N588UA

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,909 hrs · 25,616 cycles

R4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS, TESTED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,909 hrs · 25,616 cycles

L4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS , TESTED OK.

Part: ALTIMETER — READS LOW (COCKPIT) · airframe 79,756 hrs · 25,587 cycles

STANDBY ALTIMETER IS READING 3500 FT LOW, CREW REPORTED ACTUAL ALTIMETER 39000/ STBY 35700 AND DROPPING. ACP LOW RANGE LEAK CHECK PER AMM 34-11-00-735-175.

Part: LANYARD — LOOSE (R1 DOOR SLIDE) · airframe 79,352 hrs · 25,508 cycles

R1 DOOR SLIDE ARM LIGHT INOPERATIVE WHEN DOOR ISCLOSED AND ARMED. SECURED THE SLIDE LIGHT. CHECKED OK.

Part: D-RING — MISSING (L1 DOOR) · airframe 79,335 hrs · 25,505 cycles

DOOR 1L MISSING D RING AT SLIDE PACK. REPLACED LANYARD.

Part: OVEN — SMOKE (GALLEY) · airframe 79,079 hrs · 25,457 cycles

OVEN M305 STARTED TO SMOKE WHEN TURNED ON. REPLACED OVEN OPS CHECKED GOOD.

Part: ALTIMETER — STICKS (COCKPIT) · airframe 77,744 hrs · 25,198 cycles

CAPT ALTIMETER STUCK AT 36280 AND 38680 DURING CLIMB AND DISPLAYED -OFF- FLAG. BARO SET BINDS, REMOVED AND REPLACED CAPTAIN'S ALTIMETER AS PER AMM 34-13-01 004-001 AND 34-13-01-404-004. ALL CHECKS NORMAL OK TO CONTINUE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 77,640 hrs · 25,178 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 4R INOP. REPLACED LAMP AND ACCOMPLISHED OPERATIONAL TEST, MM TASK 33-51-0 0-715-003. TEST OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 77,609 hrs · 25,171 cycles

SLIDE LIGHT AT DOOR 4L INOP. REMOVED AND REPLACED SLIDE LT ASSY AT 4L. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 77,609 hrs · 25,171 cycles

1R SLIDE LIGHT INOP. RELAMPED R1 DOOR SLIDE LIGHT. OPS CHECK GOOD.

Part: NUT — LOOSE (R1 DOOR) · airframe 77,504 hrs · 25,151 cycles

CABIN DOOR 1 RT, SLIDE ARMING LINKAGE BINDS INTERMITTENTLY WITH SLIDE ARMED LIGHT INTERMITTENT AS WELL, FOUND LOOSE NUT ON THE GIRT BAR CRANK THAT WAS CAUSING THE GIRT BAR TO BIND. RESECURED THE NUT, OPS CHECK NORMAL, REF AMM 52-11- 25.

Part: SWITCH — DIRTY · airframe 77,410 hrs · 25,133 cycles

EMERGENCY ESCAPE SQUIB TEST 1 FAILS TEST, THE "L" EMERGENCY ESCAPE LIGHT REMAINS OFF. CLEANED SWITCH LEFT GND DISABLE SWITCH S528 - WD 25-65-11 AND SMP TEST 1 SELF TEST FROM P61 CKS GOOD - FIM 25-65-00-815-802.

Part: INTERCOSTAL — GOUGED (FUSELAGE) · airframe 76,701 hrs · 24,996 cycles

AFT CARGO FWD DOOR CUT-OUT BS 1380 WEB IS GOUGED AT STRINGER 30RT. REMOVED AND REPLACED AFT CARGO FWD DOOR CUT OUT BS 1380 WEB STR RT IAW SRM 51-40-02 PARA 4 AND 7 FIG 3, 8, AND 12 , -2

Part: FITTING — DAMAGED (FUSELAGE) · airframe 76,701 hrs · 24,996 cycles

WEB AT BS 1380 (AFT CARGO CUTOUT) HAS INSUFFICIENT ED DUE TO OUT OF ROUND HOLES 2 EA. IN MOUNTING ANGLE REFERENCE NR 9260412. REMOVED AND REPLACED -2 WEB AND MOUNTING ANGLE BS 1380 IAW SRM 51-40-02 PARA 4,7, AND 9 FIG 3,8, AND 12.

Part: HINGE — CRACKED (R2 DOOR) · airframe 76,701 hrs · 24,996 cycles

CRACK AT R2 DOOR UPPER HINGE CUT OUT. HFEC VERIFIED REPAIRED R2 DOOR UPPER HINGE CUT OUT IAW SRM 52-10-02 REPAIR 1.

Part: STRUCTURE — CORRODED (FWD WASTE PANEL) · airframe 76,701 hrs · 24,996 cycles

FWD LAVATORY WASTE SERVICE PANEL HAS HEAVY BLUE STAIN AND HAS SIGNS OF CORROSION ON INTERNAL SURFACE AT COUPLING ATTACHMENT FLANGE REMOVED FW LAVATORY WASTE SERVICE DRAIN PAN AND SUPPORT ASSEMBLY . ORDER AND RECEIVED NEW DOUBLER AND SUPPORT BRACKET LOCATED AND DRILLED AND ASSEMBLED NEW LAVATORY SUPPORT ASSEMBLY AND INSTALL ED NEW SUPPORT ASSEMBLY AND ORIGINAL DRAIN PAN ASSEMBLY IAW B757 -200 SRM 51-40-02 FIG 2,3,8 AND 12 DOT REMOVED.

Part: STRAP — CRACKED (FUSELAGE) · airframe 76,701 hrs · 24,996 cycles

FAIL SAFE STRAP CRACKED AT RIVET HOLES AT BS 1660 RBL 25. REMOVED AND REPLACED FAIL STRAP AT BS 1660 RBL 25 IAW SRM 51-40-02 PAR 4 FIG 8 PAR 7 FIG 12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 76,701 hrs · 24,996 cycles

CORROSION AROUND FASTENER HOLES ON THE AFT CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE RT SIDE PANEL BETWEEN BS 1380 TO BS 1440 CARGO DOOR LOWER CUTOUT AREA. REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE RT PANEL IN AFT CARGO BS 1380 TO BS 1440 CARGO DOOR LOWER CUTOUT AREA IAW SRM 51-40-02 PAR 7 FIG 12.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 76,701 hrs · 24,996 cycles

CORROSION, KEELBEAM BS 1100. ATTACH ANGLE HAS LITE CORROSION. BS 1100 REMOVED AND REPLACED KEELBEAM ATTACH ANGLE AT BS1100 IAW SRM 51-40-02 PARA 7,D FIG 12.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,053 hrs · 24,478 cycles

CORROSION AT STATION 1401, BETWEEN STRINGER 28L & 29L, REF AVO ESC160413-5688-1D. ACCOMPLISHED FASTENER INSTALLATION AS STEP 27. ACCOMPLISHED REPAIR IAW AVO ALL STEPS COMPLIED WITH AWAITING FINAL ECRA. VERIFIED REPAIR IAW AVO ALL STEPS COMPLIED WITH. FOUND OK FOR SERVICE.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,053 hrs · 24,478 cycles

CORROSION AT STATION 1401, BETWEEN STRINGER 28L & 29L. REF AVO ESC 160413-5688-1D LAST STEP COMPLIED WITH WAS FABRICATION OF REPLACEMENT SPLICE STRAP IAW STEP 13 OF AVO. OPEN HOLE INSPECTION ON ALL REPAIR FASTENERS HOLES, REF 575 NDT 51-00-11. NO DEFECTS NOTED.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,053 hrs · 24,478 cycles

CORROSION AT STATION 1401, BETWEEN STRINGER 28L & 29L IAW AVO ESC 16043-5688-1D, ACCOMPLISHED STEPS 14 & 15. FABRICATED STRAP ALODINE & PRIMED.

Part: DOUBLER — CRACKED (L2 DOOR) · airframe 70,508 hrs · 23,794 cycles

EXISTING DOUBLER ON L2 DOOR UPPER HINGE CUT OUT CRACKED. REMOVED EXISTING DOUBLER ON L2 DOOR UPPER HINGE CUT OUT AREA. REPAIRED AREA IAW AMM 52-11-00 FIG 801.

Part: OVEN — DIRTY (GALLEY) · airframe 69,909 hrs · 23,680 cycles

OVEN NR 507 SMOKES WHEN HOT. OVEN FOUND TO BE DIRTY IN SIDE WITH CARAMEL. OVEN DEACTIVATED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,907 hrs · 23,490 cycles

PER A CHECK, SEAT EEL FROM SEAT 32 TO SEAT 38, INOPERATIVE. REPLACED BATTERY & BATTERY CHARGER IAW MM 33-51-07-0201. OPERATIONS CHECKED OK.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 68,907 hrs · 23,490 cycles

PER A CHECK, SEAT EEL AT SEAT 30, INOPERATIVE. FOUND CONNECTOR UNDER SEAT DISCONNECTED. SECURED CONNECTOR. OPERATIONS CHECKED OK.

Part: OIL SYSTEM — OVERTEMP (NR 2 ENGINE) · airframe 66,359 hrs · 23,004 cycles

HIGH OIL TEMP NR 2 ENG. EMERGENCY DECLARED & EQUIPMENT REQUESTED.

Part: VENT — OUT OF POSITION (COCKPIT) · airframe 65,930 hrs · 22,921 cycles

LOUD RATTLE COMING FROM CAPTAIN`S NR 3 WINDOW AIR VENT DURING CLIMBS IN DESCENT CRUISE OK. RAN LT & RT PACKS SEPARATELY & SIMULTANEOUSLY, HEARD SOME MINOR RATTLING COMING FROM NR 3 WINDOW DISCHARGE VENT, RE-POSITIONED VENT OKAY.

Part: UNKNOWN — MALFUNCTIONED (L2 DOOR) · airframe 65,934 hrs · 22,922 cycles

DOOR 2L WILL NOT ARM. OPENED & CLOSED DOOR, DOOR NOW ARMS.

Part: RELEASE CABLE — DETACHED (EVAC SLIDE) · airframe 65,904 hrs · 22,916 cycles

DURING FCD NO 2560-02556, FOUND RT OVERWING SLIDE RELEASE CABLE NOT ATTACHED TO QUICK RELEASE PIN. RE-ATTACHED CABLE IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 65,773 hrs · 22,890 cycles

AFT EMERGENCY LIGHT AT SEAT 3AB MISSING COVER. REPLACED LENS COVER. LIGHT OPERATIONS CHECKED OK.

Part: LANYARD — FAULTY (L4 DOOR) · airframe 65,733 hrs · 22,882 cycles

DOOR 4L UNABLE TO ARM. REINSTALLED LANYARD DOOR OPERATIONS CHECKED OKAY.

Part: DOOR — OBSTRUCTED (CABIN) · airframe 65,712 hrs · 22,878 cycles

DOOR 4L WILL NOT ARM OR DISARM. CLEARED DEBRIS ON DOOR THRESHOLD, OPERATIONS CHECKED OKAY.

Part: CAM — FAULTY (R1 DOOR) · airframe 65,677 hrs · 22,871 cycles

DOOR NR 1R WILL NOT OPEN FROM THE OUTSIDE & BUTTERFLY HANDLES WILL NOT STOW. REMOVED DOOR HANDLES, FOUND OUTER SHAFT BINDING ON BEARING, TORQUED NUT, REASSEMBLED TO MM 52-11-13 STEP L PG 208, FAILED INSPECTION. REMOVED AGAIN FOUND PEDESTAL CRACKED & SPACER & SEAL ITEM 355, 360, 345, 430 MISSING. IAW IPC 52-11-13-001C REPLACED PEDESTAL, BASKET CAM ASSEMBLY & MISSING ITEMS. REINSTALLED IAW MM 52-11-13.201. OPERATIONS GOOD.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 65,671 hrs · 22,870 cycles

LT FUEL TANK INDICATOR BLANK ON WING & COCKPIT INDICATOR. SUSPECT WIRING.

Part: LANYARD — OUT OF POSITION (BATTERY PACK) · airframe 65,251 hrs · 22,789 cycles

STATION 1100, LT SIDE, BATTERY PACK UNDER CEILING PANEL FOR EMERGENCY EXIT LIGHT SYSTEM, HAS FABRIC LANYARD ATTACHED OVER THE BATTERY PACK & ATTACHED TO AN INCORRECT ATTACHMENT POINT. REPOSITIONED & SECURED LANYARD UNDER BATTERY PACK TO CORRECT ATTACHMENT POINT.

Part: DOOR FRAME — LEAKING (R2 DOOR) · airframe 65,117 hrs · 22,763 cycles

EXCESSIVE AIR NOISE COMING FROM R2 DOOR DURING DESCENT. PRESSURIZED ACFT AFTERWARD, NO LEAKS NOTED. ACCOMPLISHED REPAIR ON LWR FWD AND LOWER AFT DOOR FRAME.

Part: WIRE — BROKEN (TERMINAL BLOCK) · airframe 65,117 hrs · 22,763 cycles

DURING SQUIB TEST, FOUND BROKEN WIRE W2078-084-20 AT TB121 (C024. WD26-22-21, PG 2. REPLACED TERMINAL BLOCK MODULE TB121 Y23-Y24. CRIMPED NEW PINS ON WIRES W2078-0047-22, W2080-0041-22, W2156-A-WT, W2156-0156-24, W2078-0051-22, W2080-0043-22, W2078-0284-20, & W2156-0118-20. INSTALLED WIRES INTO TB121 Y23-Y24. SECURED WIRES. OPS CHECK P61 PANEL FUNCTIONS OK. WDM 26-22-21, 29-22-11, 33-11-61.

Part: UNKNOWN — NO TEST (APU) · airframe 65,112 hrs · 22,759 cycles

SQUIB TEST BAD ON APU TEST 1 ONLY. TEST 2 FOR APU TESTS CORRECTLY. ONLY TEST 1 FOR THE APU DOES NOT TEST. TEST 1 IS SUPPOSE TO WORK IAW AMM.

Part: WIRE — BROKEN (FWD HANDSET) · airframe 65,112 hrs · 22,759 cycles

FWD HANDSET INOPERATIVE. FOUND W0509-4251Y AND 4251B WIRES BROKEN AT HANDSET JACK D939, AND BAD HANDSET. REPAIRED AND RESOLDERED ALL 5 WIRES AT D939 REF GNMM 20-10-13 AND REPLACED HANDSET REF 23-42-11. OPS CHECK GOOD.

Part: HANDSET — INOPERATIVE (COCKPIT) · airframe 65,112 hrs · 22,759 cycles

MID HANDSET INOPERATIVE. FOUND BAD HANDSET. REPLACED HANDSET AND REF PTT 1122006 FOR ADDITIONAL REPAIRS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,108 hrs · 22,758 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 3B. REPLACED LAMP, OPS AND FUNCTIONAL CHECKED GOOD.

Part: FLOORBEAM — DAMAGED (BS 365, RBL 61) · airframe 65,108 hrs · 22,758 cycles

BS 365, RBL 61, MAIN CABIN FLOORBEAM AFT FLANGE FASTENER HOLE TOO CLOSE TO EXISTING PLUGGED FASTENER HOLE. REMOVED DAMAGE IAW SRM 51-10-2 AND 53-00-51, FIG 201. FABRICATED ANGLES, FILLERS AND STRAPS IAW REO G16837, REV B AND SRM 53-00-51, FIG 201, REPAIR 5. MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 377) · airframe 65,108 hrs · 22,758 cycles

BS 377, RBL 61, MAIN CABIN FLOORBEAM UPPER TEE FWD FLANGE, NEW FASTENER HOLE LOCATED NEXT TO EXISTING PLUGGED FASTENER HOLE. REMOVED DAMAGE, FABRICATED REPAIR ANGLES, STRAPS, AND FILLERS, AND DOUBLER AND INSTALLED IAW SRM 53-00-51, REPAIR 5 AND REO G16388, REV A AND ECRA 5310- 05801. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1600) · corrosion level 2 · airframe 65,108 hrs · 22,758 cycles

MAIN CABIN FLOORBEAM AT BS 1600, RBL 53.6, BOTTOM SURFACE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-51. REMOVED DAMAGED TEE AND FABRICATED TEE REPAIR ANGLE, SPLICE ANGLES AND STRAPS AND INSTALLED IAW SRM 53-00-51, FIG. 201, REPAIR 1. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 65,108 hrs · 22,758 cycles

FLOORBEAM, BS 1640, LBL 10 - RBL 56 HAS SPOTS OF CORROSION. FLOORBEAM REPAIRED IAW SRM 53-00-01. REPAIR 10.

Part: SEAL — LEAKING (L2 DOOR) · airframe 65,093 hrs · 22,752 cycles

L2 DOOR HAS THREE LEAKS AROUND DOOR WHEN PRESSURIZED, ONLY LOWER LEAK MAKES HISSING SOUND. ACCOMPLISHED REPAIR IAW AMM AND PRESSURIZED. NO AIR LEAK NOISES NOTED PRESSURIZED TO 6. 0 DIFFERENTIAL PRESSURE.

Part: DOOR — BINDING (L2) · airframe 65,093 hrs · 22,752 cycles

L2 DOOR FAULTS, LATCHING DOOR BINDS IN LOWER FWD LATCH CAM ROLLER. REPLACED L2 DOOR, DOOR OPS CHECKED GOOD.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 64,762 hrs · 22,644 cycles

NR 2 ENGINE HAS A MASSIVE HYDRAULIC LEAK. REPLACED HYDRAULIC LINE IN NR 2 ENGINE PYLON FOR THRUST REVERSER DEPLOYMENT. OPS AND LEAK CHECKED GOOD.

Part: MECHANISM — LACK OF LUBE (R4 DOOR) · airframe 64,523 hrs · 22,563 cycles

DOOR 4R WILL NOT ARM. LUBE DOOR ARM MECHANISM. CYCLE DOOR ARM HANDLE, OPS CHECK GOOD.

Part: LANYARD — OUT OF POSITION (L2 DOOR SLIDE) · airframe 64,400 hrs · 22,525 cycles

LONG PIECE OF STRING HANGING OUT SLIDE PACK DOOR 2L RESTOWED LANYARD.

Part: LINE — LOOSE (DUCT PRESSURE) · airframe 64,265 hrs · 22,485 cycles

DURING CLIMB RIGHT DUCT PRESSURE 15 PSI LEFT 40 PSI. LINES FOUND LOOSE. SECURED LINES, OPS CHECK PNEUMATIC SYSTEM IAW JRH 2-5-16, ALL PARAMETERS NORMAL.

Part: LANYARD — DISLODGED (L2 DOOR SLIDE) · airframe 64,175 hrs · 22,460 cycles

LANYARD HANGING OUT OF DOOR 2L SLIDE PACK. ADJUSTED HANGING LANYARD. PACKED LANYARD TO SLIDE PACK. OPS CHECKED GIRT BAR OPERATION AND WORKS CORRECTLY.

Part: SWITCH — MALFUNCTIONED (FUEL PANEL) · airframe 63,757 hrs · 22,320 cycles

FOUND FUELING PANEL DOOR LIGHT STAYS ON WHEN THE DOOR IS NOT IN FULL OPEN POSITION. REPLACED DOOR SWITCH PER MM, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,720 hrs · 22,310 cycles

LEFT AFT OVERWING ESCAPE HATCH, AFT EMERGENCY ESCAPE LIGHTING, AFT BULB INOPERATIVE. REPLACED BULB, OPS CHECKED GOOD.

Part: ARM — FAULTY (WINDSHIELD WIPER) · airframe 63,490 hrs · 22,237 cycles

F/O,S WINDSCREEN WIPER HAS METAL PIECE STICKING UP. REPLACED ARM ASSY PER MM. ADJUSTED AND OPERATIONAL CHECKS GOOD.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 63,236 hrs · 22,153 cycles

DOOR 4R HAS SEAL LEAK. FOUND BROKEN PIECE OF SEALANT STUCK ON THE AFT GIRT BAR. REMOVED DEBRIS AND CLEANED AREA. ADVICE OUT BOUND CREW TO IDENTIFIED THE AREA IF IT HAPPENS AGAIN.

Part: CHILLER — FAULTY (GALLEY) · airframe 62,661 hrs · 21,950 cycles

CREW REPORT: AFT CHILLER IN FWD GALLEY FAULTED. INSPECTED CHILLER AND ADJACENT ARE AS ALSO E&E COMPARTMENT, NO EVIDENCE OF ELECTRICAL ODOR. INOP'D THE CHILLER, PULLED AND COLLARED CHILLER C.B'S PER MEL 2520L. WHEN REPLACING CHILLER, ROUTE THE UNSERVICABLE CHILLER TO ENGINEERING HOLD, DUE TO REPORT OF ELECTRICAL SMELL WHEN CHILLER WENT INOP. REMOVED AND REPLACED CHILLER, OPS CHECK GOOD.

Part: PBE — UNSERVICEABLE (CABIN) · airframe 62,580 hrs · 21,923 cycles

FORWARD FLIGHT ATTENDANT SEAT PBE IS NOT 'FIRM AND HARD'. REPLACED PBE.

Part: START VALVE — FAULTY (RT ENGINE) · airframe 62,516 hrs · 21,907 cycles

RIGHT ENGINE FAILED TO ROTATE WHEN GROUND START INITIATED. REPLACED STARTER ROBBED AND STARTER VALVE NEW FROM STOCK PER AMM.

Part: ENGINE — FAILED (NR 2) · airframe 62,413 hrs · 21,875 cycles

ENGINE VIBRATION, RETURNED TO FIELD. FOUND SMALL METAL PARTICLES IN TAIL PIPE AND ABNORMAL NOISE DURING SHUTDOWN. REPLACED ENGINE.

Part: ENGINE — VIBRATION (NR 2) · airframe 62,413 hrs · 21,875 cycles

CREW REPORTED DURING CLIMB POWER, NR 2 ENGINE VIBRATION INDICATION AT 3.0 UNITS, AT APPROXIMATELY 88 PERCENT N1. VIBRATION FELT IN AIRFRAME. VIBRATION LEVEL DID DECREASE WITH REDUCTION IN N1 SPEED. NR 2 ENGINE REPLACED.

Part: SEAL — LEAKING (R1 DOOR) · airframe 62,294 hrs · 21,830 cycles

PRESSURE LEAK R10DOOR FROM TOP L AFT TO TOP MID DOOR. SECURED SEAL AND PRESSURIZE AIRCRAFT. FOUND NO LEAK AT 4.TO 5.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 62,052 hrs · 21,750 cycles

EMERGENCY LIGHT AT FWD CLOSET IS INOPERATIVE. CONNECTED EMERGENCY LIGHT, OPS CHECKED GOOD.

Part: PLACARD — UNSECURE (ROW 20DEF) · airframe 61,531 hrs · 21,570 cycles

EXIT ROW PLACARD IN ROW 20 DEF FELL OFF. SECURED EXIT ROW SIGN.

Part: SNUBBER — FAULTY (LIFE RAFT) · airframe 61,527 hrs · 21,569 cycles

FORWARD AND AFT LIFE RAFT COMPARTMENT GAS CARTRIDGE ARE FLAT CAUSING DOORS TO OPEN QUICKLY WITHOUT SNUBBING ACTION. SAFETY ISSUE, REMOVED AND REPLACED 4 FWD AND AFT RAFT COMPARTMENT SNUBBERS IAW AMM 25-22-03.

Part: SHEAR TIE — CORRODED (BS 1520) · corrosion level 2 · airframe 61,525 hrs · 21,568 cycles

CORROSION ON SHEAR TIE AT BS 1520 BETWEEN STRINGERS 29L-28L. REMOVED CORROSION AND FOUND SHEAR TIE TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,525 hrs · 21,568 cycles

UPPER CROWN, AT STR 6 RT, 24 TO 40 INCHES AFT OF DOOR 1 RT, 2 LIGHTNING STRIKES IN SKIN. REPAIRED IAW SRM 53-00- 01, REPAIR 6, SECT II, ITEM 5.

Part: SHEAR TIE — CORRODED (BS 1520 S29-28L) · corrosion level 2 · airframe 61,525 hrs · 21,568 cycles

CORROSION ON SHEAR TIE AT BS 1520 BETWEEN STRINGERS 29L-28L. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION AND FOUND SHEAR TIE TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1580 S27-28L) · corrosion level 2 · airframe 61,525 hrs · 21,568 cycles

CORROSION ON SHEAR TIE AT BS 1580 BETWEEN STRINGERS 27-28L. REMOVED FABRICATED AND INSTALLED SHEAR TIE IAW SRM 51-10-02 AND SRM 51-30-01.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 61,525 hrs · 21,568 cycles

STA 365 FLOORBEAM CORRODED BELOW-RBL 70. FABRICATED AND INSTALLED TEE CHORD, 2 ANGLES, AND 2 STRAPS. FABRICATED 4 CLIPS, AND 2 ANGLES, INSTALLED CLIPS & ANGLES ALONG WITH 2 PREVIOUSLY REMOVED INTERCOSTALS PER SRM'S 51-40-02 AND 53-00-51 FIG 201.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 61,525 hrs · 21,568 cycles

FLOORBEAM BS 324 RBL 42-70 CORRODED. CUT-OUT BS 324 FLOORBEAM FROM LBL10 - RBL70. ACCOMPLISHED NDT OF TRIMMED EDGE AND EXISTING HOLES COMMON TO REPAIR. NO CRACKS FOUND. FABRICATED AND INSTALLED REPAIR ANGLES, STRAPS AND REPAIR REF EA PT57-53-002 AND ECRA 5310-05492.

Part: SKIN — DAMAGED (AROUND 4R DOOR) · airframe 61,525 hrs · 21,568 cycles

R4 DOOR DAMAGED, DENTED, AND CRACKED ON INNER SKIN AT LOWER CENTER ACCESS CUT OUT. REMOVED DAMAGE PERFORMED NDT AND NO CRACKS FOUND. FABRICATED DOUBLER REPAIR AND INSTALLED PER EA57-52-001 AND ECRA 5210-02298.

Part: FLOORBEAM — CORRODED (BS 1661 LBL 15) · corrosion level 2 · airframe 61,525 hrs · 21,568 cycles

AFT CABIN AREA BS 1661 LBL 15 FLOORBEAM CORRODED. CUT-OUT CORRODED AREA REF SRM 53-00-52 FIG 201 REPAIR NR 3. FABRICATED AND INSTALLED UPPER CHORD ANGLES AND STRAP REPAIR REF SRM53-00-51 FIG 201 REPAIR NR 3.

Part: PAN — GOUGED (L2 DOOR HANDLE) · airframe 61,525 hrs · 21,568 cycles

L2 DOOR HANDLE PAN GOUGED IN TWO PLACES. REPLACED HANDLE PAN ON L2 MED PER SRM.

Part: SKIN — DAMAGED (BS 427) · airframe 61,525 hrs · 21,568 cycles

UPPER CROWN FWD OF TCAS, BS 427 BETWEEN BL 0 AND STR 1R HAS STATIC DISCHARGE. DRILLED OUT DAMAGE, PERFORMED HFEC I NSPECTION, NO CRACK NOTED. PERFORMED FHSR OF HOLE PER NDTM 51-00-16, PART 6 NO CRACKS NOTED INSTALLED SOLID FASTENER PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,525 hrs · 21,568 cycles

CORROSION ON SHEAR TIE AT BS 1580 AT STRINGER S-29L TO S-28L. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED SHEAR TIE. FABRICATED & INSTALLED NEW SHEAR TIE.

Part: SKIN — DENTED (BS 610, S16L) · airframe 61,525 hrs · 21,568 cycles

FUSELAGE DENT BS 610, S16L. CUT OUT DAMAGED SECTION OF SKIN, ACCOMPLISHED HFEC OF CUT OUT NO CRACKS NOTED. FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 53-00-01 REPAIR 2 ON NR 4619N00753. MAJOR REPAIR

Part: MODULE — FAULTY (SPEED BRAKE) · airframe 61,404 hrs · 21,528 cycles

REPEAT SPEED BRAKE W-NARM FOR LANDING EICAS MESSAGE SCM 2R FAULTS MODULE WITH HYD PWR ON. REPLACED SCM 2R REF MM. ALL TESTS PASS. CAT III LIBRARY TESTS PASS REF MM. ACFT IN CAT IIIB STATUS.

Part: RESERVOIR — LOW (HYDRAULIC SYS) · airframe 61,375 hrs · 21,517 cycles

WHEN EXTENDING FLAPS THERE IS A LOUD NOISE AND VIBRATION FELT BETWEEN UP AND FLAPS 1. SUSPECTED NOISE AND VIBRATION FROM LOW CENTER RESERVOIR HYD QTY AND LOW HEAD PRESSURE. AFTER SERVICING CENTER RES NO NOISE OR VIBRATION NOTED.

Part: PROCESSOR — MALFUNCTIONED (FUEL QTY) · airframe 61,286 hrs · 21,483 cycles

AIRCRAFT DEVELOPED A 2000 LB FUEL IMBALANCE. FOUND FAULTS LM TU7 & TU3 CONTAMINATION A01 LEG 23. LM TU7,9,3,5 LEG38. REF FIM28-41-00 PG 153. ALSO ACCOMPLISHED DRY CAPACITANCE ALL READING WITHIN LIMITS. REPLACED PROCESSOR, TESTED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,097 hrs · 21,410 cycles

EMERGENCY LIGHT OUTSIDE OF DOOR 1RT INOP. RELAMPED AND REPAIRED SOCKET.

Part: STRAP — UNSECURE (R4 DOOR) · airframe 60,554 hrs · 21,211 cycles

DOOR 4R DOES NOT ARM. RE-SECURED LOOSE D-RING STRAP BLOCKING GIRT BAR, OPS CHECKS GOOD.

Part: CONNECTOR — CORRODED (RT MLG TILT SWIT) · airframe 60,288 hrs · 21,119 cycles

FIRST OFFICER AND RT AUX PITOT HEAT ON WHEN ACFT IS ON GROUND. REPLACED CONNECTOR D4201 TO RT GEAR TILT SWITCH. ALL MESSAGES CLEARED.

Part: CLOCK — FAULTY (COCKPIT) · airframe 59,867 hrs · 20,969 cycles

CAPTAIN'S CLOCK IS FAULTY. DOES NOT MATCH F/O'S. PART NEEDED 480-0342 NOT STOCKED SEAMM. REPLACED CAPT CHRONO. CHECKS OKAY.

Part: LINE — OUT OF POSITION (EVAC SLIDE) · airframe 59,398 hrs · 20,811 cycles

WITH DOOR OPEN 3R SHOWS LINES-STRINGS HANGING OUT OF SLIDE PACK. REMOVED SHROUD. SECURE STRING. INSTALLED SHROUD. ARMED AND DISARMED DOOR. SATISFACTORY OPERATIONS.

Part: PUMP — FAILED (LT ENGINE) · airframe 58,863 hrs · 20,615 cycles

L ENG HYD PUMP OVHT, FLIGHT DIVERTED. REPLACED THE LEFT ENGINE DRIVEN HYD PUMP DUE TO PUMP FAILURE. PUMP FAILURE ALSO CAUSE OF FLUID LEAK.

Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 58,648 hrs · 20,548 cycles

F/A REPORTS DOOR 2R NOT INDICATING FULLY DISARMED WHEN DISARMED. REMOVED SLIDE COVER AND CLEANED FOD FROM SLIDE ENGAGE BAR. SATISFACTORY ARM AND DISARM FUNCTION. REINSTALLED SLIDE COVER. BRIEFED OUTBOUND FLIGHT ATTENDANT AT DOOR 2R.

Part: LANYARD — LOOSE (GIRT BAR) · airframe 61,234 hrs · 21,461 cycles

F/A UNABLE TO ARM DOOR 1R. SECURED LANYARD INSIDE GIRT, ARMING FUNCTION NORMAL.

Part: COMPRESSOR BLADE — DAMAGED (NR 1 ENGINE) · airframe 56,770 hrs · 19,861 cycles

BIRDSTRIKE ON FINAL APPROACH. 1ST STAGE COMP BLADE BENT. BIRDSTRIKE REPORTED ON NR 1 ENG. BLADE DAMAGE FOUND BLADE NR 27 BENT BEYOND LIMITS. REPLACED BLADES 7,8,25,26 IAW MM. ACP ENGINE RUN. NO ABNORMAL VIBRATIONS DETECTED.

Part: FLOORBEAM — CORRODED (STA 1380) · airframe 56,692 hrs · 19,837 cycles

AFT CARGO BAY, STA 1380, RBL 10 TO 13, FLOOR STRAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REPAIRED IAW EA PD57- 53-047 AND UAL EVA-80014, THE REPAIR IS MAJOR AND HAS RECEIVED APPROVAL FOR STATIC STRENGTH ONLY, A NEW FAA 8100-9 FINDING COMPLIANCE WITH CFR 25.571 AND 26.43 MUST BE ISSUED WITH DAMAGE TOLERANCE INFORMATION WITHIN 24 MONTHS FROM 20AUG10. CF IS CREATED FOR NEW FAA FORM 8100-9 IAW EVA-80014 TO MONITOR.

Part: FLOORBEAM — CORRODED (BS 1380) · corrosion level 2 · airframe 56,692 hrs · 19,837 cycles

AFT CARGO BAY, BS 1380, RBL 10 TO 13, FLOORBEAM CORRODED. ACCOMPLISHED REPAIR PER EA PD57- 53-047 AND UAL EVA-80014.

Part: BRACKET — CORRODED (BS 1520 S28R) · airframe 56,692 hrs · 19,837 cycles

CORROSION IS ON TOP OF STR 28R AT STA 1520. ACP SMC3 ON NR CARD 2217N0 0325. REMOVED CLIP BRACKET AT STA 1520, REMOVED CORROSION ON CLIP BRACKET AND REINSTALLED.

Part: FRAME — CORRODED (BS 1460) · airframe 56,692 hrs · 19,837 cycles

AFT CARGO BAY, STA 1460, RBL 16 TO 20, FRAME IS CORRODED. REMOVED CORROSION FROM FRAME SM1460 RBC 16-20 ORIGINAL THICKNESS .063 MATERIAL REMOVED .0004 MATERIAL REMAINING .059, FOUND TO BE WITHIN LIMITS, REINSTALLED ATTACH FITTINGS OF TRANSITION PANEL.

Part: FRAME — CORRODED (BS 1460) · airframe 56,692 hrs · 19,837 cycles

AFT CARGO BAY, STA 1460, LBL 1 TO 9, FRAME IS CORRODED. MAJOR REPAIR ACCOMPLISHED: SMC005 ON NONROUTINE CARD 2217N00334 .

Part: BEAM — CORRODED (BS 1440) · airframe 56,692 hrs · 19,837 cycles

AFT CARGO BAY, STA 1440, TOP OF BEAM IS CORRODED. REMOVED FASTENERS SEAT OF OM. REMOVED LIGHT SURFACE CORROSION FOUND TO BE WITHIN LIMITS NOMINAL MATERIAL IS .063 REMAINING MATERIAL IS .060 MATERIAL REMOVED WAS .003 TREATED AND PRIMED IAW SRM. APPLIED TOP COAT IAW AMM. INSTALLED FASTENERS IAW SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,725 hrs · 19,484 cycles

DOOR NR 4 LT EMERGENCY EXIT LIGHT INOP (EXT). RELAMPED, OPS CK GOOD.

Part: COMPRESSOR — LEAKING (ENGINE) · airframe 53,525 hrs · 18,668 cycles

SMOKE IN THE COCKPIT AND CABIN, RTFL. AFTER TAKEOFF, SMOKE IN THE COCKPIT AND AROUND CABIN ROWS 15 THRU 19, OILY ODOR, TURNED OFF RT RECIRC FAN, SMOKE CLEARED AFTER ABOUT 5 MINUTES. INOP NR 1 PACK, DUE TO SMOKE IN CABIN. FOUND OIL LEAKING FROM BETWEEN NR 2 AND NR 3 COMPRESSORS AND RUNNING DOWN FIXED GUIDE VAN AND TRAILING BACK TO THE 2.5 BLEED PORT. NR 1 ENG WAS REPLACED AND PACK BURNOUT ACP.

Part: COMPRESSOR — LEAKING (ENGINE) · airframe 53,525 hrs · 18,667 cycles

ABORTED TAKEOFF AT 50KTS DUE TO SMOKE IN THE COCKPIT. SMOKE AND OIL ODOR COMING OUT OF COCKPIT EYEBALLS ON TAKEOFF ROLL. ABORTED TAKEOFF, RETURNED TO GATE. 15 MIN IDLE RAN NR 1 ENG. NOTED: NR 1 ENG HAD JUST BEEN CHANGED DUE TO NR 5 BRG LEAKING OIL. COMPLETED POWER ASSURANCE CK ON ENG 1 AND 2. BOTH CHECKED GOOD AND NOTED ON LM1876 AT TAKE OFF POWER NO SMOKE BUT NR 1 ENG HAD SLIGHT OIL ODOR. NONE NOTED ON NR 2 ENG AT TAKE OFF POWER NO OIL ODOR AND ENGINES BLEEDS ON AND PACKS ON. COMPLETED 30 MINUTE ENG BURNOUT PROCEDURE. FOUND OIL LEAKING FROM BETWEEN NR 2 AND NR 3 COMPRESSORS AND RUNNING DOWN FIXED GUIDE VAN AND TRAILING BACK TO THE 2.5 BLEED PORT. R & R ENGINE.

Part: BOTTLE — FAULTY (R1 DOOR) · airframe 52,917 hrs · 18,443 cycles

FWD DOOR ASSIST PRESSURE BOTTLE INDICATES ZERO PSI. REPLACED DOOR 1R PASS, EMERGENCY POWER RESERVOIR BOTTLE.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 51,956 hrs · 18,041 cycles

DURING DEICING RAMP NOTICED PIECE OF SHEET METAL DELAMINATING FROM OUTBOARD L/E OF RT ELEVATOR. DELAM IS LOCATED APPROX 1FT FROM O/B EDGE AND 6 INCHES FROM LEADING EDGE ON UPPER SURFACE. ELEVATOR REMOVED & ROUTED TO SHOP. WAITING FOR SHOP EVALUATION AND ESTIMATE OF REPAIR. APPARENT METAL BONDING STRIP IS PULLED UP. ELEVATOR WAS REPLACED AT SMB. INSPECTION COMPLETE AND OP CHECK ACCOMPLISHED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,341 hrs · 17,460 cycles

NR 3 LEFT MAIN ENTRY DOOR EXT EVACUATION LIGHT INOP. *S/D* BULBS INOP. REPLACED BULBS, OPS CHECKED NORMAL.

Part: GENERATOR — FAILED · airframe 50,326 hrs · 17,456 cycles

GENERATOR FAILURE INDICATION. TAKEOFF ABORTED AT 100 KNOTS. UNKNOWN IDG FAILURE. SHOP FINDINGS NFF. REPLACED IDG AND OPS CHECKED NORMAL. NO REPEATS.

Part: SLIDE — LOW (R1 DOOR) · airframe 50,281 hrs · 17,441 cycles

NR 1 RT MED SLIDE RAFT PRESSURE INDICATION NEEDLE IS AT LWR EDGE OF GREEN BAND. *S/D* UNKNOWN PRESSURE LEAK IN SLIDE. REPLACED NR 1 RT MED SLIDE RAFT.

Part: GIRT BAR — OUT OF RIG (R3 DOOR) · airframe 50,092 hrs · 17,378 cycles

SLIDE 3R ARMED LIGHT WILL NOT ILLUMINATE. TETHER STRAP INTERFERENCE WITH ARMING MECHANISM. REROUTED TETHER FOR GIRT BAR. GND CHECKS OK, ARMS/DISARMS NORMALLY.

Part: LAMP — INOPERATIVE (EXTERIOR) · airframe 49,352 hrs · 17,144 cycles

EXTERIOR EMERGENCY LIGHTS INOP OUTSIDE DOORS 2R AND 4L. FOUND LAMPS INOPERATIVE. REPLAMPED, OPS CHECKED NORMALLY.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 49,079 hrs · 17,050 cycles

FOUND DOOR 1R GIRT BAR IS FAULTY. FOUND DIRT ACCUMULATING UNDER GIRT BAR. CLEANED GIRT BAR TRACKS, DOOR OPERATES, ARMS/DISRAMS NORMALLY.

Part: SEAL — DISLODGED (R1 DOOR) · airframe 48,961 hrs · 17,011 cycles

F/A'S UNABLE TO ARM DOOR 1R. UPPER AFT SECTION OF DOOR SEAL WAS DISLODGED FROM RETAINER. RE-INSTALLED RETAINER, DOOR OPS OK.

Part: GIRT BAR — DIRTY (R3 DOOR) · airframe 48,886 hrs · 16,979 cycles

R3 DOOR WILL NOT ARM. FOUND DEBRIS UNDER GIRT BAR AREA. CLEANED DEBRIS FROM UNDER DOOR R3 AND MOVED LANYARD (POSSIBLE INTERFERENCE), ALL DOORS ARM/DISARM NORMALLY.

Part: LANYARD — LOOSE (R1 DOOR) · airframe 48,800 hrs · 16,950 cycles

FOUND DOOR 1R HARD TO ARM. FOUND LANYARD INTERFERENCE. SECURED LANYARD, DOOR OPS NORMAL.

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 48,642 hrs · 16,888 cycles

DOOR 1R WILL NOT ARM. LANYARD INTERFERENCE. SECURED LANYARD, DOOR ARMS/DISARMS NORMALLY.

Part: BATTERY — WEAK (EMERGENCY LIGHTS) · airframe 48,421 hrs · 16,804 cycles

EMERGENCY EEL STRIP LIGHT IS NOT WORKING FROM ROWS 16-23. FOUND BATTERY CHARGE WEAK. RECHARGED FOR 30 MIN, OPS CHECKED OK. NO REPEATS.

Part: SENSOR — FAULTY (R1 DOOR) · airframe 47,813 hrs · 16,585 cycles

CREW REPORT: DOOR 1R ARMING LIGHT WILL NOT STAY ILLUMINATED IT IS OFF WITH DOOR ARMED.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 47,669 hrs · 16,533 cycles

DOOR 2L DIFFICULT TO ARM. RESECURED SLIDE LACING AND THE ARMING OF DOOR RETURNED TO NORMAL.

Part: LANYARD — UNSECURE (L2 DOOR SLIDE) · airframe 47,594 hrs · 16,509 cycles

CREW REPORT: DOOR 2L SLIDE RAFT LANYARD UNFASTENED FROM COVER. 10-30-07 SECURED LANYARD.

Part: ENGINE — MAKING METAL (NR 2) · airframe 47,464 hrs · 16,460 cycles

CREW REPORTED NR 2 ENGINE SHUTDOWN DUE TO HIGH OIL TEMPERATURE 178-179 DEGREES AND ENG OIL BYPASS MESSAGE. OIL QTY AND PRESSURE NORMAL. ENGINE WAS SHUT DOWN FOR ABOUT 20 MINUTES PRIOR TO LANDING. INSPECTED CHIP DETECTORS AND ALL DETECTORS ARE FULL WITH METAL.

Part: BEARING — FAILED (AGB) · airframe 47,464 hrs · 16,460 cycles

RTFL DUE TO HIGH OIL TEMPERATURE & ENGINE OIL BYPASS MESSAGE. 10-19-07 ON DESCENT OIL TEMP SPIKED TO 171. 161 TO 171 DURING ENTIRE DESCENT. SUPPLEMENTAL DATA UPDATE ANGLE GEARBOX AB1 BEARING FAILED AND OUTER RACE OF BEARING FRACTURED. ALUMINUM BASE MATERIAL OF AGB HOUSING RELEASED DURING THE FAILURE EVENT CLOGGED THE OIL FILTER TO TRIP THE DELTA P SWITCH. ENGINE WAS SHUT DOWN IN A TIMELY MANNER TO MITIGATE ENGINE DAMAGE.

Part: ASPIRATOR — DAMAGED (DOOR SLIDE)

DOOR SLIDE HAS A DAMAGED ASPIRATOR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,971 hrs · 16,283 cycles

EEL LIGHTS INOP ROWS 24-30. REPLACED BATTERY FOR POWER SUPPLY M735.

Part: LANYARD — OUT OF POSITION (RIGHT FWD ENTRY) · airframe 46,819 hrs · 16,227 cycles

FWD RT ENTRY DOOR WILL NOT ARM. [08-08-07] RESECURED LANYARD CORD INTERFERRING WITH GIRT BAR.

Part: LANYARD — MISLOCATED (DOOR 2L) · airframe 45,765 hrs · 15,858 cycles

DOOR 2L SLIDE PACK LANYARD NOT VISIBLE. [06-14-07] FOUND D-RING STUCK UNDER SLIDE PACK. REPLACED LANYARD.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 45,631 hrs · 15,814 cycles

DOOR 1L WILL NOT ARM. ADJUSTED GIRT BAR FLOOR LOCK, DOOR OPS CHECK OK.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 45,516 hrs · 15,779 cycles

EEL FEEDER AT ROW 28 DAMAGED. REPLACED EEL LEAD IN AND OPS CHECK GOOD.

Part: LOCK — OUT OF ADJUST (EVAC SLIDE) · airframe 45,516 hrs · 15,779 cycles

RIGHT OVERWING SLIDE CARRIER LOCK RELEASE TRIGGER IS OUT OF ADJUSTMENT, DOOR WILL NOT LATCH. [SUP 05-18-07] TROUBLESHOT AND FOUND INNER LOCK TUBE WAS NOT CLOCKED PROPERLY WITH LOCK BASE RETAINER PREVENTING CONTACT WITH BEARING. ADJUSTED LOCK BASE RETAINER AND COMPLETED FORCE CHECK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 45,516 hrs · 15,779 cycles

EMERGENCY EXIT LIGHT AT ROW 13 INOPERATIVE. [SUP 4-17-07] TROUBLESHOT AND FOUND CONNECTOR D07274 LOOSE, RECONNECTED AND PERFORMED OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (RAT SWITCH) · airframe 45,516 hrs · 15,779 cycles

AMBER UNLOCK LIGHT ON RAT SWITCH INOPERATIVE. [SUP 05-18-07] RELAMPED SWITCH AND OPS CHECK GOOD. THIS DISCREPANCY IS ATTRIBUTED TO A FUSED LAMP.

Part: PROXIMITY SENSOR — DIRTY (DOOR 1L GIRT BAR) · airframe 45,209 hrs · 15,657 cycles

DOOR 1L ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT DID NOT COME ON WHEN DOOR 1L WAS ARMED. CLEANED DEBRIS FROM PROX SENSOR,

Part: O-RING — DAMAGED (BOTTLE) · airframe 44,641 hrs · 15,444 cycles

LOW BOTTLE. REPLACED BACKUP O-RING AND O-RING.

Part: HOSE — BROKEN (EVAC SLIDE) · airframe 43,101 hrs · 14,858 cycles

HOSE BROKEN AT SWIVEL. INCORRECT PACKING PROCEDURE. REPLACED HOSE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,742 hrs · 14,726 cycles

EMERGENCY AISLE LIGHT INOP IN BULL NOSE AT ROW 13.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,807 hrs · 14,411 cycles

EEL STRIP IN FRONT OF AFT CABIN FWD LAV INOP.

Part: INDICATOR — MALFUNCTIONED (AIRSPEED) · airframe 41,465 hrs · 14,306 cycles

ABORTED TAKEOFF AT 100 KTS AND RETURNED TO THE BLOCKS DUE TO AN AIRSPEED INDICATOR PROBLEM. CAPTAIN'S MACH/AIRSPEED INDICATOR AND LEFT AIR DATA COMPUTER WERE REPLACED IN DEN FOLLOWNG THE EVENT. THE MASI HAD A BROKEN AIRSPEED POINTER RETURN SPRING AND THE DADC HAD BENT & BROKEN PINS ON THE SENSOR CALIBRATION CIRCUIT CARD.

Part: SKIN — DAMAGED (BS 1715 STR 28) · airframe 40,379 hrs · 13,900 cycles

LOWER AFT FUSELAGE LIGHTNING STRIKE AT STA 1715, S28L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME AND INSTALL REPAIR DOUBLER.

Part: SKIN — DAMAGED (BS 1787.43) · airframe 40,379 hrs · 13,900 cycles

LOWER AFT FUSELAGE LIGHTNING STRIKE AT BS 1787.43 LBL 8 AT FASTENER AND SKIN. REMOVED DAMAGE, ACP HEFC INSP, NO CRACKED NOTED. INSTALL REPAIR DOUBLER PER SRM 53-00-01, AND TIMCO REO-G10914, REV A.

Part: FRAME — DENTED (STA 1460) · airframe 40,377 hrs · 13,899 cycles

FRAME DENTED AT STA 1460 BETWEEN S25L AND S26L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10825.

Part: FRAME — DENTED (STA 1440) · airframe 40,377 hrs · 13,899 cycles

FRAME DENTED AT STA 1440 BETWEEN S26L AND S27L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10826.

Part: FRAME — DENTED (STA 1480) · airframe 40,377 hrs · 13,899 cycles

FRAME DENTED AT STATION 1480 BTWN S25L AND S26L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO G10824, REV B.

Part: FRAME — DENTED (STA 1380) · airframe 40,377 hrs · 13,899 cycles

FRAME DENTED AT STA 1380 BETWEEN S26L AND S27L. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10819, REV B.

Part: FRAME — DENTED (STA 1380) · airframe 40,177 hrs · 13,899 cycles

FRAME DENTED AT STA 1540 BETWEEN STR 25R AND STR 26R. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK. FABRICATE, ALODINE, PRIME AND INSTALL REPAIR PER TIMCO REO-G10820, REV B.

Part: FRAME — DENTED (STA 1620, STR 25) · airframe 40,377 hrs · 13,899 cycles

FRAME DENTED AT STA 1620, STR 25R. TRIMMED OUT DAMAGES, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10821, REV B.

Part: FRAME — DENTED (STA 1500 STR 25) · airframe 40,377 hrs · 13,899 cycles

FRAME DENTED AT STA 1500, STR 25L. TRIMMED OUT DAMAGE, ACP HEFC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO REO-G10823.

Part: FRAME — DENTED (STA 1420) · airframe 40,377 hrs · 13,899 cycles

FRAME DENTED AT STA 1420 BETWEEN S26L AND S27L. TRIMMED OUT DAMAGES, ACP HFEC INSP, NO CRACK FOUND. FABRICATE, ALODINE, PRIME, AND INSTALL REPAIR PER TIMCO GEO-10827.

Part: FRAME — BENT (BS 1340) · airframe 40,377 hrs · 13,899 cycles

STA 1340 LEFT HAND SIDE FRAME BENT AT STR 25L. REMOVED EXISTING PRODUCTION SPLICE AND FABRICATED A NEW PRODUCTION SPLICE ANGLE PER TIMCO REO(EVA) G10831, REV C.

Part: FRAME — DENTED (BS 1540) · airframe 40,377 hrs · 13,899 cycles

FRAME DENTED AT STA 1540 AT STR 26L, AFT PIT, INBOARD FLANGE. REPAIRED FRAME WITH NESTED J-ANGLE REPAIR TO EXISTING CHORD PER TIMCO REO (EVA) G10818, REV B

Part: FRAME — DENTED (BS 1400) · airframe 40,377 hrs · 13,899 cycles

FRAME HAS A DENT AT STA 1400 BETWEEN STR 26L AND STR 27L, AFT PIT, INBOARD FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE TO EXISTING CHORD PER TIMCO REO (EVA) G10828, REV B.

Part: SHEAR TIE — CORRODED (STA 1480-1470) · airframe 40,377 hrs · 13,899 cycles

STA 1480 TO 1470 SKIN AND FRAME HAS CORROSION AROUND VHF ANTENNA. REMOVED CORROSION ON SKIN AND FRAME, REPLACED SHEAR TIE PER MM 51-10-02, 51-40-02. MEASURE AFTER DAMAGE REMOVAL, FOUND SKIN AND FRAME ARE WITHIN LIMITS.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 40,377 hrs · 13,899 cycles

CABIN CORROSION UNDER MIKATA BLOCK AT SHEAR WEB, BS APPROX RBL 56.0. REMOVE CORROSION, ACP HEFC INSP, NO CRACK FOUND. INSTALLED REPAIR DOUBLER PER SRM 41-40-02.

Part: SKIN — LIGHTNING STRIKE (STA 860, STR 5L) · airframe 40,377 hrs · 13,899 cycles

LIGHTNING STRIKE DAMAGE AT STA 860, STR 5L. DRILLED OUT DAMAGE PER SRM 53-00-01, ACP HFEC INSP, NO CRACK FOUND. INSTALLED SOLID FASTENER PER MM 53-00-01.

Part: ODOR — DETECTED (CABIN) · airframe 37,616 hrs · 12,876 cycles

LANDED UNDER AMBER DUE TO BURNING ODOR IN CABIN. CAUSE UNKNOWN. NO PRIOR HISTORY BEFORE OR SINCE THIS INCIDENT IN ATA 21 OR 36. ENGINE RUNS, PACK RUNS AND OTHER ELECTRICAL INSPECTIONS FAILED TO PRODUCE ANY DISCREPANCIES. NO PARTS REPLACED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,246 hrs · 11,775 cycles

FUSELAGE SKIN AT STATION 525 & STRINGER 3R IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SWITCH — FAILED (APU OIL SYSTEM) · airframe 26,589 hrs · 9,051 cycles

APU OIL QUANTITY STATUS MESSAGE ILLUMINATED. RIGHT GENERATOR PREVIOUSLY DEFERRED. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED APU OIL CONSUMPTION CHECK. APU WAS CHECKED ONCE FOR OIL CONSUMPTION AND EXTERNAL OIL LEAKS, AND NO DISCREPANCIES WERE FOUND. SUSPECT THE OIL LEVEL SWITCH TO BE GIVING ERRONEOUS INDICATION. REPLACED OIL LEVEL SWITCH.

Part: ACTUATOR — FAILED (LE SLAT)

RETURNED TO ORD DUE TO A LEADING EDGE SLAT PROBLEM. *S/D* POSITION NR 15 LEADING EDGE SLAT ACTUATOR FAILED WHICH CAUSED SYSTEM BINDING AND SHUTDOWN OF THE SLAT SYSTEM AT THE POWER DRIVE UNIT. ALSO, THE OVERLOAD INDICATOR POPPED. REPLACED THE NR 15 SLAT ACTUATOR, RESET OVERLOAD INDICATOR, OPS CHECKED NORMAL.

Part: TUBE — FAILED TEST (SLIDE RAFT)

DURING SHOP OVERHAUL OF SLIDE/RAFT, IT FAILED THE AIR RETENTION TEST. FAILURE DUE TO POROSITY IN THE UPPER TUBE INFLATABLE MATERIAL. SLIDE/RAFT SENT TO VENDOR FOR REPAIR.

Part: LAMP — INOPERATIVE (CABIN)

AFT LEFT HAND EEL LIGHTS AT DOOR 4L ARE INOP. REPLACED LAMP, CHECKS OK.

Part: SHUT OFF VALVE — MALFUNCTIONED (APU)

APU AIR SHUTOFF VALVE WILL NOT GO TO CLOSED POSITION. DEACTIVATED APU AIR BLEED SHUTOFF VALVE IN CLOSED POSITION. *S/D* REPLACED RELAYS K10280 AND K23 IN P37 PANEL WITH NO HELP. REPLACED APU BLEED VALVE, CLEARED ECU AND DUCT PRESSURE WAS NORMAL.

Part: WIRE — ARCED (GALLEY)

GALLEY PIGTAIL, ELECTRICAL CORD SMOKING/SPARKING. *S/D* FRAYED CABLE WAS SHORTING CAUSING THE SMOKING/SPARKING. THE DEFECTIVE CABLE WAS REPLACED, CORRECTING THE PROBLEM.

Part: RAFT — DEPLOYED (CABIN)

LIFERAFT IN AFT CABIN INFLATED WHILE AIRCRAFT CLOSED AND LOCKED FOR OVERNIGHT. INVESTIGATION REVEALED THAT AN INCORRECT O-RING WAS USED IN THE INFLATION CYLINDER REGULATOR. ALL CARLTON REGULATORS WERE RECALLED AND CHECKED. RAFT REPLACED. OPERATION CHECKS NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY LIGHT AT DOOR 2R INOP. REPLACED BULB, OPERATION CHECKS NORMAL.

Part: VALVE BODY — LOOSE (CYLINDER ASSY)

FIRST TIME OVERHAUL ON THE 46 MAN RAFT REVEALED THAT THE VALVE BODY WAS LOOSE FROM THE PRESSURIZATION CYLINDER. CYLINDER PRESSURE WAS ACCEPTABLE, RETORQUED VALVE BODY TO CYLINDER PRIOR TO RECHARGE.

Part: BEARING — SPALLED (NR 1)

AIRCRAFT DIVERTED AND LANDED UNDER AMBER ALERT DUE TO AN OIL FILTER BYPASS LIGHT ON. THE NR 1 BEARING FAILED. FOUND HEAVY SPALLING OF THE OUTER RACE. APPEARS TO BE AN ISOLATED INCIDENT.