT LAVATORY AREA AND OPERATION CHECKS NORMAL.

Part: LEADER LINE — FAILED (CABIN)

FLOOR EMERGENCY ESCAPE LIGHTING INOP AFT LAVATORY AREA. REPLACED LEADER LINE FLOOR EMERGENCY ESCAPE LIGHTING AT AFT LAVATORY AREA AND OPERATION CHECKS NORMAL.

Part: HINGE — BROKEN (SERVICE DOOR)

RETURNED TO ORD, DUE TO LEFT OVERWING SLIDE DEPLOYED LIGHT AND OVERWING DOOR MESSAGE. A BROKEN HINGE AND IMPROPER LATCHING OF THE SERVICE DOOR AFT OF THE SLIDE COMPARTMENT ACTIVATED THE DOOR SWITCH, WHICH CAUSED THE DOOR OPEN LIGHT. REPLACED HINGE.

Part: EEL — LOOSE (CABIN)

EEL LIGHT COVER LOOSE 2C TO 4C. SECURED LIGHTS AS REQUIRED.

Part: EEL POWER CABLE — FAILED (CABIN)

EEL INOP ROW 25C-32C. REPLACED POWER CABLE. OPS CKS OK.