N580UA

Part: COVER — MISSING (CABIN) · airframe 67,764 hrs · 23,711 cycles

EMERGENCY EXIT FLOOR STRIP LIGHTING MISSING PLASTIC COVER LAST 4 FT IN AFT CABIN. REPLACED END COVER IAW IP C33-52-00.

Part: COVER — MISSING (CABIN) · airframe 67,755 hrs · 23,708 cycles

EMERGENCY EXIT LIGHT STRIP AT DOOR 4L LOOSE & PLASTIC COVER MISSING. RE-INSTALL LIGHT STRIP & RE-INSTALL PLASTIC COVER, OPERATIONS CHECKED GOOD.

Part: COVER — LOOSE (CABIN) · airframe 66,840 hrs · 23,408 cycles

PLASTIC COVER PROTECTING EMERGENCY ESCAPE LIGHTS LAST ROW OF COACH LOOSE. SECURED STRIP.

Part: COVER — MISSING (CABIN) · airframe 66,830 hrs · 23,404 cycles

EXIT FLOOR LIGHTING AT MOST AFT POSITION IS MISSING PLASTIC COVER. REPLACED DAMAGED COVER.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 66,830 hrs · 23,404 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROWS 8-12, EXCEEDS 80 INCHES. SECURED CONNECTOR AT ROW 12, ACCOMPLISHED INSPECTION IAW GMM 9-10-05.

Part: COVER — BROKEN (CABIN) · airframe 66,734 hrs · 23,368 cycles

EMERGENCY LIGHT STRIP AT 40C BROKEN. REPLACED EMERGENCY FLOOR LIGHTING COVER, OPERATIONS CHECKED OKAY.

Part: LIGHT — LOOSE (EMERGENCY LIGHT) · airframe 66,690 hrs · 23,354 cycles

EMERGENCY LIGHT LOOSE IN AFT CABIN.

Part: GIRT BAR — CLOGGED (R1 DOOR) · airframe 66,639 hrs · 23,339 cycles

1R WILL NOT ARM. CLEANED DEBRIS FROM GIRT BAR AREA. PERFORMED CK TO DOOR FUNCTIONS IAW MM 52-11 -00. CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (R3 DOOR SLIDE) · airframe 66,221 hrs · 23,215 cycles

R3 DOOR SLIDE LIGHT INOPERATIVE WITH DOOR ARMED. REPLACED R3 DOOR GIRT BAR PROXIMITY SENSOR IAW WDM 25-66-11. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,209 hrs · 23,211 cycles

RIGHT OVERWING AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, CHECKED GOOD.

Part: CAP — MISSING (CABIN) · airframe 66,159 hrs · 23,198 cycles

EEL TRACK END CAP MISSING. REPLACE END CAP.

Part: CONTROL UNIT — MALFUNCTIONED (COCKPIT) · airframe 66,133 hrs · 23,189 cycles

CAPTAIN'S O2 MASK DOES NOT TRANSMIT OVER SPEAKER. SWAPPED CAPT AND F/O AUDIO CONTROL PANELS AND REPLACED AUDIO ASSY UNIT M108, ASSOCIATED CAPT AUDIO CHECKS OK. AUDIO CONTROL PANEL SWAP COVERED BY DF0750. ABOVE REF TO "F/O" IS SWAPPED WITH FIRST OBSERVERS POS.

Part: GIRT BAR — DIRTY (R4 DOOR) · airframe 66,076 hrs · 23,169 cycles

R4 DOOR WILL NOT ARM PROPERLY. INSPECTED R4 DOOR ARMING MECHANISM, FOUND DEBRIS IN GIRT BAR HOLDER IN FLOOR BLOCKING ENGAGEMENT, CLEANED DEBRIS, R4 DOOR NOW ARMS AND DISARMS NORMALLY.

Part: PANEL — CHAFED (TE FLAP) · airframe 65,936 hrs · 23,134 cycles

LEFT INBD MAIN FLAP UPPER PANEL CHAFED AFT OF FWD SPAR. REPAIR ACCOMPLISHED IAW REO-G16264, REV B AND ECRA 5750-04553. THIS IS A PERMANENT REPAIR WITH NO FURTHER REINSPECTIONS REQUIRED.

Part: WIRE — DAMAGED (LT WING TE FLAP) · airframe 65,936 hrs · 23,134 cycles

NR 1 FLAP SLAT SENSOR CIRCUIT BREAKER WILL NOT RESET. ACCOMPLISHED SLICE REPAIR ON WIRES W3326-2510, R20 AND W3326-2510 B20 IAW WDM 27-51-41. IAW BSWPM 20-30-19, SPLICE NEW WIRES FROM FSS 720 TO FSS 812 AND TERMINATED AT CONNECTOR D2984, REF BSWPM 20-10-11. NR 1 FLAP SLAT ELECT UNIT OPS CHECKS GOOD IAW AMM. THIS ITEM CAN BE CLEARED WHEN NEW WIRES INSTALLED.

Part: ATTACH FITTING — CRACKED (GIRT BAR) · airframe 65,936 hrs · 23,134 cycles

DOOR 1R GIRT BAR FWD SIDE LEAF SPRING ATTACH FITTING IS CRACKED. INSTALLED SERVICEABLE GIRT BAR IAW AMM, OPS CHECKS NORMAL. NR 40828 .

Part: SKIN — DENTED (BS 412 S23R) · airframe 65,936 hrs · 23,134 cycles

FUSELAGE DENTED AT BS 412, S23R. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01, FIG 201, DETAIL I. MAJOR REPAIR.

Part: CONTACT — DIRTY (R1 DOOR) · airframe 65,666 hrs · 23,053 cycles

FLICKERING SLIDE LIGHT ABOVE 1R. CLEANED AND RE-SECURED CONTACT ON LIGHT MODULE, OP'S CHECK GOOD IAW 25-66-00.

Part: INDICATOR — LACK OF LUBE (L2 DOOR) · airframe 65,661 hrs · 23,050 cycles

2L DOOR NOT ARMING PROPERLY. CLEANED AND LUBED THE SLIDE ARM POP OUT INDICATOR, CHECKS GOOD.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 65,648 hrs · 23,045 cycles

NR 18 FAN BLADE REPORTED AS HAVING DAMAGE AT BLADE TIP. REF BLADE IS ON NR 2 ENGINE. DAMAGE MEASURES .156 X .5 IN. IN AREA 1 OF BLADE TIP. OK TO CONTINUE FOR 25 FLT HOURS. BLENDED BLADE 18 ON ENGINE NR 2.

Part: SEAT — LOOSE (CABIN) · airframe 65,636 hrs · 23,042 cycles

SEAT ASSY 36ABC LOOSE. SECURED SEAT 36ABC.

Part: D-RING — OUT OF ADJUST (R1 DOOR) · airframe 65,598 hrs · 23,029 cycles

D-RING NOT VISIBLE AT 1R. ADJUSTED D-RING TO MAKE VISIBLE.

Part: LIGHT — FAULTY (ROWS 37-40) · airframe 65,353 hrs · 22,947 cycles

CABIN FLOOR EMERGENCY LIGHTS ROW 37 THRU 40 COME ON BUT ARE VERY DIM. REPLACED EMERGENCY LIGHTS FROM ROW 37 THRU 40. OPS CHECKED GOOD. REF MM 33-51-00 MM 33-51-07.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,934 hrs · 22,810 cycles

EMERGENCY LIGHT INOPERATIVE AT R4 DOOR. REPLACED EMERGENCY LIGHT POWER SUPPLY M10817 REF AMM, TESTED OKAY.

Part: ROLLER — MISSING (L1 DOOR) · airframe 64,700 hrs · 22,735 cycles

DOOR 1 LEFT ENTRY DOOR UPPER AFT RIGHT ROLLER MISSING. INSTALLED NEW ROLLER DOOR 1L UPPER AFT POS.

Part: LIGHT — FAULTY (CABIN) · airframe 64,258 hrs · 22,584 cycles

CREW REPORT ELECTRICAL SMELL IN CABIN. AFTER TURNING OFF CABIN AND GALLEY LIGHTS, SMELL DISSIPATED. REPLACED CEILING LIGHT IN ROW 35ABC. TURN ON ALL LIGHTS IN CABIN AND IN AFT GALLEY. NO SMELL NOTED. ALL LIGHTS IN CABIN ARE WORKING NORMAL. INBD CREW COMPLETED QUESTIONNAIRE.

Part: MONITOR — DEFECTIVE (VIBRATION DETECT) · airframe 64,232 hrs · 22,575 cycles

BOTH VIBRATION INDICATORS BLANK ALL OTHER ENGINE INDICATIONS NORMAL. REPLACED ENGINE VIBRATION MONITOR UNIT, TESTED OKAY.

Part: LIGHT — DAMAGED (CABIN) · airframe 63,632 hrs · 22,348 cycles

LAST 3 FT OF EMERGENCY LIGHTS NOT ILLUMINATING. REPLACED DAMAGED LIGHT AND DAMAGED POWER CABLE FROM ROW 37 AFT.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 63,400 hrs · 22,271 cycles

EMERGENCY LIGHT CONNECTOR FOR MID LAV EXIT LIGHTING IS BROKEN. EMERGENCY LIGHT DOES NOT ILLUMANATE AT LAV DOOR THRESHOLD. REPAIRED EMERGENCY LIGHT CONNECTOR AND SECURED. LIGHT TESTED OKAY.

Part: GIRT BAR — UNSECURE (R4 DOOR) · airframe 63,402 hrs · 22,272 cycles

DOOR 4R WILL NOT ARM. SECURED GIRT BAR, OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 63,400 hrs · 22,271 cycles

ONE LIGHT SEGMENT FWD OF FWD AFT LAVATORY INOPERATIVE (AROUND ROW 40). SECURED CONNECTOR, OP CHECKED GOOD.

Part: COVER — BROKEN (CABIN) · airframe 63,185 hrs · 22,200 cycles

FLOOR LEVEL EMERGENCY LIGHT STRIP BROKEN LEFT SIDE AFT OF REAR MOST SEATS. EEL COVER BROKEN. REPLACED COVER.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 63,185 hrs · 22,200 cycles

EMERGENCY LIGHT COVER BROKEN, REPLACED COVER.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 62,707 hrs · 22,049 cycles

AFTER GEAR EXTESION LT HYD QTY EICAS AND FLUID QUANTITY DECREASED TOWARD ZERO. REPAIRED AND REPLACED HYD PRESSURE RETRACT ACTUATOR LINE, REF AMM 32-32-01.

Part: ATTACH FITTING — BROKEN (LT MLG ACTUATOR) · airframe 62,707 hrs · 22,049 cycles

LEFT MAIN GEAR RETRACT ACTUATOR FITTING BROKEN. REPLACED FITTING IAW MM 32-32-01, FIG 401.

Part: OXYGEN MASK — OUT OF POSITION (COCKPIT) · airframe 60,538 hrs · 21,267 cycles

CAPTAINS SPEAKER AND O2 MASK ARE MOUNTED IN WRONG POSITION AND DO NOT AGREE WITH FLIGHT MANUAL. REPAIRED AND REINSTALLED COMPONENTS PER AMM.

Part: RESERVOIR — LOW PRESSURE (L1 DOOR) · airframe 60,519 hrs · 21,260 cycles

CREW REPORT: DOOR 1L POWER ASSIST BOTTLE PRESS LOW. PRESSURE GAUGE NEEDLE IS TO THE RIGHT OF THE GREEN BAND NO MORE THAN ONE NEEDLE WIDTH. OK FOR 25 HOUR UNTIL REPLACED. REPLACED POWER RESERVOIR. ACP SAFETY AND SECURITY PER MM, NO DEFECTS FOUND.

Part: FITTING — DIRTY (GIRT BAR) · airframe 60,460 hrs · 21,236 cycles

DOOR 4L IS HARD TO DISARM. CLEANED FLOOR SILL. CLEANED AND LUBED GIRT BAR FITTINGS AND SLIDERS. CHECKED SLIDER CLEARANCE - OK. OP CHECKED ARM-DISARM MECHANISM SEVERAL CYCLES - OPERATION EFFORT WITHIN NORMAL RANGE.

Part: MECHANISM — OUT OF ADJUST (GIRT BAR) · airframe 60,464 hrs · 21,238 cycles

AFT LEFT ENTRY DOOR WILL NOT DISARM PROPERLY. ADJUSTED GIRT BAR MECHANISM. ARMED AND DISARMED DOOR SEVERAL TIMES. GIRT BAR ENGAGES AND DISENGAGES PROPERLY.

Part: SEAL — OUT OF TOLERANCE (L2 DOOR) · airframe 60,454 hrs · 21,233 cycles

PER CREW, DOOR 2LT HAS AN EXTREMELY LOUD AIR NOISE. REMOVED AND REPLACED L2 DOOR SEAL ASSY DOOR ALSO REMOVED AND RESTORED DURING THE HMV.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 60,454 hrs · 21,233 cycles

FIRST CLASS RT INBOARD SEAT TRACK LUG BROKEN OFF AT STA 536 (RBL 24.75). REPLACED SEAT TRACK SECTION FROM STA 530 TO STA 440 PER SRM. WORK ACP ON CAL NR9948488.

Part: CREASE BEAM — CORRODED (BS 430) · airframe 60,454 hrs · 21,233 cycles

CABIN INTERIOR FLOOR STRUCTURE AT CREASE BEAM STA 430 LEFT SIDE CORRODED. MAJOR REPAIR ACCOMPLISHED: REPLACED LT CREASE BEAM SECTION FROM STA 420 TO STA 440, PER 51-40-05, SRM 51-40-08 & DWG 140N0504.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 60,454 hrs · 21,233 cycles

FWD CABIN FLOORBEAM UPPER FLANGE CORRODED AT STA 365, RBL 5 TO RBL 48. MAJOR REPAIR ACCOMPLISHED: REPLACED UPPER CHORD OF STA 365 FLOORBEAM FROM LBL 11.5 TO RBL 70 PER CAL ECRA 5310-05391.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 60,454 hrs · 21,233 cycles

AFT CABIN FLOORBEAM STA 1640 CORRODED ON UPPER SURFACE BL 0 TO RBL 60. MAJOR REPAIR ACCOMPLISHED: REPLACED STA 1640 FLOORBEAM UPPER CHORD FROM LBL 10 TO RBL 70 PER CAL ECRA 5310-05388. WORK ACP ON CAL NR 9946372.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,454 hrs · 21,233 cycles

CABIN FLOORBEAM AT STA 324 CORRODED AT RBL 38 TO 62. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF T-CAP STA 324, LBL 7, TO RBL 62. EC-RA 53-10-05 389, AND EVA 81160.N-R 9946414. INSTALLED NEW T-CAP SECTION AND ANGLE DOUBLERS REF AVO IAH0 71311--03 REF STEP 7 AND TABLE 3 FLAG NOTE.

Part: FLOOR SUPPORT — CORRODED (BS 331) · airframe 60,454 hrs · 21,233 cycles

FLOOR SUPPORT CORRODED ON UPPER SURFACE STA 331, RBL 40. (GALLEY MOUNT SUPPORT). MAJOR REPAIR ACCOMPLISHED: FLOOR SUPPORT FROM STA 324 TO 345, RBL 40, REPLACED PER SRM. WORK WAS ACCOMPLISHED ON CAL NR 9947118.

Part: FLOORBEAM — CORRODED (BS 1660) · airframe 60,454 hrs · 21,233 cycles

AFT CABIN FLOORBEAM AT STA 1660 RBL 53 - 58 CORRODED ON UPPER SURFACE. CUT OUT AND REPLACED UPPER FLOORBEAM FROM RBL 17.5 TO RBL 70, PER ECRA 5310-053 87. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 324-418) · airframe 60,454 hrs · 21,233 cycles

CABIN FLOOR SUPPORT STA 324 TO 418 AT CENTER LINE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW FLOOR SUPPORT REF BOCA DWG NR 141N5191 AND SRM 51-40-02.

Part: HANDLE — DAMAGED (R4 DOOR) · airframe 60,454 hrs · 21,233 cycles

DOOR R4 INTERIOR HANDLE MOUNT HAS A BROKEN FLANGE. HANDLE MOUNT REPLACED PER SRM.

Part: HUB — CRACKED (R1 DOOR) · airframe 60,454 hrs · 21,233 cycles

DOOR 1R INTERNAL HANDLE ATTACH HUB IS CRACKED AT 1 ATTACH POINT AND BROKEN THRU AT OTHER ATTACH BOLT LOCATION. INSIDE HANDLE HELD ON WITH 1EA CRACKED LUG. INSTALLED NEW HANDLE ATTACH HUB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,454 hrs · 21,233 cycles

CABIN FLOORBEAM HAS CORR STA 1661, LBL 5 - 8. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED T-CAP AND INSTALLED REPAIR. REF COAIR N-R 9946383. RPR T-CAP AND DOUBLER ANGLES INSTALLED.

Part: SKIN — DENTED (BS 406 S17L) · airframe 60,454 hrs · 21,233 cycles

SHARP DENT IN FUSE SKIN STA 406, STR 17L. MAJOR REPAIR ACCOMPLISHED: DOUBLER REPAIR ACCOMPLISHED PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 60,449 hrs · 21,231 cycles

CABIN FLOOR EEL LIGHT COVER CRACKED AND BROKEN BTWEEN SEAT ROW 20-27. REPLACED DAMAGED COVER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,449 hrs · 21,231 cycles

CABIN FLOOR EEL LIGHT INOP SEAT ROW BETWEEN 20-27. REPLACED CHARGER AND BATTERY M10770 WORKED BUT ONLY TEMPORARILY. REPLACED BATTERY PACK M10770, CHECKS OK.

Part: SEAL — OBSTRUCTED (L2 DOOR) · airframe 60,379 hrs · 21,206 cycles

DOOR 2LT HAS AN EXTREMELY LOUD AIR NOISE. SEAMS TO BE CONCENTRATED AT THE FWD LWR CORNER OF THE DOOR. FOUND DUST SEAL (COSMETIC) BROKEN OFF STICKING BTWN MAIN SEAL AND DOOR SILL. NO DAMAGE TO MAIN SEAL. TRIMMED OFF DUST SEAL.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 60,349 hrs · 21,195 cycles

DOOR 1R WILL NOT ARM. CLEANED GIRT BAR AREA, OP CHECKS NORMAL. ARMING SYSTEMS OPERATIONAL.

Part: SEAT — UNSECURE (CABIN) · airframe 60,327 hrs · 21,189 cycles

SEAT LOOSE IN TRACKS 24ABC, 25ABC, 25DEF, 29ABC, 39ABC. SECURED SEAT ASSY IAW AMM.

Part: STRUCTURE — CORRODED (CARGO BAY) · airframe 59,988 hrs · 21,076 cycles

CORROSION ON FLOOR JUST INSIDE AFT CARGO COMPARTMENT.

Part: CONNECTOR — UNSECURE (LAVATORY) · airframe 59,806 hrs · 21,012 cycles

MID LAV SMOKE DETECTOR IS INOP. FOUND CLIPS MISSING FROM SMOKE DETECTOR CONNECTOR, PLUG WILL NOT SECURE PROPERLY. UPDATED NR PART TO REFLECT CORRECT P/N. REPLACED SLIDE LATCH. SMOKE DET OP CHECKS OK.

Part: CONNECTOR — LEAKING (GALLEY WATER) · airframe 59,776 hrs · 20,999 cycles

AFT GALLEY FLOOR SOAKED BY WATER FROM BEHIND AFT GALLEY CARTS. FOUND CONNECTOR FROM AIRCRAFT TO COFFEEMAKER M40 LEAKING. INOPED AFT GALLEY WATER AND OPENED ASSOCIATED COFFEEMAKER CB(S). NO FURTHER LEAKS NOTED. NEEDS WATER COUPLING THAT ATTACHES TO THE RAIL ASSY. THE COFFEEMAKERS ARE OKAY. NO FAULTS FROM THEM.

Part: DIFFUSER — DIRTY (CABIN AIR) · airframe 59,424 hrs · 20,871 cycles

CABIN RECIRCULATION AIR ROW 28 AND AFT IS NON EXISTENT. RT RECIRC FAN RECYCLED AND OPERATING. CHECKED AREA IAW MM FOR RESTRICTOR PROBLEMS. NO AIR FLOW FROM OVERHEAD DIFFUSER DUCT FROM ROW 25 TO 34. GASPER AIR FLOW IS GOOD IN SAME AREA. SUSPECT BLOCKAGE IN THE DIFFUSER DUCT CHANNEL. NO DAMAGE TO DUCT NOTED. REMOVED CTR DIFFUSER FROM ROW 25 TO AFT OF PLANE AND CLEANED. REINSTALLED DIFFUSER. AIRFLOW CHECKED GOOD.

Part: ENGINE — DAMAGED (LEFT) · airframe 59,016 hrs · 20,737 cycles

LT ENG SUFFERED A BIRDSTRIKE, RTFL. THRUST REVERSER BLOCKER DOOR FWD SEAL TORN. REPLACED BLOCKER DOOR. 8 FAN BLADES DAMAGED. NOSE COWL ALSO DAMAGED. INLET LINER HAS NUMEROUS DENTS. REPAIRED DENTS. FAN COWL DENTED. FAN INLET DENTS REPAIRED PER MM. FOUND SPACERS BETWEEN FAN EXIT GUIDE VANES DAMAGED. R & R BROKEN EXIT GUIDE VANE SPACERS. REMOVED 2 EXIT GUIDE VANE SPACERS. ON 2 EXIT GUIDE VANE BASES FOUND 1 WITH CRACK & 1 WITH PIECE MISSING. OK FOR SERVICE. R & R FAN BLADES. FAN BLADES NR 1, 2, 3, 4, 11, 15, 18, 26, 28, 29, 30, 31, 32, 33, 34, 35, 36 DAMAGED. FAN BLADES REPLACED. PERFORMED VIBRATION SURVEY PER JRH 2-5-6, OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 58,946 hrs · 20,712 cycles

ON TAKEOFF ROLL GOT STRONG ODOR OF OIL IT WENT AWAY DURING CLIMB. IAW CREW, ODOR WENT AWAY WITH LT PACK OFF. RAN BOTH ENG AND COULD NOT DUPLICATE ODOR. ISOLATED BOTH PACKS STILL COULD NOT DUPLICATE. RESEARCHED HISTORY. SUGGEST CLEANING OR REPLACING WATER NOZZLES. REPLACED & RAN PACKS, NO ODORS NOTED.

Part: FILTER — DIRTY (LT RECIRCULATON) · airframe 58,794 hrs · 20,648 cycles

FOUL ODOR, CHRONIC HISTORY AND POSSIBLE OIL ODOR. RECOMMEND TROUBLESHOOTING REF MM. REPLACED LEFT RECIRCULATON FILTER REF MM. ACCOMPLISHED TROUBLESHOOTING PROCEDURE OUTLINED IN MM, NO DEFECTS NOTED. CHECKED RT ENGINE AND LT PACK FOR EXTERNAL OIL LEAKAGE, NO LEAKS NOTED. CHECKED LEFT ACM FOR LEAKS, NO LEAKS NOTED. RAN ENGINES AT HIGH POWER PER JRH AND RAN PACKS. SMELL HAS NOW DIMINISHED.

Part: STOWAGE BOX — NO TEST (OXYGEN SYSTEM) · airframe 58,786 hrs · 20,644 cycles

FIRST OFFICER O2 MASK RESET-TEST SLIDER WILL NOT TEST. REPLACED FIRST OFFICER. CREW MASK STOWAGE BOX PER MM.

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR) · airframe 57,281 hrs · 20,085 cycles

DOOR 2L WON'T DISARM. ADJUSTED GIRT CURTAIN AND MOORING LINE AND REMOUNTED SLIDE PACK. OPS NORMAL.

Part: SEAL — DAMAGED (RT A/C BAY) · airframe 57,216 hrs · 20,060 cycles

UNABLE TO MAINTAIN CABIN PRESSURE IN DESCENT UNTIL FL220 . CREW REPORTED, IN DESCENT WITH BOTH THROTTLES AT IDLE CABIN ALTITUDE CLIMBED EXCESSIVELY. OPENED ISOLATION VALVE, THEN ABLE TO MAINTAIN CABIN PRESSURE BELOW FL220. FOUND NUMEROUS PACK SEALS IN RT AC BAY, REPLACED AS NEEDED. RAN PACK NO LEAKS NOTED. NOTE LT ENG HI STAGE BLEED WAS AND IS DEFERRED.

Part: COMPUTER — FAULTY (ELEVATOR FEEL) · airframe 56,896 hrs · 19,945 cycles

HIGH ELEVATOR FORCES. REMOVED FAULTY FEEL COMPUTER. FOUND TWO AIR LINES LOOSE ON THE OFF UNIT. REPLACED ELEVATOR FEEL COMPUTER. ACCOMPLISHED A VALIDATION TEST FLIGHT TO DETERMINE THAT INFLT ELEVATOR FORCES ARE NORMAL. TEST FLIGHT WAS SUCCESSFUL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,305 hrs · 19,738 cycles

NR 4 MED EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED.

Part: LIGHT — OBSTRUCTED (CABIN) · airframe 56,305 hrs · 19,738 cycles

DURING 'A' CHECK, FOUND CARPET AT AFT FWD LAV COVERING EMERGENCY LIGHTS. TRIMMED THE CARPET TO EXPOSE THE EMERGENCY LIGHT STRIP. OPS CKS NORMAL.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 56,305 hrs · 19,738 cycles

NR 5 L/E SLAT LWR INBD T/E WEDGE DELAMINATED FROM INBD EDGE OTBD 6.125 INCHES AND FROM AFT EDGE OF WEDGE FWD 7.25 INCHES WITH UPPER SKIN DELAMINATION OF 2 INCHES BY 3.125 INCHES DIRECTLY ABOVE LWR DELAM OUT OF LIMITS. NO VISIBLE LEAK PATH AND NO VISIBLE SKIN SEPARATION. REMOVED AND REPLACED NR 5 L-E SLAT. OPS CHK'D GOOD.

Part: JUMPER — FAULTY (CABIN) · airframe 55,366 hrs · 19,415 cycles

EEL LIGHT STRIP IS INOP FROM SEATS 9C TO 13C. REPLACED JUMPER CABLE AND CHECKED OKAY.

Part: FITTING — OUT OF RIG (R OVERWING SLIDE) · airframe 54,766 hrs · 19,172 cycles

RIGHT OFF WING SLIDE DOOR 196FR HARD TO CLOSE. REPLACED AND OPS CHECKED THE RIGHT OFF WING SLIDE DOOR LATCH FITTING HARDWARE. OPS CHECKED GOOD.

Part: BEARING — CORRODED (L4 DOOR) · airframe 54,766 hrs · 19,172 cycles

MAIN CABIN L4 DOOR TORQUE TUBE CENTER BEARING CORRODED. REMOVED L4 DOOR. REMOVED AND REPLACED HINGE ARM TORQUE TUBE BEARING AND RE-INSTALLED DOOR. OPS CHECK GOOD.

Part: BEARING — CORRODED (R4 DOOR) · airframe 54,766 hrs · 19,172 cycles

MAIN CABIN R-4 DOOR TORQUE TUBE BEARING CORRODED. REMOVED DOOR R-4. REMOVED AND REPLACED DOOR HINGE ARM TORQUE TUBE BEARING, RE-INSTALLED DOOR AND OPS CHECK ALL.

Part: SKIN — CHAFED (TE FLAP) · airframe 54,766 hrs · 19,172 cycles

LEFT WING INBOARD FLAP OUTBOARD UPPER EXTERNAL SKIN CHAFED. REPAIRED THE INBOARD FLAP OUTBOARD UPPER EXTERNAL SKIN. GAP CHECKED SPOILER TO FLAP UPPER PANEL. GAP CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 54,766 hrs · 19,172 cycles

AFTER JET BRIDGE REMOVAL BEFORE FLIGHT, RAMP REPORTED DENT FOUND AT APPROX STA 730, APPROX 13 INCHES AFT OF DOOR 2L AND 16 IN ABOVE THRESHOLD OF DOOR. MAJOR REPAIR ACCOMPLISHED. CLEANED PAINT AROUND DENT FOR HFEC INSPECTION A-Y AT 30. NO CRACK FOUND DURING HFEC. TRIMMED OUT SKIN DAMAGE AT BS 740 LT AT STR 15L, FABRICATED A DOUBLER - TRIPLER AND INSTALLED.

Part: TRANSDUCER — FAULTY (OXYGEN SYSTEM) · airframe 51,637 hrs · 17,974 cycles

THE O2 PRESSURE DECREASES FROM 1600 TO 160 WHEN TESTED ON BOTH CAPT - F/O POSITIONS. TRANSDUCER FOUND FAULTY. REPLACED PRESSURE TRANSDUCER. OPS CHECKS OKAY.

Part: LANYARD — UNSECURE (L2 DOOR SLIDE) · airframe 51,345 hrs · 17,872 cycles

DOOR 2L DIFFICULT TO DISARM. *S/D* LANYARD AND D-RING -WERE INTERFERING WITH GIRT BAR. SECURED LANYARD AND D-RING WERE INTERFERING WITH GIRT BAR. DOOR ARMS AND DISARMS NORMALLY.

Part: GIRT BAR — DIRTY (R4 DOOR) · airframe 49,765 hrs · 17,346 cycles

CREW REPORT: DOOR 4R WILL NOT ARM. FOUND DEBRIS UNDER GIRT BAR AREA. CLEANED AND LUBED GIRT BAR, SLIDER AND OPS CHECKED NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,847 hrs · 17,012 cycles

DOOR 2 LEFT EXTERIOR EMERGENCY LIGHT INOP. REPLACE LAMP.

Part: STRAP — OUT OF POSITION (L1 DOOR SLIDE) · airframe 48,256 hrs · 16,807 cycles

DOOR 1L SLIDE-RAFT STRAP WITH 'D' RING IS NOT VISIBLE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 47,850 hrs · 16,664 cycles

JETWAY CONTACTED LEFT SIDE OF AIRCRAFT JUST 6 FT FWD OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. DOOR 2L, DENT IS 4 INCHES BY 2 INCHES BY QUARTER OF AN INCH DEEP ON A STRINGER; SOME METAL WAS REMOVED FROM THE SCRAPE. ACCOMPLISHED DOUBLER REPAIR.

Part: UNKNOWN — VIBRATION (FUSELAGE) · airframe 47,798 hrs · 16,644 cycles

FLIGHT DIVERTED DUE TO VIBRATION IN THE AFT GALLEY FLOOR. CREW REPORTS NO WATER PRESS IN ALL GALLEY AND LAVS. ALSO REPORT VIBRATION IN AFT GALLEY FLOOR AREA , CHECKED EXTERIOR SERVICE PANEL DOOR FOR SECURITY AND VERIFIED THAT SERVICE HANDLE WAS FULLY CLOSED AND NO AIR WAS DUMPING OVERBOARD. FOUND WATER FILL VALVE HANDLE IN THE OPEN POSITION WITH DOOR CLOSED. RE-SERVICED PER UA ENGINEERING SPECIFICATIONS.

Part: CONNECTOR — DIRTY (SLIDE BOTTLE) · airframe 46,883 hrs · 16,305 cycles

LEFT OFF WING SLIDE BOTTLE SQUIB, TEST LIGHT ON P-61 PNL STAYS ON. CLEANED CONNECTOR AND OPS CHECK GOOD.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED (CENTER SYS) · airframe 44,377 hrs · 15,394 cycles

RETURNED TO FIELD DUE TO LOSS OF CENTER SYSTEM HYDRAULIC PRESSURE. INDICATION WENT TO ZERO FOR CENTER HYD TANK WHICH VISUALLY VERIFIED FULL. REPLACED CTR HYD PRESSURE QTY TRANSMITTER. NO RECURRENCE PROBLEM REPORTED.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 39,444 hrs · 13,613 cycles

RETURNED TO FIELD DUE TO NR 2 ENGINE SHUTDOWN. THE ENGINE EXPERIENCED A SURGE IN THE HPC AND WAS SHUTDOWN. THE ENGINE SURGE WAS CAUSED BY A DISRUPTION IN AIRFLOW THROUGH THE HPC THAT WAS CAUSED BY DAMAGE TO THE COMPRESSOR AIRFOILS. THE AIRFOIL DAMAGE WAS CAUSED BY FOD. THE MATERIAL THAT CAUSED THE FOD WAS NOT RECOVERED NOR IDENTIFIED AT THIS TIME. THE ENGINE WAS REMOVED FROM SERVICE AND OVERHAULED.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,784 hrs · 13,377 cycles

LT FUSELAGE SKIN AT BS 610 AND STR 16L IS DENTED ON A PREVIOUS REPAIR DOUBLER. REPAIRED SKIN WITH A DOUBLER-TRIPLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,784 hrs · 13,377 cycles

FWD PIT FRAME DENTED ON INBD FLANGE AT STA 620 JUST BELOW STR 24L. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,784 hrs · 13,377 cycles

AFT PIT STA 1480 FRAME IS DENTED ON INBD FLANGE, APPROXIMATELY STR 26L. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 38,784 hrs · 13,377 cycles

MAIN CABIN AFT SIDE OF STA 365 FLOORBEAM, RBL 45 SEAT TRACK END, TOP SURFACE OF INTERCOSTAL CORRODED BEYOND LIMITS AT FLOORBEAM ATTACHMENT. FABRICATED & INSTALLED DOUBLER AND FILLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,784 hrs · 13,377 cycles

FLOORBEAM AT STA 1640, RBL 58-RBL 60 CORRODED BEYOND LIMITS. INSTALLED REPAIR ANGLE, FILLER, STRAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,784 hrs · 13,377 cycles

MAIN CABIN, RIGHT SIDE, FLOORBEAM STA 324, RBL 28 - RBL 70, TOP T-CAP SURFACE CORRODED BEYOND LIMITS. FABRICATED & INSTALLED REPAIR STRAPS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,784 hrs · 13,377 cycles

MAIN CABIN, RIGHT SIDE FLOORBEAM STA 365, TOP TEE CAP SURFACE CORRODED BEYOND LIMITS BL 0 - RBL 70 AT R-1 DOOR THRESHOLD. FABRICATED & INSTALLED TEE CHORD, REPAIR ANGLES AND STRAPS.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 36,489 hrs · 12,587 cycles

DAMAGE TO AFT PRESS BULKHEAD & SKINS STA 1620-1787 STR 19-25L. MAJOR REPAIR ACCOMPLISHED. STA 1720 BREAK RING REPLACED FROM WL 191 TO BL 0 STA 1720 BULKHEAD 2 INCH DENT REPAIRED. SKINS REPLACED STA 1620-1720 STR 19-25L. STRINGERS AND ASSOC FITTINGS REPLACED STA 1720-1787 STR 19-25L.

Part: FRAME — DENTED (FUSLAGE) · airframe 38,784 hrs · 13,377 cycles

AFT PIT STA 1460 FRAME DENTED STR 26 LT ON INNER FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,784 hrs · 13,377 cycles

RT CABIN WINDOW FRAME NR 6 IS CRACKED DUE LIGHTNING STRIKE. INSTALLED NEW WINDOW FRAME.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 38,784 hrs · 13,377 cycles

RT CABIN WINDOW FRAME NR 4 IS CRACKED DUE LIGHTNING STRIKE. INSTALLED NEW WINDOW FRAME.

Part: FRAME — DENTED (FUSELAGE)

AFT PIT STA 1500 FRAME DENTED AT STR 25 LT ON FRAME INBD FLANGE. REPAIRED FRAME WITH NESTED J-ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,784 hrs · 13,377 cycles

AFT PIT STA 1440 FRAME DENTED STR 26 LT AT INBD FLANGE. REPAIRED FRAME FLANGE WITH NESTED J-ANGLE REPAIR.

Part: SKIN — CUT · airframe 33,268 hrs · 11,485 cycles

FWD CARGO DOOR, AFT LOWER CORNER, FOUND DAMAGE TO DOOR OUTER SKIN. 3-16 BY 1-4 INCH V CUT IN DOOR SKIN. MAJOR REPAIR ACCOMPLISHED. BELENDED OUT DAMAGE BY MANUFACTURING DOUBLER.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,490 hrs · 9,762 cycles

ODOR IN FLIGHT DECK AND FORWARD CABIN AFTER LANDING .

Part: DIODE — FAILED (IDG) · airframe 24,566 hrs · 8,383 cycles

RETURNED TO DEN AND LANDED UNDER AN AMBER ALERT DUE TO AN ELECTRICAL PROBLEM. *S/D* THE LEFT (NR 1) INTEGRATED DRIVE GENERATOR WAS REPLACED. THE IDG HAD AN INTERNAL DIODE FAILURE. C901 GEN CIRCUIT BREAKER WAS REPLACED. THE CIRCUIT BREAKER HAD BURNED AND PITTED MAIN CONTACTS. THE LEFT GENERATOR CONTROL UNIT WAS REPLACED. AN INTERNAL POTENTIOMETER R17 WAS OUT OF TOLERANCE. THE BUS POWER CONTROL UNIT WAS REPLACED. NO FURTHER DISCREPANCY HAS OCCURRED.

Part: TIRE — BLOWN (LANDING GEAR)

LANDED UNDER AMBER ALERT DUE TO A SUSPECTED BLOWN TIRE.

Part: DOOR — WILL NOT ARM (CABIN)

DOOR 1R WOULD NOT ARM AT DEPARTURE. *S/D* FOUND SLIDE LANYARD INTERFERING WITH GIRT BAR. SECURED SLIDE LANYARD AND OPS CHECKED NORMAL.

Part: FAN BLADE — DAMAGED (RT ENGINE)

DURING CLIMBOUT, CREW REPORTED BUZZING NOISE. NOISE ENDED WHEN NOSE WAS LOWERED TO CRUISE ALTITUDE. *S/D* DISCOVERED BIRD STRIKE AND FOUND DAMAGED BLADES ON RIGHT ENGINE. REPLACED THREE FAN BLADE PAIRS.

Part: IDG — FAILED (RIGHT)

ABORTED TAKEOFF AT 60 KNOTS DUE TO RIGHT GENERATOR FAILURE. IDG (INTEGRATED DRIVE GENERATOR) FAILED. REPLACED IDG. LEAK AND OPERATIONAL CHECK WAS GOOD.

Part: LAMP — FAILED (CABIN)

DOOR 3 LEFT EMERGENCY LIGHT INOP. REPLACED LAMP, OPERATION CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT ABOVE SEATS 26ABC DOES NOT ILLUMINATE. REPLACED BATTERY PACK AT M10699 MODULE, OPERATION CHECKS NORMAL.

Part: LAMP — FAILED (CARGO DOOR)

EXTERNAL EMERGENCY LIGHT INOP, RIGHT AFT CARGO DOOR. REPLACED LAMP, OPERATION CHECKS NORMAL.