N545UA

Part: APU — FAULTY (APU BAY) · airframe 85,183 hrs · 24,431 cycles

APU HAD SHUTDOWN, FAULT LIGHT ILLUMINATED & EICAS MSG APU FAULT DISPLAYED. ADDED 6 QTS OIL, RAN APU, HAD AUTO SHUTDOWN WITHIN 4 MINUTES WITH HEAVY WHITE SMOKE COMING OUT OF THE TAIL PIPE. OIL TANK WAS EMPTY WHEN CHECKED AFTER SHUTDOWN. OIL DRIPPING FROM BOTTOM OF APU & OUT OF HEAT SHIELD DRAIN TUBE AFTER SHUTDOWN. REPLACED APU IAW 49-11-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,098 hrs · 24,168 cycles

DAMAGED SKIN CUT OUT & A DOUBLER REPAIR INSTALLED IAW SRM 53-00-01, REPAIR NR 3. IAW SRM TABLE V, THIS IS A CAT B REPAIR IN ZONE A. WHERE THINNEST ORIGINAL SKIN THICKNESS IS .049.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 84,098 hrs · 24,168 cycles

FUSELAGE FRAME ON FWD SIDE OF L1 DOOR IS CRACKED & BENT. REPAIRED L1 DOORWAY BS 338 UPPER FRAME INBD CHORD IAW ECRA 5300-01886.

Part: SKIN — DENTED (FUSELAGE) · airframe 84,098 hrs · 24,168 cycles

DENT REPORTED BY CS APPROXIMATE 3FT AFT OF DOOR 3RT & 4FT UP FROM BOTTOM OF DOOR. DENT IS .075 INCH DEEP BY .5 INCHES WIDE. INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 REPAIR 3 FG 201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,098 hrs · 24,168 cycles

DOUBLER REPAIR INSTALLED 3FT AFT OF DOOR 3 RT BS 1703 AT STRINGER 12RT SKIN THICKNESS IN REPAIR AREA IS .056. REPAIR INSTALLED IAW SRM 53-00-01 RPR 3 FG 201.

Part: SKIN — DENTED (FUSELAGE) · airframe 84,098 hrs · 24,168 cycles

REF PREVIOUSLY ARCHIVED DENT CF9088, DAMAGED SKIN CUT OUT & A DOUBLER REPAIR INSTALLED IAW SRM 53-00-01, RPR 3 IAW SRM TABLE V, THIS IS A CAT B REPAIR IN ZONE A WHERE THINNEST ORIGINAL SKIN THICKNESS IS .049.

Part: SKIN — DENTED (FUSELAGE) · airframe 84,098 hrs · 24,168 cycles

FUSELAGE HAS DENT APPROXIMATELY 4FT FWD OF OUTFLOW VLV. =1 & Y=.047 & DENT IS IN MIDDLE OF BAY NOT AFFECTING INTERNAL STRUCTURE & SMOOTH. CUT OUT DAMAGED SKIN AT BS 1585 LT, BETWEEN STRINGER 22L TO STRINGER 23L. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM 53-00-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 84,098 hrs · 24,168 cycles

CORROSION ON CHORD JUST BELOW RT OVERWING EXIT DOOR CUT OUT STATION 960, JUST ABOVE STRINGER 17. REPLACED T CHORD ANGLE, PN 144N8611-28 IAW SRM 51-40-2 & DWG 144N8611 ON NON-ROUTINE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,098 hrs · 24,168 cycles

CORROSION ON CABIN FLOORBEAM UPPER CAP AT BS 1661, WL 208.10 & LBL 8-19. REMOVED CORROSION & MATERIAL REMAINING IS OUT OF LIMITS IAW SRM 53-00-51, FIG 101 & DETAIL III. FORMED -1 REPAIR ANGLE & INSTALLED IAW ECRA 5310- 05538.

Part: DIODE — WEAK (THRUST REVERSER) · airframe 83,105 hrs · 23,934 cycles

LT REVERSE FAILS TO DEPLOY. IAW WDM 32-09-11 PG5C SH2 FOUND WEAK DIODE R10319. CHECKED WIRING FROM K199 X2 TO K177 12. WIRING CONTINUITY GOOD & NO SHORTS TO GND. REPLACED DIODE R10319. LT REVERSE OPERATIONS NORMAL WITH OR WITHOUT ENGS RUNNING.

Part: SENSOR — MISSING (CARGO BAY) · airframe 83,105 hrs · 23,934 cycles

IAW DF0035, FWD CARGO LOADING SYS IS MISSING RETRACT LIMIT SWITCH SENSOR & SUPPORT BRACKET ON MODULE 3. WORK IN PROGRESS MEL 2553A IS NOT ACTIVE. REPLACED SENSOR & BRACKET.

Part: IDG — FAULTY (NR 2 ENGINE) · airframe 83,054 hrs · 23,921 cycles

RT GEN KICKED OFF WENT TO THRUST. PERFORMED BITE CHECK OF BSCU FOUND OVER SPEED FAULT. REPLACED NR 2 ENG IDG IAW AMM & RAN ENG IAW JRH CHECKED OK.

Part: MOTOR — LEAKING (LE SLAT) · airframe 82,937 hrs · 23,894 cycles

LT WING HAS EVIDENCE OF A HYD LEAK ON LOWER FWD WING ROOT TO BODY FAIRING. FOUND HYD MOTOR LEAKING FROM DRAIN TUBE. REPLACED HYD MOTOR IAW AMM 27-81-08, LEAK CHECKED OK. ACCOMPLISHED TO STEP 3 FP OF OPERATIONS CHECKED IAW 27-81-08.

Part: ADI — MALFUNCTIONED (COCKPIT) · airframe 82,825 hrs · 23,865 cycles

CAPTAIN ADI & HSI NOT GOING INTO TEST MODE.

Part: SHIM — MIGRATED (FLAP TRACK) · airframe 82,825 hrs · 23,865 cycles

ACCOMPLISHED INSPECTION OR RECHECK IAW CF9081. RT WING WSS 298 ABOVE INBD FLAP, OTBD FLAP TRACK, SHIM MIGRATING FROM UNDER WING SUPPORT BRACKET.

Part: ATTACH FITTING — MISSING (CARGO NET) · airframe 82,768 hrs · 23,847 cycles

AFT CARGO BAY , FWD RT CARGO NET MISSING CLIP. REPLACED DAMAGED NET.

Part: STARTER — FAULTY (LT ENGINE) · airframe 82,460 hrs · 23,765 cycles

DURING LEFT ENGINE START ATTEMPT, WHILE ENGINE WAS ROTATING, HAD EICAS ENGINE STARTER MESSAGE, ABORTED START. MX CLEANED CONNECTOR & PERFORMED ENGINE MOTOR VALVE APPEARS STIFF.

Part: COVER — CONTAMINATED (CABIN SEAT) · airframe 82,195 hrs · 23,695 cycles

AMMONIA OR FERMENT SMELL IN FWD GALLEY UNABLE TO DETERMINE SOURCE. PASSENGER IN ROW 1 EYES BURN. DUE TO REPORTS OF A STRONG AMMONIA SMELL AT ROW 31, REPLACE ALL SEAT COVERS & SEAT CUSHIONS AT ROW 30A,B,C,D,E,F & ROW 31 A,B,C,D,E,F & ROW 32 A,B,C,D,E,F. IN ADDITION TO THE SEAT COVERS & CUSHIONS BEING REPLACED. PLEASE REPLACE THE CARPET UNDER THOSE SEAT ROWS. REPLACED SEAT BOTTOM CUSHIONS AT 30A & C, D,E,& F, SPRAYED CABIN & CARPETS WITH OX. REPLACED CENTER CARPET ROW 30 THRU 36. RAN FANS SEVERAL HOURS THRU CABIN, SMELLS NEVER RETURNED. FOUND STAIN 1FT BY 1 FT BY 30F., NO ODORS FROM CUSHIONS OR COVERS NOTICED.

Part: LANYARD — OUT OF POSITION (R4 DOOR) · airframe 82,130 hrs · 23,673 cycles

DOOR WILL NOT ARM: 4R FOUND SURVIVAL LANYARD IN BRIDAL ON GIRT BAR. STOWED ROPE BACK IN BRIDAL, OPS CHECKED NORMAL. DOOR NOW ARMS AND DISARMS.

Part: VALVE — FAULTY (COCKPIT) · airframe 82,114 hrs · 23,668 cycles

FLIGHT DECK TOO HOT WITH LT A/C PACK IN AUTO. ALSO TOO HOT WITH COCKPIT TRIM AIR OFF. REPLACED FLIGHT DECK TRIM AIR VALVE PER MM, OPERATIONS CHECKED NORMAL

Part: O-RING — LEAKING (ACTUATOR) · airframe 81,962 hrs · 23,623 cycles

RT ENGINE THRUST REVERSER INOPERATIVE, HYD LEAK AT OTBD CENTER THRUST REVERSER ACTUATOR UPPER FLEX SHAFT. REPLACED O-RING, OPS CHECKED GOOD, NO LEAKS FOUND.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 81,962 hrs · 23,623 cycles

RT ENGINE REVERSER IS INOPERATIVE DUE TO HYD LEAK AT OTBD CENTER REV ACTUATOR UPPER FLEX SHAFT. REPLACED O-RING, OPS CHECKED, NO LEAKS FOUND.

Part: SHAFT — LEAKING (THRUST REVERSER) · airframe 81,962 hrs · 23,623 cycles

RT ENGINE REVERSER IS INOPERATIVE. ACCOUNT OF HYDRAULIC LEAK AT OUTBOARD CENTER REVERSER. ACTUATOR UPPER FLEX SHAFT.

Part: ISOLATION VALVE — INOPERATIVE (THRUST REVERSER) · airframe 81,750 hrs · 23,579 cycles

NR 1 ENGINE LT THRUST REVERSER INOPERATIVE. REPLACED LT THRUST REVERSER ISOLATION VALVE.

Part: FILTER — FAULTY (EQ COOLING) · airframe 81,671 hrs · 23,559 cycles

DURING TAXI OUT, EQUPMENT OVERHEAT EICAS WITH EQUPMENT COOLING FLOW STATUS MESSAGE. SAME INDICATION IN ALTERNATE POSITION. REPLACED EQUPMENT COOLING FILTER.

Part: FAN — NOISY (RT RECIRC FAN) · airframe 81,483 hrs · 23,508 cycles

COMMUNICATION IMPOSSIBLE WITH RT RECIRCULATION FAN ON. REPLACED RT RECIRCULATION FAN, OPS CHECKED OK. NO LEAKS NOTED.

Part: PLATE — CRACKED (FWD CARGO SILL) · airframe 81,462 hrs · 23,503 cycles

FWD CARGO BAY THRESHOLD PLATE HAS ONE PREVIOUSLY WELD REPAIR THAT IS CRACKED. STOP DRILLED ONE INCH CRACK IAW ECRA 5310-04203. FILLED CRACK WITH SEALANT APPLIED ALUMINUM TAPE OVER CRACK.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 81,320 hrs · 23,469 cycles

L1 LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED SMOKE DETECTOR, OPS CHECKED GOOD.

Part: START VALVE — FAILED (NR 1 ENGINE) · airframe 81,175 hrs · 23,431 cycles

NR 1 ENGINE HUNG START BEFORE STARTER CUTOUT. REPLACED STARTER AND VALVE IAW AMM.

Part: CONTROL UNIT — MALFUNCTIONED · airframe 80,831 hrs · 23,351 cycles

ACFT IS NOT SENDING TAKEOFF DATA POINTS. FOUND INCORRECT SOFTWARE INSTALLED AND "DMM" LIGHT ON FRONT OF UNIT WOULDN'T EXTINGUISH. INSTALLED SOFTWARE, NO HELP. REPLACED UNIT REF MM 31-31-03-401, INSTALLED SOFTWARE, NO DEFECTS NOTED.

Part: FRAME — DENTED (BS 1400 S26L) · airframe 63,649 hrs · 18,522 cycles

AFT CARGO BAY FRAME DENTED BS 1400 S26L. CUT OUT DAMAGED AREA AND FABRICATED A REPAIR ANGLE AND INSTALLED PER SRM 53-00-07, REPAIR 5. MAJOR REPAIR.

Part: SKIN — DENTED (BS 628 S26-27L) · airframe 63,649 hrs · 18,522 cycles

DENT IN FUSELAGE BS 628 S26-27L. FOUND TO BE OUT OF LIMITS PER SRM 53-00-01. CUT OUT DAMAGED SKIN AND FABRICATED AND INSTALLED A REPAIR DOUBLER PER SRM 53-00-01, REPAIR 3. MAJOR REPAIR.

Part: CONNECTOR — DAMAGED · airframe 80,635 hrs · 23,300 cycles

STAB TRIM LIGHT AND UPPER EICAS ILLUMINATED WHEN STAB MOVED. STAB TRIM SHUTOFF LEFT CIRCUIT BREAKER ON P-11 WILL NOT RESET. FOUND D1851 CONNECTOR INSULATION DAMAGED. REPLACED CONNECTOR D1851 PER WDM 27-41-11.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 80,627 hrs · 23,297 cycles

HYDRAULIC QUANTITY DECREASED TO 47. QUANTITY STABLE WITH PUMPS OFF, LEFT SYSTEM. CONFERENCE WITH CREW FOLLOWING QRH 130.2 FLUID LEAKING FROM ENGINE DRIVEN PUMP CASE DRAIN PRESSURE MODULE. REPLACED O-RINGS ON DIFFERENTAL PRESSURE INDICATOR, LEAK CHECKED GOOD. SERVICED SYSTEM TO FULL REF CMM 29-11-13.

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 80,588 hrs · 23,286 cycles

L1 DOOR SLIDE LIGHT DOES NOT COME ON WITH SLIDE ARMED. CLEANED GIRT BAR AREA AND CYCLED DOOR. ARM LIGHT CHECKED OKAY.

Part: MODULE — FAILED (STAB TRIM) · airframe 80,587 hrs · 23,285 cycles

EICAS MESSAGE 'STAB TRIM' DISPLAYED AND STAB TRIM LIGHT ON. REPLACED RIGHT STAB TRIM ASSY MODULE.

Part: STARTER — FAILED (APU) · airframe 80,587 hrs · 23,285 cycles

APU WILL NOT START, APU FADEC SHOWS LRU STARTER FAULT . REPLACED STARTER.

Part: SWITCH — FAILED (LT A/C PACK) · airframe 80,587 hrs · 23,285 cycles

LEFT A/C PACK BITE EICAS MESSAGE. REPLACED CABIN ALTERNATE SWITCH IAW AMM, BITE CHECKED GOOD.

Part: LIGHT — UNSECURE · airframe 80,565 hrs · 23,280 cycles

LEFT EMERGENCY ESCAPE TEST 1 LIGHT INOP. SECURED LIGHT IN SOCKET.

Part: SEAT — LOOSE (LAVATORY) · airframe 80,113 hrs · 23,164 cycles

LAV AT 2L HAS A BROKEN TOILET SEAT FOUND SEAT ASSY JUST LOOSE. SECURED AND INSTALLED MISSING PLACARD.

Part: PRESSURE SWITCH — FAILED (HYD SYSTEM) · airframe 80,024 hrs · 23,142 cycles

LEFT ENGINE LOW PRESSURE LIGHT TESTED OK. LIGHT OFF WITH ENGINE SHUT DOWN. REPLACED LOW PRESSURE EDP SWITCH AS PER AMM, LIGHT OPS NORMAL.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 79,991 hrs · 23,135 cycles

FAINT ODOR LIKE BURNING RUBBER ON F/O'S SIDE ONLY, INTERMITTENT. NO SIGNS OF ANY OVERHEATING. PER CREW, NOT AN ELECTRICAL ODOR. RAN PACKS BOTH HOT AND COLD, OPERATED FOOT AND SHOULDER HEATERS, PERFORMED ENGINE RUNS AND SUPPLIED PACKS WITH ENGINE AIR, APU AIR. NO DISCERNIBLE ODOR DETECTED. INSPECTED FWD E & E AREA, INSPECTED LIGHTS IN COCKPIT, NO DEFECTS NOTED.

Part: GROUND WIRE — DAMAGED (LT A/C PACK) · airframe 79,847 hrs · 23,097 cycles

LEFT PACK, GROUNDING WIRE PULLED FROM SHIELD SPLICE AT PACK COMPRESSOR OUTLET TEMP SENSOR. REPAIRED GROUND WIRE FOR SHIELD SPLICE PER SWPM 20-10-15.

Part: HEAT EXCHANGER — CRACKED (LT A/C PACK) · airframe 79,847 hrs · 23,097 cycles

LEFT A/C PACK SECONDARY HEAT EXCHANGER IS CRACKED. REMOVED LEFT PACK PRIMARY AND SECONDARY HEAT EXCHANGERS.

Part: JACK — INOPERATIVE (COCKPIT) · airframe 79,150 hrs · 22,930 cycles

NR 2 MINITEL MICROPHONE JACK INOPERATIVE. HAND MICROPHONE OPERATES NORMALLY. REPLACED F/O MICROPHONE JACK. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 79,092 hrs · 22,918 cycles

DURING SHUTDOWN OF LEFT ENGINE FUEL VALVE LIGHT DID NOT ILLUM, NEEDS FURTHER TROUBLESHOOTING. SPAR VLV OPS OK, ONLY ENGINE VLV LIGHT DOES NOT ILLUMINATE AT ALL. ACCOMPLISHED CHECK, LEFT ENGINE START UP AND SHUTDOWN NORMALLY.

Part: DOOR — OBSTRUCTED (L1) · airframe 79,042 hrs · 22,903 cycles

FLIGHT ATTENDANT REPORTS DOOR 1R WILL NOT ARM. REMOVED WATER BOTTLE CAP FROM DOOR SILL AREA. CLEANED AND LUBRICATED SLIDE GIRT BAR.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 79,029 hrs · 22,901 cycles

AT CRUISE LEFT DUCT PRESS AT 38 PSI & RIGHT AT 22 PSI. PLACED ON MEL CW MEL DDP LOCKED VALVE CLOSED AND PILOT PLUG DISCONNECTED. REPLACED HIGH STAGE PILOT CONTROLLER PER AMM. REACTIVATED CONTROLLER REF MEL3611C. RUN WITHIN LIMITS.

Part: IDG — FAULTY (NR 2 ENGINE) · airframe 78,934 hrs · 22,874 cycles

NR 2 ENGINE IDG NOT OPERATIONAL DURING POST ENGINE CHANGE IDLE RUN. REPLACED NR 2 AND OPS CHECKED PER MM, OPS CHECKED GOOD.

Part: EEC — FAULTY (NR 1 ENGINE) · airframe 78,923 hrs · 22,870 cycles

STATUS MESSAGE "L ENG PRI CONTROL" AFTER ENGINE START. FOUND P AC EX-EEC MESSAGE ON EPCS PAGE. PER FIM 71 EPCS MESSAGE INDEX REPLACED NR 1 ENGINE EEC PER MM, OPS CHECKS GOOD WITH NO MESSAGES PRESENT.

Part: SWITCH — BROKEN (THRUST REVERSER) · airframe 78,918 hrs · 22,868 cycles

LEFT ENGINE REVERSER DID NOT DEPLOY UPON LANDING. LEFT REV DOES NOT DEPLOY DURING GROUND CHECK. DUE HISTORY, INOPED LEFT REVERSER IN THE FWD THRUST POSITION. T-S PER MM 78-31-00 FIG 1 03B AND WD 78-34-51. FOUND NO 28VDC AT PIN 11 OG AIR GND RELAY K167. FOUND REV SW S21 BROKEN AT MICROSWITCH PACK. REPLACED MICROSWITCH PACK ASSY, REV OP CHECKED OKAY.

Part: VALVE — FAULTY (ENGINE OIL) · airframe 78,829 hrs · 22,841 cycles

MAINTENANCE STATUS MESSAGE, RT OIL SCAVANGE VALVE, AFTER TAKEOFF. ALL SYS NORMAL. REMOVED AND REPLACED SCAVENGE VALVE.

Part: PRESSURE SWITCH — FAULTY (LT ENGINE) · airframe 78,717 hrs · 22,803 cycles

LEFT ENGINE OIL PRESS EICAS AFTER ENGINE START. REPLACED LOW OIL PRESS SWITCH PER MM 79-33-01 LEAK CHECK RUN PER JRH.

Part: CONTROL UNIT — FAULTY (LT ENGINE) · airframe 78,513 hrs · 22,744 cycles

ON TAXI OUT WITH BOTH ENGINES RUNNING BOTH GENERATOR TRIPPED OFF LINE. REPLACED BPCU & CLEANED LEFT ENGINE IDG FEEDER CABLE DISCONNECT CONTACTS D1092P & D1092J, PINS A & B, GMM 20-61-01. ACP'D HIGH POWER RUNUP WITH ELECTRICAL LOAD & APU OFF. LEFT & RIGHT GENERATORS OPERATED OK - VOLTS 115VAC, FREQ 400 TO 404 HZ.

Part: LINE — CRACKED (LT ENGINE) · airframe 78,483 hrs · 22,738 cycles

LEFT ENG BLEED VALVE WONT OPEN AFTER START. REPLACED CRACKED SENSE LINE FROM PRC TO 450 DEG SENSOR. RAN ENG, OPS CHECKED GOOD.

Part: CONTROL PANEL — FAILED (WX RADAR SYS) · airframe 78,483 hrs · 22,738 cycles

RADAR UNRELIABLE LEVEL 4-5 TRW CONFIRMED BY ATC EXTREME PRECIP DISPLAY L. REPLACED PANEL AND REPLACED WXR RT.

Part: IDG — LOW (RIGHT) · airframe 78,385 hrs · 22,710 cycles

CREW REPORTED RT GEN TRIPPED ON TAKEOFF ROLL. TAKEOFF ABORTED AT 70KTS. ITEM ROLLED FORWARD. BIT BPCU FOUND MESSAGE SERVICE IDG SERVICED IDG PER AMM. RAN ENGINE PER JRH 2-5-5 SYSTEM OPERATES NORMAL. NO LEAKS ON IDG NOTED. CREW REPORTED NO EXCESSIVE BRAKING DURING ABORTED TAKEOFF.

Part: WIRE — SHORTED (LT SPAR VAVLE) · airframe 78,357 hrs · 22,702 cycles

LEFT ENGINE SPAR VALVE LIGHT ILLUMINATED FOUND SHORT IN WIRE; W3384-1009-18 10" FROM D2142 L SPAR FUEL SHUTOFF VALVE. REMOVED AND REPLACED 50.5 FT RUN FROM D40218P TO D2142. REF WDM 28-22-21WIRE TYPE CODE "GE" OPS CHECKED OKAY.

Part: CONNECTOR — MISSING (LT SPAR VALVE) · airframe 78,357 hrs · 22,702 cycles

LEFT SPAR VALVE CONNECTOR REMOVED. REPLACED SPAR VALVE CONNECTOR, OPS CHECK NORMAL. ACCOMPLISHED VISUAL INSPECTION ON THE INSTALLATION OF SPAR CONNECTOR CHECK RESISTANCE CHECK OKAY PER STD PRACTICE AMM.

Part: GENERATOR — FAULTED (LEFT) · airframe 78,244 hrs · 22,667 cycles

LEFT GENERATOR OFF CHRONIC PROBLEM RESET OKAY

Part: TRANSCEIVER — ERRATIC (WX RADAR) · airframe 78,143 hrs · 22,635 cycles

WEATHER RADAR RETURNS ARE ERRATIC ON DISPLAY. PRECIPITATION NOT PROPERLY DISPLAYING AND TILT SEEMS OUT OF ADJUSTMENT. REPLACED WEATHER RADAR TRANSCEIVER, GROUND TESTED OK.

Part: IDG — FAULTY (RT ENGINE) · airframe 78,144 hrs · 22,636 cycles

RT GEN EICAS, RTFL. REMOVED AND REPLACED NR 2 ENGINE IDG PER AMM. FUNCTIONAL CHECK GOOD. NO LEAKS NOTED.

Part: CARBON SEAL — LEAKING (NR 1 IDG) · airframe 78,105 hrs · 22,624 cycles

LEFT GEN DRIVE EICAS AND GENERATOR DRIVE DISC ON FOR 3 MIN THEN ALL APPEAR NORMAL. AFTER REMOVAL OF NR 1 IDG FOUND CARBON DRIVE SEAL LEAKING. REPLACED IDG CARBON SEALS REF MM. RAN ENG AT IDLE. NO LEAKS NOTED. RAN ENG, DISCONNECTED LT IDG DDP CW. REPLACED IDG. RAN ENGINE AT IDLE AND NO GEN DRIVE LIGHT OR IDG EICAS MESSAGES. NO LEAKS NOTED FROM IDG.

Part: OIL COOLER — FAULTY (LT GENERATOR) · airframe 78,088 hrs · 22,619 cycles

LEFT GENERATOR DRIVE LIGHT ILLUMINATED TWICE FOR 3 MINUTES EACH THEN NORMAL OPS THEREAFTER. NR 1 ENG GEN INOP. REPLACED FUEL OIL HEAT EXCHANGER PER MM. RAN ENG, POS CHECKED GOOD.

Part: HEAT EXCHANGER — FAILED (NR 1 GENERATOR) · airframe 78,088 hrs · 22,619 cycles

LEFT GENERATOR DRIVE LIGHT ILLUMINATED TWICE FOR 3 MINUTES EACH THEN NORMAL OPS THEREAFTER. SUPPLEMENTAL DATA UPDATE, NR 1 ENG GEN INOPERATIVE. REPLACED FUEL OIL HEAT EXCHANGER PER MM. RAN ENG, POS CHECK GOOD.

Part: MECHANISM — WORN (SLIDE ARMING) · airframe 78,077 hrs · 22,616 cycles

DOOR 1R HARD TO ARM-DISARM. FOUND BALL IN CAM MECHANISM WORN. REMOVED BALL FROM CAM MECHANISM R1 DOOR. REPLACED BALL FOR CAM MECH AND SAFETIED.

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 78,061 hrs · 22,613 cycles

ENGINE PRI CONT STATUS MESSAGE WILL NOT CLEAR. SHUTDOWN ENGINE, EPCS SHOWS (P) AC EX EEC, RESET "L02", "L04" AND "L07" NO HELP, CYCLED EEC CHANNEL SELECT SWITCH, NO HELP. UNABLE TO CLEAR LT ENGINE PRI CONT STATUS MESSAGE. REF AMM 71-EPCS MESSAGE INDEX FIG 107 (SHEET 1) PAGE 123 FOR TROUBLESHOOTING. REPLACED EEC MR73237 PER MM 73-21-04 (401). RAN LT AND RT ENG PER JRH 2-5-1, ALL PARAMETERS NORMAL. NO STATUS MESSAGE ON EICAS PER FIM 73-21-00 FIG 115.

Part: POTABLE WATER — CONTAMINATED · airframe 78,005 hrs · 22,595 cycles

POTABLE WATER HAS AN ODOR AND TASTES ODD. SUSPECT MOLD. COLD, HOT, AND THRU COFFEEMAKER ALL AFFECTED. WATER SYSTEM DRAINED. ACCOMPLISHED POTABLE WATER IONIZATION IAW EQ8006 USING MM 38-10-00-201.

Part: IDG — FAILED (RT GENERATOR) · airframe 77,993 hrs · 22,592 cycles

RIGHT GEN DRIVE LIGHT CAME ON AFTER TAKEOFF. DISCONNECTED. AT ARRIVAL, IDG NEEDED BETWEEN 45-50 PUMPS TO OVERFLOW. REPLACED IDG PER MM, ENGINE RUN CHECKED GOOD.

Part: ACTUATOR — FAILED (REVERSER HALF) · airframe 77,993 hrs · 22,591 cycles

LT REVERSER ISOLATION EICAS ON LANDING. LT THROTTLE WILL NOT MOVE. FOUND LT REVERSER HALF NOT STOWED, LOWER ACTUATOR AFT ATTACH HARDWARE MISSING, CHECKED THROTTLES FOUND NO BINDING AND FREE MOVEMENT. LOWER ACTUATOR REPLACED. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO CAT III STATUS REF 22-10-00-501.

Part: IDG — FAILED (NR 1) · airframe 77,850 hrs · 22,553 cycles

LEFT GENERATOR DRIVE EICAS. REPLACED NR 1 ENGINE IDG. OPS CHECKED GOOD.

Part: IDG — LOW (NR 1 ENGINE) · airframe 77,850 hrs · 22,553 cycles

LEFT GEN EICAS MESSAGE AND LOW PRESSURE LIGHT OVERHEAD. CHECKED IDG AND FOUND OIL LEVEL VERY LOW. SERVICE IDG WITH 4 PINTS OF OIL. RPL NR 1 ENG IDG, OP CKS GOOD.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 77,572 hrs · 22,481 cycles

LEFT ENGINE SPAR VALVE LIGHT ILLUMINATED, WITH ENGINE SHUT DOWN. REPLACED LEFT ENGINE SPAR VALVE ACTUATOR PER MM, OPS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 77,522 hrs · 22,467 cycles

CORROSION ON FLOORBEAM TEE AT BS 1640, BL 0 TO LBL 10. REPAIRED.

Part: SKIN — DENTED (BS 1695) · airframe 77,522 hrs · 22,467 cycles

DENT IN SKIN BS 1695, LBL 20. CUT OUT DAMAGE, ACCOMPLISHED HFEC PER NDTM 51-00-19, PRT 6. FABRICATED AND INSTALLED FILLER AND DOUBLER PER ECRA 5360-01194. MAJOR REPAIR

Part: SKIN — CORRODED (BS 1400 S29-30R) · corrosion level 2 · airframe 77,522 hrs · 22,467 cycles

BUTT SPLICE CORRODED AT BS 1400, BTW STR 29 - 30R. REMOVED DOUBLER, CUT OUT DAMAGE, ACCOMPLISHED HFEC PER NDTM 51-00-19, PRT 6, FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER. MAJOR REPAIR

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,522 hrs · 22,467 cycles

FWD CLOSET EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD PER AMM 33-51-11-301.

Part: SKIN — DENTED (BS 610 S16L) · corrosion level 2 · airframe 77,522 hrs · 22,467 cycles

DENT IN SKIN AT BS 610, APPROX STR 16L. FABRICATED AND INSTALLED DOUBLERS PER ECRA 5330-04241 AND EA PT57-53-007 ON NR 4807N00437.

Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 77,522 hrs · 22,467 cycles

CORROSION ON FLOORBEAM TEE BS 1661, LBL 34 AND 56. BLENDED AREA, FOUND TO BE WITHIN LIMITS PER SRM 53-00-51. CUT OUT CORROSION, ACCOMPLISHED HFEC PER NDTM 51-00-19 PRT 6, NO CRACKS NOTED, FABRICATED AND INSTALLED FLOORBEAM TEE, ANGLES AND SPACERS PER SRM 53-00-51.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 77,522 hrs · 22,467 cycles

FLOORBEAM BS 365, RBL 62 CORRODED. FABRICATED AND REPLACED FLOORBEAM, SPLICE ANGLES AND STRAP PER ECRA 5310-05514 AND EA PT57-53-004.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 77,522 hrs · 22,467 cycles

MAIN CABIN BS 1640 FLOORBEAM UPPER TEE CAP CORRODED BETWEEN BL 0 AND LBL 10. BLENDED CORROSION AND FOUND MATERIAL LOSS OUT OF SRM LIMITS. CUT OUT DAMAGE FROM RBL 3 - LBL 10. ACCOMPLISHED NDT OF REPAIR CUT-OUT AREA. NO DEFECTS. FABRICATED AND INSTALLED TEE, ANGLES AND STRAPS REPAIR REF SRM 53-00-51 FIG 201 REPAIR 3.

Part: CONTROL VALVE — DEFECTIVE (LEFT) · airframe 77,320 hrs · 22,404 cycles

LEFT PACK OFF IN DESCENT. REPLACED LEFT FLOW CONTROL VALVE. RAN LEFT ENGINE FLOW CONTROL VALVE. OPS CHECKED NORMAL.

Part: WIRE — UNSECURE (ROCKER SWITCH) · airframe 77,287 hrs · 22,396 cycles

YOKE TRANSMIT ROCKER SWITCH INTERMITTANT CAPTAIN'S SIDE. SECURED WIRES ON YOKE SWITCH AND SWITCH OPERATED NORMALLY RE-ACTIVATED.

Part: PRESSURE SWITCH — FAULTY (LT HYD SYSTEM) · airframe 77,258 hrs · 22,386 cycles

LEFT HYD SYS PRESSURE LIGHT NOT ON WITH HYD PUMPS OFF. REPLACED LT HYD SYS PRESSURE SWITCH, OPS & LEAK CHECKED NORMAL.

Part: PRESSURE SWITCH — DEFECTIVE (HYD PUMP) · airframe 77,134 hrs · 22,351 cycles

STATUS MESSAGE; FLAP ISOLATION VALVE AND ELEVATOR LT HYD PRESSURE WON'T CLEAR. REPLACED EDP PRESSURE SWITCH PER AMM. ERASED MESSAGES, OPERATED SYSTEMS, NO MESSAGES.

Part: INDICATOR — FAULTY (FUEL TOTALIZER) · airframe 77,090 hrs · 22,338 cycles

FUEL TOTALIZER INDICATOR HAS NUMBERS FAULTY, TEST FAILED. NEW FUEL TOTALIZER INSTALLED, OPS CHECKED GOOD.

Part: KNOB — BROKEN (RADAR PANEL) · airframe 77,090 hrs · 22,338 cycles

WX RADAR SWITCH KNOB "SKIRT" IS BROKEN. SWITCH FUNCTION IS OKAY. KNOB IS STILL FUNCTIONAL KNOB SHOULD BE REPLACED. NEW WX RADAR PANEL INSTALLED PER MM, OPS CHKS GOOD.

Part: CONNECTOR — DIRTY (RT ENGINE) · airframe 77,045 hrs · 22,325 cycles

RT ENG ANTI-ICE EICAS MESSAGE. CLEANED CONNECTOR, NO MSG.

Part: HYDRAULIC LINE — LOOSE (HYDRAULIC SYS) · airframe 76,900 hrs · 22,279 cycles

LEFT HYDRAULIC SYSTEM QTY AND PRESSURE DROPPED TO ZERO. LT ENG DRIVEN PUMP AND ELEC SWITCH TURNED TO OFF POSITION AFTER PRESSURE LOSS. FOUND LEFT EDP SUPPLY LINE LOOSE AND BACKSHELL LOOSE. REPLACED LEFT EDP REF MM AND BOTH LEFT HYD CASE FILTERS. NOTED THAT FILTERS WERE DIRTY BUT NOT WITH ANY HEAVY DEBRIS (REF MM 29-11-17). NOTE EXAMINED BOTH FILTERS FOR METAL NONE PRESENT.

Part: INTAKE — DAMAGED (APU) · airframe 76,900 hrs · 22,279 cycles

TWO HUNG STARTS RIGHT ENG START APU PRESS 20. APU PNEUMATICS DEFERRED PER MEL. -INF- :ON MES MODE APU EGT IS 521 DEG REF FIM 49-11-00 PG 162 BLOCK 12. IF EGT EXCEEDS 500 REPLACE APU. REMOVED APU AND FOUND AIR INTAKE DUCT MATERIAL BLOCKING APU PLENUM. INSP FOUND APU AIR INTAKE DUCT DAMAGED AT AFT END.

Part: METERING VALVE — FAULTY (NLG) · airframe 76,786 hrs · 22,246 cycles

REPLACED NLG STEER METERING VALVE PER MM. ACCOMPLISHED NLG STEERING SYS ADJUSTMENT & RIG PER MM.

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 76,596 hrs · 22,186 cycles

ENG PARAMETERS FLUCTUATING IN CRUISE. DISCUSSED WITH ENG CONTROLLER REPLACE FCU AND FUEL PUMP. REMOVED FUEL CONTROL. STARTED TO REMOVE FUEL PUMP PER MM. FUEL PUMP JUST NEEDS ATTACH BOLTS LOOSENED TO BE REMOVED. REPLACED NR 1 ENGINE FUEL PUMP PER MM. CHANGED NR 1 ENGINE FUEL CONTROL PER MM.

Part: HYDRAULIC LINE — LOOSE (RT MLG WW) · airframe 76,566 hrs · 22,179 cycles

FLUID LEAK IN AREA OF LEFT GEAR DOOR. MAINT TEXT: CORRECTION FLUID LEAK IN AREA OF RIGHT GEAR DOOR. SECURED UNION ON HYD RETURN LINE PRESSURIZED HYD FOR 30 MINUTES, NO LEAKS DETECTED.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 76,191 hrs · 22,073 cycles

NR 1 ENGINE HAS FUEL POURING FROM FUEL PUMP, ACFT RTB. REMOVED & REPLACED FUEL CONTROL & FUEL PUMP.

Part: FUEL/OIL COOLER — LEAKING (NR 1 ENGINE) · airframe 75,925 hrs · 22,000 cycles

CREW REPORTED OIL LEAK NR 1 ENGINE. OPENED ENG COWL, CLEANED AND INSPECTED NR 1 ENGINE. NO LEAK FOUND. ACCOMPLISHED ENGINE IDLE RUN. FOUND OIL DRIPS FROM FUEL-OIL HEAT EXCHANGER. THREE DROPS PER MINUTE AFTER SHUTDOWN. LEAK RATE IN LIMITS.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 75,925 hrs · 22,000 cycles

LEFT PACK OFF LIGHT ON AFTER ENG START. REPLACED LEFT PACK CONTROLLER, NO HELP. CLEANED CONNECTOR ON FLOW CONTROL VALVE, NO HELP. ALL DONE WITH REFERENCE TO LOG 1. REPLACED LT PACK FLOW CONTROL VALVE AND PACK OPS NORMAL PER MM.

Part: PLUG — FAULTY (WINDOW) · airframe 75,871 hrs · 21,985 cycles

WINDOW R2 MISSING WINDOW HEAT WIRE CAPS. FOUND PLUG ASSY WILL NOT ACCEPT CAP. REPLACED 566-1610 PLUG ASSY, OPS CHECK GOOD.

Part: FMC — MALFUNCTIONED (COCKPIT) · airframe 75,571 hrs · 21,899 cycles

FMC SPONTANEOUSLY DUMPED ROUTE AND ALTITUDE DATA WHEN A DESCENT ALTITUDE WAS ENTERED. TALKED WITH CREW AND TOMC UNABLE TO DUPLICATE BY CREW. ALL DATA ENTERED AGAIN NO MESSAGE OR STATUS. NO PAST HISTORY. CYCLED CBS AND FMC IS NORMAL.

Part: HEATING ELEMENT — FAILED (PITOT PROBE) · airframe 75,426 hrs · 21,859 cycles

AFTER PUSHBACK AND ENGINE START HAD EICAS MESSAGE: 'CAPT PITOT' ALSO HAD DISCRETE LIGHT. REPLACED CAPT PITOT PROBE AFTER CONFIRMING PROBE HEATING ELEMENT OHMED OUT WITH BAD ELEMENT IAW MM34-11-01 PG 401 & MM 34-11-01 PG 501. STARTED NR 2 ENGINE AND CONFIRMED PROBE OVERHEAD AMBER LIGHT OUT. PROBE LEAK TESTED AT 300 KNOTS NO LEAK DOWN IN ONE MINUTE.

Part: SELECTOR PANEL — IMPROPER PART (COCKPIT) · airframe 75,185 hrs · 21,785 cycles

F/O COM SELECTOR PANEL INCORRECT, NO HF. REPLACED F-O'S AUDIO SEL PANEL PER MM, CHECKS OKAY.

Part: EEC — FAULTY (NR 1 ENGINE) · airframe 75,183 hrs · 21,783 cycles

DUE TO REPEAT L. ENG SEC CONT STATUS MSG ALONG WITH EPCS MSG'S S-EEC, S273-14, S273-15, S273-16, S273-22 REPLACE NR 1 ENGINE EEC. REPLACED LEFT ENG EEC PER M1597 INSTRUCTIONS AND MM, NO FAULTS FOUND. PCN 481-9246.

Part: FASTENER — DAMAGED (LT WING) · airframe 75,173 hrs · 21,780 cycles

DAMAGED RIVET ON PANEL 29" OUTBOARD OF LT ENG PYLON SAILTAIL AREA, LEADING EDGE OF PANEL. REPLACED FASTENER.

Part: AIR FILTER — FAULTY (E&E BAY) · airframe 75,077 hrs · 21,754 cycles

EQUIPMENT OVHT EICAS ACCOMPANIED BY OVHT LIGHT. SWITCHED TO ALTN COOLING AND LIGHTS EXTINGUISH. REPLACED EQUIPMENT COOLING AIR FILTER. SWITCHED EQUIPMENT COOLING SWITCH TO NORMAL POSITION, NO EICAS MESSAGES. OP CHECKS GOOD.

Part: MODULE — MALFUNCTIONED (APU BLEED) · airframe 74,742 hrs · 21,659 cycles

APU DOES NOT PUT OUT MORE THAN 3 PSI. WILL NOT OPEN PACK OR STARTER VALVES. NO APU PNEUMATICS SEE HISTORY. APU BLEED VALVE IS CLOSED. REPLACED FLOW SENSE MODULE OPS CHECKED OK. RAN BOTH PACKS, MOTORED BOTH ENGINES, DUCT PRESSURE READS 35 PSI.

Part: CONTROL VALVE — FAILED (THRUST REVERSER) · airframe 74,637 hrs · 21,629 cycles

L ENG REV WILL NOT GO INTO REVERSE. REPLACED ISOLATION VALVE, NO HELP. NO VOLTAGE TO ISOLATION VALVE. REPLACED LT REVERSER DIRECTIONAL CONTROL VALVE PER MM.REPLACED PSEU. REVERSER DEPLOYS AND NO FAULT MESSAGES. OPS CHECKED PER MM, PASSED.

Part: CLAMP — BROKEN (CABIN & COCKPIT) · airframe 74,705 hrs · 21,646 cycles

UNCONTROLLABLE CABIN AND FLT DECK TEMPS. FOUND BROKEN BONDING STRAP CLAMP, LOOSE SENSE LINE AND HOT AIR TUBE LOOSE. REPLACED BROKEN BONDING CLAMP AND SECURED LOOSE HOT AIR TUBE. NEED TO OP CHECK TO CONFIRM FIX. ABLE TO CONTROL TEMP TO FULL COLD AND HOT. CHECKED GOOD IN AUTO AND STBY.

Part: RELAY — FAULTY (BLEED AIR SYS) · airframe 74,660 hrs · 21,635 cycles

APU BLEED JUST SHUT ITSELF OFF AFTER SEVERAL MINUTES OF NORMAL OPERATION. DUE TO RECENT APU BLEED HISTORY, ACCOMPLISH SERVICE TIP. IF NO FAULTS FOUND REPLACE K10645 (562-0439). CONSULT ON-LINE IPC TO VERIFY PARTS LIST CURRENCY. ACP'D SERVICE TIP 36-11-00 P500A AND NO FAULT NOTED AFTER 30 MINUTES APU RUNNING. REPLACED K10645 ON P36. RAN PACKS AND MOTORED ENGINE WITH APU BLEED SHUTOFF VALVE OPERATING OKAY.

Part: UNKNOWN — NOISY (CABIN AIR) · airframe 74,638 hrs · 21,630 cycles

LOUD LOW FREQUENCY NOISE NOTED DURING FLT. LOUDEST ON LEFT SIDE OF AIRCRAFT COCKPIT. INSPECTED ALONG AIR DUCT RISER BEHIND FWD LAV SIDEWALL WITH RVI BOROSCOPE WHILE PACKS & RECIRC FANS RUNNING. NO DEFECTS NOTED. ACP SERVICE TIP 21-22-00 PARA 4 THRU 7 ALL CONDITIONS NORMAL. TESTED FLIGHT DECK NOISE LEVEL PER MM. FOUND DECIBEL LEVELS ACCEPTABLE.

Part: EEC — FAILED (NR 1 ENGINE) · airframe 74,637 hrs · 21,629 cycles

NR 1 ENG "LIMIT PROTECTION LIGHT " ON PEDESTAL AND EICAS MSG DISPLAYED. REPLACED NR 1 ENGINE EEC IAW AMM. MR73237 ON 26 OFF 2. IDLE RUN AFTER 30 SECONDS INCREASES IN FF 1.6 AND N2 73 PERCENT ON OWN. NOW HAVE P PMA EEC AND S PMA EEC MSGS ON EPCS. EEC NO HELP. REPLACED L-PDIU REF MM. BITE CHK NO FAULT. RAN ENGINES FOR HI POWER ASSURANCE & ALSO IDLE RAN BOTH ENGINES. PARAMETERS NORMAL, NO MSG .

Part: PROBE — FAULTY (EPR) · airframe 74,581 hrs · 21,614 cycles

TOP OF DESCENT NOTED LEFT ENG EPR RADIAL AND NUMBERS MISSING ON UPPER CRT AND SEI DISPLAY. SFO INF- :PT2-TT2 PROBE 564-0122 NOT AVAIL SFO. ORDERED PROBE AOG LAX. REPLACED NR 1 PT2-TT2 PROBE IAW AMM. TEST OKAY IAW AMM. IDLE RUN NR 1 ENGINE, NO MSG DISPLAYED, AC RETURNED TO CAT III.

Part: FIRE LOOP — DEFECTIVE (NR 4) · airframe 74,519 hrs · 21,599 cycles

L ENG FIRE LP 2 STATUS MSG ON TAXI IN. FOUND NR 4 FIRE LOOP ON LOOP 2 SIDE OPEN. LOOP IS LOCATED ON RT SIDE FAN COWL. REPLACED NR 4 FIRE LOOP ON LOOP 2. FIRE TEST OPS CHECK GOOD. EICAS MSG CLEARED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 74,181 hrs · 21,506 cycles

NOSE GEAR UNSAFE LIGHT INOP AT TEST SWITCH. REPLACED LAMP 1665, OPS GOOD.

Part: NUT — LOOSE (SEAT) · airframe 74,081 hrs · 21,477 cycles

SEAT ASSY LOOSE 27DEF. REPLACED DAMAGED FRONT ANTI RATTLE NUTS AND SECURED SEAT ASST PER AMM.

Part: UNKNOWN — NOISY (COCKPIT) · airframe 74,081 hrs · 21,477 cycles

NOISY FLIGHT DECK.

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 73,826 hrs · 21,397 cycles

F/O O2 MASK COMM CHORD WIRES EXPOSED. REPLACED MASK.

Part: FAN BLADE — DAMAGED (NR 2 ENGINE) · airframe 73,579 hrs · 21,326 cycles

NR 2 ENG N1 FAN 3EA FAN BLADES EVIDENCE OF FOD DAMAGE. NEED TO DRESS BLADES. REPAIRED 3 EA FAN BLADES (MARKED ON BLADE ROOT) ON NR 2 N1 FAN.

Part: MODULE — FAULTY (STALL WARNING) · airframe 73,224 hrs · 21,224 cycles

STALL WARNING OPS CHECK FAILS STEP B8, ALL OTHER STEPS CHECK OKAY. CAPT'S SIDE DOES NOT DISPLAY PITCH LIMIT INDICATOR AND NO STICK SHAKER WITH AIR DATA SWITCH IN ALT. FOUND 115V AC ON PIN 5 WITH SOURCE SWITCH IN ALT. FOUND 115V AC AT PIN 6 WITH SOURCE SWITCH IN NORMAL. MEASURED AT CONNECTOR D3925. SWAPPED STALL WARNING COMPUTERS, NO HELP. RETURNED TO ORIGINAL POSITIONS PER MM. REPLACED AIR DATA SOURCE SWITCH MASTER MODULE PER MM.

Part: STATOR — FAULTY (LT ENGINE) · airframe 73,152 hrs · 21,206 cycles

LEFT ENGINE LIM PROT AFTER ENGINE START. CREW SHUTDOWN ENGINE AND TRIED A 2ND START, ENGINE WILL NOT START, ALSO GOT LT ENGINE PRI CONT STS MESSAGE WITH (P) & (S) PMA-EEC AS EPCS MESSAGES. CHECKED PMA ELECTRICAL CONNECTOR-RECEPTACLE FOR CONDITION, BURNED PINS AND REPLACE PMA STATOR-EEC ALTERNATOR PCN 564-0294 IAW AMM. REMOVED STATOR. INSPECTED CONNECTOR FOUND OK. REPLACED STATOR IAW MM. ACCOMPLISHED 5 MIN IDLE RUN. RAN ON BOTH PRI AND SEC NO MSG ON SHUTDOWN. ALSO IAW MM 71-EPCS PG128 FIG 108 LT ENGINE.

Part: WIRE — BROKEN (WINDOW HEAT) · airframe 73,054 hrs · 21,181 cycles

RT SIDE WINDOW HEAT INOPERATIVE. FOUND 3 BROKEN WIRES AT WINDOW 2R PIGTAIL JUST ABOVE WINDOW. SPLICED BROKEN WIRES & REPAIRED INSULATION. ALSO OP CKD WINDOW 2R AND CONTROLLER. FOUND NO FAULTS.

Part: EEC — FAULTY (LT ENGINE) · airframe 72,951 hrs · 21,151 cycles

TURN ON EEC MAIN POWER SWITCH ON P61 TO ALTERNATE POSITION, ECPS PAGE LT ENGINE HAS NO HIGH LIGHT ON ANY CHANNEL AND NO LT EEC POWER MESSAGE ON UPPER EICAS. TRIED LT PDIU UNIT, NO HELP. REPLACED ENG 1 EEC UNIT, NO HELP. LT EEC POWER MSG APPEAR ON UPPER EICAS NORMALLY WHEN EEC ALTN POWER IS ON.

Part: CABLE — FAILED (EMERGENCY LIGHTS) · airframe 72,789 hrs · 21,099 cycles

FWD CLOSET EMERGENCY LIGHT AND DOOR EXIT LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY PER MM, NO HELP. REPLACED FEEDER CABLE IN FIRST CLASS CABIN.

Part: SHIM — MIGRATED (LT WING) · airframe 72,529 hrs · 21,026 cycles

LT WING SHIM MIGRATION UNDER WING SUPPORT BRACKET ABOVE INBD FLAP OTBD TRACK. COMPLETED OPEN UP OF AREA. FOUND SHIM GAPS WITHIN LIMITS. DURING REINSPECTION ADDITIONAL SHIM MIGRATION WAS FOUND. ACCOMPLISH REPAIR PER UAL-EVA 73927. REPAIR WAS ACCOMPLISHED PER UA-EVA-73927 AT C05 VISIT ON SMB N-R R5127H. EXPOSED SHIM WAS TRIMMED AND SEALED. REOADED TO MAX PTC 21027 PER EVA 73927 PER OPBLM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,332 hrs · 20,971 cycles

EMERGENCY LIGHTS BY FWD COAT CLOSET AND FWD MEDS WILL NOT OPERATE. REPLACED BATTERY PACK, EMERGENCY LIGHTS OPERATE NORMAL.

Part: WIRE — BROKEN (ENGINE) · airframe 72,142 hrs · 20,921 cycles

NR 1 EGT ON EICAS FLUX BETWEEN 0 AND 430 STBY ENG INST OKAY. REPLACED LEFT EICAS COMPUTER AND CROSSLOADED OPC SOFTWARE 3174-BCG-006-06, PER MM. BITE CHECKS OKAY, NO MSGS. DURING EEC STATIC TEST NO WHITE BOX APPEARED AROUND PRI AND SEC DISPLAY ON EPCS PAGE. REPLACED EEC PER MM. ALSO, REPLACED LEFT PDIU PER MM. INSPECTED W31 HARNESS ASSY, FOUND BROKEN GROUND WIRE. REPLACED WIRE. ACCOMPLISHED EEC STATIC TEST, EPCS PT5-EEC MSG DID NOT REAPPEAR.

Part: EEC — FAULTY (LT ENGINE) · airframe 72,033 hrs · 20,887 cycles

LEFT ENGINE SEC CONT STATUS MESSAGE. LT ENG SEC CONT STATUS MESSAGE ON LOWER EICAS WITH ASSOC EPCS AUTO EVENT MESSAGES 'SVA-EEC' AND 'P SVA F-B INT'. REPLACED EEC LT ENG.

Part: FUEL CONTROL — FAILED (NR 2 ENGINE) · airframe 72,023 hrs · 20,884 cycles

NR 2 ENG NO START WITH FUEL COMING FROM TAILPIPE. FUEL MISTING OUT OF TAILPIPE. MOTORED ENG DUPLICATED PROBLEM HAD F.F AND VALVE LIGHT WITH FUEL LEVER OFF. REPLACED FUEL CONTROL PER MM. ALSO ACCOMPLISHED IDLE LEAK CHECK AND TEST 15 ACCEL RUN UP PER JRH. ALL TIMES GOOD, NO FAULTS ON EPCS.

Part: BEARING — FAULTY (SCAV VALVE) · airframe 72,010 hrs · 20,878 cycles

STATUS MESSAGE. LT OIL SCAVENGE VALVE. REPLACED NR 4 BEARING SCAVENGE VALVE. LEAK CHECK AND OP CHECKED OK. SERVICED WITH MAINT OIL.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 71,875 hrs · 20,840 cycles

RUDDER TRIM IS INTERMITTENT. TRIM KNOB WILL NOT MOVE RUDDER. REPLACED RUDDER TRIM ACTUATOR AND OPS CHECKED OKAY.

Part: SLEEVE — DAMAGED (THRUST REVERSER) · airframe 71,488 hrs · 20,716 cycles

ON WALK AROUND, FOUND DAMAGE TO NR1 ENG LT SIDE REVERSER SLEEVE. DAMAGE MEASUREMENTS FALL WITHIN LIMITS OF SVC TIP. COMPLIED WITH SVC TIP. THRUST REV LOCKED OUT. ACFT REMOVED FROM CAT III. SLEEVE REPLACED IAW MM. NEED TO ADJUST SPRING BUMPERS AND ACCOMPLISH AUTO-RESTOW, SYNC LOCK TEST. REACTIVATED NR 1 REVERSER. ACP SPRING BUMPER ADJUSTMENT. ACP SYNC LOCK TEST 6 AND OP CHECKS OK. REINSTATED CATIII. REVERSER OP CHECKS OK.

Part: AUDIO PANEL — FAULTY (VHF SYSTEM) · airframe 71,434 hrs · 20,702 cycles

NR 2 VHF RADIO BLEEDS OVER TO NR 1 VHF RADIO FLT IN PH. RADIO IS MALFUNCTIONING. REPLACED F-O AUDIO SELECT PANEL. OPS GOOD.

Part: PANEL — MALFUNCTIONED (NR 1 NACELLE) · airframe 71,317 hrs · 20,668 cycles

"ENG BTL 1 DICHR" LIGHT INOPERATIVE. REPLACED FIRE PANEL. OPS CHECKS GOOD.

Part: STRUCTURE — DAMAGED (RT WING TE FLAPS) · airframe 71,103 hrs · 20,608 cycles

RT T/E INBD AFT FLAP NEEDS REPLACEMENT. REPLACED RT INBD T/E AFT FLAP ASSY IAW MM. INSTALLED T/E FLAP CANOE FAIRING. ADJUSTED FIT-FAIR.

Part: PANEL — DAMAGED (LT WING) · airframe 70,947 hrs · 20,565 cycles

LT WING LWR LEADING EDGE PANEL 511DB COUNTERSUNK HOLES TOO LOOSE FOR FASTENERS TO SECURE PANEL. PANEL WAS SENT TO SHOP 273 R&R R25419. PANEL REPAIRED ON R&R R25419, RE-INSTALLED PANEL.

Part: SKIN — DAMAGED (TE FLAP) · airframe 70,809 hrs · 20,527 cycles

APPROX 4 DROPS PER SEC DRIPPING FROM I/B TRAILING EDGE FLAP I/B END & SEVERAL AREAS OF DELAMINATION AT LOWER SURFACE. ACCOMPLISHED ON DOCK WU W4611N. REPLACED AFT FLAP PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 70,809 hrs · 20,527 cycles

LEFT I/B FLAP ASSY, AFT FLAP LWR SURFACE HAS 3 EACH AREAS OF DELAM AT I/B MOST 30 INCHES. ACP'D ON DOCK WU T6483X. RII INSP ACP'D. REPLACED LEFT INBOARD AFT FLAP.

Part: STRAP — FAULTY (L1 DOOR) · airframe 70,809 hrs · 20,527 cycles

NR 1 LT PAX ENTRY DOOR EVAC SLIDE - V - STRAP HARNESS LWR METAL -U- CHANNEL NOT PROPERLY SECURED TO GIRT MOUNT BRACKET. U - CHANNEL MOUNT HOLE AT FWD END NOT SECURED THROUGH BRACKET PIN. REPLACED STRAP ASSY AND SECURED SLIDE.

Part: LAMP — INTERMITTENT (CHART LIGHT) · airframe 70,491 hrs · 20,441 cycles

CAPT CHART LIGHT FLICKERS BRIGHT AND DIM. REPLACED LAMP. CHECKS OK.

Part: PRESSURE SWITCH — LEAKING (FUEL SYSTEM) · airframe 70,380 hrs · 20,410 cycles

FUEL LEAKING FROM NR 1 FUEL FILTER DIFF PRESS SWITCH. REPLACED FUEL PUMP FILTER DIFFERENTIAL PRESSURE SWITCH.

Part: DISPLAY — FAULTY (POSITION 1) · airframe 70,187 hrs · 20,356 cycles

1 NR ENG PRIMARY CONTROL EICAS MSGS AND BLANKING EPR. REPLACED LT PDIU. REPLACED THE NR 1 ENGINE PMA AND TESTED IAW MM.

Part: WINDSHIELD — DAMAGED (COCKPIT L1) · airframe 70,151 hrs · 20,342 cycles

L1 WINDOW HAS BURN MARK AT TOP & SAW BRIEF SPARK WHEN WINDOW HEAT TURNED OFF. NO TIME TO TROUBLESHOOT. VISIBILITY NOT AFFECTED. OK FOR SVC. REPLACED WINDSHIELD. L1 WINDOW NEEDS 1EA FASTENER INSTALLED AT WINDOW FRAME. REPLACED FASTENER. REPLACED SEALANT AS REQ.

Part: GENERATOR — FAULTY (POSITION A) · airframe 70,127 hrs · 20,336 cycles

APU GEN UNABLE TO CONNECT AT ENGINE SHUTDOWN. REPLACED APU GENERATOR AND FEEDER HARNESS ASSY. APU GENERATOR POWER FEEDER CABLES BURNED AND MELTED AT APU GENERATOR TERMINAL BLOCK. REPLACED FEEDER CABLE ASSY. OPS CHECKS GOOD ALL GEN OUTPUTS NORMAL AT RUN.

Part: GCU — FAULTY (POSITION A) · airframe 70,127 hrs · 20,335 cycles

GENERATOR CONTROL UNIT REQUIRES REPLACEMENT. REPLACED GENERATOR CONTROL UNIT.

Part: BLADE — DAMAGED (COMPRESSOR NR 2) · airframe 70,133 hrs · 20,337 cycles

RIGHT ENG HAS ONE DAMAGED FAN BLADE. REPAIRED NR 2 ENG FAN BLADE IAW MM. EDDY CURRENT INSP ACP'D. NO DEFECTS FOUND. RPR WITHIN LIMITS FOR CONTINUING SERVICE.

Part: VALVE — FAULTY (THRUST REVERSER) · airframe 70,086 hrs · 20,318 cycles

LT THRUST REVERSER WOULD NOT DEPLOY. REPLACED NR1 THRUST REV DIRECTIONAL CONTROL VALVE. OPS CHECK GOOD.

Part: FAN — FAULTY (LT POSITION) · airframe 69,923 hrs · 20,265 cycles

CREW REPORT ELECTRICAL ODOR AND HAZE PRESENT IN THE CABIN. UTILITY BUS TURNED OFF AND LT RECIRC OFF WITH OVERRIDE SELECTED CABIN AIR NOW CLEAR. HAZE AND ODOR HAS DISSIPATED. R & R LT RECIRC FAN, OPS GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER SYS) · airframe 69,614 hrs · 20,176 cycles

RUDDER TRIM ISSUE, FLT DIVERTED. REPLACED RUDDER TRIM CTRL PANEL, OPS CHECK OKAY.

Part: MICROPHONE — INOPERATIVE (COCKPIT) · airframe 69,603 hrs · 20,173 cycles

NR 1 COCKPIT HAND MIKE DEFECTIVE (O1=CAPT, O2=1ST OFF, O3=1ST OBS). CREW COMMENTS: CAPTS HAND MIC INOPERATIVE. NO IPC REF FOR CAPTAIN HAND MIC. MINITEL OPERATES NORMALLY. REPLACED CAPTAIN HAND MIC.

Part: UNKNOWN — ODOR (CABIN) · airframe 69,300 hrs · 20,091 cycles

BURNED ELECTRICAL ODOR IN COCKPIT AND FWD CABIN. CHECKED AVIONICS COMPARTMENTS NO ODORS, ODOR OCCURED WHEN GROUND AIR CONDITIONING STARTED. OKAY FOR SERVICE.

Part: EEC — FAULTY (NR 1 ENGINE) · airframe 69,057 hrs · 20,026 cycles

NR 1 ENG WITH EEC MAINT POWER SELECT SWITCH IN ALTN POSITION. EPCS PAGE DISPLAYS NO CHANNEL SELECTED. CHANNEL SELECT SWITCH HAS NO EFFECT. SQUARE BOX AROUND PRI, SEC, NOT DISPLAYED. THRUST REV WILL NOT DEPLOY. REPLACED EEC. PROBLEM STILL PERSISTS. REPLACED NR1 PDIU SYS OPS, CHECKED OK.

Part: COMPUTER — INOPERATIVE (LT EICAS) · airframe 68,957 hrs · 19,999 cycles

CREW REPORTED LT EICAS COMPUTER INOPERATIVE. COMPUTER FOUND FAULTY. INSTALLED NEW EICAS COMPUTER. VERIFIED OPS & OPC SOFTWARE ON LT EICAS COMPUTER IAW MOPS.

Part: LINE — DAMAGED (HYD SYSTEM) · airframe 68,639 hrs · 19,906 cycles

CTR HYD LOW PRESSURE/QUANTITY, RTFL. RPL 2EA FLEX LINES. FOUND HOLE IN ONE AND THE OTHER FRAYED. THE UPPER LINE WAS THE COMPONENT THAT FAILED INDEPENDENTLY AND WAS A LINE FAILURE. HYD QTY DOWN TO 59 PERCENT, RESERVICED TO FULL. OPS CHK GOOD, NO LEAKS.

Part: SLIDE — UNSECURE (DOOR 1L) · airframe 68,309 hrs · 19,812 cycles

WHEN OPENING DOOR 1L FOUND SLIDE HAD FALLEN OFF AND WAS RESTING ON FLOOR. RESECURED SLIDE PACK DOOR 1L.

Part: RESERVOIR — READS LOW (L1 DOOR ASSIST) · airframe 68,309 hrs · 19,812 cycles

DOOR 1L PASSENGER DOOR POWER RESERVOIR LOW. REPLACED DOOR 1L POWER RESERVOIR.

Part: PCU — FAILED (ELEVATOR) · airframe 68,193 hrs · 19,784 cycles

ELEV PCU STATUS MESSAGE. TROUBLESHOT ELEVATOR, FOUND LEFT SYSTEM PCU BAD. REPLACED PCU. LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,128 hrs · 19,765 cycles

LEFT OVERWING EXTERIOR EVAC LT INOP. RELAMPED EXTERIOR EVAC LIGHT.

Part: IDG — MALFUNCTIONED (NR 1 ENGINE) · airframe 67,918 hrs · 19,707 cycles

L GEN DRIVE LIGHT NOT ON WITH ENGINES OFF. ACP'D ENG RUN WITH VERIFICATION OF GEN DRIVE EICAS MSG, RESET IDG RING. REPLACED NR 1 ENG IDG. OPS CHECK GOOD.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 67,757 hrs · 19,661 cycles

DOOR 1L SLIDE PACK FELL OFF WHEN DOOR WAS OPENED. RE-INSTALLED SLIDE PACK.

Part: TRANSMITTER — DEFECTIVE (HYDRAULIC SYS) · airframe 67,725 hrs · 19,650 cycles

LOSS ALL RIGHT HYD QUANTITY. RT SYS SHOWS ZERO ON EICAS. GAUGE AT SVC PANEL ALSO ZERO FOR RT SYSTEM. FOUND NO EVIDENCE OF HYD LEAK AFTER OPERATING ALL SYSTEMS. SITE GAUGE FOUND RESERVOIR TO BE SERVICED TO BOTTOM OF SIGHT GAUGE. PER MEL SERVICED TO TOP OF SIGHT WINDOW OF RT RESERVOIR. RAN RT ENG AND CYCLED ALL FLT CONTROLS AND CONFIRMED NO LEAKS AND FLUID LEVEL STILL SERVICED TOP OF WINDOW. REPLACED RT HYDRAULIC QUANTITY TRANSMITTER. REFILLED SYSTEM, OPS CHECK OKAY.

Part: ACTUATOR — UNRELIABLE (RUDDER TRIM) · airframe 67,504 hrs · 19,584 cycles

RUDDER TRIM KNOB UNRESPONSIVE FOR RUDDER TRIM. INTERMITTENT, WHEN TRIMMING LT OR RT. REPLACED RUDDER TRIM ACTUATOR. INSPECTED INSTALLATION OF RUDDER TRIM ACTUATOR.

Part: FIRE LOOP — INOPERATIVE (LT NACELLE) · airframe 67,377 hrs · 19,541 cycles

LEFT ENGINE LOOP 1 FIRE DETECTION INOPERATIVE. REPLACED NR 1 LOOP (UPPER RESPONDER). TESTED OK BUT FOUND LOOP RUBBING AGAINST SUPPORT TUBE. AFTER INSTALLATION CHECKS OK.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 67,308 hrs · 19,520 cycles

DOOR 1L SLIDE CAME LOOSE. RE-INSTALLED SLIDE. ACP RII INSP OF DOOR 1L SLIDE, PER METHOD NR 4, CONFIRMED SLIDE SAFETY PIN REMOVED FROM SLIDE & DOOR ASSIST BOTTLE, ARMS & DISARMS NORMAL.

Part: FLAP TRACK — DAMAGED (RT WING TE FLAP) · airframe 67,219 hrs · 19,496 cycles

RT WING INBD FLAP OTBD FLAP TRACK ASSY STRUT ASSY HAS DEEP CUTS. REMOVED AND REPLACED THE RT I/B FLAP, O/B FLAP TRACK SUPPORT ASSY STRUT.

Part: CONTROLLER — FAULTY (TEMP CONTROL) · airframe 66,870 hrs · 19,389 cycles

HIGH PACK TEMP OUT. REPLACED PACK TEMP CONTROLLER. INSTALLED LEFT PACK CONDENSER. OPERATION CHECK NORMAL. LEAK CHECKED. NO LEAK FOUND.

Part: CONTROLLER — FAULTY (LT PACK) · airframe 66,870 hrs · 19,389 cycles

HIGH PACK TEMP OUT. REPLACED PACK TEMP CONTROLLER. INSTALLED LT PACK CONDENSER. OPERATION CHECK NORMAL. LEAK CHECKED. NO LEAK FOUND.

Part: INDICATOR — ERRATIC (RUDDER TRIM) · airframe 66,816 hrs · 19,375 cycles

RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. ACCMP'D TRIM TEST. TRIM INDICATION ERRATIC AT P8 PANEL, NORMAL ON EICAS DISPLAY. PULLED TRIM IND N83 AND NOTED INCREASE IN ERRATIC DISPLAY WITH LIGHT TAPPING ON CASE. REPLACED TRIM INDICATOR. RUDDER TRIM OPS AND INDICATION NORMAL.

Part: CONTROLLER — FAULTY (CABIN TEMP) · airframe 66,717 hrs · 19,342 cycles

AFT CABIN AUTO TEMP CONTROLLER INOP. LIGHT ON WITH SWITCH IN AUTO POSITION. REPLACED CABIN TEMP CONTROLLER. OP CHECKS GOOD.

Part: PAN — DAMAGED (NR 1 PYLON) · airframe 66,244 hrs · 19,200 cycles

NR 1 PYLON LOWER PAN DAMAGE, OUT OF LIMITS. ACCMP'D RE-CHECK INSPECTION OF DENT ON THE BOTTOM OF NR 1 ENGINE PYLON. CHECKED OK TO FOR SERVICE.

Part: WIRE — SHORTED (OIL SYSTEM) · airframe 65,768 hrs · 19,065 cycles

L OIL SCAV VALVE STATUS MSG. FOUND WIRE W3384-1005-18 SHORTED TO GROUND POPPING C-B C1482 T-R CONT-SCAV PRESS-L. SHORT IS BETWEEN CONNECTOR D41948P AT P36 PANEL AND CONNECTOR D5020 AT LEFT ENG T-R ISOLATION VALVE. T/S SYSTEM SUSPECT SHORT IS IN NR 1 ENG SAIL TAIL GOING UP TO PYLON OVER ENG, VERY LIMITED ACCESS. SUGGEST REPLACING WIRE. WIRE ON HAND (564-1452). CONNECTORS ON AOG 566-1548 AND 563-1775. REPAIRED WIRING PER GNMM 2-0-15-001. RE-ASSEMBLED CLAMPS, CONNECTORS, LACING.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 65,758 hrs · 19,061 cycles

FLASHLIGHT DOOR 3L DOES NOT FLASH. REPLACED BATTERY, OPS CHECK NORMAL.

Part: START VALVE — FAULTY (NR 1 ENGINE) · airframe 65,599 hrs · 19,015 cycles

NR 1 ENG START VALVE EICAS MESSAGE DISPLAYED DURING ENG START WITH STARTER ENGAGED. REPLACED NR 1 ENGINE START VALVE. OPS CHECK OK.

Part: START VALVE — FAULTY (NR 1 ENGINE) · airframe 65,599 hrs · 19,015 cycles

NR 1 ENG START VALVE EICAS MESSAGE DISPLAYED DURING ENG START WITH STARTER ENGAGED. REPLACED NR 1 ENGINE START VALVE. OPS CHECK OKAY.

Part: START VALVE — FAULTY (NR 1 ENGINE) · airframe 65,599 hrs · 19,015 cycles

NR 1 ENG START VALVE EICAS MESSAGE DISPLAYED DURING ENG START WITH STARTER ENGAGED. REPLACED NR 1 ENGINE START VALVE. OPS CHECK OKAY.

Part: EEC — FAILED (RT ENGINE) · airframe 65,456 hrs · 18,976 cycles

CREW COMMENTS: R ENG REV CONT STATUS MSG CAME ON IN CRUISE 4 HOURS INTO FLT. REPLACED EEC. CHECKED RIGHT REV STOW LVDT AND IS GOOD. FOUND LOOSE BACKSHELL ON PMA, TIGHTENED AND CLEANED CONNECTORS. ALSO REPLACED PMA AS PRECAUTION. IDLE CHECK GOOD. NO MESSAGE.

Part: EEC — FAULTY (RT ENGINE) · airframe 65,456 hrs · 18,976 cycles

CREW COMMENTS: R ENG REV CONT STATUS MSG CAME ON IN CRUISE 4 HOURS INTO FLT. REPLACED EEC. CHECKED RIGHT REV STOW LVDT AND IS GOOD. FOUND LOOSE BACKSHELL ON PMA, TIGHTENED AND CLEANED CONNECTORS. ALSO REPLACED PMA AS PRECAUTION. IDLE CHECK GOOD. NO MESSAGES.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 65,456 hrs · 18,976 cycles

CREW COMMENTS: R ENG REV CONT STATUS MSG CAME ON IN CRUISE 4 HOURS INTO FLT.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 65,311 hrs · 18,942 cycles

BIRD STRIKE TO NR 2 ENGINE. RTFL.

Part: ENGINE — DAMAGED (NR 2) · airframe 65,311 hrs · 18,942 cycles

BIRD STRIKE TO NR 2 ENGINE. RTFL. NR 2 ENG ACOUSTIC FAN EXIT SOUND ABSORBING LINER DAMAGED BEYOND 1 FT SQ. REMOVED NR 2 ENGINE. REPLACED WITH S/N 726538.

Part: BYPASS VALVE — FAULTY (FUEL/OIL COOLER) · airframe 64,758 hrs · 18,800 cycles

NR 2 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. DUE TO INCREASE IN OIL CONSUMPTION & NO LEAKS REPORTED DURING HIGH POWER REPLACED FCOC & BYPASS VALVE.

Part: APU — FAULTY · airframe 64,031 hrs · 18,619 cycles

APU HAS LOW BLEED AND HIGH EGT. REPLACED APU. NO LEAKS NOTED, NO FAULTS NOTED. OPS CHECK NORMAL.

Part: LANYARD — UNSECURE (R1 DOOR SLIDE) · airframe 63,800 hrs · 18,557 cycles

DOOR 1R WILL NOT ARM. SECURED LOOSE LANYARD ON SLIDE.

Part: SKIN — CORRODED (BS 1446 S30) · airframe 63,649 hrs · 18,522 cycles

CORROSION ON FUSELAGE SKIN WHERE AFT AIRFONE MOUNTS, BS 1446 AT STR 30. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING DOUBLER, CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR.

Part: SKIN — DAMAGED (BS 630) · airframe 63,649 hrs · 18,522 cycles

EXT FUSELAGE STA 630, FWD OF L-2 DOOR, FUSELAGE DOUBLER DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER REPAIR.

Part: PUMP — FAILED (FUEL BOOST) · airframe 63,649 hrs · 18,522 cycles

RIGHT AFT MAIN TANK FUEL BOOST PUMP FAILS RESISTANCE CHECK. FOUND HIGH INTERNAL RESISTANCE IN FUEL BOOST PUMP. REPLACED RT AFT BOOST PUMP. BONDING RESISTANCE CHECK GOOD, OPS, AND LEAK CHK GOOD

Part: STRINGER — DAMAGED (BS 1430 S30R) · airframe 63,649 hrs · 18,522 cycles

STR 30R AT STA 1430 REQUIRES REPAIR DUE TO PREVIOUS DAMAGE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF STRINGER. FABRICATED & INSTALLED A NEW STRINGER SECTION & SPLICE PLATE.

Part: STRINGER — DAMAGED (BS 1430 S29R) · airframe 63,649 hrs · 18,522 cycles

STR 29R AT STA 1430 REQUIRES RPR DUE TO PREVIOUS DAMAGE. MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED STRINGER WITH NEW STRINGER SECTION (P/N 146N3300-183).

Part: SKIN — DENTED (BS 630 S16L) · airframe 63,649 hrs · 18,522 cycles

EXT FUSELAGE STA 630 FWD OF L-2 DOOR, STR 16L HAS DENTED FASTENER HOLES. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED STRINGER SECTION. FABRICATED & INSTALLED A NEW SECTION AND SPLICE ANGLES.

Part: SKIN — DENTED (BS 628 S26-27L) · airframe 63,649 hrs · 18,522 cycles

DENT IN FUSELAGE AT BS 628 AND BETWEEN STR 26L-27L. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN. FABRICATED AND INSTALLED A REPAIR DOUBLER.

Part: FLOORBEAM — DAMAGED (BS 1661) · airframe 63,649 hrs · 18,522 cycles

MAIN CABIN, BLEND OUT ON UPPER CHORD OF BS 1661 FLOORBEAM AT RBL 60. *S/D* MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA. FABRICATED & INSTALLED A NEW T-SECTION AND SPLICES.

Part: FRAME — DAMAGED (BS 1420 S26L) · airframe 63,649 hrs · 18,522 cycles

BS 1420 STR 26L FRAME HAS DAMAGE. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED PREVIOUS REPAIR INCLUDING STRINGER CLIPS AND PRODUCTION SPLICE. FABRICATED & INSTALLED A REPAIR ANGLE.

Part: FRAME — DENTED (BS 1400 S26L) · airframe 63,649 hrs · 18,522 cycles

AFT PIT FRAME DENTED AT STA 1400 AND STR 26L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR ANGLE.

Part: MOTOR — FAULTY (BLOWER) · airframe 63,649 hrs · 18,522 cycles

IN AFT CARGO PIT, FIRE DETECTION BLOWER M1 0464 NEEDS TO BE REPLACED. (WHITE LIQUID OOZING FROM MOTOR HOUSING) INSTALLED NEW FIRE DETECTION MOTOR M10464.

Part: FRAME — DENTED (BS 500 S25L) · airframe 63,649 hrs · 18,522 cycles

FWD PIT FRAME DENTED UPPER FLANGE AT BS 500 AND STR 25L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (BS 660 S25L) · airframe 63,649 hrs · 18,522 cycles

FWD PIT AT STA 660 STR 25L, FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR.

Part: GATE — CORRODED (R4 DOOR) · airframe 63,649 hrs · 18,522 cycles

LOWER GATE CORRODED R-4 DOOR. REPLACED LOWER GATE.

Part: SKIN — DAMAGED (LT WING) · airframe 63,649 hrs · 18,522 cycles

FOUND LEFT WING AFT LOWER FIXED SKIN PANEL DAMAGED ON ARRIVAL. PANEL IS LOCATED JUST AFT OF LEFT GEAR AND FORWARD OF TRAILING EDGE FLAPS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN AND CORE. INSTALLED A LAY-UP REPAIR.

Part: STRUCTURE — GOUGED (L1 DOOR) · airframe 63,649 hrs · 18,522 cycles

L-1 HANDLE BOX GOUGED AT FASTENER POINTS. UNKNOWN DAMAGE/WEAR. REMOVED DAMAGED BOX ASSY, INSTALLED NEW BOX ASSY.

Part: STRUCTURE — DAMAGED (R2 DOOR) · airframe 63,649 hrs · 18,522 cycles

DOOR 2R HAS HANDLE BOX CRACKED AT INSERT HOLE. *S/D* UNKNOWN DAMAGE/WEAR. REMOVED DAMAGED HANDLE BOX AND INSTALLED NEW BOX.

Part: SKIN — DAMAGED (R2 DOOR) · airframe 63,649 hrs · 18,522 cycles

R-2 DOOR REQUIRES DOUBLER AT UPPER HINGE ARM CUTOUT. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR.

Part: SKIN — DAMAGED (L2 DOOR) · airframe 63,649 hrs · 18,522 cycles

L-2 DOOR REQUIRES DOUBLER AT UPPER HINGE ARM CUTOUT. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR.

Part: STRUCTURE — GOUGED (L4 DOOR) · airframe 63,649 hrs · 18,522 cycles

L-4 DOOR LOWER GATE LOWER EDGE HAS MATERIA L LOSS AND GOUGES. UNKNOWN DAMAGE. REMOVED DAMAGED LWR GATE AND INSTALLED NEW GATE.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 63,649 hrs · 18,522 cycles

MAIN CABIN STA 1640 FLOORBEAM TEE CAP CORRODED AT RBL 55. MAJOR REPAIR ACCOMPLISHED: CUTOUT CORRODED SECTION & INSTALLED REPAIR PER MM 53-00-98.

Part: STRUCTURE — DAMAGED (L2 DOOR) · airframe 63,649 hrs · 18,522 cycles

L-2 DOOR HANDLE BOX ASSY HAS SEVERAL CRACKS AT THE FASTENER HOLES, VIEWED EXTERNALLY. *S/D* UNKNOWN DAMAGE/WEAR. REMOVED DAMAGED BOX, ASSEMBLED AND INSTALLED NEW BOX.

Part: GROUND WIRE — DAMAGED (RUDDER TRIM) · airframe 63,005 hrs · 18,342 cycles

RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. WIRING SHORT AT S3 SWITCH. REPAIRED GROUND TO S3 SWITCH ON M74 PANEL, SYSTEM CHECKED OK.

Part: IDG — FAILED (RIGHT) · airframe 62,960 hrs · 18,329 cycles

RIGHT GENERATOR DISCONNECTED. RTFL. IDG FAILURE (LOW OIL) - TEARDOWN INCONCLUSIVE. REPLACED IDG.

Part: GIRT BAR — OUT OF ADJUST (R3 DOOR) · airframe 62,945 hrs · 18,323 cycles

DOOR 3R WILL NOT ARM. GIRT BAR SETTING OUT OF ADJUSTMENT. ADJUSTED GIRT BAR SETTING, ARMS/DISARMS NORMALLY.

Part: GIRT BAR — OUT OF POSITION (R4 DOOR) · airframe 62,867 hrs · 18,304 cycles

SLIDE ARMED LIGHT INOP 4R. FOUND AFT END OF GIRT BAR NOT IN THE FLOOR CLEET WHEN IN THE ARMED POSITION. POSITIONED GIRT BAR AND CYCLED SEVERAL TIMES AND LIGHT OP CHECKS OK.

Part: BEARING — FAILED (COOLING VALVE) · airframe 62,497 hrs · 18,204 cycles

E/E VALVE IS CLOSED W-NO AIR COMING OUT. BEARING FAILURE IN UNIT. REPLACED EQUIPMENT COOLING VALVE.

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 62,497 hrs · 18,204 cycles

OXYGEN MASK HOSE DEFECTIVE AT 2 (1=CAPT, 2=1ST OF, 3= 1ST OBS). CREW COMMENTS, HEADBAND HAS A HOLE IN IT. SUPPLEMENTAL DATA UPDATE, UNKNOWN DAMAGE. REPLACED O2 MASK ASSY-FO.

Part: GIRT BAR — OUT OF ADJUST (R3 DOOR) · airframe 62,454 hrs · 18,193 cycles

DOOR 3R SLIDE LIGHT WILL NOT COME ON AFTER ARMING. FOUND SLIDER OUT OF ADJUSTMENT ADJUSTED SLIDER ASSY ON AFT END OF GIRT BAR, OPS CHECKED NORMALLY.

Part: GIRT BAR — OUT OF ADJUST (R3 DOOR SLIDE) · airframe 62,420 hrs · 18,184 cycles

FOUND DOOR 3R WILL NOT ARM. ADJUSTED GIRT BAR, DOOR ARMS/DISARMS NORMALLY.

Part: CONTROL MODULE — MALFUNCTIONED (AILERON TRIM) · airframe 62,588 hrs · 18,231 cycles

RUDDER TRIM INOP INTERMITTENT. PER CREW INBOUND CREW, AC REQUIRED FREQUENT RETRIMMING AND AT TIMES, RUDDER TRIM WOULD BE INOP AND OTHERS IT WOULD TRIM NORMALLY, ALL AT CRUISE. OCCURRED ON THE GROUND AS WELL AFTER ARRIVAL. SUSPECT INTERMITTENT TRIM COMMAND FROM CONTROL PANEL. PRIOR TO REPLACING CONTROL PANEL, ATTEMPT (CONT). INTERMITTENT TRIM CONTROL MODULE, NO SHOP DATA. REPLACED AILERON AND TRIM CONTROL MODULES, ALL OPS CHECKS NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,220 hrs · 18,129 cycles

RIGHT AFT OVERWING EXIT LIGHT INOP. FOUND BULB INOP. REPLACED BULB.

Part: OXYGEN SYSTEM — LOW (CREW) · airframe 61,933 hrs · 18,045 cycles

CREW O2 NEEDS SERVICE 1400 PSI. SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME OF SERVICE.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 61,939 hrs · 18,047 cycles

DOOR ONE RIGHT SLIDE LIGHT WILL NOT ILLUMINATE AND UNABLE TO DISARM DOOR. FOUND DOOR SLIDE HARDWARE OUT OF ADJUSTMENT. ADJUSTED DOOR SLIDE HARDWARE, OPS CHECKED OK.

Part: SEAL — LEAKING (AILERON PCA) · airframe 61,875 hrs · 18,030 cycles

RT OTBD AILERON INBD PCA ACTIVE LEAK 50 DROPS PER MINUTE. FOUND LEAKING ROD SEAL ON PCA. REPLACED RT OUTBOARD AILERON INBOARD PCA.

Part: RESERVOIR — LOW (HYD SYSTEM) · airframe 61,870 hrs · 18,029 cycles

'CTR SYST RSVR' EICAS MSG DISPLAYED, QTY RDG .38. DEPARTED WITH CTR QTY AT .95. SELECTED PUMPS AND QTY CAME BACK UP A LITTLE TO .53. SERVICED CENTER HYD RES TO FULL. RAN ALL COMPONENTS ON CENTER SYSTEM FOR MORE THAN 1 HOUR NO FLUID LOSS NOTED. NO HISTORY.

Part: BRACKET — MISALIGNED (GIRT BAR) · airframe 61,825 hrs · 18,016 cycles

DOOR 3R NO DOOR ARMED LIGHT. FOUND GIRT BAR BRACKET MISALIGNED. REINSTALLED GIRT BAR BRACKET, OPS CHECKED NORMAL.

Part: RESERVOIR — MALFUNCTIONED (HYDRAULIC SYS) · airframe 61,630 hrs · 17,965 cycles

R HYD RESERVOIR PRESSURE EICAS AND ASSOCIATED OVERHEAD AMBER ILLUMINATED. REPLACED RESERVOIR AND ALL SWITCHES AND SENSORS.

Part: PRESSURE SWITCH — FAULTY (HYD SYSTEM) · airframe 61,562 hrs · 17,944 cycles

RIGHT HYDRAULIC SYSTEM RESERVOIR LIGHT ILLUMINATED. FOUND PRESSURE SWITCH FAULTY. REPLACED PRESSURE SWITCH, NO REPEATS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,328 hrs · 17,874 cycles

DOOR 2L EXTERIOR EMERGENCY LIGHT INOP. RELAMPED.

Part: OXYGEN SYSTEM — READS LOW (CREW) · airframe 61,106 hrs · 17,810 cycles

CREW OXYGEN LOW. SERVICED CREW O2- NO NOTED LEAKS PRESENT AT THIS TIME.

Part: TRIM SYSTEM — MALFUNCTIONED (RUDDER) · airframe 60,684 hrs · 17,682 cycles

CREW REPORT: UNABLE TO MOVE RUDDER TRIM WITH RUDDER TRIM KNOB.

Part: FMC — FAILED (RIGHT) · airframe 60,186 hrs · 17,533 cycles

RIGHT FMC ON TOP OF DESCENT WOULDN'T HOLD VNAV=GLIDE PATH HSI WOULD VARY+-1200-MIN PROG 2-2. 10-19-07 THE PROBLEM IS ATTRIBUTED TO A FAILED FLIGHT MANAGEMENT COMPUTER. REPLACED RT FMC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,980 hrs · 17,480 cycles

CEILING EMERGENCY EXIT LIGHT AT SEAT 12ABC INOP WHEN EMERGENCY LIGHTS SELECTED ON.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,502 hrs · 17,341 cycles

DOOR R2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED. OPS CHECK OK.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 59,172 hrs · 17,236 cycles

LEFT GENERATOR FAILED IN FLIGHT. COULD NOT RESET. [08-08-07] LT IDG REMOVED FOR INSPECTION AND TROUBLESHOOTING. IDG REPLACED.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 58,675 hrs · 170,092 cycles

RETURNED TO THE FIELD AFTER THE LOSS OF THE MAIN FUEL PUMP. [SUP 06-06-07] LEFT AFT BOOST PUMP IS REPAIRED TO CONFIRM FIX. AIRCRAFT REMAINED NON-ETOPS UNTIL A POSITIVE FIX OF FUEL PUMP WAS DETERMINED. REPLACED ENGINE FUEL FEED BOOST PUMP.

Part: CONNECTOR — LOOSE (BOOST PUMP) · airframe 58,578 hrs · 17,063 cycles

RTFL DUE TO LEFT AFT FUEL BOOST PUMP INOPERATIVE. [SUP 06-06-07] LEFT AFT FUEL PUMP ANNUNCIATED EICAS & LOW PRESS ON IN SWITCH. FOUND NR 1 ENG DRIVEN HYD PUMP CONNECTOR LOOSE. SECURED NR 1 ENGINE EDP DEPRESSURIZATION SOLENOID AS REQUIRED.

Part: JUMPER — FAULTY (EMERGENCY LIGHT) · airframe 58,135 hrs · 16,928 cycles

CABIN FLOOR EEL LIGHT STRIP FEEDER AND JUMPER CONNECTION. REPLACED FEEDER AND JUMPER AND OPS CHECKED OK.

Part: SQUIB — NO TEST (CABIN) · airframe 54,487 hrs · 15,914 cycles

EMERGENCY SLIDE LEFT SQUIB DOES NOT TEST.

Part: SLIDE — LEAKING (CABIN) · airframe 53,640 hrs · 15,671 cycles

THE SLIDE IS LEAKING IN BETWEEN THE GIRT ON THE SEAM. THE FAILURE IS ATTRIBUTED TO WEAR DAMAGE ON LOWER TUBE SEAM OF THE INFLATABLE AT THE GIRT ATTACHMENT.

Part: SKIN — DENTED (BS 750) · airframe 51,563 hrs · 15,078 cycles

SKIN DENT AT STA 750, STR 16L. TRIMMED OUT DAMAGE, INSURE CUT, INSTALLED FILLERS, DOUBLER, AND TRIPLER REPAIR PER REO-G11 002-C AND EVA-50676

Part: SKIN — DENTED (BS 258) · airframe 51,563 hrs · 15,078 cycles

FUSELAGE EXTERIOR AT BS 258 AND STR 28L HAS 1 DENT. REMOVED DAMAGE AND ACP HFEC NO CRACK INDICATION FABRICATED DOUBLER RPR IAW MM 53-30-95.

Part: TRANSCEIVER — MALFUNCTIONED (HF SYSTEM) · airframe 49,810 hrs · 14,550 cycles

RETURNED TO LAX DUE TO LOSS OF HF RADIOS. MAINTENANCE OPERATED SYSTEM ON GROUND AND COULD NOT DUPLICATE THE PROBLEM. THE HF SYSTEM FOR LEFT AND RIGHT SIDE OPERATED NORMALLY ON GROUND. AIRCRAFT HAS FLOWN WITHOUT HF PROBLEMS SINCE 4/19/2005. MAINTENANCE DID REPLACE THE RT HF TRANSCEIVER AND COMPONENT SHOP FINDINGS REPORT INDICATE THAT THERE WERE NO PROBLEMS FOUND WITH THE UNIT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,241 hrs · 13,571 cycles

DURING CLIMBOUT COULD NOT MAINTAIN NORMAL AIRSPEED AND PITCH ATTITUDE. FLIGHT LEVEL 300-340 MAX EPR 1.45. FLIGHT DATA RECORDER INDICATED AIRCRAFT WAS OPERATING WITHIN THE NORMAL FLIGHT ENVELOPE PARAMETERS.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 45,148 hrs · 13,270 cycles

GEAR DISAGREE EICAS MESSAGE WITH THE GEAR HANDLE IN THE UP POSITION. AMBER CAUTION LIGHT ILLUMINATED. THE CAUSE WAS A GEAR POSITION PROXIMITY SENSOR. MAINTENANCE JACKED THE AIRCRAFT AND CLEANED MULTIPLE PROXIMITY SENSOR TARGETS.

Part: LIGHT — BURNED (PARK BRAKE IND) · airframe 45,058 hrs · 13,244 cycles

ON ENGINE SHUTDOWN, ELECTRICAL ODOR IN COCKPIT. FOUND PARKING BRAKE ANNUNCIATOR BASE AND LENS ASSEMBLY FAILED. REPLACED LIGHT ASSEMBLY AND BASE L413.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,068 hrs · 11,911 cycles

LT FUSE STA 1701 DENTED IN 2 PLACES, JUST ABOVE STRINGER 19 AND JUST BELOW STRINGER 20.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,068 hrs · 11,911 cycles

CABIN FLOOR BEAM EXCESSIVE MATERIAL LOSS DUE TO CORROSION STATION 1640 RBL36-38.5 UPPER CAP. MAJOR REPAIR ACCOMPLISHED. REMOVED 2 STRAPS AND ANGLE INSTALLED.

Part: WEB — GOUGED · airframe 40,068 hrs · 11,911 cycles

1 RIGHT HAND MAIN ENTRY DOOR BODY TORQUE FUSE PRESSURIZED SUPPORT WEB GOUGED. MAJOR REPAIR ACCOMPLISHED. NEW WEB INSTALLED.

Part: FRAME — DENTED · airframe 40,068 hrs · 11,911 cycles

AFT CARGO FUSELAGE FRAME DENT STATION 1420 STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED J ANGLE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,068 hrs · 11,911 cycles

STATION 365 RBL10-RBL62 WL208 TOP OF FLOORBEAM HAS PAINT WORN OFF AND LT CORROSION IN SEVERAL SPOTS. MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER T-CAP.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,068 hrs · 11,911 cycles

CABIN LEFT HAND CREASE BEAM WEB CORRODED STATION 1000-1020. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,068 hrs · 11,911 cycles

CABIN LEFT HAND CREASE BEAM WEB CORRODED STATION 970. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,068 hrs · 11,911 cycles

CABIN FLOOR BEAM INBOARD CHORD EXFOLIATED AT STATION 681 LBL 62. MAJOR REPAIR ACCOMPLISHED. REPLACED CHORD ANGLE WITH NEW.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,068 hrs · 11,911 cycles

CABIN CREASE BEAM EXCESSIVE CORROSION STATION 690-740 STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM SECTION.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,068 hrs · 11,911 cycles

CABIN RIGHT HAND CREASE BEAM CORRODED STATION 970. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,068 hrs · 11,911 cycles

CABIN FLOORBEAM UPPER CAP AFT FLANGE STATION 1640 HAS EXCESSIVE MATERIAL LOSS FROM CORROSION REMOVED AT RBL 51 TO RBL 52. MAJOR REPAIR ACCOMPLISHED. BEAM CAP STRAP REPAIR INSTALLED.

Part: SENSOR — MALFUNCTIONED (RT MLG) · airframe 39,417 hrs · 11,718 cycles

GEAR DISAGREE LIGHT EICAS MESSAGE. PSEU BITE CHECK SHOWS SENSORS 59 AND 239 (SYSTEM 1 & 2 RIGHT GEAR UPLOCK). SENSORS PASSED TARGET TEST FOR TARGET FAR AND WHEN SLUGGED. NO OTHER DISCREPANCIES.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 38,310 hrs · 11,409 cycles

RIGHT FORWARD FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED. REPLACED THE RIGHT FORWARD FUEL BOOST PUMP.

Part: SWITCH · airframe 36,168 hrs · 10,841 cycles

LEFT EMERGENCY ESCAPE SLIDE SQUIB TEST FAILED IN #1 TEST POSITION. CLEANED TEST SWITCH, SLIDE SQUIB CHECK OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,618 hrs · 10,177 cycles

DENT FOUND APPROXIMATELY 2 FEET BELOW 3L DOOR. DOUBLER REPAIR INSTALLED WITH BLIND FASTENERS. THIS WAS A MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,618 hrs · 10,177 cycles

DENT FOUND APPROXIMATELY 3 FEET BELOW DOOR 3L. DOUBLER REPAIR INSTALLED WITH BLIND FASTENERS. THIS WAS A MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,619 hrs · 10,445 cycles

DENT IN FUSELAGE SKIN 42 INCHES AFT OF DOOR 2L, STRINGER 16L. INSTALLED DOUBLER AND REPAIRED STRINGER 16L BS 770-780 PER SRM.

Part: CONNECTOR — DAMAGED (EEC) · airframe 33,988 hrs · 10,270 cycles

LEFT ENGINE CONTROL MESSAGE DISPLAYED 3 HOURS INTO FLIGHT. *S/D* REPLACED EEC ALTERNATOR AND CONNECTOR D4858 ON EEC. EEC ALTERNATOR STATOR WAS REPLACED PRIOR TO DEPARTURE FOR MESSAGES. THREE HOURS INTO OUTBOUND FLT MESSAGE REOCCURRED. FOUND TWO PINS PUSHED BACK AND LOCKS DAMAGED ON EEC ALTERNATOR CONNECTOR D4858. REPLACED CONNECTOR D4858 AND AS A PRECAUTIONARY MEASURE THE EEC ALTERNATOR WAS REPLACED AGAIN.

Part: SLIDE — FAILED (CABIN)

SLIDE/RAFT FAILED AIR RETENTION CHECK DURING OVERHAUL BY VENDOR. *S/D* POROSITY, DUE TO EXCESS MOISTURE, WAS THE CAUSE OF THE FAILED SLIDE/RAFT. VENDOR REPLACED THE INFLATABLE.

Part: POWER STRIP — FAILED (ROW 9-16)

EEL LIGHTING FROM ROW 9 TO ROW 16 INOP. REPLACED EEL FEEDER POWER STRIP FROM ROW 9 TO ROW 16.

Part: FSEU — FAILED (NR 1)

FLAPS WOULD NOT MOVE PAST 20 DEGREES. DIVERTED TO LAX. *S/D* FOUND FAULTY NR 1 FSEU. REPLACED FSEU, OPERATIONALLY CHECKED AND FOUND SYSTEM NORMAL.

Part: CDU — FAILED (RT COCKPIT)

FIRST OFFICERS' FLIGHT MANAGEMENT COMPUTER, CENTRAL DATA UNIT INOPERABLE AFTER TAKEOFF. AIRCRAFT RETURNED TO HNL. VERIFIED THAT GOOD AIR FLOW WAS PASSING TO CDU (CENTRAL DATA UNIT) THROUGH INLET SCREEN. REPLACED CDU.

Part: WIRE — BROKEN (CABIN)

AFT CABIN FLOOR EMERGENCY ESCAPE LIGHTING INOP AT LAVATORY. DISCOVERED FEEDER WIRE TO LIGHT STRIP BROKEN. REPLACED BROKEN SECTION, LIGHT CHECKS NORMAL.