N566UA

Part: GUARD — OUT OF ADJUST (CABIN) · airframe 69,613 hrs · 25,553 cycles

EMERGENCY EXIT LIGHTS COME ON IN THE OFF POSITION. CREW REPORTS WHEN EMERGENCY LIGHTS SWITCH IS TURNED OFF, EMERGENCY LIGHTS ILLUMINATE. FOUND AFT ATTENDANT PANEL SWITCH GUARD FOR EMERGENCY LIGHT BLOCKING SWITCH FROM PUSHING COMPLETELY OUT. ADJUSTED AFT ATTENDANT SWITCH GUARD IAW AMM, OPERATIONS CHECKED GOOD.

Part: IDG — FAILED (NR 1 ENIGNE) · airframe 69,446 hrs · 25,502 cycles

LT GEN OFF LIGHT ILLUMINATED, RTFL. CREW CYCLED IAW FM & GEN RETURNED. CLIMBING THRU 24K LOSS OF LT BUS WITH ASSOCIATED LIGHT, LT GEN OFF LIGHT & APU ON SPEED. REPLACED NR 1 IDG, LBCU & GCU. RAN ENGINES, NO FAULTS.

Part: O-RING — DAMAGED (THRUST REVERSER) · airframe 68,997 hrs · 25,355 cycles

ON WALK AROUND FLT CREW REPORTS NR 1 ENG STRUT DRAIN LINE, LARGE LINE NR 2 LEAKING. REPLACED O-RING ON UPPER INBD HYD UNION ON THRUST REVERSER DIRECTIONAL CONTROL VLV. OPERATION CHECKED RAN REVERSER SEVERAL TIMES, NO LEAKS NOTED. NR 1 ENG OIL LEAKING, REPLACED "O" RING.

Part: SWITCH — CONTAMINATED (LT MLG) · airframe 68,894 hrs · 25,324 cycles

LT MLG DOOR UNSAFE LIGHT IS INOPERATIVE. RELAMPED, NO HELP. FOUND SW S10371 FULL OF HYD FLUID & DETERIORATED ON TOP OF SW. CLEANED LIGHT ASSEMBLY, CONTACTS & GND'S, STILL NO JOY. PIGGY NEW GROUND TO LIGHT ASSEMBLY, NO HELP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,126 hrs · 25,070 cycles

EMERGENCY LIGHT JUST AFT OF L1 DOOR INOPERATIVE. INSTALLED NEW EMERGENCY LIGHT, OPS CHECKED SATISFACTORY.

Part: LIGHT — CONTAMINATED (CABIN) · airframe 68,126 hrs · 25,070 cycles

EMERGENCY LIGHT JUST AFT OF L2 DOOR INOPERATIVE. FOUND WATER UNDER EMERGENCY LIGHT COVER. DRIED OUT WATER. OPS CHECKED SATISFACTORY.

Part: LAMP — WRONG PART (DOOR SLIDE) · airframe 67,932 hrs · 25,009 cycles

R3 DOOR EVAC SLIDE LIGHT ABOVE DOOR ILLUMINATED. DOOR SLIDE LIGHT STAYS ON ALL THE TIME. FOUND INCORRECT LAMP ASSY, CLEANED AND REPLACED LAMP ASSY, OPS NORMAL VARIOUS TIMES.

Part: MICROPHONE — MALFUNCTIONED (OXYGEN MASK) · airframe 67,921 hrs · 25,005 cycles

CREW O2 MASK MICROPHONE HOT. R & R MASK IAW MM. MASK OPS NORMAL BUT STILL HAVE HOT MICROPHONE PROB. PERFORMED OPS CHECK, MASK MIC IS NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 67,916 hrs · 25,002 cycles

EMERGENCY LIGHT IN FRONT OF L2 DOOR IS INOPERATIVE. CONNECTED EMERGENCY LIGHT. OPS CHECKED GOOD, OK FOR SERVICE.

Part: FILTER — FAILED (LT ENGINE OIL SY) · airframe 67,820 hrs · 24,972 cycles

DURING CLIMB, OIL FILTER ON EICAS. RETURNED TO FIELD. R & R OIL FILTER IAW IAW, NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,455 hrs · 24,855 cycles

EEL LIGHT INOP AT FWD CLOSET. REPLACED LEAD IN P/N 5879 -1 & CONNECTOR P/N 5878-1 PER MM & REPLACED LAMP P/N 36262-4 PER MM. REPLACED END CAPS & LENS COVER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,455 hrs · 24,855 cycles

EEL LIGHT INOP AT ROW 38. REPLACED LAMP P/N 36262-4 PER MM. ACP'D IDT OF EEL LIGHT INSTALLATION AT ROW 38.

Part: FEEDER CABLE — DEFECTIVE (CABIN) · airframe 67,227 hrs · 24,789 cycles

FLOOR EEL LIGHT LOCATED IN FRONT OF FORWARD CLOSET IS INOP. OTHER EEL LIGHTS IN AREA WORK FINE. REPAIRED EEL LIGHT FEEDER. OP CHECK SATISFACTORY.

Part: FAN — INOPERATIVE (NR 1) · airframe 67,001 hrs · 24,720 cycles

HOT ODOR FOR 2-3 MINUTES AFTER TAKEOFF, WENT AWAY BY ITSELF, DE ICE WAS NOT AN ISSUE. ACCOMPLISHED AC SYSTEM CHECK. REF MM 21-00-01-301 PROCEDURE 1. BEGAN FIM UP TO PROCEDURE 13A. INSPECTED LEFT RECIRCULATION FAN IN FORWARD CARGO FOR BURNED WIRES AND ODOR. NO PROBLEM FOUND. LEFT FAN WORKS NORMAL. REPLACED NR 1 FWD COOLING SUPPLY FAN.

Part: FEEDER CABLE — DEFECTIVE (EMERGENCY LIGHT) · airframe 66,887 hrs · 24,677 cycles

CABIN 'A' ZONE EMERGENCY LIGHT INOPERATIVE. REPAIRED 'A' ZONE EMERGENCY LIGHT FEEDER CABLE, OPS CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 66,887 hrs · 24,677 cycles

AFT FUSELAGE SKIN DENTED AT STA 1606 STR 23L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN, ACP'D HFEC OF SKIN CUT-OUT & FASTENER HOLES. NO DEFECT NOTED. FAB & INSTALLED .050 DOUBLER ON STA 1606 STR 23L-24L PER SRM 53-00-01 RPR 3.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,887 hrs · 24,677 cycles

RIGHT OVERWING EXIT LIGHT INOPERATIVE. REPLACED RIGHT OVERWING EXIT LIGHT BATTERY PACK PER AMM, OPS CHECK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 66,887 hrs · 24,677 cycles

AFT FUSELAGE SKIN DENTED AT STA 1549 STR 23L. MAJOR REPAIR ACCOMPLISHED. MAINT TEXT: CUT OUT DAMAGED SKIN, ACP'D HFEC OF SKIN CUT-OUT & FASTENER HOLES. NO DEFECT NOTED. FAB & INSTALLED .050 DOUBLER ON STA 1549 STR 23L-24L PER SRM 53-00-01 REPAIR 3.

Part: FEEDER CABLE — DEFECTIVE (CABIN) · airframe 66,887 hrs · 24,677 cycles

'C' ZONE EEL ROW 29 ABC 37ABC INOPERATIVE. REMOVED AND REPLACED FEEDER IAW B757 MM, OPS CHECKS GOOD.

Part: SKIN — DENTED (BS 1549-1606) · airframe 62,979 hrs · 23,311 cycles

SMALL DENTS IN AFT FUSELAGE BS 1549 - 1606 JUST ABOVE CARGO FLOOR LINE. ACCOMPLISHED HFEC INSPECTION AND FOUND NO CRACKS. REPAIRED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,887 hrs · 24,677 cycles

DENT ARCHIVE ITEM APPEARS TO HAVE ADDITIONAL DAMAGE OVER WHAT IS DESCRIBED IN ARCHIVED TXT. AT BS 610, STR 16L TO 17L. REPAIRED AREA IAW SRM 53-00-01 REPAIR 2, FIG 201.

Part: STRINGER — DAMAGED (BS 610 S17L) · airframe 66,887 hrs · 24,677 cycles

BS 610 STRINGER 17L HAS DOUBLE DRILLED HOLE. REPAIRED STRINGER IAW ECRA 5361-01040 AND REO 615957 REV A. MAJOR REPAIR.

Part: FRAME — GOUGED (CARGO DOOR) · airframe 66,887 hrs · 24,677 cycles

FWD CARGO DOOR LOWER END ATTACH FRAME IS GOUGED IN SEVERAL PLACES. REMOVED AND REPLACED LOWER ATTACHED FRAME IAW SRM. MAJOR REPAIR.

Part: SKIN — DENTED (BS 610 S16-17L) · airframe 37,740 hrs · 13,826 cycles

SKIN DENTED BS 610, S16-17L. HFEC INSPECTED, NO CRACKS NOTED. REPAIRED. MAJOR.

Part: WEB — CORRODED (BS 1680) · corrosion level 2 · airframe 66,887 hrs · 24,677 cycles

MAIN CABIN SUB FLOOR WEB, CORRODED SEVERAL PLACES BS 1680, RBL 40 - 60. REMOVED AND REPLACED WEB IAW 51-40 02 AND ECRA 5330-04259. REPAIR DOUBLER INSTALLED. MAJOR REPAIR.

Part: STRINGER — CRACKED (STA 620 S18L) · airframe 66,887 hrs · 24,677 cycles

MAIN CABIN STRINGER 18L AT BS 620 CRACKED ON LOWER FLANGE. REPAIRED STRINGER IAW SRM 53-00-03, REPAIR 1. CATEGORY 'A' MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 66,887 hrs · 24,677 cycles

MAIN CABIN FLOORBEAM UPPER TEE CORRODED AT BS 1640, LBL 5 - RBL 62. FABRICATED & INSTALLED NEW FLOORBEAM TEE IAW SRM 53-00-51, FIG 201. MAJOR REPAIR.

Part: RECEPTACLE — FAILED (FIRE WARNING) · airframe 66,764 hrs · 24,639 cycles

CARGO FIRE LIGHT FAILED TO ILLUMINATE DURING ENGINE APU CARGO FIRE OVERHEAT TEST. EICAS MESSAGE (AFT CARGO FIRE) WAS NOT DISPLAYED. AFT CARGO ARM SWITCH DOES NOT ILLUMINATE DURING FIRE TEST OR MASTER TEST. REPLACED RECEPTACLE. OPS CHECKED GOOD.

Part: WEDGE — DAMAGED (TE FLAP) · airframe 65,642 hrs · 24,241 cycles

DAMAGE TO RIGHT I/B FLAP AFT I/B TRAILING EDGE WEDGE. MEASURES APPROX 8IN BY 3IN. WILL REQUIRE PERM REPAIR PER SRM. MATERIAL ETA 0730 UNDER OSTF'S LISTED. REPAIRED DAMAGED FLAP PER SRM 57-53-01 & SRM 51-70-17. PRIMED & PAINTED TO MATCH.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 65,635 hrs · 24,239 cycles

NR 1 RIGHT WINDSHIELD DELAMINATION. REPLACE NR 1 RT WINDSHIELD PER AMM. ENSURE COA 507402 IS ACCOMPLISHED WHICH REPLACES THE WINDSHIELD WITH A PIN & SOCKET ELECTRICAL CONNECTION. WINDSHIELD (120-4147), KIT-COA (103-2282),GREEN TYSTRAPS (586-1594).

Part: SEAL — LEAKING (R1 DOOR) · airframe 65,429 hrs · 24,174 cycles

CHRONIC DOOR 1R SQUEAL. RECONDITIONED AND SANDED REN AND CLEANED SEALING SURFACES. DOOR 1 RT UPPER GATE SEAL OUT OF RETAINER AT FWD EDGE. REINSTALLED UPPER GATE SEAL INTO RETAINER REF MM.

Part: GATE — CRACKED (R2 DOOR) · airframe 65,154 hrs · 24,085 cycles

DOOR 2R UPPER HINGE CUTOUT CRACKED AND SMC5 DOOR 1R UPPER GATE CRACKED. REMOVED DOOR 2R. ACCOMPLISHED CHECK. REPAIRED PER MM.

Part: GATE — CRACKED (R1 DOOR) · airframe 65,154 hrs · 24,085 cycles

DR 2R HAS CRACK .25 LONG AT UPPER HINGE CUTOUT. ALSO FOUND R1 DOOR UPPER GATE CRACKED AT SECOND RIVET.

Part: IGNITER — ARCED (NR 1 ENGINE) · airframe 65,992 hrs · 24,341 cycles

NR 1 ENGINE LOWER IGNITER AND LEAD SHOW EVIDENCE OF ARCING. REPLACED LOWER IGNITER AND LEAD ASSY.

Part: COVER — DAMAGED (CABIN) · airframe 65,066 hrs · 24,056 cycles

EMERGENCY FLOOR PATH LIGHTING, CLEAR PLASTIC COVER DAMAGED FROM ROWS 8 TO 12C. INSTALLED NEW CLEAR PLASTIC COVER SECTION AND OP CHECKED LIGHT STRIP. EEL STRIP CHECK'S GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 64,888 hrs · 23,999 cycles

EMERGENCY LIGHT INOPERATIVE APPROXIMATELY SEAT ROW 11. ONE EACH ORANGE AND WHITE SECTION INOPERATIVE. SPLICED IN A NEW CONNECTOR IAW MM 33-51-96.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,893 hrs · 24,000 cycles

UPON IDT INSPECTION OF LM3881 FOUND ONE EMERGENCY LIGHT STRIP ORANGE INOPERATIVE. LOCATED AT FWD LT OVERWING DOOR AREA. LIGHT STRIP OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,893 hrs · 24,000 cycles

EMERGENCY LIGHT INOPERATIVE AT DOOR 2 LEFT, IN FRONT OF LAVATORY DOOR. REPLACED LIGHT.

Part: FLAP — MALFUNCTIONED (WING) · airframe 64,106 hrs · 23,731 cycles

FLAPS ASYMMETRY FLAP STUCK AT 20 ONLY ONE SIDE WILL EXTEND PAST 20. INSPECTED FLAPS & SLATS. NO DISCREPANCIES FOUND. ACCOMPLISHED OPERATIONAL CHECK PER MM.

Part: ARMREST — FAULTY (CABIN) · airframe 63,957 hrs · 23,675 cycles

SHOULD READ SEAT 27C ARMREST CAP STUCK IN UP POS. MADE TEMP REPAIR WITH TAPE TAP2502-1-0300. REPLACED ARMREST AT 27C.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 63,951 hrs · 23,674 cycles

RIGHT TANK WILL NOT TAKE FUEL. TRIED OPENING VALVE MANUALLY, NO HELP. REPLACE RT FUELING VALVE ACTUATOR PER MM. OPS CHECK GOOD, NO LEAKS.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 63,313 hrs · 23,444 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 11. SECURED CONNECTOR AT LIGHT ASSY.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 63,313 hrs · 23,444 cycles

EMERGENCY LIGHT LOOSE BY FWD LAVATORY. THE PROBLEM IS WITH THE MALE POWER CONNECTOR WHICH RUNS FROM THE BATTERY PACK TO THE LIGHT. BOTH PINS ARE BROKEN. REPLACED LIGHT AND OPS OKAY.

Part: UNKNOWN — ODOR (CABIN) · airframe 62,861 hrs · 23,265 cycles

F/A REPORTED ODOR OF BURNING RUBBER AT DOOR 2 ON DESCENT. PERFORMED INSPECTION OF AREA. MID LAV, MID GALLEY, LIGHTS, DOOR AREA, VIDEO MONITOR, ALL IN ON CONDITION. NO ABNORMALITIES OR ODORS NOTED. ALSO INSPECTED OUTSIDE DOOR AREAS AND LANDING GEAR AREAS. ALL NORMAL.

Part: DOOR — LEAKING (R1) · airframe 62,832 hrs · 23,251 cycles

DOOR 1R MAKES AIR LEAK NOISES DURING CLIMBOUT. PRESSURIZED TO 4 PSI, FOUND MULTI AIR LEAKS. REPAIRED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,811 hrs · 23,241 cycles

EMEGENCY LIGHT DAMAGED LEFT SIDE FROM EMERGENCY EXIT TO DOOR 2L. REPLACED AND INSTALLED NEW LAMP AND CLEAR STRIP COVER.

Part: LIGHT — INOPERATIVE (R3 DOOR) · airframe 62,787 hrs · 23,234 cycles

AFT R DOOR SLIDE LIGHT WON'T ILLUMINATE. DOOR 3R DOOR SLIDE RELAMPED.

Part: ENGINE — MAKING METAL (NR 2 ENGINE) · airframe 62,439 hrs · 23,103 cycles

ENGINE NR 2 VIB N1 3.7 IN CLIMB TO FL390 CRUISE. SAMC TEXT: CREW REPORTS VIBES FELT AND INDICATION AMPLITUDE MATCHED THROTTLE MOVEMENT. NEED TO TROUBLESHOOT PER FIM 71-05-00 FIG 106. **METAL FOUND IN TAILPIPE, REPLACE ENGINE, SEE LM1400. REPLACED ENG PER MM. OPS AND LEAK CHECKS GOOD.

Part: ENGINE — MAKING METAL (NR 2) · airframe 62,439 hrs · 23,103 cycles

CREW REPORT: ENGINE NR 2 VIB N1 3.7 IN CLIMB TO FL390 CRUISE1.1. SAMC TEXT: CREW REPORTS VIBES FELT AND INDICATION AMPLITUDE MATCHED THROTTLE MOVEMENT. NEED TO TROUBLESHOOT PER FIM. METAL FOUND IN TAILPIPE, REPLACE ENGINE, SEE LM1400.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,920 hrs · 22,920 cycles

DOOR NR 1 LT AND RT EMERGENCY EXIT LIGHTS INOPERATIVE. RELAMPED, OPERATES NORMAL.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 61,511 hrs · 22,769 cycles

CREW REPORTS ON APPROACH WHEN FLAP HANDLE MOVED FROM 5 TO 15, RT NEEDLE NEVER MOVED FROM 5 AND LEFT NEEDLE MOVED TO 15. FLAPS LOCKED OUT WITH EICAS MESSAGE T/E FLAP ASYM DISPLAYED. SAMC TEXT: PER DEBRIEF, T/E FLAP ASYM MSG WAS NOT DISPLAYED. REPLACED FLAP POSITION INDICATOR PER MM. TEST IS GOOD.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHTS) · airframe 61,403 hrs · 22,729 cycles

AT 16ABC EMERGENCY EXIT LIGHTS DETACHED. FOUND LOOSE CONNECTION IN EMERGENCY LIGHT WIRE HARNESS, RECONNECTED AND ALL OPS CHECKED NORMAL.

Part: ATTACH BRACKET — OUT OF TOLERANCE (RT WING TE FLAP) · airframe 61,265 hrs · 22,677 cycles

RIGHT INBOARD TE AFT FLAP, INBOARD PUSHROD ATTACH BRACKET HAS BEARING LOOSE AND COMING OUT OF BRACKET. REPLACED BRACKET AND BEARING ASSY. BRACKET IS SECURED ON FLAP.

Part: STEERING SYS — OUT OF ADJUST (NLG) · airframe 61,265 hrs · 22,677 cycles

AIRPLANE PULLS LEFT DURING TAXI. ADJUSTED NOSE WHEEL STEERING, TAXI TEST GOOD.

Part: PAN — CORRODED (FUSELAGE) · airframe 61,257 hrs · 22,672 cycles

GALLEY G4B FLOOR PAN IS CORRODED FROM STA 1680 TO 1686 LBL 20 TO RBL 58. MAJOR REPAIR ACCOMPLISHED: REPAIRED WITH PTT SEQ 2572135 UNDER PEMCO EA PD57-53-097. REMOVED CORROSION AND FOUND AREAS TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGE AND ACCOMPLISHED NDT INSPECTION OF AREA WITH NO CRACKS FOUND. ACCOMP THE FABRICATION OF A REPAIR PER PEMCO EA PD57-53-097. THIS IS CONSIDERED A PERMANENT REPAIR PER SR 1-1825027235 WITH APPROVAL OF FORM 8100-9 DATED MAR 24,2011.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 61,257 hrs · 22,672 cycles

GALLEY G4B FLOOR DECK IS CORRODED FROM STA 1686, LBL 20 TO RBL 58. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION AND FOUND AREAS TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGE AND ACCOMPLISHED NDT INSPECTION OF AREA WITH NO CRACKS FOUND. ACCOMP THE FABRICATION OF A REPAIR PER PEMCO EA PD57-53-097. THIS IS CONSIDERED A PERMANENT REPAIR PER SR 1-1825027235 WITH APPROVAL OF FORM 8100-9 DATED MAR 24,2011.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,257 hrs · 22,672 cycles

RIGHT CREASE BEAM UPPER SURFACE HAS CORROSION AT BS 975 AT RBL 71. MAJOR REPAIR ACCOMPLISHED: CORROSION FOUND TO BE OUT OF LIMITS PER SRM. FABRICATED NEW CREASE BEAM WEB OUT OF 7075-0 .063 PER SRM. HEAT TREATED AND PRIMED PER AMM. TOP COATED CREASE BEAM WEB AMM. INSTALLED RT CREASE BEAM WEB IAW 757-200 SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,257 hrs · 22,672 cycles

LEFT CREASE BEAM O/B FLANGE COMMON TO INTERNAL FUSELAGE CORRODED AT STA 1006, LBL 71. AGING ACFT INSP FINDINGS. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION, FABBED ANGLE, ACP'D HFEC ON ALL HOLES AND AREA FOR CRACKS. NO DEFECTS NOTED. INSTALLED ANGLE PER PEMCO EA PD57-53-098.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,257 hrs · 22,672 cycles

STATION 324 RBL 41 FLOORBEAM HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED FLOORBEAM STA 324, RBL 41 IAW PEMCO EA PD57-536-096.

Part: BEAM — CORRODED (FUSELAGE) · airframe 61,257 hrs · 22,672 cycles

AFT CARGO COMPARTMENT STATION 1620 LAP BEAM AT SW-30 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION, FABBED AND INSTALLED REPAIR DOUBLER PER PEMCO EA PD57-53-103.

Part: FLOORBEAM — CORRODED (BS 1661) · airframe 61,257 hrs · 22,672 cycles

FLOORBEAM HAS CORROSION AT STATION 1661 LBL 11 AND RBL 4. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA OF TOP CHORD AND FABRICATED REPLACEMENT BEAM AND 2 SUPPORT ANGLE AND 2 STRAPS IAW SRM. TREATED AND PRIMED ALL PARTS PER 757 SRM. INSTALLED REPAIR PER SRM AND TOP COATED PER SRM.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 61,257 hrs · 22,672 cycles

CORROSION ON CABIN FLOOR BEAM AT STA 1640 AT RBL 14 TO RBL 40. MAJOR REPAIR ACCOMPLISHED: REMOVED TEE ANGLE IAW SRM, DUE TO EXCESSIVE MATERIAL REMOVED AND OUT OF LIMITS. FABRICATED REPLACEMENT TEE CHORD & INSTALLED PER SRM. TREATED AND PRIMED IAW SRM. TOP COATED PER SRM.

Part: FLOORBEAM — CORRODED (BS 365.25) · airframe 61,257 hrs · 22,672 cycles

STATION 365.25 RBL 0 TO RBL 40 FLOORBEAM IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION AND FOUND ARE TO BE OUT OF LIMITS. REMOVED TEE CHORD AND ATTACHING ANGLE. FABRICATED TEE CHORD AND SUPPORT ANGLES. TREATED & PRIMED PARTS PER SRM. INSTALLED TEE CHORD AND SUPPORTS PER SRM. TOP COATED REPAIR PER SRM.

Part: SHEAR TIE — CORRODED (BS 1620 S30) · airframe 61,257 hrs · 22,672 cycles

AFT CARGO PIT CORROSION DISCOVERED AT BS 1620 ON SHEAR TIE AT S-30. MAJOR REPAIR ACCOMPLISHED: AFTER CORROSION REMOVAL IT WAS DISCOVERED TO BE BEYOND LIMITS IAW SRM. FABRICATED A NEW SHEAR TIE FROM 7075-T6, 063 PER SRM AND INSTALLED PER SRM.

Part: SMOKE DETECTOR — UNKNOWN (EQ COOLING) · airframe 61,257 hrs · 22,672 cycles

EQUIP COOL SMOKE DETECTORS NEEDS REPLACEMENT. REPLACED EQUIP COOL SMOKE DETECTORS ON TASKCARD.

Part: FAN — FAULTY (EQUIP COOLING) · airframe 60,769 hrs · 22,474 cycles

ELECTRICAL ODOR IN COCKPIT, FLIGHT DIVERTED. FOUND EQP COOLING SUPPLY FAN NR1 TO BE SOURCE OF ODOR. REPLACED EQUIPMENT COOLING FAN NR 1, OPS CHESKED OK.

Part: SWITCH — FAULTY (FUEL SYSTEM) · airframe 60,644 hrs · 22,426 cycles

RT ENG FUEL FILTER MSG, FLIGHT DIVERTED. IAW CREW AFTER TAKEOFF FROM SNA, NR2 ENG FUEL FILTER ADVISORY AND STATUS MSG. ALL OTHER INDICATIONS AND ENGINE IS RUNNING NORMAL. REPLACED NR2 ENG FUEL FILTER & DP SW ON LM7019, RAN NR2, ENG 5 MIN IDLE, NO LEAKS NO FAULTS.

Part: ADC — FAILED (NR 2) · airframe 60,553 hrs · 22,387 cycles

LOSS INSTRUMENTS, RTFL. FOUND STATIC LINE LOOSE ON RT AIR DATA COMPUTER. MCDP LAST FLIGHT FAULTS CONFIRMED FAULT. REPLACED RT AIR DATA COMPUTER IAW MM. VERIFIED PITOT AND STATIC LINES SECURED USING 2 MECH IAW MM. ACCOMPLISHED CURRENT 30 FAULTS, GROUND TEST OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,732 hrs · 22,062 cycles

DOOR 3 RT EMERGENCY EXIT LIGHT INOP EXT. RELAMPED, OPS CHECK GOOD.

Part: RELAY — FAILED (CABIN PRESSURE) · airframe 59,020 hrs · 21,784 cycles

ACFT LOST PRESSURIZATION, FLT DIVERTED. REPLACED PRSOV, RT EICAS BLEED CONFIG CARD M10312, RELAYS K10646, K10436, K10204, K10206 & K10281. ALL NO HELP, FINALLY THE REPLACEMENT OF RELAY K10555 FIXED FAULT. SYS CHECKS OK PERFORMED PNEU TEST.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 58,581 hrs · 21,618 cycles

RT HORIZONTAL STAB LOWER SKIN DENTED. DENT ON LOWER SKIN 41.5" OTBD OF FUSELAGE AND 12" AFT OF L/E. DENTS ARE BETWEEN AUX SPAR AND FRONT SPAR. MOST FWD DENT MEASURES 1.5" LONG BY 1.125 IN WIDTH. AFT DENT 1.250 LONG BY 1" WIDE. DENTS HAVE APROX. .250" SEPARATION. ACCOMPLISHED HEFC INSP OF DENT. NO CRACKS FOUND AT THIS TIME. THIS AS 1 DENT, 3 INCHES LONG BY 1 (PARTIAL). IAW INTERIM RPR MADE TO DENTS. ACP 10X MAGNIFICATION VISUAL INSPECTIONS AT EVERY 50 FLT HOURS. PERMANENT REPAIR SHALL BE ACCOMPLISHED WITHIN 100 FLT HRS NOT TO EXCEED PTT 58,681. COMPLETED RE-CHECK. AT THIS TIME FOUND NO FURTHER DAMAGE.

Part: BEARING — DAMAGED (TORQUE TUBE) · airframe 57,833 hrs · 21,326 cycles

R MED NR 4 RT BODY TORQUE TUBE BEARING BROKEN. PART OF BEARING STUCK IN CAM PLATE, PART OF BEARING STUCK ON BODY TORQUE TUBE. (LOWER MOST BEARING) CHECKED MED 4 RT AND FOUND SAFE FOR FERRY FLIGHT. REPLACED BEARING. REINSTALLED BODY TORQUE TUBE. OPS CHECK OK.

Part: BOTTLE — READS LOW (L1 DOOR ASSIST) · airframe 57,758 hrs · 21,294 cycles

DOOR 1L EMERGENCY ASSIST BOTTLE NO PRESSURE. R & R DOOR ASSIST BOTTLE. VERIFIED DOOR 1L SLIDE PACK DISCHARGE SAFETY PIN WAS REMOVED AND STOWED.

Part: O-RING — LEAKING (EVAC SLIDE)

LOW PSI. LEAKING AT FILL VALVE. O-RING REMOVED & REPLACED. REFILLED CYLINDER.

Part: SLIDE — UNSERVICEABLE (CABIN)

LOW BOTTLE PRESSURE. PERFORMED LEAK TEST. COULD NOT FIND A LEAK. DISCHARGED THE BOTTLE AND VALVE WILL BE FULLY DISASSEMBLED AND REWORKED.

Part: BOTTLE — FAULTY (R1 DOOR ASSIST) · airframe 55,517 hrs · 20,398 cycles

FOUND DOOR ASSIST BOTTLE FOR DOOR 1R LOW. REPLACED DOOR 1R ASSIST BOTTLE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,939 hrs · 20,170 cycles

EMERGENCY FLASHLIGHT DOOR 2 RIGHT DOES NOT FLASH TEST. REPLACED BATTERY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,874 hrs · 19,748 cycles

DOOR NR 2 LT AND RT EMERGENCY EXIT LIGHT INOP (EXT). LAMPS INOP. RELAMPED, OPS NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,874 hrs · 19,748 cycles

DOOR 4 RT EMERGENCY EXIT LIGHT INOP (EXT). LAMPS INOP. RELAMPED EMERGENCY LIGHT, SYS IS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,406 hrs · 19,567 cycles

EXTERIOR EMERGENCY LIGHT INOP AT DOOR 3R.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,406 hrs · 19,567 cycles

EXTERIOR EMERGENCY LIGHT INOP AT DOOR 1L. RELAMPED DOOR 1L EMER LIGHT. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,463 hrs · 19,227 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 2L INOP. LAMP INOP. RELAMPED LIGHT AT DOOR 2L.

Part: LIGHT — MISSING (CABIN) · airframe 52,188 hrs · 19,125 cycles

EMERGENCY EXIT LIGHT STRIP MISSING AT 34C. FOUND MISSING STRIP AND RESECURED IT. OPS TESTED OK.

Part: LIGHT — UNSECURE (CABIN) · airframe 49,812 hrs · 18,266 cycles

EMERGENCY LIGHT STRIP AT ROW 13-14 ON FLOOR NOT ATTACHED. RESECURED EMERGENCY EQUIPMENT LIGHT COVER.

Part: STRIP — OUT OF POSITION (CABIN) · airframe 49,301 hrs · 18,078 cycles

EMERGENCY LIGHT STRIP IS OFF THE FLOOR ABOUT TWO INCHES AT 12ABC & 13ABC. [06-22-07] FOUND EEL LIGHT STRIP SLIGHTLY DETACHED (TAPE DEGENERATED) AT ROW 13. REATTACHED. LIGHT STRIP FUNCTION WAS NEVER IMPAIRED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,148 hrs · 18,024 cycles

THE FOLLOWING EMERGENCY LIGHTS ARE INOP: SLIDE LIGHT DOOR 2L, EXTERIOR AFT OF WING RIGHT SIDE, EEL LIGHTS ROWS 23-30, EXIT SIGN ROW 29, AISLE LIGHTS ROWS 19, 21 & 23. AFT HATCH HANDLE LIGHT AT ROW 16. REPLACED BATTERY PACK.

Part: LAMP — INOPERATIVE (EMEGENCY LIGHTS) · airframe 48,182 hrs · 17,674 cycles

EMERGENCY SLIDE LIGHT INOP AT DOORS 1R & 4R. RELAMPED NR 767 LAMP

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 47,824 hrs · 17,532 cycles

DOOR 2L SLIDE ARMED LIGHT WILL NOT ILLUMINATE. REPLACED LAMP.

Part: SMOKE — DETECTED (CABIN) · airframe 45,309 hrs · 16,611 cycles

FOUND SMOKE REPORTED IN CABIN. RECIRCULATING FAN MESSAGE. WIRE BUNDLE W4104 FOR THE RT SIDE CABIN AIR RECIRCULATION FAN SHORTED ON ADJACENT SUPPORT BRACKET. THE SUBJECT WIRE HARNESS WAS REPLACED WITH HARNESS. THE RT SIDE CABIN AIR RECIRCULATION FAN WAS ALSO REPLACED FOR PRECAUTION.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

LT EXTERNAL FUSELAGE RIVET HOLE AT STA 520 AND STR 19L HAS EGG SHAPED HOLE. CUTOUT DAMAGE AND INSTALLED STRUCTURAL FILLER AND DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

FWD PIT FRAME DENTED AT BS 580 STR 23L. INSTALLED J-ANGLE REPAIR.

Part: TEAR STRAP — CORRODED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

BS 1400 STR 27L-28L TEAR STRAP AND SHEAR TIE CORRODED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

MAIN CABIN STA 1681 FRAME SUPPORT ANGLE CORRODED AT STR 17R AT CREASE. SUPPLEMENTAL DATA UPDATE CORRODED SUPPORT ANGLE WAS FABRICATED AND REPLACED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

AFT PIT STA 1400, FWD SHEAR TIE IS CORRODED BETWEEN STR 27L AND 28L. FABRICATED & INSTALLED NEW SHEAR TIE.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · airframe 39,988 hrs · 14,635 cycles

CABIN FLOORBEAM CAP IS CORRODED AT BS 365 FROM RBL 28 TO RBL 42. TYPICAL CORROSION FOUND ON EXISTING STRAP REPAIR. STRAP REPAIR WAS REMOVED, CORROSION CLEANED, AND STRAP REPAIR REPLACED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

AFT PIT FRAME DENTED AT BS 1460 AND STR 26L, ON IB FLANGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

FWD PIT FRAME AT BS 520 AND STR 24L IS DENTED ON IB FLANGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME DOUBLER ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

FWD PIT MAIN FRAME AT BS 540, BETWEEN STR 24L- STR 25L, DENTED ON IB FLANGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED A DOUBLER REPAIR ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

AFT PIT FRAME AT BS 1440 IS DENTED BETWEEN STRINGERS 25L AND 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCING ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

AFT PIT MAIN FRAME AT BS 1420, STR 26L IS DENTED. INSTALLED REINFORCING ANGLE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

MAIN CABIN STA 1641 AND RBL 26 TO CENTER LINE, PREVIOUS FLOORBEAM REPAIR CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED ANGLES, STRAP AND BEAM SECTION.

Part: FRAME — DENTED (STR 25L & 26L) · airframe 39,988 hrs · 14,635 cycles

AFT PIT FRAME STA 1480 IS DENTED BETWEEN STR 25L AND 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR.

Part: BEAM — UNKNOWN (MLG WW) · airframe 39,988 hrs · 14,635 cycles

LT AND RT WHEEL WELL CANTED BEAMS. INSTALLED DOUBLER TO MLG CANTED BEAMS.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

AFT PIT FRAME DENTED STA 1540 AT STR 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

AFT PIT MAIN FRAME STA 1400, STR 25L TO 26L DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

CABIN FLOORBEAM CAP CORRODED BS 310, RBL 44. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED L ANGLE DOUBLER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,988 hrs · 14,635 cycles

AFT PIT STA 1600 BETWEEN STR 28R AND 29R, SHEAR TIE IS CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: IDG — FAILED (APU) · airframe 38,450 hrs · 14,070 cycles

LEFT GENERATOR CONTROL OFF LIGHT AND EICAS MESSAGE CAME ON. THREE ATTEMPTS TO START THE APU WERE UNSUCCESSFUL. REPLACED THE LEFT IDG.ONE PISTON IN THE HYDRAULIC UNIT FAILED CONTAMINATING THE IDG WITH METAL SHAVINGS.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,740 hrs · 13,826 cycles

SKIN DENTED AT STA 732, STRINGER 28R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: VALVE — DEFECTIVE (CROSS FEED) · airframe 37,314 hrs · 13,663 cycles

FUEL IMBALANCE BETWEEN LT AND RT TANKS. THE CAUSE OF THE FUEL IMBALANCE CONDITION WAS DUE TO A DEFECTIVE CROSS-FEED VALVE BODY ASSY. SHOP FINDINGS REVEALED THAT THE SPLINE AND SEAL ON THE VALVE DISK WERE WORN OUT. THIS WAS THE FIRST TIME THE VALVE WAS REMOVED SINCE THE DELIVERY OF A/C IN AUG OF 1992. THIS PARTICULAR FAILURE MODE WILL SET UP A CONDITION WHERE BOTH THE LEFT AND RIGHT MAIN TANK PUMPS ARE FEEDING BOTH LEFT AND RIGHT ENGINES. THE STRONGER MAIN TANK PUMPS FROM EITHER THE LEFT OR RIGHT WILL OVERRIDE THE WEAKER SIDE THEREFORE ALLOWING A FUEL IMBALANCE TO OCCUR DURING THE FLIGHT. IN THIS CASE, THE STRONGER PUMPS WERE FROM THE LEFT AS EVIDENCED BY THE FUEL QUANTITY INDICATION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 36,208 hrs · 13,243 cycles

LEFT AFT OFF-WING EMERGENCY SLIDE LIGHT, AFT OF AFT OVERWING HATCH IS INOPERATIVE. RELAMPED LIGHT.

Part: BOTTLE — DISCHARGED (PAX DOOR) · airframe 36,127 hrs · 13,214 cycles

DOOR 1R ASST BOTTLE FOUND WITH NO PRESSURE. BOTTLE PRESSURE EVACUATED DUE TO RUPTURED BURST DISC ON ASSIST BOTTLE. DOOR ASSIST BOTTLE REPLACED. NO ADDITIONAL DISCREPANCIES NOTED AND NO HISTORY THAT COULD HAVE RESULTED IN EMERGENCY OPERATION OF DOOR.

Part: FAN — FAILED (RECIRCULATION) · airframe 28,486 hrs · 10,431 cycles

'EQUIPMENT OVERHEAT' EICAS MESSAGE FOLLOWED BY ADI BACKGROUND TURNING BLACK. SUPPLEMENTAL DATA UPDATE THE AIRCRAFT EXPERIENCED A LEFT RECIRCULATION FAN FAILURE. AFTER BEING DEFERRED, THE EQUIPMENT COOLING CIRCUIT BREAKERS WERE NOT RESET. THIS CAUSED THE EQUIPMENT TO OVERHEAT DUE TO LACK OF COOLING AIR. THIS WAS A HUMAN ERROR - NO MECHANICAL SYSTEMS WERE DESCREPANT.

Part: ACCESS DOOR — DAMAGED (HORIZONTAL STAB) · airframe 27,403 hrs · 10,048 cycles

TAIL CONE AND AUXILIARY POWER UNIT DOOR ON LEFT SIDE, AFT OF HORIZONTAL STABILIZER, IS DAMAGED. *S/D* MAJOR REPAIR ACCOMPLISHED WHERE THE FOLLOWING PARTS WERE REPLACED: APU DOOR SUPPORT LONGERON (148N8201-1), APU COMPARTMENT FRAME (148N1604-1), APU COMPARTMENT SKIN (148N3730-1).

Part: FUEL CAP — FAILED (LT WING)

DURING FLIGHT, LEFT OVERWING FUEL CAP DEVELOPED A LEAK. AIRCRAFT DIVERTED TO DEN. REPLACED FUEL CAP, OPERATION CHECKS NORMAL.

Part: STRIP — LOOSE (CABIN)

EMERGENCY EXIT LIGHT STRIP DAMAGED AND LOOSE. SECURED THE EMERGENCY EXIT LIGHT STRIP TRACK TO FLOOR USING TAPE AND LEAVING THE EMERGENCY EXIT LIGHT STRIP ELEMENT VISIBLE. NEEDS TO BE CLEANED UNDERNEATH TRACK AND RESECURED.

Part: LIGHT — INOPERATIVE (LT DOOR)

NR 1 LEFT DOOR OUTER EMERGENCY LIGHT INOP. ACCOMPLISHED LIGHT SYSTEM TEST PER MAINTENANCE MANUAL 33-51-00 AND DETERMINED LIGHT OPERATION NORMAL.