N507UA

Part: O-RING — LEAKING (HYDRAULIC SYS) · airframe 73,940 hrs · 27,933 cycles

HYDRAULIC QUANTITY LOW - SYSTEM RT. FOUND HYDRAULIC LEAK AT SPOILER NR 11. FOUND DAMAGED O-RING AT FITTING, REPLACED SAME NAS1612-16, LEAKS AND OPS CHECKS GOOD. HYDRAULIC SYSTEM SERVICED TO FULL.

Part: LIGHT — INOPERATIVE (CABNI) · airframe 73,719 hrs · 27,848 cycles

EEL AT RIGHT OVERWING ESCAPE HATCH, FORWARD HATCH FORWARD MOST BULB INOP. REPLACED FWD MOST EEL AT RIGHT FWD ESCAPE HATCH, OPS CHECKED GOOD. PART NUMBER BULB 1317.

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 73,570 hrs · 27,804 cycles

HIGH PITCH SQUEAL FIRST OFFICER SLIDING WINDOW TOP, ADJUSTED UPPER REAR STOP AND PRESSURIZED AIRCRAFT, NO SQUEAL NOTED.

Part: PROXIMITY SWITCH — OUT OF ADJUST (R1 DOOR) · airframe 73,197 hrs · 27,671 cycles

R1 DOOR EICAS MESSAGE ILLUMINATED. VERIFIED DOOR CLOSED, LATCHED, AND LOCKED. ADJUSTED DOOR PROXIMITY SWITCH, OPS CHECKED GOOD.

Part: FUEL LINE — LEAKING (LT WING) · airframe 72,693 hrs · 27,507 cycles

FUEL LEAKING OUT OF LEFT WING DRY BAY. FOUND LEFT WING DRY BAY RUNNING LEAK WHEN ENGINE MANIFOLD IS PRESSURIZED. NEEDS TANK ENTRY. NEW LINE IN HAND. LINE INSTALLED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 72,676 hrs · 27,502 cycles

PUNGENT ODOR IN COCKPIT DURING CLIMBOUT AND WENT AWAY. RAN LT & RT PACKS ISOLATED WITH APU AS BLEED SOURCE AND HAD NO ODOR PRESENT. RAN RT & LT PACKS WITH NR 1 & 2 ENGINE BLEEDS AND ISOLATED. ALSO RAN EACH PACK WITH JUST ONE ENGINE AS BLEED SOURCE, NO ODOR PRESENT. BOTH ENGINES AT CLIMB SETTING EPR 1.3, PAST BLEED SHIFT. FOUND CAPTAIN'S SIDE DUCT EXIT SCREENS FULL OF LINT.

Part: CARBON SEAL — DEFECTIVE (NR 1 ENGINE) · airframe 72,447 hrs · 27,419 cycles

SOUR AND FOUL SMELL FROM AC SYSTEM SMELLS LIKE DIRTY SOCKS OCCURED AFTER TAKEOFF. A-C SYS OIL CONTAMINATION ISOLATION PER AMM 21-00-01 PB200 REVEALED OIL CONTAMINATION LIKELY FROM NR 1 ENGINE. NR 1 ENGINE HAS OIL POOLING IN NR 3 AFT CARBON SEAL AREA VIEWED THRU AP1. REPLACED NR 1 ENGINE PER TOD 71-00-02.

Part: SKIN — DAMAGED (BS 255 - 288) · airframe 72,399 hrs · 27,400 cycles

LEFT FUSELAGE SKIN CRACKED AND DENTED BS 255 TO 288. ACCOMPLISHED MAJOR REPAIR PER ECRA 5310-05519 REV A.

Part: ANGLE — CRACKED (NR 2 NACELLE) · airframe 72,399 hrs · 27,400 cycles

NR 2 ENGINE PYLON LT SIDE ANGLE CRACKED AT NACELLE STA 156.00 AND STA 161.00. MAJOR REPAIR ACCOMPLISHED: REMOVED AND FABRICATED NEW ANGLE. INSTALLED NEW ANGLE PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 324 RBL 46-55) · corrosion level 2 · airframe 72,399 hrs · 27,400 cycles

MAIN CABIN BS 324 FLOORBEAM UPPER CHORD HAS CORROSION FROM RBL 46 TO RBL 55. MAJOR REPAIR ACCOMPLISHED: PERFORMED REPAIR TO MAIN CABIN STA 324 FLOORBEAM PER ECRA 5310-05518 AND EA PT57-53- 006.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 72,399 hrs · 27,400 cycles

AFT GALLEY FLOORBEAM AT BS 1640 CORRODED AT FASTENER HOLES BETWEEN BL 0 AND RBL 55. SUPPLEMENTAL DATA UPDATE ALL WORKS PERFORMED ON FLOORBEAM AT STA.1640, BL0 - RBL 55 ACCOMPLISHED IAW PEMCO EA PT57-53-008 AND EC-RA 5360-01201.

Part: FLOORBEAM — CORRODED (BS 1661 LBL14-15) · corrosion level 2 · airframe 72,399 hrs · 27,400 cycles

MAIN CABIN STA 1661 FLOORBEAM LBL14 - LBL15 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA, FABRICATED TOP STRAP, FILLER, 2 ANGLES PER SRM 53-00-51. INSTALLED IAW SRM 53-00-01, PG 201, REPAIR 5, FIG 201.

Part: FLOOR PANEL — CORRODED (BS 1720) · corrosion level 2 · airframe 72,399 hrs · 27,400 cycles

AFT GALLEY DECL PLATE CHORD CORRODED AT BS 1720 AT RBL 55. REPAIRED AFT GALLEY DECK PLATE AT STA 1720 RBL 50-55 PER ECRA 5360-01200 AND EA PT57-53-0 09 BY FN 720565 AND IQ Q861 ON NR 4903N00218.

Part: FLOORBEAM — CORRODED (BS 365.25) · corrosion level 2 · airframe 72,399 hrs · 27,400 cycles

RIGHT SIDE CABIN FLOORBEAM CORRODED AT BS 365.25 BETWEEN RBL 24-56. REMOVED AND REPLACED REPAIR SECTION IAW 53-00-51, REPAIR NR 3. MAJOR REPAIR .

Part: UNKNOWN — LEAKING (LT ENGINE) · airframe 71,097 hrs · 26,940 cycles

CREW REPORT: DARK FLUID DRIPPING 1 DROP EVERY 10 SECONDS FROM LEFT ENGINE. SAMC TEXT: REF AMM 71-71-00 (601) FOR ENGINE DRAINS LEAK RATE LIMITS, IDENTIFY LEAKY COMPONENT, NOTIFY OPBLM TOMC-EMC WITH FINDINGS. OPBLM EMC 20DEC11. CREW ACCOMPLISHED LEFT ENGINE IDLE RUN, MAINT ENG RUN BY FLT CREW CHECK LIST COMPLETED WITH CREW, MAINT & NOC DIRECTOR, LCL MAINT REPORTS EVIDENCE OF OIL WETNESS AT DE-OILER BREATHER OUTLET, OIL CONSUMPTION IS NORMAL, WITHIN LIMITS OF AMM79-00-95 PARA 6E & 6F ON PAGE 203-204. NO LEAKS NOTED AT IDLE RUN, LCL MAINT, OPBLM TOMC-EMC 20DEC1 1.

Part: VALVE — FAILED (FUEL SYSTEM) · airframe 70,762 hrs · 26,815 cycles

FUELER REPORTED POSSIBLE UNWANTED FUEL TRANSFER DURING FUELING AT GATE. WITH ALL DEFUELING VALVES CLOSED AND AIRCRAFT MANIFOLD PRESSURIZED FROM GROUND FUELING HYDRANT CENTER TANK TAKES ON APPROX "00.2" POUNDS OF FUEL IN A 5 MIN TIME SPAN. REPLACED LEFT CENTER FILL VALVE CONTROLLER, NO HELP. AFTER TANK ENTRY FOUND LEFT CENTER TANK FILL VALVE STUCK OPEN (TANK SIDE). REPLACED FAULTY CTR LEFT FILL VALVE PER AMM, OP CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,624 hrs · 26,400 cycles

EMERGENCY GROUND ILLUM LIGHT AT DOOR 4L WILL NOT ILLUMINATE. RELAMPED, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,624 hrs · 26,400 cycles

EMERGENCY GROUND ILLUM LIGHT AT 2R WILL NOT ILLUMINATE. SEE PTT 6242015 FOR PARTS NEEDED. NEED SOCKET AND REFLECTOR OR LIGHT ASSY. N-S PN 30-2041-3, (LIGHT ASSY), 31-4964 -5 (SOCKET), 31-5506-1 (REFLECTOR). SECURED AND CLEANED LIGHT ASSY CONTACTS, OPS CHECKED OKAY.

Part: HANDSET — INOPERATIVE (CABIN) · airframe 69,565 hrs · 26,378 cycles

NO CHIME IN COCKPIT WHEN CALLING FROM AFT F/A STATION. REPLACED AFT ATTENDANT HANDSET. SYSTEM OPS OKAY.

Part: MICROPHONE — FAULTY (OXYGEN MASK) · airframe 68,531 hrs · 25,982 cycles

FIRST OFFICER OXYGEN MASK MIC INOP. REPLACED MASK. OPS NORMAL.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 67,798 hrs · 25,706 cycles

EMERGENCY LIGHTING STRIP DISCONNECTED IN THE BACK OF THE CABIN. EMERGENCY LIGHT TRACK SECURED WITH TAPE ON THE END. ALL EMERGENCY LIGHT FUNCTIONS OKAY.

Part: MONITOR — ODOR (NR 6) · airframe 67,542 hrs · 25,597 cycles

FLT ATTENDANT REPORTED SMELLING ELECTRICAL ODOR VICINTY OF OVERHEAD MONITOR BY ROW 19. SECURED POWER TO MONITOR. WHEN VIDEO SYSTEM TURNED OFF ODOR WAS NO LONGER PRESENT. NR 6 MONITOR INOPERATIVE, TURNED MONITOR OFF AND CAP AND STOWED THE CONNECTOR. OPERATED VIDEO SYSTEM WITH NO ODORS NOTED. REPLACED MONITOR. OPERATES NORMALLY.

Part: WARNING MESSAGE — ACTIVATED (RUDDER RATIO) · airframe 66,604 hrs · 25,248 cycles

MECHANICAL ISSUE. RTFL ON T-O ROLL AT 125 KIAS GOT RUDDER RATIO AND MACH-SPEED TRIM EICAS AND LIGHTS. REFLY. CREW REPORTED THAT RUDDER RATIO AND MACH SPEED TRIM EICAS MSG APPEARED ON TAKEOFF AT ROTATION. REPLACED RT AIR DATA COMPUTER IAW MM. AFTER TEST FLIGHT. AIR DATA COMPUTER WAS NOT AT FAULT, MACH SPEED TRIM AND RUDDER RATIO EICAS MESSAGES STILL REAPPEARED. CONTINUING TO TROUBLESHOOT. REINSTALLED ORIGINAL ADC.

Part: PUMP — FAULTED (RT ENGINE) · airframe 66,060 hrs · 25,050 cycles

RT ENG HIGH OIL TEMP, RTFL. REPLACED LUBRICATION AND SCAVENGE OIL PUMP NR 2 ENGINE IAW AMM. REPLACED NR 2 ENG OIL TEMP PROBE IAW AMM. RAN ENG, ALL PARAMETERS NORMAL. EEC NOT REPLACED AFTER TALKING WITH SFOLM AND SFOEP.

Part: LIGHT — NO TEST (CABIN) · airframe 65,719 hrs · 24,924 cycles

EEL LIGHT STRIP AT ROW 27 WILL NOT TEST. REPLACED EEL LIGHT STRIP, OPS CHECK OK.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 65,213 hrs · 24,722 cycles

EMERGENCY FLOOR LIGHTING BUCKLED ROW 9-15. REPAIRED EMERGENCY LIGHT COVER.

Part: GATE — CRACKED (R1 DOOR) · airframe 65,079 hrs · 24,665 cycles

1 RT MED UPPER GATE IS CRACKED OUT OF MOST FWD RIVET HOLE DOWN TO LWR EDGE. REPLACED NR 1 RT UPPER GATE.

Part: FEEDER CABLE — DISCONNECTED (EMERGENCY LIGHT) · airframe 64,863 hrs · 24,579 cycles

EMERGENCY TRACK LIGHTING FROM SEAT ROW 9 TO ROW 14 INOP. FOUND EMERGENCY LIGHT STRIP POWER FEEDER DISCONNECTED. REPLACED DAMAGED LIGHT STRIP CHKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 63,999 hrs · 24,247 cycles

STANDBY INVERTER EICAS MSG AND ELEC SMOKE SMELL THROUGHOUT ENTIRE AIRCRAFT. STATIC INVERTER CHECK TESTED GOOD. CHECKED CABIN FOR SOURCE OF SMELL. SUSPECT SMELL ORIGINATED DURING RAIN STORM. SUSPECT ODOR CAME IN THRU APU PACK SYSTEM. VISUALLY INSPECTED E&E COMPARTMENT AND STBY INVERTER FOR SIGNS OF OVERHEATING. ALL NORMAL CONDITION. NO FURTHER OCCURRENCES.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,273 hrs · 23,977 cycles

DOOR NR 2 RIGHT EMERGENCY EXIT LIGHT INOP (EXT). RELAMPED, OPERATES NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,273 hrs · 23,977 cycles

DOOR NR 4 LT EMERGENCY EXIT LIGHT INOP (EXT). RELAMPED, OPERATES NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,350 hrs · 23,618 cycles

EXTERNAL FUSE DOOR 2 LT AND 4 RT EMERGENCY EXIT LIGHTS INOP. REPLACED LAMPS, OPS GOOD P/N 767.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 61,074 hrs · 23,105 cycles

FWD NOSE COMPARTMENT DOOR FWD CUTOUT FRAME IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. ADJUSTMENT CHECKED FWD LATCH FITTING. SENSOR ADJUSTED & OP CHECKED DOOR SENSOR SYSTEM.

Part: EXTINGUISHER — DEFECTIVE (AFT CARGO BAY) · airframe 61,074 hrs · 23,105 cycles

AFT PIT ENG FIRE BOTTLE NR 1 PRESSURE SWITCH IS BAD. NR 1 ENGINE FIRE EXTINGUISHER REPLACED. OP CHECK ACCOMPLISHED.

Part: OXYGEN MASK — NO TEST (CAPTAIN'S) · airframe 60,975 hrs · 23,071 cycles

CAPTAIN'S O2 MASK DOES NOT TEST OK. REPLACED O2 MASK STOWAGE BOX. TESTS OKAY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,994 hrs · 22,713 cycles

DOOR 4L EXT EMERGENCY LIGHT INOP. BULB INOP. RELAMPED DOOR 4L EXT EMERGENCY LIGHT, OPS CHECK OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,994 hrs · 22,713 cycles

DOOR 2R EXT EMERGENCY LIGHT INOP. BULB INOP. RELAMPED DOOR 2R EXT EMERGENCY LIGHT, OPS CHECK OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,994 hrs · 22,713 cycles

DOOR 4R EXT EMERGENCY LIGHT INOP. BULB INOP. RELAMPED DOOR 4R EXT EMERGENCY LIGHT, OPS CHECK OK.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 59,752 hrs · 22,625 cycles

EEL LIGHT AT ROW 13ABC IS DISCONNECTED AND CLEAR COVER IS MISSING FOR A 10 INCH SECTION. RECONNECTED WIRE AND REPLACED MISSING OR IMPROPER LENGTH COVERS. SYSTEM TEST OK.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 59,511 hrs · 22,523 cycles

EEL LIGHTS INOP AT ROW 16 THRU 20. FOUND INVERTER FAULTY, BLOWN FUSE. REPLACED EEL LIGHT INVERTER M10830, BLOWN FUSE IN M10770 EMER LIGHT PWR SUPPLY AND LAMP IN BULLNOSE AT SEAT 14ABC. EEL LIGHTS AT ROW 16-20 AND AISLE LIGHT AT 14ABC. CHECKS OK

Part: O-RING — LEAKING (SLIDE BOTTLE)

LOW BOTTLE. FOUND CENTER SHAFT O-RING LEAKING. REPLACED O-RING, SERVICED O2 SYSTEM, NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,084 hrs · 22,008 cycles

EXTERIOR EMERGENCY LIGHTS AT DOOR 2R, 4L, 4R AND AFT CARGO DOOR INOP WHEN EMERG LT TEST SW ON NOSE GEAR PUT IN MOM POSITION. RELAMPED.

Part: LIGHT — INOPERATIVE (ROW 17-22) · airframe 57,960 hrs · 21,960 cycles

EEL LIGHTS AT 1ST CLASS CLOSET AND ROWS 17 - 22 ARE INOP. REPLACED LIGHT. CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,467 hrs · 21,785 cycles

CREW REPORTED EMERGENCY LIGHT ABOVE SEATS 22 ABC IS OUT.

Part: WINDOW — OPEN (COCKPIT) · airframe 57,194 hrs · 21,689 cycles

ON TAKEOFF, FIRST OFFICERS WINDOW OPENED IN FLIGHT. ACCOMPLISHED COMPLETE INSPECTION OF FIRST OFFICER WINDOW RIGGING. ADJUSTED WINDOW MECHANICAL LATCH AND LOCK. LUBED ROLLER AND TRACK.

Part: HYDRAULIC LINE — BROKEN (LT AILERON) · airframe 56,849 hrs · 21,562 cycles

AILERON MOVEMENT ON EICAS DOESN'T MATCH MOVEMENTS FROM CONTROL WHEEL. TURNING WHEEL TO LEFT GETS STIFF FROM 3 TO 6 DEG. ON INSPECTION FOUND NUT -LOOSE HARDWARE- IN RT LATERAL CONTROL OVERRIDE QUADRANT. PART REMOVED. NO DAMAGE NOTED TO CABLE OR QUADRANT. ADJUSTED TRIM ACTUATOR, LT AILERON O/B PCU HYDRAULIC PRESSURE LINE BROKEN NEAR PCU ATTACH. INSTALLED AILERON POWER CONTROL TUBE ASSY LINE.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 56,517 hrs · 21,438 cycles

DOOR 2R SLIDE PRESSURE OUT OF LIMITS. [06-14-07] THERE WAS A SMALL LEAK AT THE SHAFT O-RING. REPLACED NR 2 RT SLIDE.

Part: DISK — RUPTURED (SLIDE BOTTLE) · airframe 55,641 hrs · 21,118 cycles

LOW BOTTLE PRESSURE. *S/D* RUPTURE DISK FAILURE. CAUSE UNKNOWN. REPLACED RUPTURE DISK.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 55,641 hrs · 21,118 cycles

FOUND ROW 13 OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND OPS CHECK GOOD.

Part: FRAME — DENTED (BS 1400 S26L) · airframe 55,641 hrs · 21,118 cycles

FOUND AFT PIT STA 1400 AT STR 26L, FRAME UPPER FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A NESTED J-ANGE L REPAIR THIS REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 13FEB07. THIS REPAIR BECOMES UNAIRWORTHY UNLESS A NEW FAA 8100-9 IS ISSUED PRIOR TO THAT TIME.

Part: FRAME — CORRODED (BS 1681) · airframe 55,641 hrs · 21,118 cycles

FOUND CABIN FRAME INBOARD CHORD CORRODED AT BS 1681.8 AND RBL 57. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR DOUBLER, FILLER AND STRAP. THIS REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 16FEB07.

Part: SKIN — DAMAGED (BS 646 S0-1R) · airframe 55,641 hrs · 21,118 cycles

FOUND UPPER CROWN, BS 646 BETWEEN STR 0 AND 1R HAS STATIC DISCHARGE AROUND FASTENER AND BLEND OUT EXCEEDS LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A REPAIR DOUBLER. THIS REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 18FEB07.

Part: FRAME — DENTED (BS 1440 S25L) · airframe 55,641 hrs · 21,118 cycles

FOUND AFT PIT STA 1440 BELOW STR 25L, FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME WITH A PRODUCTION SPLICE REPAIR ANGLE. THIS REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 13FEB07.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,641 hrs · 21,118 cycles

FOUND EEL FLOOR LIGHTS INOP AT ROWS 22-16 AND ROW 13 FWD. REMOVED AND REPLACED BATTERY PACK AND CHARGER.

Part: SKIN — CHAFED (LT TE FLAP) · airframe 55,641 hrs · 21,118 cycles

FOUND LT WING INBOARD FLAP UPPER SKIN, OUTBD UPPER CORNER IS CHAFED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A SINGLE REPAIR DOUBLER AND BONDED DOUBLER. PERFORMED RIG CHECK FLAP TO SPOILER NR 6 CLEARANCE.

Part: DOOR — UNRELIABLE (LAV OXYGEN MASK) · airframe 55,641 hrs · 21,118 cycles

FOUND S-LAV OXYGEN MASK DOOR DID NOT OPEN WHEN MASKS WERE DEPLOYED. REPACKED S-LAV O2 MASK. ACCOMPLISHED DROP CHECK TO ASSURE PROPER FUNCTIONALITY.

Part: LIGHT — INOPERATIVE (ROW 31DEF) · airframe 55,641 hrs · 21,118 cycles

FOUND ROW 31 DEF BULLNOSE EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT AND OPS CHECK GOOD.

Part: SKIN — DAMAGED (BS 500 S0-1R) · airframe 55,641 hrs · 21,118 cycles

FOUND UPPER CROWN AT STA 560, APPROX BETWEEN STR 0 AND 1R, SKIN HAS STATIC DISCHARGE AT FASTENER AND BLENDED OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A REPAIR DOUBLER. THIS REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 18FEB07.

Part: FRAME — DENTED (BS 1420 S26L) · airframe 55,641 hrs · 21,118 cycles

FOUND AFT PIT STA 1420 AND STR 26L, FRAME UPPER FLANGE IS DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A NEW PRODUCTION SPLICE ANGLE REPAIR. THIS REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 13FEB07.

Part: SKIN — DAMAGED (RT TE FLAP) · airframe 55,641 hrs · 21,118 cycles

FOUND RT WING TRAILING EDGE INBD FLAP, UPPER SURFACE EVEN WITH AFT FLAP, OUTBD END FOUND CHAFED AND GOUGED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP AND BOND INSTALLED DOUBLER. PERFORMED FLAP TO SPOILER CLEARANCE RIG CHECK.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 55,641 hrs · 21,118 cycles

BS 1120 LEFT SIDE, INBOARD OF CREASE BEAM, WEB IS CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND MACHINED 1 EA FITTING AND REINSTALLED WEB FITTING.

Part: DOOR FRAME — UNKNOWN (R2 DOOR) · airframe 55,641 hrs · 21,118 cycles

R-2 DOOR FWD FRAME HINGE POINT REQUIRES PREVENTATIVE FRAME REPAIR. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: GATE — CRACKED (R2 DOOR) · airframe 55,641 hrs · 21,118 cycles

DOOR 2R UPPER GATE, INBOARD GATE FRAME CRACKED. WELD REPAIR ACCOMPLISHED FOR 2 EA CRACKS ON DOOR GATE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,641 hrs · 21,118 cycles

MAIN CABIN FLOORBEAM UPPER TEE CAP CORRODED STA 324.0 AND RBL 50 WL 208. MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM TEE CAP FROM LBL 50 TO LBL 55. INSTALLED TEE CAP SPLICE AND STRAP REPAIR.

Part: GATE — CORRODED (L1 DOOR) · airframe 55,641 hrs · 21,118 cycles

DOOR L1 LOWER GATE HAS CORROSION. FOUND AFTER RUB STRIP REMOVED. CONFIRMED CORROSION. NEEDED TO REPLACE LOWER GATE ON DOOR FRAME.

Part: GATE — CRACKED (R1 DOOR) · airframe 55,641 hrs · 21,118 cycles

DOOR 1R LWR GATE BOTTOM MID PORTION GATE FRAME CRACKED, FOUND AFTER REMOVING DOOR PRESSURE SEAL. REPLACED GATE ON DOOR FRAME.

Part: LIFTER — WORN (GIRT BAR) · airframe 55,641 hrs · 21,118 cycles

FOUND DOOR 4L AND 4R FWD GIRT BAR LIFTERS HAVE WORN AREAS. WEAR OUT OF LIMITS, REPLACED LIFTER.

Part: LIFTER — WORN (GIRT BAR) · airframe 55,641 hrs · 21,118 cycles

FOUND DOOR 4R AND 4L AFT GIRT BAR LIFTERS HAVE WORN AREAS.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 55,641 hrs · 21,118 cycles

MAIN CABIN FLOOR SEAT TRACK ATTACH PLATE CORRODED AT FLOORBEAM UPPER CHORD, BS 365, RBL 28, WL 208.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,641 hrs · 21,118 cycles

FUSELAGE SKIN AT STA 1700, STR 17L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN REPAIR AT STA 1700, S17L APPLIED WITH BLIND FASTENER. REPLACED DOUBLER & ADDED EXTRA ROW OF FASTENERS ON BOTTOM END. ALL FASTENERS INSTALLED ARE SOLID. HFEC PER NDT, NO CRACKS NOTED.

Part: LENS — LOOSE (CABIN) · airframe 55,630 hrs · 21,114 cycles

THE -EMERGENCY EXIT- LIGHT PANEL AT 15 ABC IS LOOSE FROM SIDEWALL. LIGHT IS SECURE. LENS IS LOOSE ON ONE END, SECURE ON OTHER END. MADE INTERIM REPAIR OF EXIT SIGN OVERWING LENS WITH TAPE. VERIFIED LENSE SECURE EVEN WITHOUT TAPE. REPAIR IS TO KEEP LENS FROM BEING SNAGGED ACCIDENTLY BY PASSENGER.

Part: LANDING GEAR — INOPERATIVE · airframe 55,614 hrs · 21,107 cycles

RTFL DUE TO INABILITY TO RETRACT LANDING GEAR. ON TAKEOFF GEAR HANDLE WOULD NOT COME UP PAST OFF & GEAR WOULD NOT RETRACT. REPLACED LEFT AND RIGHT GEAR TRUCK TILTED SENSORS. ALSO REPLACED PSEU.

Part: DUCT — CONTAMINATED (APU) · airframe 55,335 hrs · 20,992 cycles

RETURNED TO THE FIELD DUE TO SMOKE IN THE CABIN. AFTER RETURN TO GATE FOR SMOKE IN CABIN BEGAN CLEANING APU BLEED COMPONENTS AND DUCTS. FOUND AND CLEANED OIL IN DUCTS AS FAR AS APU FIRE BOTTLE ACCESS DOOR. NEED TO CHECK DUCTS THRU AFT BODY ACCESS DOOR FOR ANY ADDITIONAL OIL. OIL IS PUDDLING IN LOWER SECTIONS OF DUCTS AND IN FLANGES. ALL DUCTS CHECKED AND CLEANED.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 53,011 hrs · 20,114 cycles

LEFT AFT FUSELAGE HAS PUNCTURE IN UNPRESSURIZED SKIN JUST BELOW SKIN LAP AND JUST FWD OF STAB COMPT ACCESS DOOR. DAMAGE WAS CUT OUT AND DOUBLER INSTALLED PER EVA 60177. A 8100-9 RECEIVED FROM BOEING. DTA INFORMATION TO FOLLOW FROM BOEING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,056 hrs · 19,777 cycles

EXT EMERGENCY LIGHT AT DOOR 4L INOP.

Part: ACTUATOR — FAILED (NR 6 SLAT) · airframe 50,981 hrs · 19,356 cycles

LEADING EDGE SLAT DISAGREE MESSAGE. LEADING EDGE SLAT DISAGREE MSG PER CREW. FOUND NR 6 SLAT ACTUATORS NR 11 AND 12 OVERLOAD INDICATORS POPPED. REPLACED BOTH NR 11 AND 12 SLAT ACTUATORS.

Part: ACTUATOR — FAILED (NR 6 SLAT) · airframe 50,981 hrs · 19,356 cycles

DIVERTED TO EWR WITH A SLAT DISAGREE PROBLEM. FOUND NR 6 SLAT ACTUATORS NR 11 AND 12 OVERLOAD INDICATORS POPPED. REPLACED BOTH NR 11 AND 12 SLAT ACTUATORS.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 50,856 hrs · 19,317 cycles

DIVERTED TO SFO DUE TO FLAP RETRACTION PROBLEM.

Part: WARNING SYSTEM — ACTIVATED (SLATS) · airframe 50,850 hrs · 19,315 cycles

RETURNED TO FIELD DUE TO LE SLAT DISAGREE EICAS MESSAGE. FOUND FSCU HAD INTERMITTE FAULT ON SLAT PDU XMIT. CLEANED CONNECTOR. ACP SYSTEM CYCLE OPS NORMAL.

Part: LIGHT — INOPERATIVE (EMERGENCY SLIDE) · airframe 49,226 hrs · 18,691 cycles

EMERGENCY SLIDE LIGHT ON EXTERIOR OF AIRCRAFT AFT OF LT WING INOP. RELAMPED PER AMM 33-51-06-201

Part: LIGHT — INOPERATIVE (LAV DOOR AREA) · airframe 46,436 hrs · 17,658 cycles

EEL IS INOPERATIVE AT AFT FWD LAV DOOR OPENING. REPLACED EEL STRIP, OPS NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,194 hrs · 16,490 cycles

TWO SMALL DENTS FWD OF DR2L. DENTS ARE APPROX 3 X .062 INCH D. SMOOTH, CRACK FREE AND NO PULLED FASTENERS. LOCATED APPROX 3 INCHES ABOVE WATERLINE BETWEEN STA 600 AND 620. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.

Part: IDG — FAILED (RT GENERATOR) · airframe 42,561 hrs · 16,261 cycles

RT GENERATOR FAILED. RT AC INTEGRATED DRIVE GENERATOR (IDG) FAILURE. REPLACED THE RT IDG AND REPLACED IDG CONNECTOR D5134. THE IDG PASSED ALL PRELIMINARY TESTS. NO FAULTS FOUND.

Part: TURBINE BLADES — CRACKED (NR 1 ENGINE) · airframe 38,679 hrs · 14,789 cycles

NUMBER 1 ENGINE LPT 3 BLADE IS CRACKING WITH SULFIDATION. REPLACED ENGINE.

Part: HYDRAULIC SYSTEM — LEAKING (LEFT) · airframe 38,129 hrs · 14,601 cycles

LEFT HYDRAULIC QUANTITY WENT TO ZERO.

Part: FRAME — WORN (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

STA 1640 STR 5L FRAME FLANGE WORN. MAJOR REPAIR ACCOMPLISHED.REPAIRED FRAME FLANGE PER AMM.

Part: ACTUATOR — CORRODED (HORIZ STAB) · airframe 37,293 hrs · 14,298 cycles

HORIZONTAL STABILIZER TRIM ACTUATOR PRIMARY BRAKE FAILURE INSIDE UNIT. FOUND EXTREME CORROSION INSIDE AND OUTSIDE OF UNIT. BREAKDOWN OF GREASE DUE TO EXCESSIVE WATER INSIDE UNIT. REPLACED ACTUATOR.

Part: PLATE — DAMAGED (FUSELAGE) · airframe 37,293 hrs

LOWER SURFACE OF DECK PLATE HAS TOOLING DAMAGE STA 1704 TO 1707 LBL 62. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. AFT DECK PLATE WAS BLENDED TO REMOVE TOOLING DAMAGE PER FORM 8110-3 .

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

MAJOR REPAIR. DAMAGE TO FUSELAGE SKIN AND STRINGER AT CREASE BEAM STA 600 - 630 ON LEFT SIDE AT FLOOR LINE. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FUSELAGE SKIN AND STRINGER PER SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

FUSELAGE REPAIR DOUBLER AT STA 1300 STR 24L DOES NOT MEET MINIMUM FASTENER SPACING. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED SKIN PER SRM.

Part: STRINGER — TOOL DAMAGE (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

MAJOR REPAIR. STR 24L STA 1296 - 1304 HAS TOOLING DAMAGE. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER PER SRM.

Part: BULKHEAD — CRACKED (NR 1 PYLON) · airframe 37,293 hrs · 14,298 cycles

MAJOR REPAIR. NR 1 PYLON INNER WEB CASTING AT NAC STA 191.86 IS CRACKED AND DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED BULKHEAD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

MAJOR REPAIR. FWD GALLEY FLOOR SUPPORT CHANNEL STA 310 - 324, RBL 39-41 IS CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT CHANNEL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

MAJOR REPAIR. FWD GALLEY TIE DOWN SUPPORT BEAM STA 324 TO 345 RBL 2 HAS EXCESSIVE MATERIAL LOSS, MEASURES .018 LOSS ON .110 ORIGINAL THICKNESS. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

FWD PIT FRAME IS CRACKED AT STA 540 BETWEEN STR 24L AND 25L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

AFT CABIN CENTER LINE INTERCOSTAL CRACKED BETWEEN STA 1580 TO 1600. *S/D* MAJOR REPAIR ACCOMPLISHED. L-ANGLE REPLACED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

MAJOR REPAIR. FWD GALLEY FLOOR CHANNEL CORRODED STA 331 - 333 RBL 5-21. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

FWD CABIN FLOOR SUPPORT CHANNEL CORRODED FROM UNDER DOOR DRAIN PAN STA 324-344 RBL 58-60. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

CABIN FLOOR INTERCOSTAL REQUIRES REPLACEMENT STA 365 TO 377, RBL 57. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

MAJOR REPAIR. GALLEY FLOOR SUPPORT CORRODED WITH EXCESSIVE MATERIAL REMOVED STA 331 TO 333, RBL 25 TO 37. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED FLOOR SUPPORT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

RIGHT CREASE BEAM INNER CHORD STA 324 AT RBL 61 HAS EXESSIVE MATERIAL REMOVED, (25 PERCENT) .018 FRAME, .071 CHORD ANGLE. REF SRM 51-40-02. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED ANGLE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

MAJOR REPAIR. CABIN INTERCOSTAL CORROSION BS 1638 TO 1640 RBL 13. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED INTERCOSTAL PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

MAJOR REPAIR. CABIN FLOORBEAM T-CAP CORROSION BS 1640 FROM LBL 9 TO RT SIDE CREASE BEAM. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM T-CAP.

Part: PLATE — CORRODED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

AFT DECK PLATE STA. 1681 BLENDED EXCESSIVELY RBL 39, 40, 46.5-47.5, 50-52. CORROSION STILL EXISTS AROUND REVET HOLES AT RBL 47. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED DECK PLATE.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

FWD PIT FRAME FLANGE IS DENTED STA 600 BETWEEN STR 23L ABD 24L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,293 hrs · 14,298 cycles

STA 1200 - 1220 BL 0 INTERCOSTAL CRACKED SEVERAL PLACES. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED UPPER ANGLE TO INTERCOSTAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,748 hrs · 12,997 cycles

THE LT SIDE OF THE FUSELAGE AT STA 263, WL 216 WAS DAMAGED FROM CONTACT WITH A JETWAY. THE DAMAGE INVOLVED AN AREA OF SKIN 18 INCHES LONG BY 5 INCHES WIDE AND INCLUDED STA 263 O/B CHORD. THE DAMAGED FRAME CHORD WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM GUIDELINES. THE SKIN WAS REPAIRED PER SRM GUIDELINES AS WELL. THIS WAS A MAJOR REPAIR. REF MAJOR REPAIR NUMBER 108, FILE NUMBER C50-53-10.

Part: ACTUATOR — FAILED (LE SLAT)

LEADING EDGE SLAT DISAGREE MESSAGE AND LIGHT DURING CLIMB. RESET FLAP/SLAT ELECTRONIC UNIT (FSEU) BUT FAILURE OCCURRED AGAIN WHEN FLAPS MOVED. AIRCRAFT RETURNED TO FIELD. LEADING EDGE SLAT ROTARY ACTUATOR FAILED CAUSING THE EICAS MESSAGE. REPLACED ROTARY ACTUATOR AND RETURNED AIRCRAFT TO SERVICE.