N556UA

Part: STRAP — UNSECURE (CRASH AXE) · airframe 70,324 hrs · 25,779 cycles

CRASH AXE RETENTION STRAP FALLING OFF, NEEDS ANCHORING. SECURED STRAP & STOWED CRASH AXE.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT DOOR) · airframe 70,089 hrs · 25,704 cycles

UPON RETURN TO AIRCRAFT THE COCKPIT DOOR WAS CLOSED. ATTEMPTED TO GAIN ACCESS USING EMERGENCY PROCEDURES, FLIGHT CREW ENTERED CODE SEVERAL TIMES TO GAIN ENTRY TO CONTROL CABIN, NO HELP. HAD TO SHUT OFF APU USING FIRE HANDLE. FLT CREW TRIED 2 TIMES TO OPEN DOOR WITH CODES AFTER ENTRY WAS GAINED. FLT CREW COULD NOT OPEN DOOR AFTER ENTRY WAS GAINED, DF0237 MEL 5251C.

Part: BUMPER — DAMAGED (THRUST REVERSER) · airframe 70,040 hrs · 25,689 cycles

NR 2 ENG REVERSER SLEEVE OTBD SIDE AT 3 O'CLOCK POSITION BUMPER ASSEMBLY DAMAGED PREVENTING TRANSLATING SLEEVE FROM PROPERLY STOWING. REPLACED POSITION BUMPER ASSEMBLY IAW IPC 78-31-10-005 ITEM 148.

Part: STRIKER — INOPERATIVE (COCKPIT DOOR) · airframe 69,456 hrs · 25,477 cycles

FLT DECK DOOR ENTRY PAD NR 1 DOES NOT SOUND FOR ENTRY. R & R FLIGHT DECK DOOR ELECTRIC STRIKER IAW AMM. OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN (R4 ARM LIGHT) · airframe 69,148 hrs · 25,380 cycles

R4 DOOR ARM LIGHT DOES NOT ILLUMINATE. REPLACED LAMP IN R4 DOOR ARMED LIGHT. LIGHT WORKS FOR A COUPLE OF CYCLES THEN DOES NOT WORK.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 69,034 hrs · 25,342 cycles

EMERGENCY FLOOR LIGHT IS PEELING AT ROW 10. SNAP BACK ON FLOOR LIGHT STRIP COVER. ACFT OK TO CONT.

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 68,874 hrs · 25,290 cycles

NR 1 ENGINE ACCUMULATED A LARGE PUDDLE OF HYD FLUID ON GROUND IN LESS THAN 30 MINS. RAN THRUST REVERSER AND FOUND ACTIVE LEAK COMING FROM ROD END OF INBD CENTER ACTUATOR. STARTED REMOVAL AND INSTALLATION IAW AMM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 68,647 hrs · 25,219 cycles

EMERGENCY EXIT LIGHTS ROW 11-12 ABC SEPARATING FROM THE FLOOR. INSURED 11 ABC EXIT LIGHT COVER IS SECURE. CHECKED OK.

Part: HANDSET — MALFUNCTIONED (FIRST OFFICER'S) · airframe 68,578 hrs · 25,194 cycles

HANDSET HAS A LOUD SQUEAL WHEN FIRST OFFICER TRANSMITS. REPLACED HANDSET.

Part: SENSOR — FAULTY (RT A/C PACK) · airframe 68,525 hrs · 25,175 cycles

CREW REPORTED CABIN HOT & SLOW TO COOL, TOOK TWO HOURS. RT PACK CONTROLLER SHOWS RT PACK SENSOR FAULT. REPLACED RT PACK NR 1 TEMP SENSOR IAW MM. LEAK AND OPS CHECKED GOOD.

Part: SEALANT — DETERIORATED (WINDOW) · airframe 68,416 hrs · 25,144 cycles

ABNORMAL NOISE, VIBRATION AROUND L GLARESHIELD OR L WINDSHIELD AREA. CREW COMMENTS: CONSTANT SOUND OF AIR ESCAPING ON CAPT SIDE UPPER PART OF SIDE WINDOWS. FOUND SILICONE DETERIORATING UPPER FORWARD CORNER. APPLIED NEW SEALANT PER MM 56-11-02.

Part: COVER — DETACHED (COCKPIT) · airframe 68,405 hrs · 25,140 cycles

TOP PLATE COVER FOR CARGO FIRE DISCHARGE BUTTONS NOT ATTACHED. COMPLIED WITH ECRA 2623-0104.

Part: WINDOW FRAME — LOOSE (EMERGENCY EXIT) · airframe 68,180 hrs · 25,078 cycles

20F EMERGENCY EXIT WINDOW FRAME LOOSE. SECURED WINDOW FRAME.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 68,180 hrs · 25,078 cycles

SEAT 1B EMERGENCY LIGHT MISSING END CAP. REPLACED END CAP.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 68,180 hrs · 25,078 cycles

SEAT 8C EMERGENCY LIGHT END CAP IS MISSING. REPLACED END CAP.

Part: LIGHT — LOOSE (CABIN) · airframe 68,174 hrs · 25,077 cycles

EMERGENCY LIGHT AT ROWS 11A AND 11B LOOSE. SECURED LIGHT.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 68,166 hrs · 25,075 cycles

EMERGENCY LIGHT ROW 11 UNSECURE. SECURED EMERGENCY LIGHT COVERED, OPS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN FLOOR) · airframe 68,147 hrs · 25,067 cycles

AIRCRAFT MISSING FLOOR EMERGENCY LIGHT IN FRONT OF MID LAV DOOR. REPLACED MISSING EMERGENCY LIGHT AT DOOR 2 LAV IAW DWG 15F6889 AND MM 33-51-95. OP CHECKED OK.

Part: LIGHT — MISSING (CABIN FLOOR) · airframe 68,147 hrs · 25,067 cycles

AIRCRAFT IS MISSING ORANGE EMERGENCY LIGHT BY FIRST CLASS CLOSET DOOR. INSTALLED MISSING EMERGENCY LIGHT PER MM, OPS CHECKED OKAY.

Part: CARPET — MISMANUFACTURED (CABIN) · airframe 68,147 hrs · 25,067 cycles

PER IPC 33-52-00 AIRCRAFT IS MISSING EEL FLOOR LAMP IN FRONT OF AFT FWD LAV DOOR. EEL FLOOR LAMP IS PRESENT BUT IS COVERED BY CARPET. TRIMMED CARPET AND REPAIRED EEL LAMP PER MM AND IPC. OP CHECKS OKAY.

Part: CHARGER — FAULTY (MAIN BATTERY) · airframe 67,726 hrs · 24,930 cycles

MAIN BATTERY CHARGER MESSAGE ON STATUS PAGE. T-SHOT PER FIM 24-31-00. REPLACED BATTERY CHARGER PER MM 24-31-02.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 67,726 hrs · 24,930 cycles

EMERGENCY EXIT SIGNS DO NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. SECURED LOOSE CONNECTOR ON INVERTER M110834.

Part: FAN — DAMAGED (CARGO BAY) · airframe 67,726 hrs · 24,930 cycles

DUE TO REPORTED HEAT DAMAGE TO INSULATION IN AREA OF FORWARD EQUIPMENT COOLING FANS, IDENTIFY SOURCE OF HEAT, REPAIR ANY DISCREPANCIES AND REPORT FINDINGS TO 757 FLEET CONTROLLER. CONCLUSION OF HEAT SOURCE WAS RECIRC FAN IN FWD CARGO PIT. PERFORMED EG7709. NO FINDINGS WHERE NOTED.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 67,710 hrs · 24,924 cycles

DURING EMERGENCY LIGHT TEST OVERWNG EXIT AT 21F INOP. SECURED CONNECTOR AT SEAT 21ABC, IT POWERS 21F ALSO. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 67,710 hrs · 24,924 cycles

DURING EMERGENCY LIGHT TEST OVERWING EXIT AT 20A INOP. TROUBLESHOOTING FOUND CONNECTOR ON INVERTOR AT SEAT 21ABC LOOSE, IT POWERS SEAT 20A ALSO. OPS CHECK NORMAL.

Part: SKIN — DENTED (BS 720) · airframe 67,694 hrs · 24,919 cycles

FOUND DENT JUST UNDER MID LAVATORY SERVICE PANEL TWO INCHES ABOVE STRINGER 23 AT BS 720. NO CRACKS PRESENT. BLENDED OUT SCRATCH, INSTALLED DOUBLER REPAIR PER ECRA 5330-04439 AND EA 130164.

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 67,694 hrs · 24,919 cycles

LEFT MLG CENTER MOUNT FITTING VERTICAL FLANGE IS CORRODED. INSTALLED NEW FITTING IAW EA 130167IR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,694 hrs · 24,919 cycles

CORROSION ON EXISTING REPAIR STA 365 FLOORBEAM UPPER CORD AT LBL 11 TO THE RIGHT END OF JOINT. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR PER ECRA 5310-05680 AND ARR EA 130071 IR.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 67,694 hrs · 24,919 cycles

LEFT WING INBD MAIN FLAP OUTBOARD UPPER SURFACE WORN. INSTALLED REPAIR DOUBLER AND TRIPLER PER ECRA 5750-04524 AND EA 130134 REV IR.

Part: WIRE — BROKEN (EXHAUST FAN) · airframe 67,694 hrs · 24,919 cycles

AFT EQUIP EXHAUST FAN CONNECTOR D2360, WIRE W2634-0006-16 IS BROKEN ONE INCH FROM CONNECTOR. SPLICED IN NEW PIECE OF WIRE, TERMINATED AND INSTALLED IN CONNECTOR D2360. OPS CHECKED GOOD REF AMM 21-58-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,694 hrs · 24,919 cycles

RIGHT EXT SKIN STA 800-860, WL 200 - 212 ALONG CONTACT SURFACE FOR BODY FAIRING PANEL HAS SCRIBE MARKS. MAINT TEXT: INSTALLED DOUBLER RPR PER ECRA 5330-04430, AND AAR EA 130084IR.

Part: BEAM — DAMAGED (BS 570) · airframe 67,694 hrs · 24,919 cycles

FWD CARGO BAY, BS 570, RBL 22, DOOR CUTOUT, LOWER MAIN SILL BEAM UPPER ANGLE HAS EXISTING MISDRILLED HOLES ADJACENT TO NUT PLATE HOLE. INSTALLED FREEZE PLUG REPAIR PER ECRA 5330-04433, & EA 130118 REV IR.

Part: SKIN — DENTED (BS 664) · airframe 67,694 hrs · 24,919 cycles

SKIN DENTED AT BS 664, WL 209, S17L. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR PER ECRA5330-04423 AND EA 130077 REV IR. STAGE II CATEGORY B MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,694 hrs · 24,919 cycles

EXT FUSELAGE SKIN HAS DENT, STA 800, BETWEEN STR 13R AND 14R. MAINT TEXT: CUT OUT DAMAGED SKIN DOUBLER RPR REF ECRA 5330-04427 AND AAR EA 130078 REV IR. RPR DOUBLER STA 790 - 803, STR 12R - 15R.

Part: WIRE — DAMAGED (R4 DOOR) · airframe 67,694 hrs · 24,919 cycles

WIRE REPAIR. DOOR 4R FWD GIRT BAR PROX SWITCH, S10224, HAS DAMAGE HISTORY. SPLICE WIRE W3682E PA (RED) AT STA 1644 PER WDM25-66-11, AND SWPM20-30-12. OPS CHECKS GOOD REF AMM 52-11-96 STEP E. THIS IS PERMANENT RPR.

Part: WIRE — DAMAGED (R4 DOOR) · airframe 67,694 hrs · 24,919 cycles

WIRE REPAIR. DOOR 4R AFT GIRT BAR PROX SWITCH WIRING HAS DAMAGE TO PRIMARY INSULATION. MAINT TEXT: SPLICED REPAIRED WIRES W3682-F-PA AND W3682-F-GA PER SWPM20-10-13, WDM25-66-11. STA 1644, WL 240, RBL 40. OPS CHECKS GOOD REF AMM 52-11-96. PERMANENT RPR.

Part: WIRE — DAMAGED (R1 DOOR) · airframe 67,694 hrs · 24,919 cycles

DAMAGED WIRES. DOOR 1R, FWD GIRT BAR FITTING HAS DAMAGED WIRES. SPLICE RPR WIRES W3682-003-20 AND W3682- 001-20 PER SWPM 20-30-12 AND GNMM 05-30-40, WDM25-66-11. OPS CHECKS GOOD REF AMM52-11-96, PG 607. LOCATED STA 344.

Part: SKIN — DAMAGED (BS 366 S27R) · airframe 67,694 hrs · 24,919 cycles

FORWARD LOWER FUELAGE SKIN HAS LIGHTNING STRIKE AT BS 366, ABOVE STR 27R. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER ECRA 5330-04422. CAT B MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 310.5) · corrosion level 2 · airframe 67,694 hrs · 24,919 cycles

FORWARD CABIN WET AREA TRANSVERSE FLOORBEAM UPPER TEE CORRODED BS 310.5, RBL 35 TO 41. CUT OUT DAMAGE AND INSTALLED REPAIR PER ECRA 5310-05675 AND AAR EA 130069 REV IR. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 355-365) · corrosion level 2 · airframe 67,694 hrs · 24,919 cycles

CABIN FWD WET AREA CREASE BEAM WEB CORRODED UNDER R1 DOOR THRESHOLD, BS 355-365, RBL 63. REMOVED AND INSTALL NEW CREASE BEAM IAW DWG 141N8422. MAJOR REPAIR

Part: WINDOW — SCRATCHED (L3) · airframe 67,694 hrs · 24,919 cycles

L3 WINDOW SCRATCHED. L3 WINDOW REPLACED IAW TC 521140001.

Part: ATTACH ANGLE — CORRODED (BS 1816) · corrosion level 2 · airframe 67,964 hrs · 24,919 cycles

BS 1816 AT S6R APU INLET DOOR ATTACH ANGLE CORRODED. FABRICATED NEW ATTACH ANGLE, STRAPS, & ANGLE. INSTALLED IAW SRM 53-80-15 FIG 202, DETAIL I, AND SRM 51-40-02. MAJOR REPAIR

Part: SKIN — DENTED (L1 DOOR) · airframe 67,694 hrs · 24,919 cycles

L1 DOOR HAS A DENT, 5.5 INCHES FROM LOWER EDGE. CUT OUT DAMAGE, INSTALLED DOUBLER REPAIR WITH FLUSH FASTENERS PER SRM 52-10-01, REPAIR 7, FIG 201. HFEC DAMAGE REMOVE PER NDT PT 6, 51-00-19, ALL DAMAGE REMOVED. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 333) · corrosion level 2 · airframe 67,694 hrs · 24,919 cycles

CABIN FWD WET AREA. FLOORBEAM CORRODED BS 333 RBL 7-23. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED NEW FLOORBEAM IAW SRM 53-00-04, 51-10-02, 51-21-01 & GMMN 1-0-1-007. MAJOR REPAIR.

Part: SKIN — DENTED (TE FLAP) · airframe 67,694 hrs · 24,919 cycles

RIGHT WING I/B FLAP LOWER SURFACE 25 INCH OF O/B EDGE AND 2. 5 FWD OF T/E HAS SMALL DENT. MAJOR REPAIR ACCOMPLISHED. EVALUATED DAMAGE ON RT WING I/B FLAP LWR SKIN & FOUND TO BE OUT OF LIMITS SRM 57-53-01, REMOVED DAMAGE VERIFIED MATERIAL & FABRICATED DOUBLER POTTED REPAIR AREA APPLIED PRE-BOND TREATMENTS. BONDED DOUBLER.

Part: CREASE BEAM — CORRODED (BS 415-419) · corrosion level 2 · airframe 67,694 hrs · 24,919 cycles

CABIN FWD WET AREA. CREASE BEAM INNER STRUCTURE CORRODED AT BS 415-419 RBL 63. REMOVED CORROSION FROM BEAM OUT OF LIMITS. REMOVED & FABRICATED NEW CREASE BEAM IAW 53-00-51, 51- 40-02, 51-40-05, 51-20-01 AND INSTALLED CREASE BEAM SRM 51-40-02 & DWG 141N 8422-140N6504. MAJOR REPAIR

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,694 hrs · 24,919 cycles

CABIN FWD AREA CREASE BEAM INNER CHORD CORRODED AT STA 439 RBL 63. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM STA 349 FABRICATED NEW BEAM TAG A42735, INSTALLED BEAM IAW SRM 53-00-51,51-4 0-02, 51-40-05, 51-40-05, 51-20-01, 53-60-51 & DWG 140N0504.

Part: SKIN — DAMAGED (BS 1706-1708) · airframe 64,394 hrs · 23,768 cycles

DURING THE SCRIBE INSPECTION AN AREA OF DAMAGE WAS NOTED NOT A SCRIBE BUT POSSIBLE TOOLING DAMAGE AT STRINGER 10L TWO INCHES LONG BETWEEN BS 1706 AND 1708 .072 FROM BELOW LAP .0064 DEEP PER SRM 53-00-01 PAGE 105 ZONE A.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 67,694 hrs · 24,919 cycles

FWD CABIN, TRANSVERSE FLOORBEAM UPPER TEE HAS CORROSION AT BS 324, BL 0 - RBL 63. INSTALLED NEW TEE SECTION FROM LBL 10 TO RBL 25 PER SRM 53-10-08 RPR 1. MAJOR REPAIR

Part: SKIN — DENTED (BS 752 S20L) · airframe 67,694 hrs · 24,919 cycles

FUSELAGE SKIN DENTED BELOW STRINGER 20L, BS 752. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM. MAJOR REPAIR

Part: SKIN — DENTED (BS 1710 S16L) · airframe 67,694 hrs · 24,919 cycles

SKIN DENTED BS 1710, 1 INCH ABOVE STRINGER 16L. CUTOUT DAMAGE AND INSTALLED DOUBLER RPR PER SRM 53-00-01, REPAIR 2, FIG 201. MAJOR REPAIR

Part: SKIN — DAMAGED (BS 210) · airframe 67,694 hrs · 24,919 cycles

SKIN HAS SEVEN BUTTONHEAD RIVETS WITHOUT SUFFICIENT PITCH, BS 210, 6 INCHES BELOW STRINGER 19R. INSTALLED SKIN DOUBLER REPAIR PER SRM 53-00-01 REPAIR 3. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 67,694 hrs · 24,919 cycles

FLOORBEAM TEE HAS CORROSION BS 1661, LBL 20. REMOVED DAMAGED SECTION OF TEE AND INSTALLED NEW SECTION AND TWO SPLICE ANGLE DOUBLERS PER ECRA 5310-05538. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 67,694 hrs · 24,919 cycles

CABIN FLOORBEAM BS 1661, LBL 25 TEE HAS CORROSION AROUND FLOORBOARD FASTENER HOLES. REMOVED DAMAGED TEE AND INSTALLED NEW TEE WITH DOUBLERS PER ECRA 5310-05538. MAJOR REPAIR.

Part: PCU — LEAKING (LT ELEVATOR) · airframe 66,891 hrs · 24,636 cycles

LEFT OUTBOARD ELEVATOR PCA BAD. LEAKING AT ACTUATOR ROD END. REPLACED LEFT OUTBOARD ELEVATOR PCU, OPS CHECK GOOD.

Part: WIRE — BROKEN (COCKPIT) · airframe 65,968 hrs · 24,333 cycles

REPAIRED BROKEN WIRE W2070-0313-22 WDM33- 51-12 PAGE 5A CAN BE VIEWED BY OPENING LOWER LEFT COCKPIT CB PANEL LOCATED ABOVE ANNUNCIATOR PANEL. NEED TO PERFORM EMERGENCY LIGHT CHECK TO VERIFY SPLICE REPAIR. OBSERVE COCKPIT DOME LIGHT- EMERGENCY LIGHT MODULE AND EMERGENCY LIGHTS DOOR 1L & 1R AND FIRST CLASS, ALL OTHER EMERGENCY LIGHTS. OPS CHECKED GOOD.

Part: SENSOR — MALFUNCTIONED (TE FLAP PDU) · airframe 64,510 hrs · 23,807 cycles

AIRCRAFT FAILED ALTERNATE EXTEND TEST. RIGHT NEEDLE GOES TO APPROXIMATELY 12 DEGREES WHEN KNOB TURNED TO 1 DEGREE POSITION. TEST THAT FAILS IS JOB CARD 5-5010-B STEP 6D3. THE REST OF TEST PASSED. CHANGED RELAY K1024 4. SWAPPED & RETURNED FSEU2 AND FSEU3. REPLACED AND RETURNED ORIGINAL FSEU1. ALL NO HELP. CLEANED AND SECURED PDU POSITION SENSOR, OPERATED ALT FLAPS FEW TIMES, OP CHECK OK.

Part: OXYGEN SYSTEM — DISCHARGED (CREW O2) · airframe 64,397 hrs · 23,769 cycles

CREW O2 ZERO. SERVICED TO 1950 PSI.

Part: SKIN — DAMAGED (BS 1706-1708) · airframe 64,394 hrs · 23,768 cycles

DURING INSPECTION, AN AREA OF DAMAGE WAS NOTED ON SKIN AT STRINGER 10L 2" LONG BETWEEN BS 1706 & 1708 .072 FROM BELOW LAP .0064 DEEP PER SRM 53-00-01 PAGE 105, ZONE A. MAJOR REPAIR ACCOMPLISHED. TRIMMED OUT SKIN DAMAGE. PERFORMED HFEC OF DAMAGE CUTOUT AS PER NDT. PERFORMED ROTARY SCAN HFEC OF ALL EXISTING FASTENER HOLES COMMON TO THE REPAIR. REF NDT MANUAL PART 6, 51-00-16. NO DEFECTS NOTED. WORK PERFORMED IAW STEP A,3. AVO CGH-11-12-13-1A. FABRICATED REPAIR PARTS PER AVO CGH-11-12-13-1A STEP B 1 A AND B. INSTALLED REPAIR PARTS IAW AVO CGH-11-12.

Part: PLATE — FAULTY (GALLEY) · airframe 64,336 hrs · 23,745 cycles

GALLEY HOT PLATE WON'T HEAT AT 411H. CREW COMMENTS: WON'T HEAT. FWD GALLEY LOWER HOT PLATE H12 IS INOP. REPLACED HOT PLATE AT FWD GALLEY POSITION H12, OPS NORMAL.

Part: LIGHT — OBSTRUCTED (CABIN) · airframe 64,037 hrs · 23,638 cycles

AFT LAVATORY EMERGENCY LIGHT COVERED BY CARPET. TRIMMED BACK CARPET, OPS CHECKED OK.

Part: RETAINER — DAMAGED (RT MLG DOOR) · airframe 63,976 hrs · 23,614 cycles

RIGHT MLG DOOR TRAILING EDGE SEAL RETAINER CRACKED. RT MLG DR TE SEAL RETAINER CRACKED. REPAIRING SUPPORT SEAL WITH A PATCH. AWAITING RETAINER (U1745) AND BULB SEAL ASSY (J6603). RT MLG DOOR, FOUND AFT SEAL RETAINER SUPPORT DAMAGED. REPAIRED SUPPORT. TRAILING EDGE SEAL RETAINER DAMAGE. REMOVED SEAL & RETAINER. SEAL & RETAINER DAMAGE WILL REQUIRE REPLACEMENT. RPLC'D SEAL & SEAL RETAINER -NO FURTHER ACTION REQUIRED.

Part: DOOR FRAME — DAMAGED (L4 DOOR) · airframe 63,677 hrs · 23,501 cycles

CREW REPORTS LT AFT SVC DOOR (4LT) SQUEALING AGAIN. PRESSURE SQUEAL CAME BACK THRU FL230 7.25 DIFF AND STOPPED ONCE LEVEL AT FL360. IN DESCENT, SQUEAL CAME BACK AGAIN WHILE PASSING THRU FL270 7.25D PSI. REF LM1575, REPAIRED BOTH LOWER DOOR FRAME CORNERS WITH REN, RESEALED BOTH UPPER CORNER LINER SEALS AND RESEALED TORQUE TUBE COVER PANEL. SEE SEQ 6772002, 6772004, 6772003. PRESS TO 4.5 PSI NO SQUEALS NOTED.

Part: PANEL — LOOSE (4L DOOR) · airframe 63,675 hrs · 23,500 cycles

CREW REPORT: LOUD SQUEAL NEAR BACK GALLEY DURING CLIMB, GOES AWAY DURING CRUISE. COULDN'T DETERMINE DOOR. SAMC TEXT: FLIGHT ATTENDANT REPORTED RIGHT AFT DOOR SQUEAL. CHECKED AND CLEANED SEAL AREA. PRESSURIZED, NO SQUEAL NOTED. CREW REPORTS DOOR (4LT) SQUEAL. FOUND UPPER AND LOWER GATE SEALS AND TORQUE BOX LEAKING. REPAIRED SEAL ON ALL. LEAK CHECK AT 1000. BOTH DOOR 4L UPPER CORNER LINER SEALS SEALANT TORN. RESEALED BOTH UPPER CORNER LINER SEALS. DOOR 4L BODY TORQUE TUBE EXTERIOR COVER PANEL LOOSE AND NEEDS TO BE RESEALED. REF LM1575 FOR DOOR LEAKS. REMOVED AND RESEALED TORQUE TUBE COVER PANEL.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 63,671 hrs · 23,498 cycles

RT ENGINE EPR EICAS INDICATION BLANK. STANDBY INDICATION ALSO ABNORMAL. OK TO DEFER EPR INDICATION INOP REF MEL 7711D. REVIEWED WITH SAMC-EMC. INF- :FND 'T2 0R TAT,P T2 OR ADC -EEC,T2-EEC,P EEC,P275-17' MSGS ON EPCS. CLEARED AND MSGS DID NOT RETURN ON POWER UP. NO FAULT BALLS ON ADC. PARTS RPL-P2T2 ON JUL28, EEC ON AUG6, TAT ON AUG22.^28AUG DEN RDF-R :REF CREW EPR WORKS NORMAL SEE PTT 6662001", REOPENED BY OPBLM ON 28AUG11 FOR: REQUESTED ITEM REOPENED^28AUG DEN CQT- A/C WAS REMOVED FROM CAT III, DUE TO EPR WRITE UPS, SUSPECT INTERMITTENT EPR IND PROBLEM FOUND LOOSE B-NUT ON EEC AND REF 71-EPCS MESSAGE INDEX FOUND NO FAULTS ON ADC. REPLACED NR 2 ENG PT2-TT2 PROBE, ACP'D ENG RUN, EPR AND STAND BY ENG INDICATOR, OP CHECK'S NORMAL.

Part: SHUTOFF VALVE — LEAKING (FUEL SYSTEM) · airframe 63,613 hrs · 23,472 cycles

FUEL LEAKING FROM OUTBD LT FUEL SHUTOFF ACTUATOR. FUEL LEAK ONLY PRESENT DURING FUELING PROCESS. REPLACED LT OTBD FUELING SHUTOFF VALVE PER MM. OPS CHECKS GOOD, NO LEAKS NOTED.

Part: TUBE — RUPTURED (FUEL SYSTEM) · airframe 63,560 hrs · 23,449 cycles

UNWANTED FUEL IN CENTER TANK DURING FUELING. WKRG SMC007, LOCATED & REMOVED RUPTURED SECTION OF FUELING MANIFOLD IN CENTER TANK. PART ON OSTF F2171 COMING FROM AA ORD ETA 1300 VIA STERLING. CENTER FUEL TANK CONTINUES TO TAKE FUEL WITH BOTH CENTER TANK FUEL VALVES CLOSED. CYCLED FUEL VALVE SWITCHES- NO HELP. PREVIOUS FINDINGS ON OTHER ACFT WITH SAME PROBLEM HAVE FOUND TO HAVE CRACK OR LEAKING FUEL MANIFOLD IN CENTER TANK. NEED TANK ENTRY FOR T-S AND RPR. WKRG SMC007, LOCATED & REMOVED RUPTURED SECTION OF FUELING MANIFOLD IN CENTER TANK. PART ON OSTF F2171 COMING FROM AA ORD ETA 1300 VIA STERLING*. REPLACED BROKEN FUEL PIPE. CENTER TANK LEFT AND RIGHT FUELING VALVES SHUTOFF ACTUATORS DO NOT OPEN. REPLACED LEFT AND RIGHT CENTER TANK FUEL SHUTOFF VALVES ACTUATORS. RMV'D AND REPLACED FUEL QTY PROCESSOR UNIT, NO HELP. CHECKED VOLTAGE TO L&R CTR TANK REFUEL VALVES PIN 2 AND 28 VOLTS PRESENT. NEED TO CHANGE BOTH CENTER REFUEL VALVES. REPLACED LEFT AND RIGHT CENTER TANK FUEL SHUTOFF VALVES ACTUATORS. OP'S AND STATIC PRESSURE CHECK, OP'S CHECK GOOD AND NO LEAK FOUND.

Part: PLATE — MISSING (COCKPIT WINDOW) · airframe 63,509 hrs · 23,428 cycles

AFTER PRESSURIZATION 2L SLIDING WINDOW VERY DIFFICULT TO UNLOCK. ACCOMPLISHED RIG CHECK PER MM. WITHIN LIMITS, OPS CHECKED NORMAL. PRESSURIZED AFTER RIGGING CHECK, LATCH HANDLE STILL HARD TO MOVE. SUSPECT INTERNAL CAMS BINDING. CANNOT RIG 2L SLIDING WINDOW. UPPER CENTERING ROLLER MISSING SERRATED PLATE FOR ADJUSTMENT. WINDOW DISASSEMBLED, FOUND SERRATED PLATE. REMOVED SERRATED PLATE FROM ROLLER BRACKET. REPLACED UPPER ROLLER AND SERRATED PLATE. REINSTALLED FASTENERS AND WINDOW TRIM. WINDOW OPERATES SMOOTHLY.

Part: MODULE — FAILED (MLG LEVER) · airframe 63,189 hrs · 23,314 cycles

AT ARRIVAL PSEU BITE SHOWED LANDING GEAR LEVER SYSTEM NR 1 AND NR 2 UP AND DOWN. REPLACED LANDING GEAR CONTROL LEVER MODULE. CLEARED PSEU MEMORY.

Part: LANYARD — LOOSE (L3 DOOR SLIDE) · airframe 62,310 hrs · 23,009 cycles

DOOR 3L WILL NOT ARM. SECURED LOOSE LANYARD IN POUCH. ARM DISARM FUNCTION CHECKS OKAY.

Part: FAN — NOISY (CABIN) · airframe 62,222 hrs · 22,972 cycles

R RECIRC FAN VERY LOUD MAKING COCKPIT COMM DIFFICULT. ACP CHRONIC REVIEW TRIED TO CLEAN DUCTS ON LEFT SIDE OF FLT DECK, NO HELP. CHECK VALVES CHECK GOOD NEEDS MULTI SHIFT SLOT FOR DUCT CLEAN. REPLACED RIGHT RECIRC. FILTER PER MM. CLEANED LT FLEX DUCT AND SECURED. NEED TO DISCONNECT RT FLEX DUCT AND CLEAN. CLEANED RT DIFFUSER PLATE. PERFORMED OP CHECK. DB LEVEL 72 WITH AN INCREASE TO 74 WITH RT RECIRC FAN ON. ALL ITEMS ACCOMPLISHED ASSIGNED TO DF0659. CLOSE UP ACCOMPLISHED ON PTT 2222008 AND PTT 2222009.

Part: SWITCH — MELTED (COCKPIT) · airframe 61,800 hrs · 22,821 cycles

ACFT RETURN TO GATE DUE TO BURNED RUBBER ODOR, STRONGEST IN COCKPIT. REPLACED OVERHEAD SWITCH PANEL P-5 DUE TO RT RUNWAY TURNOFF SWITCH MELTED.

Part: PANEL — UNSECURE (L1 DOOR) · airframe 61,769 hrs · 22,805 cycles

EVAC ALARM SOUNDED ON ROLLOUT IN COCKPIT AND CABIN. FOUND PANEL AT L1 DOOR LOOSE FROM MOUNTS. SECURED PANEL TESTED OK.

Part: BLADES — DAMAGED (COMPRESSOR) · airframe 61,769 hrs · 22,805 cycles

RT ENGINE SURGE DURING CRUISE WITH LIGHT TURBULENCE AT FL380. EPR DROPPED .20 & N1 10 PERCENT. NO YAW FELT OR AUDIBLE STALL. PARAMETERS RECOVERED AND ARE NORMAL NOW IN SMOOTH AIR. NO EICAS MSGS. REFER TO FAULT CODE 71-05-21-02. CHECK IAW FIM. COMPLETED INSP EGT NOT EXCEEDED. NO METAL IN MCDS OR 14 AND 10 STAGE BLEED DUCTS. NO EPCS MSGS NOTED. ACCOMPLISHED BIRDSTRIKE, FOD INSP OF NR 2 FAN AREA, FOUND DAMAGE TO 1 EA FAN BLADE OUTER L/E. ACCOMPLISHED BOROSCOPE IAW AMM. REPLACED BLADES NR 3 AND NR 21 AND COMPLETED 5 MIN IDLE RUN. DAMAGE WAS BEYOND BLEND LIMITS.

Part: INDICATOR — FAULTY (L3 DOOR SLIDE) · airframe 61,753 hrs · 22,801 cycles

SLIDE INDICATOR DOOR 3L INDICATES DISARMED. COMPLIED WITH MEL CARD. CKD INDICATOR OPERATION, NEEDS TO REMOVE SLIDE COVER AND PROBABLY DOOR INNER PANEL TO ADJUST INDICATOR. CLEANED AND ADJUSTED ARMED INDICATOR.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 61,742 hrs · 22,797 cycles

CREW REPORT: DOOR 1L SLIDE ARMED LIGHT IS NOT ILLUMINATED WITH DOOR ARMED. REPLACED LENS CAP ASSY, CHECKS OK.

Part: GUIDE VANE — CRACKED (LT ENGINE) · airframe 61,732 hrs · 22,793 cycles

LT ENG VANE BENT WITH CRACK VISIBLE BEHIND FAN BLADES. FBO REPORTED ALUMINUM EXIT GUIDE VANE AT 05:30 IS BOWED AND CRACKED. NO CRACKS ALLOWED IAW MM. R & R THE VANE IAW MM. REMOVED FAN CASE EXIT GUIDE VANE AT THE 7 O'CLOCK POSITION AS VIEWED FROM THE REAR OF THE ENGINE NR1 LOOKING FWD. OK TO CON FOR 50 HOURS MUST BE REPLACED BY PTT 61782.11. USE PCN 230-0565 (PN 1B4419). VANE 230-0565 PLACED ON OSTF W4731. 1 EA 230-0565 IN HB 1 OSTF W4731 JAN 24 11. REPLACED EXIT GUIDE VANE IAW MM.

Part: SKIN — PUNCTURED (PAX DOOR) · airframe 61,726 hrs · 22,789 cycles

PUNCTURE DAMAGE AT 4L CABIN DOOR INNER SKIN AT UPPER HINGE LINE. MAJOR REPAIR ACCOMPLISHED: REPAIRED WITH APPROVED STRAP AND DOUBLER IAW PD 57-52-011, PROJECT 809 DATED 20 JAN 2011.

Part: TORQUE BOX — GOUGED (R1 DOOR) · airframe 61,726 hrs · 22,789 cycles

MED R1 DOOR TORQUE TUBE BOLT HAS GOUGED INBD SKIN-FRAME OTBD OF THE COCKING ROD. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND INSTALLED DOUBLER IAW REPAIR 6 ON NR 2426N00494.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,726 hrs · 22,789 cycles

FLOORBEAM AT STA 324, RBL 58 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REPAIRED FLOORBEAM T-CHORD PER EA PD 57-53-071 AND UA EVA 80477. MECH P531 INSP Q834 A NEW FAA FORM 8100-9 SHOWING COMPLIANCE TO 14CFR 25.571 AND 26. 43 (D) MUST BE ISSUED WITHIN 24 MONTHS FROM JAN 13,2011 FOR THIS REPAIR TO REMAIN VALID AND THE AIRCRAFT TO REMAIN AIRWORTHY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,726 hrs · 22,789 cycles

EMERGENCY EXIT LIGHT INOP INSIDE DOOR 1 RT AT THRESHOLD. REPLACED DOOR 1 RT EMERGENCY LIGHT PER MM. OPS CHECKED GOOD.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 61,726 hrs · 22,789 cycles

CORROSION ON SHEAR WEB BETWEEN BS 1681 AND STA 1720 AT RBL 50 UNDER GALLEY FLOOR FRAME. MAJOR REPAIR ACCOMPLISHED: REPLACED AFT SHEAR DECK WEB PER EA PD 57-53-070 AND SRM 53-60-51 REPAIR 2. THIS REPAIR IS CONSIDERED A PERMANENT WITH NO FURTHER ACTION REQUIRED.

Part: FLOORBEAM — CORRODED (BSS 365) · airframe 61,726 hrs · 22,789 cycles

CORROSION FOUND AT STATION 365 AT WL 208. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED REPAIR AT STA 365 FLOORBEAM FROM LBL 12 TO RBL 70 IAW SRM 53-00-5 1 REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 61,726 hrs · 22,789 cycles

CORROSION ON FLOORBEAM AT STATION 1640 RBL 3. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND REPLACED FLOORBEAM UPPER CHORD STA 1640 BTWN RBL 3 AND RBL 69 IAW.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,726 hrs · 22,789 cycles

EXTERNAL EMERGENCY LIGHT INOP AT DOOR 1R. RELAMPED R1 DOOR EXTERNAL EMER LIGHT AND OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,714 hrs · 22,783 cycles

SHORT EMERGENCY STRIP AT AFT LAV INOPERATIVE. REPLACED EMERGENCY STRIP AT AFT LAV LOCATION, OPS CHECK NORMAL.

Part: CONTROL UNIT — FAULTED (E/E BAY DOOR) · airframe 61,583 hrs · 22,741 cycles

EE ACCESS DOOR EICAS, RTFL CAPTAIN DESCRIBED SMOOTH LANDING AT 215K LBS. ACCOMPLISHED OVWT LANDING PHASE 1 INSPECTION. NO DISCREPANCIES FOUND. PERFORMED SENSOR TEST PER MM PROCEDURE WITH LCM TESTER AND OHMMETER. PSEU FAILS BITE TEST WITH CODE 006. REPLACED PSCU. TESTS OKAY.

Part: CONNECTOR — BURNED (PMA) · airframe 60,899 hrs · 22,497 cycles

RIGHT ENGINE SEC CONTROL, RT ENG REVERSER CONTROL AND RT ENG LIMIT PROTECTION EICAS & LIGHT CAME ON. FOUND CONNECTOR OR RT ENG PMA WITH BURNED PINS. REPLACED PMA. RAN ENGINE AT IDLE FOR 5 MIN, ENG OPERATES OK.

Part: DUCT — DAMAGED (CABIN) · airframe 59,988 hrs · 22,163 cycles

HOT AIR BLOWING IN CABIN AT ROWS 11-14, OKAY ELSEWHERE. POSSIBLE LEAK IN DUCT WORK. DUCTS REPAIRED SFOOV, LEAK CHECK GOOD.

Part: SIGN — UNSECURE (EMERGENCY LIGHTS) · airframe 59,649 hrs · 22,040 cycles

EXIT SIGN ABOVE DOOR 2L FELL OFF. SECURED SIGN.

Part: SKIN — DENTED (BS 760) · airframe 57,569 hrs · 21,216 cycles

FUSELAGE DENTED AFT OF DOOR 2L, AT STA 760, 9" ABOVE WL. MAJOR REPAIR ACCOMPLISHED: DENT IS 1"W BY .200" D, IS SMOOTH, NO GOUGES OR CRACKS. DENT IS NOT ON ANY FRAMES OR STRINGERS. REMOVED DAMAGE AND ACP HFEC INSP TO VERIFY CUT OUT CRACK FREE. FABRICATED DOUBLER. INSTALLED DOUBLER & FASTNERS. WORK IS ON NR 2983242026N0017 AND INSP BY QC.

Part: SOCKET — FAULTY (LAV MIRROR LIGHT) · airframe 58,918 hrs · 21,757 cycles

LAV 3L MIRROR LIGHT INOP. NEED NEW LAMP SOCKET. CHANGED LAMP SOCKET, OPS CHECKED OK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 58,918 hrs · 21,757 cycles

FROM AISLE ROW 9C BACK TO MID CABIN EMERGENCY LIGHT STRIP INOPERATIVE. REPAIR POWER CONNECTOR, CHECKS NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,743 hrs · 21,678 cycles

EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REPLACED BATTERY FOR ROWS 18 T0 23. ACCOMPLISHED SPLICE REPAIR FOR ROWS 8 TO 14.

Part: SIGN — BROKEN (OVERWING EXIT) · airframe 58,562 hrs · 21,605 cycles

EXIT SIGN BROKE OVER RT WING. OVERWING EXIT SIGN IS NOT BROKE, BUT IT IS BENT UP. IT CAN BE SEEN, READ AND USED WITH NO DIFFICULTY AS IS. SECURED SIGN OK.

Part: WIRE — SHORTED (PUMP) · airframe 57,814 hrs · 21,310 cycles

L HYD PRESS & RUD RATIO EICAS, ABORTED TAKEOFF. ACP INSPECTION. ENERGY LEVELS FOUND TO BE IN THE NO SPECIAL PROCEDURE RANGE. ACP VISUAL INSPECTION OF WHEELS AND BRAKES, WITH NO DEFECTS NOTED. FAULT RECURRED 5 SEGMENTS LATER. FOUND WIRE SHORTING TO GRD AT S27. REPAIRED WIRING AND REPINNED D3100. ABLE TO DUPLICATE PROBLEM BEFORE REPAIR. ACCOMPLISHED TAXI TEST, ALSO RAN UP BOTH ENGINES TO TAKEOFF POWER FOR 1 MIN. NO DISCREPANCIES OR MESSAGES NOTED. UNABLE TO DUPLICATE PROBLEM AFTER REPAIR.

Part: CHARGER — FAULTY (BATTERY PACK) · airframe 57,759 hrs · 21,288 cycles

R1 EXTERNAL EMERGENCY LIGHT INOP. REPLACED AND OPS CHECKED THE M730 EMERGENCY LIGHT BATTERY CHARGER AND BATTERY PACK AND INSPECTED. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 1615 S14L) · airframe 57,759 hrs · 21,288 cycles

SKIN AT STR 14L DAMAGED AT STA 1615. MAJOR REPAIR ACCOMPLISHED. STR 14L AT STA 1615 REPAIRED PER UAL EVA 72939. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER FILLER REPAIR.

Part: SKIN — DAMAGED (BS 1650) · airframe 57,759 hrs · 21,288 cycles

DENT REPORTED ON FUSELAGE FWD OF DOOR 4L AT STA 1650. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED SKIN AND INSTALLED DOUBLER FILLER REPAIR. ALL SUBSTRUCTURE REINSTALLED. RESTORING CABIN AND LAV RMVED FOR ACCESS, NEED TO LEAK CK LAV & CHLORINATE H2O SYS.

Part: UNKNOWN — ODOR (CABIN) · airframe 56,432 hrs · 20,767 cycles

ELECTRICAL ODOR NOTED. FLIGHT DIVERTED. INSPECTED AIRCRAFT AND NO DISCREPANCIES FOUND.

Part: APU — FAULTY · airframe 55,748 hrs · 20,486 cycles

CREW COMMENTS: SHORTLY AFTER APPLYING APU AIR TO PACKS, SMOKE BEGAN APPEARING IN COCKPIT AND CABIN. FOUND OIL LEAKING IN APU AT BLEED DUCT OUTLET. SMOKE DISSIPATED RAPIDLY. FOUND OIL LEAKING IN APU BLEED OUTLET. ALSO APU FUEL LINE LEAKING AT FIREWALL BETWEEN UNION AND FUEL LINE TO APU. APU NEEDS TO BE REPLACED. REPLACED APU.

Part: UNKNOWN — SMOKE (CABIN) · airframe 55,746 hrs · 20,485 cycles

POWERED UP A-C AND CABIN AND COCKPIT FILLED WITH ELECTRICAL SMOKE. RESET CIRCUIT BREAKERS, APPLIED POWER TO AIRCRAFT FOUND NO SMOKE. PERFORMED PACK BURNOUT PRECAUTIONARY LEFT AND RIGHT PACKS, RAN PACKS OFF BOTH ENGINES, CHECKED WIRING AND BALLASTS ABOVE AND AROUND CENTER LAV, INSPECTED P31, P32, P34 P37 & P70 FOR ANY DAMAGED WIRING, NO DISCREPANCIES FOUND. RECHECKED WIRING PREVIOUS REPAIRS OK. SUSPECT SMOKE WAS DUE TO RESIDUAL SMOKE BEING RECIRCULATED BY RIGHT RECIRCULATION FAN AFTER REPAIRS WERE ACCOMPLISHED THE DAY BEFORE.

Part: UNKNOWN — ODOR · airframe 55,083 hrs · 20,223 cycles

BURNING ODOR REPORTED. RFTL.

Part: RECEPTACLE — DAMAGED (MID LAVATORY) · airframe 55,083 hrs · 20,223 cycles

BURNING ODOR REPORTED. MID LAV FLOW LIGHT AFT LAMP RECEPTACLES ARE CHARRED. NEED REPLACEMENT. REMOVED LAMPS FROM MIRROR LAMP. DOME LAMP WORKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,712 hrs · 20,073 cycles

EXTERIOR EMERGENCY EXIT LIGHT AT DOOR NR 4 RT. LIGHT FOUND DEFECTIVE. REPLACED LAMP. OPS CHK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,712 hrs · 20,073 cycles

EXTERIOR EMERGENCY EXIT LIGHT INOP AT LT NR 1 DOOR. LIGHT FOUND INOP. REPLACED LAMP. OP CKS GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 54,685 hrs · 20,063 cycles

WHILE DESCENDING TO FL 350 AT FL 390 F/A REPORTED SMOKE ALARMS SOUNDED IN LAVS 2L AND FWD-AFT. ALSO A LIGHT HAZE WAS NOTICED IN THE AFT CABIN. NO ODOR OF OIL OR ELECTRICAL BURNING. UPON REACHING FL350 HAZE CLEARED. SMOKE ALARMS WERE RESET AND DID NOT RESOUND. ALL PACK OPERATIONS APPEARED NORMAL.

Part: UNKNOWN — FUMES (CABIN) · airframe 54,300 hrs · 19,925 cycles

SMOKE IN CABIN. FLIGHT DIVERTED. *S/D* DUE TO REPORT OF SMOKE AND FUMES IN CABIN, WHICH TRIGGERED THE MID LAV SMOKE DETECTOR TO GO OFF AND AFTER MANY SYSTEM AND COMPONENT CHECKS NOTHING WAS FOUND THAT WOULD HAVE CAUSED THIS PROBLEM. CHECKED ALL LIGHTS IN CABIN AND LAVS FOUND NO FAULTS. RAN PACKS AND FOUND NO FAULTS WITH APU AIR. RAN RT PACK WITH NR 2 ENG AT IDLE AND FOUND NO PROBLEMS. CREW STATED THAT THERE MAY HAVE BEEN VERY MINIMAL SENT OF FUMES BUT NOT DEFINITIVE PRIOR TO THEM DAWNING O2 MASKS.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 53,610 hrs · 19,677 cycles

STRONG ODOR LIKE FAILING BEARING IN COCKPIT. CHRONIC WRITE-UP. ACP FULL INSPECTION IAW FI M 21-00-01 SMOKE OR FUMES. RAN ENGINES INDEPENDANTLY WITH PACKS ISOLATED. RAN APU AND PACKS. DID VISUAL OF ALL ASSOCIATED SYSTEM FOR HYD OR OIL LEAKS. NO OBVIOUS LEAKS OR CRACKS FOUND. COULD NOT DETECT SMELL OR REPEAT DEFECT ON GROUND. NO KNOWN SORCE. PACKS OPERATED NORMAL.

Part: JACKSCREW — GOUGED (HORIZONTAL STAB) · airframe 53,289 hrs · 19,551 cycles

HORIZONTAL STAB JACKSCREW MIDDLE SECTION HAS .001 GOUGE. HORIZONTAL STAB BALLSCREW SHOWS SIGNS OF GALLING AND WEAR ALONG MIDDLE 2 FOOT LENGTH OF BALLSCREW, JACKSCREW REMOVED AND REPLACED,

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,289 hrs · 19,551 cycles

FOUND EMERGENCY LIGHTS AT DOOR 4R AND FWD LEFT OVERWING INOP. RELAMPED BULBS AND OPS CHECKED GOOD.

Part: METERING VALVE — FAULTY (NLG STEERING) · airframe 52,904 hrs · 19,415 cycles

ON TAXI-OUT TO RUNWAY, ON RH TURN AN AUDIBLE POP WAS HEARD AND NWS TILLER IS STUCK TO THE RIGHT. AFTER EXTENSIVE TROUBLE SHOOTING, THE METERING VALVE WAS REPLACED AND ISSUE WENT AWAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,894 hrs · 19,024 cycles

THE 4L EMERGENCY EGRESS LIGHT INOPERATIVE.

Part: METERING VALVE — MALFUNCTIONED (NLG STEERING) · airframe 51,840 hrs · 19,002 cycles

A/C PULLS RT DURING TAXI. FOUND NLG DOES NOT CENTER. NEW NLG STEERING METERING VALVE INSTALLED AND RIGGING ACCOMPLISHED BEFORE TEST RUN.

Part: SIGN — UNSECURE (EMERGENCY LIGHTS) · airframe 51,808 hrs · 18,989 cycles

AFT EMERGENCY EXIT SIGN FELL OFF. SECURED SIGN.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 51,146 hrs · 18,769 cycles

CAPTAINS OXYGEN MASK LEAKING OXYGEN CONTINUOUSLY.

Part: TRIM SYSTEM — FAILED (RUDDER) · airframe 50,877 hrs · 18,683 cycles

RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION.

Part: PROXIMITY SWITCH — FAULTY (L3 DOOR) · airframe 50,789 hrs · 18,654 cycles

CREW REPORT, 3L SLIDE ARM LIGHT DOES NOT ILLUMINATE. [08-08-07] SUSPECT FLOOR MOUNTED PROX SWITCHES MIGHT BE BAD. REPLACED AND TESTED OKAY.

Part: REGULATOR — FAULTY (COCKPIT) · airframe 49,817 hrs · 18,286 cycles

OXYGEN MASK DEFECTIVE AT 1=CAPT, 2=1ST OFF, 3=1ST OBS. CREW COMMENTS: INFLATABLE HARNESS DOESN'T INFLATE. [06-14-07] REPLACED MASK AND REGULATOR AI NR 1 POSITION OF PILOT AND 1ST OFFICER SEATS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 49,499 hrs · 18,176 cycles

EMERGENCY LIGHT AT DOOR 4 LEFT EXTERIOR INOPERATIVE. RELAMPED. OPS CHK GOOD.

Part: O-RING — LEAKING (REGULATOR) · airframe 47,018 hrs · 17,227 cycles

LOW BOTTLE PRESSURE. O-RING ON FILL VALVE WAS LEAKING AND FOUND DAMAGED. REPLACED O-RING ON FILL VALVE.

Part: RELIEF VALVE — OPEN (CABIN PRESSURE) · airframe 44,730 hrs · 16,405 cycles

LOSS OF CABIN PRESSURE. LOWER POSITIVE PRESSURE RELIEF VALVE FOUND OPEN. REPLACED VALVE, OPS CHECKED OK. RETURNED AIRCRAFT TO SERVICE.

Part: SLIDE — WILL NOT TEST (NR 2) · airframe 41,739 hrs · 15,274 cycles

EMERGENCY ESCAPE SLIDE 2 WILL NOT TEST. CYLINDER ASSEMBLY TEMPERATURE COMPENSATED PRESSURE SWITCH (TCPS) WAS DETERMINED TO HAVE BEEN DAMAGED DUE TO HANDLING.

Part: SKIN — DAMAGED (FUSELAGE CROWN) · airframe 40,087 hrs · 14,649 cycles

FUSELAGE CROWN SKIN AT BS 1240 AND STRINGER 3L HAS DAMAGE TO STRINGER RADIUS DUE TO LIGHTNING STRIKE. *S/D* MAJOR REPAIR ACCOMLISHED. REPAIRED STRINGER 3L WITH REPAIR ANGLE & FILLERS AND FUSELAGE SKIN WITH EXTERNAL DOUBLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,087 hrs · 14,649 cycles

LEFT FUSELAGE HAS 2 DENTS FWD DOOR 2L. MAJOR REPAIR ACCOMPLISHED. JETWAY DAMAGE. SKIN REPAIR DOUBLERS INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,087 hrs · 14,649 cycles

AFT PIT LEFT SIDE STA 1400 FRAME BETWEEN STRS 23L AND 26L HAS 2 EACH DENTS ON FRAME. *S/D* MAJOR REPAIR ACCOMPLISHED. FRAME DENTS FROM LOADING OF LUGGAGE. CUT OUT DAMAGED AREA AND FABRICATED ANGLE REPAIR AND INSTALLED IAW SRM.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,087 hrs · 14,649 cycles

FRAME AT STA 1500 ABOVE STR 26L DENTED. MAJOR REPAIR ACCOMPLISHED. FRAME DENTS FROM LOADING OF LUGGAGE. CUT OUT DAMAGED AREA AND FABRICATED ANGLE REPAIR AND INSTALLED IAW SRM.

Part: SKIN — CRACKED (APU DOOR) · airframe 40,087 hrs · 14,649 cycles

FWD CORNER OF APU DOOR 315AR SKIN CRACKED. *S/D* MAJOR REPAIR ACCOMPLISHED. DAMAGED FROM CONTACT WITH MAINTENANCE VEHICLE. REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER PER SRM AND INSTALLED DOUBLER AND FILLER MATERIAL.

Part: FRAME — DENTED (FUSELAGE) · airframe 40,087 hrs · 14,649 cycles

AFT PIT LT SIDE STA 1420 BETWEEN STRS 23L AND 26L HAS 2 EACH DENTED AREA ON FRAME. *S/D* MAJOR REPAIR ACCOMPLISHED. FRAME DENTS FROM LOADING OF LUGGAGE. REMOVED DAMAGED AREA AND FABRICATED FRAME REPAIR ANGLE AND INSTALLED IAW SRM.

Part: LAP JOINT — DENTED (FUSELAGE) · airframe 40,087 hrs · 14,649 cycles

FUSELAGE STATION 1710 STR 20L LAP SEAM SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED. SERVICE TRUCK DAMAGE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR AND FILLER MATERIAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,087 hrs · 14,649 cycles

TOP OF FLOORBEAM CORRODED AT STA 324 AT RT CUSP. MAJOR REPAIR ACCOMPLISHED. CORROSION CAUSED FROM WET AREA OF GALLEY. FLOORBEAM REPAIR ACCOMPLISHED.

Part: WIRE HARNESS — DAMAGED (P34 PANEL) · airframe 39,517 hrs · 14,471 cycles

EQUIPMENT CTR LIGHT, DRAIN MAST HTR GND, SEAT BELT SIGNS, RT FWD ENTRY AND ATTENDANT LIGHTS, FUEL VALVE QTY CTL LIGHT, SIDEWALL LIGHT, RT SIDEWALL LIGHT, CONT SIDEWALL LIGHT, ENTRY GALLEY LIGHTS, RT CEILING LIGHT AND CTL CEILING CIRCUIT BREAKERS FOUND POPPED. *S/D* WIRES BELONGING TO BUNDLES: W2070, W2072, W2356, W3576 AND W3614 WERE FOUND WITH EXTENSIVE OVERHEAT DAMAGE NEAR THE P34 ELECTRICAL PANEL. THERE IS NO CONCLUSIVE INDICATION OF WHAT INITIATED THE WIRE OVERHEAT DAMAGE, POSSIBLE EXISTING DEGRADATION TO THE WIRE INSULATION, TYPICAL TO THE WIRE TYPE BMS13-51 - PLAIN KAPTON. WIRE BUNDLES WERE REPAIRED USING ENVIRONMENTAL SPLICES PER BSWM 20-10-13.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 37,502 hrs · 13,892 cycles

NR 2 PYLON OUTBOARD WEB CRACKED AT FORWARD ACCESS PANEL INBOARD SKIN LOWER AFT RADIUS. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED REPAIR OF PYLON SKIN PER MM 54-31-99 FIGURE 803.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,755 hrs · 13,829 cycles

EXIT FLOOR LIGHTING INOP FROM ROWS 23-30. REPLACED BATTERY PACK.

Part: MODULE — SHORTED (COCKPIT) · airframe 37,279 hrs · 13,652 cycles

A/C RECEIVED WHEEL WELL FIRE INDICATION. WHEEL WELL FIRE INDICATION FOUND TO BE CAUSED BY P-3 WHEEL WELL FIRE ANNUNCIATOR L445. ANNUNCIATOR MODULE REPLACED AND OPERATED NORMAL. REMOVED PART TO BE EVALUATED BY VENDOR.

Part: SEAL — DIRTY (R2 DOOR) · airframe 35,853 hrs · 13,123 cycles

NOISE AND VIBRATION NEAR THE R2 AFT DOOR. INSPECTED AND CLEANED DOOR SEALS AT DOOR 2R AND 4R. SEALS FOUND SERVICEABLE AND NO DAMAGE PRESENT.

Part: FLAP — MALFUNCTIONED (WING) · airframe 33,898 hrs · 12,408 cycles

TAKEOFF ROLL 120 KTS TRAIL EDGE DISAGREE LIGHT ON EICAS AND FWD PANEL. USING NORMAL FLAP LEVER WOULD NOT MOVE. TRAILING EDGE ALTN SWITCH CLEARED DISAGREE LIGHT. USING ALTN METHOD LOWERED FLAPS TO 20. ACP CK OF FLAP SYSTEM. RAN FLAPS UP ELECTRIC AND FULL UP AND DOWN WITH HYD, BITE CK OF FSEU OK. ALL FLAP TRANSMISSIONS CHECKED NO OVERLOAD TRIP, NO ISOL VLV MSG.

Part: FIRE WARNING — FALSE INDICATION (MLG WW) · airframe 28,980 hrs · 10,637 cycles

WHEEL WELL FIRE INDICATION ILLUMINATED. *S/D* REPLACED DEFECTIVE DUCT LEAK AND WHEEL WELL FIRE CONTROL CARD. VENDOR REPORTED PART RECEIVED (P/N 3500838 38) WAS VERY DUSTY WITH FASTENERS FOUND LOOSE ON RELAY BOARD SIDE; CODE 84 IN MEMORY.

Part: HPC VANE — OUT OF ADJUST (NR 2 ENGINE)

RIGHT ENGINE FUEL FLOW AND EPR GAUGES STARTED SURGING PASSING THROUGH FL330 ON CLIMB. CREW ALSO FELT RIGHT ENGINE SURGING. FLIGHT DECENDED TO FL250 AND ENGINE RETURNED TO NORMAL INDICATIONS. FLIGHT RETURNED TO SFO WITH EQUIPMENT STANDING BY. *S/D* ENGINE WAS REPLACED DUE TO SURGING. DURING REPAIR AS ORDER NUMBER D345, IT WAS REPAIRED PER SFOEP FIX LETTER. ACCOMPLISHMENT WAS TO CHECK VSV AND 2.5 SYSTEMS. REMOVED THE FUEL CONTROL AND THE 14 STG CONVERTER VALVE. INVESTIGATIVE FINDINGS FOUND 6TH STG HPC VANES OUT OF RIG / SCHEDULE. THE 2.5 BLEED OUT OF RIG OPEN, AND THE BLEED RING AFT SEAL WORN AND LEAKING DUE TO AIR EROSION FROM BEING MISRIGGED.

Part: STRIP — INOPERATIVE (MID LAV)

EMERGENCY EVACUATION LIGHTING AT FORWARD MID LAVATORY AREA INOP. REPLACED EMERGENCY EVACUATION LIGHTING STRIP AT MID LAVATORY AREA AND OPERATION CHECKS NORMAL.

Part: SLIDE BOTTLE — FAILED (R2 DOOR)

RT NR 2 SLIDE PRESSURE WILL NOT TEST IN COCKPIT. REPLACED SLIDE BOTTLE.