N584UA

Part: APU — LEAKING (APU BAY) · airframe 64,103 hrs · 22,436 cycles

AT FL220 FLIGHT REPORTED MID LAV SMOKE DETECTOR ACTIVATED. GRAY HAZE IN CABIN. OIL CONTAMINATION RMVL DUE TO RECENT BLEED DUCT CONTAMINATION CAUSED BY APU OIL LOSS. APU REMOVED AND REPLACED, ACCP TOD MM49- 11-01, UP TO AND INCLUDING, INSTALLATION STEP 5, ITEM 5, PAGE 408. COMPLETED APU INSTALLATION.

Part: APU — FAILED (APU BAY) · airframe 64,102 hrs · 22,435 cycles

CABIN FILLED WITH SMOKE WHILE BROADING PASSENGERS. APU CONFIRMED FAILURE. APU PNEUMATIC DUCT FROM APU FWD BULKHEAD TO STA 1743 NEEDS CLEANING DUE TO OIL INSIDE OF DUCT CAUSED BY APU MALFUNCTION. FOUND KEVLAR, MATERIAL (FOD) IN INLET OF OLD APU INLET SCREEN, NEED TO INVESTIGATE SOURCE, BEFORE INSTALLATION OF NEW APU. INSPECTED INLET DUCT, FOUND NO DETERIORATION. APU INLET DOOR APPEARS TO BE CHANGED IN RECENT HISTORY. SUSPECT LEFT OVER MATERIAL FROM OLD APU INLET DOOR. FIREWALL INSP COMPLETED, APU AIR INLET EXAMINED, FOUND GOOD. CABIN RECIRC FILTERS NEED TO BE RPL'D. RPL'D LEFT AND RIGHT RECIRCULATING FILTERS.

Part: CHIP DETECTOR — UNSECURE (NR 2 ENGINE) · airframe 63,774 hrs · 22,331 cycles

AFTER PARKING GRND CREW REPORTS NR 2 ENGINE PANEL OPEN LEAKING OIL. FOUND LATCH ACCESS PANEL OPEN. LATCHED CLOSED. OPEN FAN COWL AND FOUND NR 4 BEARING MAGNETIC CHIP DETECTOR LAYING IN COWL. NO LEAK FROM HOUSING. REPLACED MAGNETIC PROBE. RAN NR 2 ENGINE FOR 5 MINUTES AT IDLE. CHIP DETECTOR LEAK CHECKS GOOD AND NO OTHER LEAKS FOUND.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 63,651 hrs · 22,285 cycles

R4 DOOR WILL NOT ARM. FOUND LIQUOR CART SAFETY SEAL UNDER AFT GIRT BAR SLIDER OF DOOR 4R. REMOVED SEAL. DOOR 4R ARM'S AND DISARM'S NORMAL PER AMM.

Part: TRACK — DIRTY (COCKPIT WINDOW) · airframe 63,558 hrs · 22,250 cycles

BOTH COCKPIT SLIDING WINDOWS HARD TO OPEN. CLEANED AND LUBED TRACKS, OPS NOW NORMAL.

Part: STRINGER — DENTED (BS 580 S16L) · airframe 62,178 hrs · 21,794 cycles

STRINGER 16 LT AT STA 580 FWD OF DOOR 2L IS DENTED BEYOND SRM LIMITS. INSTALLED REPAIR FILLER, DOUBLER AND FASTENERS FROM STA 590 TO 620 REF AVO1301. FASTENERS AFT OF STA 620 REQUIRE INSTALLATION. STRINGER 16 IS WITHIN LIMITS PER SRM PAGE 102. REINSPECTED AFTER CUTOUT WAS MADE. LT IS WITHIN LIMITS PER SRM AFTER CUTOUT WAS MADE REMEASURED AREA IS 2 INCH BY .062.

Part: MODULATING VALVE — FAULTY (COCKPIT) · airframe 61,535 hrs · 21,562 cycles

COCKPIT TEMP WILL NOT COOL BELOW 86 CABIN TEMPS ARE 74 & 69. DOES NOT OPERATE IN MANUAL OR AUTO TO COOL COCKPIT. DF'D PER MEL. REMOVED & REPLACED COCKPIT TRIM AIR MODULATING VALVE, OPS CHECK GOOD.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 61,015 hrs · 21,373 cycles

R4 DOOR WILL NOT ARM OR DISARM. CLEANED DEBRIS FROM GIRT BAR, CHECKED OKAY.

Part: AUDIO PANEL — MALFUNCTIONED (COCKPIT) · airframe 60,659 hrs · 21,240 cycles

CREW REPORT: ATC REPORTED STUCK MIC IN FLIGHT UNABLE TO COMMUNICATE W/ATC CAUSE UNDETERMINED ALL RADIOS. SAMC TEXT: F-O WAS USING THE RADIOS. COULD NOT XMIT OR RCV UNTIL OBS AUDIO PANEL WAS USED. SWAPPED WITH OBSERVERS AUDIO SEL PANEL, ALL VHF OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,629 hrs · 21,228 cycles

DOOR 1R SLIDE LIGHT DID NOT COME ON DURING EEL BATTERY DRAIN TEST. RELAMPED AND OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,629 hrs · 21,228 cycles

LAST SECTION OF EMERGENCY LIGHT EEL DID NOT COME ON DURING EEL BATTERY DRAIN CHECK. INSTALLED NEW SECTION EEL STRIP AND OPS CHECKS NORMAL JIC 5R33AD216 DURING HMV 3 VISIT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,629 hrs · 21,228 cycles

DOOR 1R SLIDE LIGHT DID NOT COME ON DURING EEL BATTERY TEST. RELAMPED AND OPS CHECKS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 60,629 hrs · 21,228 cycles

EMERGENCY LIGHTS L56, L57, L60, AND L1065 DID COME ON DURING EEL BATTERY DRAIN TEST (COMMON TO POWER SUPPLY M10817). REPLACED M10818 BATTERY CHARGER AND OPS CHECKS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,629 hrs · 21,228 cycles

DOOR 4R CUTOUT HAS 2 EA ATTACH HOLES FOR SCUFF PLATE THAT ARE ELONGATED ALONG FUSE SKIN EDGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER-TRIPLER-QUAD REPAIR REF EC-RA 5330-04171 AND EVA 81518.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,629 hrs · 21,228 cycles

L-H NO-W EMERGENCY ESCAPE LIGHT DID NOT COME ON DURING EEL BATTERY DRAIN TEST. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,629 hrs · 21,228 cycles

EMERGENCY EEL AISLE LIGHT AT ROW 34L DID NOT COME ON DURING EEL BATTERY DRAIN TEST. RELAMPED, OPS CHECKS NORMAL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,629 hrs · 21,228 cycles

FRAME STA 1400 HAS CORROSION FROM RBL 7 TO RBL 12. MAJOR REPAIR ACCOMPLISHED IAW ECRA 5311-01536, EVA 81492, AND S-CO NR 9953206.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,629 hrs · 21,228 cycles

CARGO DOOR LOWER T-CHORD AT STA 1377 HAS CORROSION ON VERT AND HORIZ LEGS. MAJOR REPAIR ACCOMPLISHED IAW ECRA 5310-05421, EVA 81493, AND S-CO NR 9954083.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 60,629 hrs · 21,228 cycles

LEFT SIDE STUB BEAM AT STA 984 FASTNER HOLE NR 3 AND NR 5 OUT OF ROUND. INTERIM REPAIR INSTALLED IAW ECRA 5340-01452 AND EVA 81474. REF ECRA 5340-01452 LEFT STUB BEAM STA 984 TO BE REPLACED WITHIN 24 MONTHS FROM 02NOV11 OR WITHIN 3000CYCLES. CURRENT PTC 21228.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,629 hrs · 21,228 cycles

AFT PIT STA 1400, CORROSION AT INTERNAL SKIN STRAP BETWEEN STR 29R-28R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER RPR REF EC-RA 5330-04169 AND EVA 81500. N-R 9953560.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 60,629 hrs · 21,228 cycles

LEFT SIDE STUB BEAM AT STA 984 FASTENER HOLE NR 5 OUT OF ROUND. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5340-01452, EVA 81474, AND S-CO NR 9953892.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 60,629 hrs · 21,228 cycles

RIGHT SIDE STUB BEAM STA 984 FASTENER HOLE NR 3 OUT OF ROUND REF AVO ESC111018-5684-1. INTERIM REPAIR INSTALLED PER ECRA 5340-01453, EVA 81473, AND S-CO NR 9953844.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 60,629 hrs · 21,228 cycles

RIGHT SIDE STUB BEAM AT STA 984 FASTENER HOLE NR 5 ELONGATED. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5340-01453, EVA 81473A, AND S-CO NR 9953846. STUB BEAM REQUIRES REPLACEMENT WITHIN 24 MONTHS FROM 02NOV11, OR 3000C, WHICHEVER OCCURS 1ST.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,629 hrs · 21,228 cycles

AFT CARGO STA 1400, IGC CORROSION AT INTERNAL STRAP BETWEEN STR 29R AND 28R BELOW RIB. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR. CF9088 CREATED FOR DTA. REF EVA 81500 AND EC-RA 5330-04169.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 60,629 hrs · 21,228 cycles

RIGHT SIDE STUB BEAM STA 984 NR 3 AND NR 5 HOLES OUT OF ROUND. BOTH REPAIRED IAW ECRA 5340-01453,EVA 81473A,TIME LIMITED REPAIR TO BE REPLACED WITHIN 24 MONTHS FROM 02NOV11 OR WITH 3000 CYCLES. REF ECRA 5340-01453, REPLACE RIGHT SIDE STUB BEAM STA 984 WITHIN 24 MONTHS FROM 2NOV11 OR WITHIN 3000 CYCLES.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 60,629 hrs · 21,228 cycles

LEFT SIDE STUB BEAM AT STA 984 FASTENER HOLE OUT OF ROUND. INTERIM REPAIR INSTALLED PER ECRA 5340-01452, EVA 81474, AND S-CO NR 9953891, STUB BEAM REQUIRES REPLACEMENT BEFORE 24 MONTHS FROM 2NOV11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,629 hrs · 21,228 cycles

DEEP BLEND OUT ON CROWN STA 1280 TO 1300, STR 2L. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED IAW SCAL ECRA 5360-01166, EVA 81469, AND SCAL NR 9951619.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,629 hrs · 21,228 cycles

DEEP BLEND OUTS FOUND ON CROWN AT STR 2L, STA 1418. ITEM REPAIRED IAW ECRA 53 60-01167, EVA 81468. EXT SKIN DOUBLER REPAIR INSTALLED AT STA 1418, STR 2L PER SCAL ECRA 5360-01167 AND EVA 81468. SKIN REPAIR MUST RECEIVE NEW FAA FORM 8100-9 SHOWING COMPLIANCE TO 14 CFR 25.571 AND 26.43 (D) AND DTA INCORPORATED IN AC MAINTENANCE PROGRAM WI 24 MONTHS FROM 11-3-11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,629 hrs · 21,228 cycles

SKIN HAS PREVIOUS DEEP BLEND OUT FROM LIGHTNING STRIKE WITH COUNTER SUNK RIVET IN CENTER OF BLEND, STA 240, 3' OTBD OF LT SIDE ACCESSORY DOOR CUTOUT (E&E DOOR). MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED PER SCAL ECRA 5330-04161, EVA 81452, AND NR 9951763.

Part: SHIM — OUT OF ADJUST (ESCAPE HATCH) · airframe 60,629 hrs · 21,228 cycles

LEFT AFT OVERWING ESCAPE HATCH - UNABLE TO OPEN FROM THE OUTSIDE HANDLE - DIFFICULT FROM THE INSIDE. ADJUSTED LT AFT OVERWING ESCAPE HATCH SHIM PER AMM, ON S-CAL NR 9954366.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 60,629 hrs · 21,228 cycles

CABIN FLOORBEAM UPPER CAP STA 365 FROM BL 0 TO RBL 63. (P54-221-011). MAJOR REPAIR ACCOMPLISHED: ITEM REPAIRED IAW SCAL EC RA 5310-05413, EVA81445, AND SCAL NR 9952160.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,629 hrs · 21,228 cycles

CABIN FLOORBEAM STA 324, RBL 44 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REPLACED UPPER T-CHORD SECTION AT STA 324 BETWEEN LBL 14 TO RT FRAME JOINT PER SCAL ECRA 5310-05412 AND EVA 81446.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,629 hrs · 21,228 cycles

CABIN FLOORBEAM STA 1640 LBL 33 TO RBL 58 HAS CORROSION ON UPPER CAP. ITEM REPAIRED IAW SCAL EC RA 5310-05411, EVA 81444, AND CAL NR 9952002.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 60,629 hrs · 21,228 cycles

LEFT OVERWING EMERGENCY ESCAPE SLIDE LIGHT DID NOT COME ON DURING EEL BATTERY DRAIN TEST. LEFT OFF WING SLIDE LIGHT L568 WAS RELAMPED. WORK ACP PER AMM. OPS CHECKS OKAY.

Part: WINDSHIELD — DEFECTIVE (COCKPIT) · airframe 60,402 hrs · 21,137 cycles

1ST OFFICER'S WINDSHIELD'S VISIBILITY IS AFFECTED BY DEFECTS. REPLACE FIRST AVAILABLE. CREW COMMENTS: F/O FWD WINDSHIELD HAS TWO SCORCH MARKS, BOTTOM JUST LEFT OF CENTER AND BOTTOM LEFT CORNER. REPLACED 1ST OFFICERS WINDSHIELD PER MM.

Part: SENSOR — FAULTY (AC PACK) · airframe 60,331 hrs · 21,109 cycles

COCKPIT TEMP UNCONTROLLABLY HOT IN ALL MODES. USE STBY PLZ. GRN CHECK OK STBY. AUTO INOP. OK GRN CHECKS OK BOTH MODES. RDF-T :ZONE PACK & STBY CONTROLLERS ALL BITE TEST OK. REPLACED FLT DECK DUCT TEMP SENSOR TS175 PER MM AND REPLACED FLIGHT DECK ZONE TEMP SENSOR FILTER, BOTH NO HELP. WILL NEED TO CONTINUE TROUBLESHOOTING PER MM. RAN BOTH PACKS FOR 10 MIN. MOVED TEMP CONTROL KNOBS FULL COLD TO HOT AND BACK. FLT DECK AT .01 AND NEVER MOVED. REPLACED LT PACK CONTROLLER, PACK CTRL VALVE, L PACK 2 TEMP SENSOR, L PACK COMP OUTLET 2 TEMP SENSOR. ALL NO HELP. PACK OUT TEMP STILL SHOWS 50 DEGREES. REPLACED PACK TEMP SENSOR AS SUGGESTED BY AMM PG 130 FOR OUT OF CALIBRATION. RAN PACK IN AUTO FOUND PACK WOULD COOL AND ABLE TO VARY COCKPIT TEMP AS DEMANDED WITH TEMP KNOB.

Part: FMU — LEAKING (NR 2 ENGINE) · airframe 60,312 hrs · 21,101 cycles

NR 2 ENG FMU LEAKING FUEL. REMOVED FMU PER AMM. REPLACED FMU, LEAK CHECKS GOOD.

Part: CONVERTER — FAULTY (WINDSHIELD WIPER) · airframe 60,096 hrs · 21,030 cycles

F/O WINDSHIELD WIPER KEPT WIPING WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED THE RIGHT WIPER CONVERTER AS PER MM, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (RT WING) · airframe 60,029 hrs · 21,004 cycles

ONE LAMP INOP IN THE RIGHT WING POSI-NAV LIGHT ASSY. RELAMPED, OPS CHECKED NORMAL.

Part: UNKNOWN — DAMAGED · airframe 60,018 hrs · 21,001 cycles

HAIL DAMAGE. WILL CONTINUE TO MAP OUT AND EVAL DAMAGE.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 59,431 hrs · 20,798 cycles

DOOR 2L WILL NOT ARM. SECURED SURVIVAL KIT LANYARD AT SLIDE GIRT FOR DOOR 2 LEFT.

Part: SKIN — DAMAGED (BS 297) · airframe 59,398 hrs · 20,787 cycles

LT FUSELAGE IS CREASED APPROX 6FT STARTING JUST FWD OF DOOR 1L EXTENDING FWD. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SKIN SECTIONS, AND ACCOMPLISHED GVI AND HFEC INSPECTIONS. FABRICATED 2 EACH DOUBLERS, AND INSTALLED ONE FWD OF BS 297 BUTT SPLICE AND ONE AFT OF SPLICE PER 085625 REO G13659, REV. C ON NON ROUTINE.

Part: LANYARD — OUT OF POSITION (L2 DOOR) · airframe 59,158 hrs · 20,701 cycles

CREW REPORT: DOOR 2L WILL NOT ARM PROPERLY, IT IS DIFFICULT TO MOVE ARMING LEVER. SAMC TEXT: INSPECT DOOR SILL AREA FOR ANY FOREIGN OBJECTS AND CONTACT SAM FOR ARM-DISARM CHECK PAPERWORK. FOUND SURVIVAL LANYARD INTERFERING WITH GIRT BAR. REPOSITIONED LANYARD, OP CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (AFT LAVATORY) · airframe 57,854 hrs · 20,223 cycles

AFT LAVATORY EMERGENCY LIGHT STRIP INOP. REPLACED EMERGENCY LIGHT STRIP AT AFT LAV LOCATION, OPS CHECKED NORMAL.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 57,373 hrs · 20,046 cycles

EXTERIOR EVACUATION LIGHT AT L4 DOOR HAS LENS CRACKED. REPLACED LENS ON LIGHT COVER AND INSTALLED AT 4L DOOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,002 hrs · 19,904 cycles

L4 DOOR EMERGENCY SLIDE LIGHT L56 IS INOPERATIVE. RELAMPED L-4 DOOR EMER SLIDE LIGHT PER MM AND OPS CHECK GOOD ON NON ROUTINE 2198N00005.

Part: FUSE — FAULTY (POWER SUPPLY) · airframe 57,002 hrs · 19,904 cycles

EMERGENCY LIGHT AT L568, BS 1368, WL 180 AND LBL 62 IS INOPERATIVE. REMOVED AND REPLACED FUSE ON EMERGENCY POWER SUPPLY. OPS CHECK GOOD ON NON ROUTINE 2198N00023.

Part: COMPRESSOR BLADE — DAMAGED (LT ENGINE) · airframe 56,861 hrs · 19,852 cycles

L ENG STALL/SURGE, FLIGHT DIVERTED. HPC STAGES 6 THROUGH 17 BLADES DAMAGED BEYOND LIMITS. ENGINE REMOVED.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,574 hrs · 19,748 cycles

FWD CARGO HOLD DOOR AREA AFT OF OPENING NET TIE DOWN HAS CORROSION AND IS BULGED AND HAS ONE POPPED RIVET HEAD. PICTURES HAVE BEEN SENT TO RVI SITE. BEGAN REMOVING FLOOR AND SIDEWALL PANELS FOR ACCESS.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 56,211 hrs · 19,608 cycles

NR 1 ENG LEAKING HYD FLUID. FOUND HYD SUPPLY LINE FOR NR 1 REVERSER, MFG NEW LINE, PRESSURE TESTED LINE. INSTALLED LINE, LEAK CHECKED GOOD.

Part: ENGINE — FLAMED OUT (RIGHT) · airframe 55,912 hrs · 19,493 cycles

RT ENGINE SHUT DOWN ON ITS OWN. PER DISCUSSION WITH F/O, ENGINE FLAMED OUT DURING EXTREMELY HEAVY SNOWSTORM ON TAXI IN. DID NOT ATTEMPT TO RESTART, SINCE ALMOST TO GATE. ACP'D QRC AND SECURED ENG. AFTER AIRCRAFT LANDED AND WAS ON THE GROUND WAITING FOR A GATE TO OPEN UP DURING THE SNOW STORM, APPROX. 1 - 1.5 HOURS THE RIGHT ENGINE INGESTED SNOW AND SLUSH TO THE POINT THE ENGINE SHUT DOWN. INSPECTED INLET AND EXHAUST. NO DISCREPANCIES NOTED. ACCOMPLISHED ENGINE START AND RAN UNDER DIFFERENT ELECTRICAL AND PNEUMATIC LOADS. ALL INDICATIONS NORMAL.

Part: SKIN — DAMAGED (BS 1416 S2L) · airframe 55,912 hrs · 19,493 cycles

LIGHTNING STRIKE ON CROWN AT FRAME STA 1416 AT STR 2L. SKIN NDT'S AT .050. SF HOLE EVALUATED THE OVERSIZE HOLE CONDITION ACCEPTABLE TO INSTALL FREEZE PLUG. BLENDED AREA, ULTRASOUND SHOWS .004" OF MATERIAL LOSS, BLEND WITHIN LIMITS, TREATED PRIMED AND PAINTED.

Part: OXYGEN MASK — FAULTY (1ST OBSERVER) · airframe 55,900 hrs · 19,488 cycles

COPILOT'S OXYGEN MASK HAS A LEAK. SWAPPED F-O O2 MASK WITH FIRST OBSERVER'S SEAT. F-O O2 MASK CHECKED, NO LEAK. F-O O2 MASK CHECKED. NO LEAK WHEN IT IS STOWED IN THE BOX. FIRST OBSERVER'S O2 MASK INOP AND SEAT CONSIDERED INOP.

Part: SLIDE — DISLODGED · airframe 55,556 hrs · 19,354 cycles

WHILE OPENING MED 1 RT SLIDE ASSY AND BUSTLE DISENGAGED FROM DOOR. REINSTALLED SLIDE ASSY AND BUSTLE.

Part: SKIN — DAMAGED (BS 621-633) · airframe 55,499 hrs · 19,331 cycles

FOUND 3 LIGHTENING STRIKES ON FWD UPPER FUSELAGE, NR 1 AT STA 621, 1 INCH BELOW STR 4R, .100 INCH IN DIAMETER AND .020 INCH DEEP. NR 2 AT STA 626, 1-4 INCH BELOW STR 4R, .150 INCH IN DIAMETER AND .002 INCH DEEP. NR 3 AT STA 633,1-4 INCH BELOW STR 4R, .100 INCH IN DIAMETER AND ,009 INCH DEEP. LIST NR 1 AND NR 3 WITHIN LIMITS. NR 2 REPAIRED WITH SOLID RIVET. ALL STRIKES INSP WITH EDDY CURRENT. NO CRACKS NOTED RII AND EDDY CURRENT INSP ACCOMPLISHED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,466 hrs · 19,319 cycles

EMERGENCY LIGHT FLOOR STRIP LIGHTING AFT 3 ROWS INOP. AFT EMERGENCY STRIP FWD OF AFT LAV INOP. INSTALLED NEW LIGHT STRIP PN 36262-4, CHECK OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,282 hrs · 19,259 cycles

L1 & L2 EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK FOR L1-L2 EXTERIOR EMERGENCY LIGHTS, OPS CHECK GOOD.

Part: SCAVENGE PUMP — CRACKED (LT ENGINE) · airframe 55,055 hrs · 19,167 cycles

LT ENG OIL ISSUES, RTFL. FOUND OIL TEMP RED IN EPCS PAGE AND ECS PAGE SHOWS L OIL PUMP LOW MESSAGE. SERVICED NR 1 OIL WITH 4 QTS OIL. PER SFOLM POSSIBLE ENG SCAVENGE PUMP FAILURE. DRAINED OIL TANK, REMOVED LUBE UNIT AND FOUND SCAVENGE IN PORT HOUSING CRACKED AT IMPELLER. RE-INSTALLED UNIT. REPLACED ENG. ALSO FOUND LEFT ENG INBOARD REVERSER UPPER ACTUATOR LEAKING STATIC. REMOVED & REPLACED ACTUATOR, OP CHECKS GOOD. AT THE NR 1 ENG INBOARD UPPER REVERSER ACTUATOR THE SYNC LOCK ATTACHED TO UPPER PART OF ACTUATOR IS LEAKING RAPIDLY. REPLACED SYNC LOCK (P/N TY1878-22 S/N 38).

Part: OXYGEN MASK — DIRTY (COCKPIT) · airframe 54,341 hrs · 18,871 cycles

CAPS SMOKE MASK NEEDS TO BE CLEANED OR REPLACED. VISION OBSCURED. REPLACED MASK.

Part: LIGHT — UNSECURE (SEAT 34C) · airframe 54,286 hrs · 18,852 cycles

EMERGENCY ESCAPE PATH LIGHTING SEAT 34C TORN LOOSE FROM PLASTIC HOUSING. FOUND BLACK END CAP ON THE END OF FLOOR EMERGENCY LIGHT STRIP OFF, TAPED DOWN AS AN INTERM REPAIR WITH TAPE. SECURED CAP, LIGHTS CHECK NORMAL.

Part: FITTING — OBSTRUCTED (GIRT BAR) · airframe 54,130 hrs · 18,798 cycles

DOOR 3R ARMED LIGHT NOT COMING ON. REMOVED LEMON WEDGE FROM AFT GIRT FITTING. DOOR SLIDE LIGHT OPERATION IS NORMAL.

Part: FEEDER CABLE — CUT (EMERGENCY LIGHTS) · airframe 53,797 hrs · 18,676 cycles

LAV-K LIGHT BAR INOP. FOUND CABLE CUT. SPLICED IN NEW SECTION OF CABLE. OPS CHECKS GOOD.

Part: PROXIMITY SWITCH — FAILED (EVAC SLIDE) · airframe 52,733 hrs · 18,267 cycles

SLIDE LIGHT OVER 3L INOPERATIVE. REPLACED FWD PROXIMITY SWITCH S10223, OPS CHECKED OKAY.

Part: LIGHT — BROKEN (CABIN) · airframe 51,392 hrs · 17,781 cycles

EMERGENCY LIGHT STRIP, LAST FEW FEET BROKEN OFF. REPAIRED EMERGENCY LIGHT WIRING AND REPLACED TRACK.

Part: O-RING — LEAKING (SLIDE BOTTLE)

ESCAPE SLIDE HAS A LOW BOTTLE. BOTTLE TO VALVE O-RING LEAKING. REPLACED O-RING

Part: WIRE — MISSING (CABIN TEMP) · airframe 48,709 hrs · 16,855 cycles

FLIGHT DIVERTED DUE TO CABIN TEMPERATURE PROBLEMS. INDICATION PROBLEMS - FOUND SEGMENT OF AFT CABIN TEMP INDICATION WIRING MISSING. REPLACED MISSING SEGMENT.

Part: STAB SYSTEM — MALFUNCTIONED · airframe 48,387 hrs · 16,728 cycles

PRIOR TO TOUCHDOWN STABILIZER RAN UNCOMMANDED TO FULL UP TO LIMIT.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 48,363 hrs · 16,718 cycles

FOUND CORROSION IN AFT PIT AFT OF DOOR. FOUND CRACKED FLOOR SUPPORT WHICH WAS REPAIRED. AFT CARGO PIT WAS FOUND DAMAGED AT ALL THREE AFT PIT FLOORBOARDS. SEVERAL PULLED SCREWS AT MULTI SPOTS TO CAUSE EDGE DELAMINATION DAMAGE. SOME DAMAGE IS LARGER THAN 1 INCH AND AT LEAST ONE HAD PUNCTURED THROUGH IN PANEL. THIS IS A MAJOR CORROSION REPAIR. REPLACED AFT CARGO FLOORBOARDS THAT ARE NOT REPAIRABLE.

Part: OXYGEN MASK — BROKEN (FIRST OFFICER'S) · airframe 48,194 hrs · 16,652 cycles

FIRST OFFICER'S O2 MASK BROKEN.

Part: GIRT BAR — CONTAMINATED (R1 DOOR SLIDE) · airframe 48,011 hrs · 16,589 cycles

LIGHT FOR SLIDE AT DOOR 1R INOPERATIVE. 10-11-07 FOUND DEBRIS IN GIRT SLIDER AREA ON FLOOR CLEANED DEBRIS, LUBED SLIDE TRACKS AND CYCLED DOOR SEVERAL TIMES AND FOUND NORMAL OPERATIONS OF SLIDE LIGHT AND NORMAL ENGAGEMENT OF GIRT BAR.

Part: STATIC LINE — TANGLED (R1 DOOR GIRT BAR) · airframe 47,611 hrs · 16,446 cycles

ARMING LIGHT DID NOT ILLUMINATE DOOR 1R. 08-31-07 FOUND STATIC LINE TANGLED IN GIRT BAR CAUSING NO INDICATION. SECURED STATIC LINE PER UAL ENGINEERING SPECIFICATIONS AND SERVICE TIP.

Part: GIRT BAR — FAULTY (R1 DOOR) · airframe 46,857 hrs · 16,181 cycles

DOOR 1R WILL NOT ARM.

Part: BEARING — FAILED (GEARBOX) · airframe 46,504 hrs · 16,057 cycles

FLIGHT LANDED UNDER AMBER ALERT DUE TO ENGINE SHUT-DOWN ON FINAL. [SUP 05-24-07] THIS OCCURRENCE WAS DUE TO ANGLE GEARBOX BEARING FAILURE CAUSED BY EXCESSIVE VIBRATORY STRESS. THIS IS BELIEVED TO HAVE BEEN THE RESULT OF AN IMPROPER BALANCING OF THE LOWER TOWER SHAFT WHICH COULD HAVE OCCURRED DURING INITIAL STAGE OF MANUFACTURE AT THE OEM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,677 hrs · 15,384 cycles

LIGHTNING STRIKE DAMAGE ABOVE STR 6 RT AND STA 465. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA. NDT CUT- OUT AND FASTENER HOLES. INSTALLED DOUBLER.

Part: LIGHT — INOPERATIVE (DOOR 1R) · airframe 44,282 hrs · 15,237 cycles

EMERGENCY SLIDE LIGHT INOPERATIVE AT DOOR 1R.

Part: INDICATOR — MALFUNCTIONED (AIRSPEED) · airframe 41,648 hrs · 14,321 cycles

RETURNED TO THE FIELD DUE TO AN ERRATIC AIRSPEED INDICATOR. NUMBER 2 MACH AIRSPEED INDICATOR WAS REPLACED. THE AIRSPEED POINTER RETURN SPRING WAS FOUND BROKEN.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,463 hrs · 13,519 cycles

AFT CARGO FRAME STA 1520 AT STR 25L, FRAME IS DENTED. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,463 hrs · 13,519 cycles

AFT CARGO FRAME STA 1500 AT STR 25L-27L. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,463 hrs · 13,519 cycles

AFT CARGO FRAME STA 1540, NEAR STR 26L, FRAME DENTED. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,463 hrs · 13,519 cycles

AFT CARGO FRAME IS DENTED AT STA 1420 AT STR 25-26L. FRAME DENT WAS CUTOUT AND A DOUBLER REPAIR WAS INSTALLED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 39,460 hrs · 13,517 cycles

STRINGER 22L CORRODED AT STA 700 TO 720. DAMAGE CAUSED BY CORROSION. MAJOR REPAIR ACCOMPLISHED. STRINGER DAMAGE WAS TRIMMED OUT AND A DOUBLER REPAIR WAS INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,460 hrs · 13,517 cycles

DENT WAS FOUND AT BS 1708 STR 17R APPROX 2 INCHES LONG. DENT DAMAGE ON FUSELAGE SKIN CAUSED BY IMPACT. DAMAGE TO THE SKIN WAS CUTOUT AND A DOUBLER, TRIPLER, AND FILLER REPAIR STACKUP WAS INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,460 hrs · 13,517 cycles

AFT PIT STA 1580 AT STR 26L FRAME DENTED. FRAME DENT DAMAGE WAS TRIMMED AND A DOUBLER REPAIR WAS INSTALLED.

Part: O-RING — LEAKING (EVAC SLIDE)

LOW BOTTLE PRESSURE. PRESSURE LEAKING AT SHAFT O-RING. REPLACED SHAFT O-RING, BACK-UP O-RING, BALL SEAT, GAGE ADPATER O-RING.

Part: LIGHT — INOPERATIVE (ESCAPE SLIDE) · airframe 33,936 hrs · 11,645 cycles

EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE AT DOOR 4L.

Part: SKIN — CRACKED · airframe 33,007 hrs · 11,318 cycles

FUSELAGE EXTERNAL SKIN IS DENTED AND CRACKED AT BS 1520, STRINGER 23R. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED WITH DOUBLER.

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 30,981 hrs · 10,574 cycles

LT ENGINE COMPRESSOR STALL AT CLIMB THRUST CLIMBING THROUGH 10,000 FT. ENGINE RECOVERED AND CONTINUED NORMAL OPERATION. THE 14TH STAGE BLEED CONVERTER VALVE WAS REPLACED AS PRECAUTIONARY ALONG WITH EEC AS A RESULT OF EICAS MESSAGE 275-27. COMPONENT SHOP CURRENTLY INVESTIGATING 14TH STAGE BLEED CONVERTER VALVE AND EEC TO VERIFY FAILURE.

Part: ENGINE — STALLED (NR 1) · airframe 28,195 hrs · 9,558 cycles

NR 1 ENG STALLED DURING DECELERATION TEST AFTER FMU REPLACEMENT. STABLIZED AT IDLE FOR 10 MIN. ENG STALLED ON SECOND ATTEMPT AT APPROX 80 PERCENT N1 ON DECELERATION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,653 hrs · 8,292 cycles

ELECTRONIC INDICATION AND CREW ALERT SYSTEM MESSAGE, MAIN BATTERY CHARGER DISPLAYED AND BATTERY DISCHARGER LIGHT EXTINGUISHED. *S/D* REPLACED BATTERY CHARGER AND MAIN BATTERY. SHOP FINDINGS REPORTS BATTERY DISCHARGED.

Part: CONNECTOR — FAILED (HYD PUMP) · airframe 24,474 hrs · 8,237 cycles

LEFT HAND ELECTRIC HYDRAULIC PUMP FAILED. *S/D* CONNECTOR PIN WAS FOUND BURNED FROM ARCING. REPLACED PUMP AND AC CONNECTOR.

Part: UNKNOWN — ODOR (GALLEY) · airframe 24,137 hrs · 8,114 cycles

RETURNED TO MSP DUE TO ELECTRICAL ODOR IN THE CABIN. *S/D* ODOR REPORTED TO COME FROM MID GALLEY. LINE MAINTENANCE RAN UTILITY BUSSES WITH LOAD FROM MID GALLEY. REMOVED COFFEEMAKER, HOT PLATE AND GALLEY CONT PNL. CHECKED ALL VISIBLE WIRES AND CONNECTIONS IN MID GALLEY. INSTALLED REMOVED COMPONENTS, RESET CIRCUIT BREAKERS. OPERATED HOTPLATE, COFFEEMAKER AND LIGHTS FOR SEVERAL HOURS. NO ODOR OF ANY KIND WAS DETECTED. COFFEEMAKER WARMER MAY HAVE BEEN LEFT ON WITH NO POT ON BURNER. THERE IS NO OTHER PREVIOUS HISTORY AND PRESENTLY NO OPEN LOG WRITE UPS RELATED TO THIS EVENT.

Part: HANDLE — NOT CLOSED (POTABLE WATER)

NO WATER PRESSURE AND LOUD NOISE FROM REAR OF AIRCRAFT. RETURNED TO FIELD. *S/D* THE POTABLE WATER SERVICE FILL VALVE HANDLE HAD BEEN LEFT IN THE OPEN POSITION DURING SERVICING. POTABLE WATER SERVICE FILL HANDLE WAS CLOSED. NO DEFECTS WERE FOUND.

Part: EXTINGUISHER — LOW PRESSURE (APU)

APU FIRE BOTTLE DISCHARGE LIGHT ON. APU FIRE BOTTLE LOW ON PRESSURE, SO APU RENDERED INOP. *S/D* APU FIRE EXTINGUISHER WAS FOUND TO HAVE LOW PRESSURE. REPLACED THE APU FIRE EXTINGUISHER AND RELATED SQUIB PER 757MM 26-22-01. PERFORMED OPERATIONAL CHECK AFTER REPLACEMENT PER SAME 757 MM, AND FOUND THAT SYSTEM CHECKED OK.

Part: SHOCK MOUNT — FAILED (CABIN)

OVERHEAD VIDEO MONITORS NR 5 AND NR 6 FELL TO FLOOR DURING LANDING. AIRCRAFT EXPERIENCED EXCESSIVE VIBRATION AFTER LANDING AT SFO. THE VIDEO MONITOR SHOCK MOUNTS FAILED TO SUPPORT MONITORS NR 5 AND NR 6. UAL COA 50403 IMPLEMENTED BOEING SERVICE BULLETIN 757 23 0045 (INSTALL SOLID MOUNTS). LANDING CONDITIONS ARE STILL UNDER INVESTIGATION.

Part: PIN — FAILED (NLG)

AIRCRAFT EXPERIENCED HEAVY VIBRATION AND UNDER FUSELAGE SMOKE DURING LANDING SFO. AIRCRAFT TOWED TO GATE. NOSE LANDING GEAR LOWER TORSION LINK PIN FRACTURED CAUSING THE NOSE GEAR TO ROTATE 90 DEGREES AND THE AIRPLANE TO SKID DOWN THE RUNWAY TO A STOP. REPLACED PIN, LOWER TORSION LINK, AND INNER CYLINDER. TESTED AND OPERATION CHECKS NORMAL. PIN SENT TO BOEING FOR EVALUATION 7/14/96. EXPECT RESPONSE BY 10/15/96.

Part: UPPER TUBE — WORN (SLIDE/RAFT)

SLIDE/RAFT REMOVED FOR FIRST TIME OVERHAUL AND FAILED THE AIR RETENTION TEST. ONE SCREW HEAD SECURING THE PRESSURE RELIEF VALVE WORE A HOLE THROUGH THE RELIEF VALVE CHAFE COVER, TUBE SEAM TAPE, 2 LAYERS OF TUBE FABRIC, AND THE TUBE FABRIC OPPOSITE THE TUBE SEAM. THE DAMAGED SLIDE/RAFT RETURNED TO ORIGINAL EQUIPMENT MANUFACTURER FOR WARRANTY REPAIR.