N538UA

Part: COVER — DAMAGED (CABIN) · airframe 73,317 hrs · 26,817 cycles

EMERGENCY FLOOR TRACK LIGHT COVER AT ROW 28 - 30 DAMAGED. INSTALLED EMERGENCY LIGHT COVER CLEAR LENS AT ROW 29, OK FOR SERVICE.

Part: DUCT — CONTAMINATED (AC BAY) · airframe 73,310 hrs · 26,813 cycles

CABIN BECAME HAZY SHORTLY AFTER TURNING APU BLEED ON & RT PACK ON. ACCOMPLISHED PACK BURNOUT IAW PG 204 THROUGH V AFTER CLEANOUT OF REHEATER & PACK DUCTS OF DEICING FLUID. NO ODOR OR HAZE IN CABIN AFTER 15 MIN RUNS WITH BOTH BLEEDS & PACKS.

Part: SMOKE DETECTOR — ACTIVATED (LAVATORY) · airframe 73,291 hrs · 26,806 cycles

LAVATORY 2L SMOKE DETECTOR ACTIVATED, RTFL.

Part: FILTER — DIRTY (CABIN) · airframe 73,291 hrs · 26,805 cycles

MIST IN CABIN WHEN CREW ARRIVED CALLED MX. ACCOMPLISHED PACK BURNOUT. REPLACED RECIRCULATING FILTERS & EQUIPMENT COOLING FILTERS, CHECKED GOOD.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 72,824 hrs · 26,655 cycles

NR 1 ENG IS LEAKING FUEL OUT OF LOWER SIDE OF FUEL PUMP CASE TRANSFER TUBE JOINT. REMOVED FUEL PUMP & FUEL CONTROL, DISCONNECTED MAIN FUEL LINE.

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 72,664 hrs · 26,610 cycles

FIRST OFFICER`S O2 MASK EMERGENCY PRESSURE KNOB BROKEN. SWAPPED OBSERVER'S SEAT 02 MASK TO FIRST OFFICER`S POSITION. FIRST OFFICER`S MASK NOW SERVICEABLE. DEFERRED OBSERVER`S SEAT CONSIDERED INOPERATIVE. REPLACED OBSERVER`S SEAT 02 MASK.

Part: INDICATION SYS — INACCURATE (FUEL QTY) · airframe 72,298 hrs · 26,478 cycles

FUEL INDICATOR NOT CORRECT, LT WING READS 0, RT READS 9.5.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 72,195 hrs · 26,446 cycles

R4 DOOR HARD TO ARM. INSPECTED DOOR ARMING MECHANISM. FOUND DEBRIS, REMOVED. ARMED DOOR SEVERAL TIMES, OPS GOOD.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 72,171 hrs · 26,438 cycles

R4 DOOR CAN'T CLOSE AND AND DIFFICULT TO ARM. OPS CHECKED R4 DOOR. DID FIND DEBRIS IN GIRT BAR ANCHORS. CLEANED DOOR, OPS NORMAL AT THIS TIME.

Part: INDICATOR — MISSING (CABIN) · airframe 72,343 hrs · 26,469 cycles

EMERGNECY EXIT LIGHT STRIP ADJACENT TO OW EXIT HATCH HAS ONLY ONE ORANGE OVERLAYING INDICATOR. THERE SHOULD BE TWO, ONE PER HATCH. INSTALLED NEW ORANGE OVERLAY INDICATOR ADJACENT TO OW EXIT HATCH IAW IPC 33-52-00. EMERGENCY EXIT LIGHT ELECTRICAL SYSTEM WAS NOT DISTURBED.

Part: SWITCH — DAMAGED (CARGO FIRE LIGHT) · airframe 72,122 hrs · 26,422 cycles

AFT CARGO FIRE LIGHT DOES NOT ILLUMINATE DURING TEST. REPLACED AFT CARGO SWITCH BODY IAW MM, SYS OPS NORMAL.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 72,113 hrs · 26,419 cycles

NR 1 PYLON SKIN CRACKED AT FWD HOLE OUTER SKIN SURFACE. STOP DRILLED CRACK, FABRICATED TWO REPAIR DOUBLERS AND INSTALLED. MAJOR REPAIR.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 72,113 hrs · 26,419 cycles

NR 2 PYLON INBD STRUT SKIN CRACKED AT AFT HOLE INNER SURFACE SKIN 3-4 INCHES LENGTH. REMOVED REPAIR DOUBLER, STOP DRILLED CRACK, FABRICATED TWO DOUBLERS AND INSTALLED REF REO-G 16432 AND ECRA 5450-02054. NR 20700. MAJOR REPAIR.

Part: WINDOW FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,113 hrs · 26,419 cycles

SECOND WINDOW FRAME FWD OF LT FWD OVERWING HATCH HAS LIGHT CORROSION. REMOVED CORROSION AND MATERIAL REMAINING EXCEEDED LIMITS OF SRM 56-20-02. REMOVED WINDOW FRAME AND INSTALLED SERVICEABLE FRAME.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 72,113 hrs · 26,419 cycles

MAIN CABIN FLOORBEAM, BS 1640 BL 0 - RBL 60 CORRODED. REMOVED DAMAGED SECTION OF TEE ANGLE AND FABRICATED A NEW TEE ANGLE SECTION, SPLICE ANGLES AND STRAPS AND INSTALLED IAW SRM 53-00-51, REPAIR 8. MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 324) · corrosion level 2 · airframe 72,113 hrs · 26,419 cycles

MAIN CABIN FLOORBEAM CORRODED AT BS 324, BETWEEN RBL 40-64. REMOVED DAMAGED SECTION OF TEE ANGLE, FABRICATED AND INSTALLED TEE ANGLE SPLICE REPAIR ANGLES AND STRAPS. IAW ECRA 5310-05795.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 72,113 hrs · 26,419 cycles

MAIN CABIN FLOORBEAM CORRODED, FOUND AT BS 365, LBL 2-RBL 64. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-00-51 REPAIR 8. CAT A REPAIR.

Part: FRAME — DENTED (BS 1420 S27L) · airframe 56,638 hrs · 20,767 cycles

AFT CARGO BAY FRAME DENTED BS 1420 S27L. CUT OUT DAMAGED AREA OF FRAME INBOARD FLANGE, AND FORMED A REPAIR ANGLE PER SRM 53-00-07, REPAIR 5. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1540, S26L) · airframe 56,638 hrs · 20,767 cycles

AFT CARGO BAY FRAME DENTED BS 1540 S26L. CUT OUT DAMAGED SECTION OF INBOARD FLANGE, AND FORMED REPAIR ANGLE PER SRM 53-00-07, REPAIR 5. MAJOR REPAIR.

Part: FRAME — BENT (BS 1400 S26-27L) · airframe 56,638 hrs · 20,767 cycles

AFT CARGO BAY FRAME BENT BS 1400, S26-27L. REPAIRED DAMAGED FRAME IAW SRM 53-00-07 REPAIR 5 DETAIL I. MAJOR REPAIR.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 71,418 hrs · 26,205 cycles

DOOR 4R EMERGENCY SLIDE UNABLE TO BE ARMED. CLEAN DEBRIS UNDER GIRT BAR AND CYCLE ARMING LEVER, OPS CHECKED GOOD.

Part: SPRING — FAULTY (R1 HINGE COVER) · airframe 71,228 hrs · 26,143 cycles

R1 DOOR LOWER FWD HINGE COVER WILL NOT SPRING OUT. REMOVED THE HINGE COVER AND ALL PARTS, REPLACED SPRING .

Part: CHILLER — INOPERATIVE (GALLEY) · airframe 71,228 hrs · 26,143 cycles

GALLEY CHILLER INOPERATIVE. REMOVED AND REPLACED GALLEY CHILLER. OPS CHECKED NORMAL.

Part: WINDSHIELD — DELAMINATED (NR 1) · airframe 71,071 hrs · 26,096 cycles

FIRST OFFICER'S WINDSHIELD'S VISIBILITY IS AFFECTED BY DEFECTS. DELAMINATED ON UPPER RIGHT CORNER 2 X 5 INCHES. REPLACED NR 1 WINDSHIELD, OPS CHECKED OK.

Part: WINDSHIELD — DELAMINATED (NR 1) · airframe 71,071 hrs · 26,096 cycles

FIRST OFFICER'S WINDSHIELD'S VISIBILITY IS AFFECTED BY DEFECTS. DELAMINATED ON UPPER RIGHT CORNER 2 X 5 INCES. REPLACED NR 1 WINDSHIELD, OPS CHECKED OKAY.

Part: THRESHOLD — DAMAGED (CARGO BAY) · airframe 70,840 hrs · 26,019 cycles

AFT CARGO PIT ALUMINIUM THRESHOLD FLOOR PANEL HAD DAMAGE AT CENTER OF DOOR THRESHOLD APPROX ONE INCH INBOARD OF THRESHOLD.

Part: UNKNOWN — UNKNOWN (R4 DOOR) · airframe 70,819 hrs · 26,012 cycles

R4 DOOR FAILED TO ARM. DOOR ARMS ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. ACCOMPLISHED OPS CHECK OF DOOR ARMING PER AMM, OPS CHECKS GOOD.

Part: FUSE — LEAKING (HYD SYSTEM) · airframe 70,758 hrs · 25,986 cycles

FOUND HYD FUSE ASSY RIGHT MLG WHEEL WELL LEFT SYS LEAKING BEYOND DISPATCH LIMITS. REMOVED AND REPLACED LEAKING FUSE EXTENSION HYDRAULIC FLOW FUSE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,621 hrs · 25,940 cycles

DURING EMERGENCY EXT LIGHT TEST FOUND DOORS 2R AND 4L EXIT LIGHTS INOPERATIVE. ACCOMPLISHED EMERGENCY LIGHT TEST, EXIT LIGHTS AT DOOR 2R AND 4L OP NORMAL.

Part: BRACKET — BROKEN (CARGO DOOR) · airframe 70,535 hrs · 25,915 cycles

RAMP REPORTS PART FELL OUT OF FWD CARGO DOOR HANDLE AREA WHEN THEY OPENED THE DOOR. FOUND BRACKET FOR BUMPER UNDER DOOR HANDLE BROKEN. REPLACED BRACKET. OPS CHECKED GOOD.

Part: GROUND WIRE — LOOSE (CABIN) · airframe 70,147 hrs · 25,789 cycles

FORWARD RIGHT WING EMERGENCY LIGHT IS INOP. RELAMPED, NO HELP. FOUND GROUND WIRE FOR LIGHT ASSEMBLY L561 LOOSE ON GROUND STUD. TIGHTENED WIRE ON GROUND STUD. OP CHECKED OKAY.

Part: LINE — LEAKING (RT WING FUEL) · airframe 69,946 hrs · 25,717 cycles

FUEL COMING OUT OF RIGHT WING DRYBAY HOLE NR 1, WHILE TROUBLESHOOTING WITH PUMPS ON FUEL COMING OUT OF HOLE. REPLACED DRY BAY NR 2 ENGINE FLEX FUEL FEED LINE, LEAK CHECKED AND RAN ENGINE.

Part: STUD — STRIPPED (CABIN SEAT) · airframe 69,913 hrs · 25,706 cycles

SEAT ROW 21ABC AFT LEGS SAFETY SCREWS STRI0PPED. REPLACED REAR STUD ASSY. REF AMM 25-25-92.

Part: UNKNOWN — ODOR (CABIN) · airframe 69,437 hrs · 25,552 cycles

INTERMITTENT STRONG ELECTRICAL ODOR EMANATING FROM AREA FROM 2L TO MID CABIN. FLIGHT ATTENDANT DETECTED AN ELECTRICAL OR RUBBER ODOR, NO SMOKE, LOCALIZED AT DOOR 2L AND MID LAV, ODOR INTERMITTENT LIGHTS WERE OFF. INSPECTED LAVATORY AND SIDEWALL BALLAST AND GALLEY AREA, NO ODORS NOTED. RAN PACKS AND RECIRCULATION FANS, STILL NO DEFECTS OR REPEAT ODOR NOTED.

Part: SMOKE GOGGLES — MISSING (COCKPIT) · airframe 69,254 hrs · 25,482 cycles

FIRST OFFICER SMOKE GOGGLES MISSING. REPLACED SMOKE GOGGLES.

Part: HINGE FITTING — WORN (LT MLG DOOR) · airframe 68,616 hrs · 25,280 cycles

LEFT MLG DOOR AFT ATTACH FITTING BOLT HOLES WORN. OVERSIZED HOLES, HOLE FINAL SIZE IS .437,EM WITHIN LIMITS PER AVO 1283. REWORKED LT MLG DOOR AFT HINGE FITTING COUNTERSUNK HOLES REF AVO 1283 AND ECRA 5340- 01464 AND INSTALLED FITTING WITH OVERSIZED HARDWARE.

Part: ADC — MALFUNCTIONED (LEFT) · airframe 67,588 hrs · 24,902 cycles

ALTITUDE AND IAS DISAGREE. CAPTAIN`S AIR DATA SWITCH SELECTED RESTORES PROPER INDICATIONS. FOUND LEFT ADC FAULTING LEFT AOA, FOUND LEFT AOA STIFF, AND BINDING. REPLACED LEFT AOA AND LEFT ADC, OPS CHECKED GOOD. COMPLETED CAT III TEST 30, TESTED GOOD.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 67,489 hrs · 24,870 cycles

EEL IMPROPERLY INSTALLED AT STA 891.75 TO STA 898.25. INSTALLED EEL STRIP AT BS 891.75 TO 898.25 PROPERLY IAW DRAWING 1SF6889- 504 & AMM 33-51-11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,489 hrs · 24,870 cycles

EMERGENCY EXIT LIGHT STRIP AT LAV K INOP. SPLICED EEL STRIP AT 'K' LAV. OPS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 67,489 hrs · 24,870 cycles

EMERGENCY EXIT LIGHT STRIP AT LAVS INOP. FOUND PIGTAIL CONNECTION FOR THE EMERGENCY EXIT LIGHT STRIP AT LAVS DISCONNECTED. RE-CONNECTED PIGTAIL AND PERFORMED SUCCESSFUL OPS CHECKS IAW B757 AMM.

Part: LAMP — INOPERATIVE (FUEL CONTROL SWI) · airframe 67,469 hrs · 24,862 cycles

FIRE WARNING LIGHT DOES NOT ILLUMINATE ON LEFT ENGINE FUEL CONTROL SWITCH DURING TEST. RELAMPED LEFT ENG FUEL CONTROL SWITCH. FIRE TEST NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,469 hrs · 24,862 cycles

(.125) OF AN INCH CRACK VERIFIED IN CROWN SKIN AT STATION 407. FOUND CRACK INDICATION AT STR 4L STA 406 APPROX 1-8TH IN LONG AT CHEM MILL RADIUS.

Part: WIRE — SHORTED (LT ENGINE) · airframe 67,379 hrs · 24,832 cycles

LEFT ENG FUEL FILTER EICAS, FLIGHT DIVERTED. FOUND WIRE W3394-1019-18 SHORTED APPOX 10 INCHES FROM CONNECTOR D42036P PIN 4. REPAIRED WIRE PER GN-MM. WIRE HAS INSULATION DAMAGE ONLY. GRD CHECK GOOD. NO SHORT TO SHIELD, AFTER REPAIR.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 66,968 hrs · 24,685 cycles

CREW REPORT: RIGHT RVSM CRITICAL AREA BOX MISSING MULTIPLE AREAS OF PAINT. CONDITION CONSIDERED ACCEPTABLE PER MM. OK TO CF FOR PAINT. ALL REPAIRS DONE IN RVSM CRITICAL-EXTRA CRITICAL AREA WILL BE TREATED AS A MAJOR REPAIR. PAINT APPLIED TO 3 EACH PAINT CHIPS .10 INCH DIA EACH.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 66,968 hrs · 24,685 cycles

CREW REPORT: L RVSM CRITICAL AREA BOX MISSING ONE AREA OF PAINT. CONDITION CONSIDERED ACCEPTABLE PER MM. OK TO CF FOR PAINT. ALL REPAIRS DONE IN RVSM CRITICAL-EXTRA CRITICAL AREA WILL BE TREATED AS A MAJOR REPAIR. PAINT APPLIED TO PAINT CHIP OF .10 INCH DIA.

Part: HEAT SHIELD — DELAMINATED (LT MLG DOOR) · airframe 66,610 hrs · 24,545 cycles

LEFT MAIN LANDING GEAR DOOR HEAT SHIELD HAS AN AREA 30 INCH BY 5 INCH. THAT IS DELAMINATED. REPLACED HEAT SHIELD PER MM.

Part: SEAT — LOOSE (CABIN) · airframe 66,146 hrs · 24,380 cycles

SEAT ASSY LOOSE 32ABC, 37DEF, 39ABC, 39DEF, 40DEF. SECURED SEAT ASSY IAW AMM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 66,017 hrs · 24,328 cycles

FWD FLOOR EMERGENCY LIGHT STRIP AT COAT CLOSET INOP. REPAIRED BROKEN WIRE TAPE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,695 hrs · 24,199 cycles

EMERGENCY FLOOR PATH LIGHTING HAS SECTION INOP JUST AFT OF ROW 6 TO MID LAV APPROX 27 INCHES INOP. JUST AFT OF ROW 6 TO MID LAV APPROX 27 INCHES INOP. REPLACED EEL LIGHT ASSY, OPS CHK NORMAL.

Part: DUCT — DIRTY (CABIN) · airframe 65,284 hrs · 24,052 cycles

RIGHT RECIRCULATION FAN EXTREMELY LOUD. TOO LOUD FOR USE IN FLIGHT. RT RECIRCULATION FAN INOP. 4SS FOR DUCT CLEANING. CHECK DB NOISE LEVEL WITH APU ONLY, DUCT PRESS 14PSI BASE LEVEL,105-DB LT RECIRC FAN ON RT OFF 107DB, LT FAN OFF RT FAN ON 109 DB.ACCOMPLISHED DUCT CLEAN OF ENTIRE CABIN. DB NOW 73 WITH FAN OFF AND 75 WITH FAN ON.

Part: FAN — NOISY (RIGHT) · airframe 65,054 hrs · 23,957 cycles

COCKPIT COMMUNICATIONS DIFFICULT DUE TO EXCESSIVE NOISE. RT RECIRCULATION FAN OFF HELPS CHRONIC PROBLEM. REPLACED RT CABIN AIR RECIRCULATION FAN.

Part: STRUCTURE — DAMAGED (MLG DOOR) · airframe 65,054 hrs · 23,957 cycles

RIGHT MLG DOOR, DAMAGE FOUND ON THE INSIDE FWD HALF OF DOOR. TWO GOUGES IN THE HONEYCOMB AND HALF OF THE INSIDE SKIN IS TORN AND MISSING. MLG DOOR REMOVED, DOOR SENT TO REPAIR SHOP. REPAIR AND RETURN TAG R74249.

Part: FAN — FAULTY (RECIRCULATION) · airframe 65,045 hrs · 23,955 cycles

COCKPIT AIR NOISE DANGEROUSLY LOUD. WORST DURING CLIMBOUT & DESCENT. NUMEROUS MISSED RADIO CALLS. REPLACED THE LT CABIN AIR RECIRCULATION FAN IAW ACCOMPLISHED FLIGHT DECK AIR FLOW CHECK IAW MM.

Part: COMPRESSOR BLADE — DAMAGED (NR 1 ENGINE) · airframe 63,706 hrs · 23,460 cycles

NR 1 ENG BIRDSTRIKE. ENG PARAMETERS WERE ABNORMAL. ON WALKAROUND FOUND EVIDENCE OF BIRDSTRIKE IN LT ENG AND COWL. ON EFAN BLADE IS DAMAGED. IAW CAPTAIN, NO ABNORMAL PARAMETERS WERE NOTED. ONE FAN BLADE HAS BEND 2" FROM TIP 4" LONG X 1.25" RADIAL X 1.0" CIRCUMFERENTIAL DISPLACEMENT. EXCEEDS MM LIMITS AND MUST BE REPLACED. REPLACED DAMAGED BLADE (NR 26) & OPPOSITE BLADE (NR 8) IAW MM.

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 63,653 hrs · 23,445 cycles

FLUID LEAKING NR 1 ENGINE. NR 1 ENGINE INBOARD (RT) REVERSER HALF, MIDDLE LOCK ACTUATOR MR78330 PCN 643-9215 LEAKS HYDRAULIC STAEDY STREAM AT ACT ROD END, BEYOND DISPATCH LIMITS OF AMM 78-31-13, PAGE 425, REPLACED ACTUATOR.

Part: DUCT — UNKNOWN (CABIN AIR) · airframe 63,650 hrs · 23,444 cycles

FWD & AFT CABIN TEMP HARD TO CONTROL. INOPED FWD AND AFT TRIM AIR, NO TIME ORD. REPLACED OVERHEAD DISTRIBUTION DUCTS. REACTIVATED TRIM AIR SYS AND CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,650 hrs · 23,444 cycles

EEL LIGHTS NOT WORKING IN SEVERAL COACH SECTIONS. REPLACED BATTERY AT M614 AND CHARGER AND BATTERY AT M733, OP CHECKS OKAY.

Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 63,074 hrs · 23,228 cycles

CAPTAIN OXYGEN MASK MICROPHONE INOP, R & R OXYGEN MASK. OPS ARE GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 62,980 hrs · 23,192 cycles

LIGHT STRIP ON FLOOR NEXT TO FWD AFT LAV HAS TAPE COMING OUT OF IT. INTERM REPAIR ACP USING 3M CLEAR TAPE 8686. WILL REQUIRE A NEW END CAP. LIGHTS WORK CORRECTLY AND NO PART IS OBSTRUCTED FROM VIEW. REPLACED MISSING END CAP, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,762 hrs · 23,108 cycles

EMERGENCY EXIT LIGHT ABOVE 13DEF INOP. RELAMPED, OPS CHECKED OKAY.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 62,762 hrs · 23,108 cycles

EMERGENCY LIGHT DOES NOT ILLUMINATE ON FLOOR AT 'K' LAV. SPLICED RIBBON CABLE TO LIGHT, 560-3325

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 61,806 hrs · 22,748 cycles

RT WING INBD FORE FLAP UPPER SKIN CHAFING ON THE NR 8 SPOILER PANEL. REPAIRED RT INBD FORE FLAP UPPER SKIN IAW REO G-13248. THE REPAIR IS A MAJOR REPAIR AND RECEIVED STG 1 APPROVAL FROM BAC VIA FAA FORM 8100-9. THE COMPLIANCE OF 14 CFR 25.571 AND 26.43 HAS NOT BEEN EVALUATED. A NEW FAA FORM 8100-9 MUST BE ISSUED WITHIN 24 MONTHS. A CF ITEM IS CREATED TO MONITOR. REPAIR WORK IS ACP ON NR 09497243611 AND REF EVA 73393.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 61,806 hrs · 22,748 cycles

NR 2 NACELLE STRUT SIDE SKIN IB SIDE FWD ACCESS HOLE IS CRACKED AT THE 11:00 POS, APPROX .50" INCH LONG. MAJOR REPAIR ACCOMPLISHED: STOP DRILLED CRACK. ACP HFEC INSP FOR CRACK TERMINATION. FABRICATED AND INSTALLED DOUBLER.

Part: SKIN — DAMAGED (NR 1 NACELLE) · airframe 61,806 hrs · 22,748 cycles

NR 1 NACELLE STRUT OTBD SIDE SKIN AT THRUST REV HINGE AREA, 2ND LIGHTENING HOLE, APPROX 7:30 POS, ONE CRACK IN SKIN EXTENDING APPROX .185" BEYOND END OF EXISTING SKIN TRIM OUT REPAIR. ROUTED OUT DAMAGE AND ACP HFEC INSP AND VERIFIED WEB PANEL CRACK FREE. WORK IS ACP ON NR 43674 AND INSP BY QC384.

Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 61,806 hrs · 22,748 cycles

NR 2 NACELLE STRUT OB SIDE SKIN AT THRUST REV HINGE AREA, AFT LIGHTNING HOLE AT 1:30 POS, ONE CRACK IN SKIN EXTENDING APPROX .185" BEYOND END OF EXISTING SKIN TRIM OUT REPAIR. ROUTED OUT DAMAGE. ACP HEFC INSP AND VERIFIED CRACK FREE ON WEB PANEL.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 60,934 hrs · 22,411 cycles

AFTER INSTALLATION OF NEW DOOR 1R SLIDE UNABLE TO ENGAGE GIRT BAR IN TRACK. NEW SLIDE REJECTED DUE TO GIRT BAR MATERIAL NOT FORMED AROUND GIRT BAR. THIS FORCES THE GIRT BAR TO RISE UP, RUBBING AGAINST CONTROL ROD. DID NOT HAVE A SECOND SLIDE ASSY IN SEA, RE-INSTALLED ORIGINAL SLIDE: DASH 1024 AT DOOR 1R. INSPECTED INSTALLATION OF SLIDE AND FOUND OKAY. REPLACED FAULTY DOOR 1R SLIDE THE FOLLOWING DAY. VERIFIED INSTALLATION OF SLIDE AND PINS REMOVED.

Part: UNKNOWN — ODOR (CABIN) · airframe 60,920 hrs · 22,404 cycles

PAX AT ROW 24 REPORTED SLIGHT ELECTRICAL SMELL, CONFIRMED BY F/A. NO SMOKE NOTICED. SMELL WENT AWAY AFTER SWITCHING CEILING LIGHTS OFF. OPERATED ALL CABIN LIGHTS, VIDEO PROJECTORS, AND SEAT PES SYSTEMS, AND READING LIGHTS IN AREA OF ROW 24. NO SMELL NOTED. COULD NOT DUPLICATE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,541 hrs · 21,876 cycles

NR 2 RT MAIN DOOR EXTERIOR EMERGENCY EXIT EVACUATION LIGHT INOP. RELAMPED WITH LAMP NR 767.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,074 hrs · 21,696 cycles

AFT FWD LAV EEL STRIP INOP. REPLACED EEL LIGHT STRIP, OPS CHECK NORMAL.

Part: IDG — INOPERATIVE (NR 1) · airframe 57,171 hrs · 20,960 cycles

LT GEN DRIVE LIGHT. RTFL. FOUND FAULTY IDG. INSTALLED NEW NR 1 IDG. ACCOMPLISHED OPS CHK & LEAK CHECK. ALL CHECKS GOOD. OK FOR SERVICE.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 56,935 hrs · 20,869 cycles

CREW REPORTED EMERGENCY FLOOR LIGHTING LAST 2 FEET AFT CABIN INOP. *S/D* EEL DISCONNECTED AT STRIP. RECONNECTED LIGHT STRIP, OPS NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 56,640 hrs · 20,768 cycles

EEL'S RIGHT SIDE BY DOOR 1R, OVER DOOR 1R AND CTR, EXIT BETWEEN 1ST CLASS AND ECONOMY, EEL ABOVE SEAT 14C ARE INOP. LOOSE CONNECTOR. SECURED CONNECTOR FOR POWER SUPPLY FOR EMERGENCY EXIT SIGNS AT DOOR 1R AND CTR AND TEST, FOUND GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,180 hrs · 19,494 cycles

DENT AT APPROX STA 630 LT APPROX 2' BELOW WINDOW. ACCOMPLISHED A MAJOR REPAIR AT DEN. THIS IS A CAT B RPR AND REQUIRES SUPPLEMENTAL INSP TO BEGIN AT 37500FC. 5 CF ITEMS BEING CREATED TO ACP THIS TASK PER EVA 71659 CREATED CF9049, CF9050, CF9051, CF9052 AND CF 90 53 FOR THE SUPPLEMENTAL INSPECTIONS STARTING AT 37,500FC CURRENT PTC IS 20618. INSP TO BEGIN IN 16882FC.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,638 hrs · 20,767 cycles

EXTERNAL FWD OVERWING EMERGENCY EXIT LIGHT INOP RT. LAMP INOP. RELAMPED EXIT LIGHT ASSY, OPS CHECKED NORMAL.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 56,638 hrs · 20,767 cycles

K-LAV SMOKE DETECTOR IS INOPERATIVE. SMOKE DETECTOR IS INOP. REPLACED K LAV SMOKE DETECTOR. OPS CHECKED NORMAL.

Part: CONNECTOR — DEFECTIVE (SMOKE DETECTOR) · airframe 56,638 hrs · 20,767 cycles

LOCK MISSING FOR S LAV SMOKE DETECTOR CONNECTOR (P15). REPLACED P15 CONNECTOR ON S LAV SMOKE DETECTOR, OPS CHECKS GOOD.

Part: WIRE — SHORTED (COCKPIT) · airframe 56,638 hrs · 20,767 cycles

FIRST OBSERVER'S MASK P/A DOES NOT TRANSMIT. WIRE SHORT. REPLACED FIRST OBSERVERS O2 MASK STOWAGE BOX, OPS CHECK GOOD.

Part: FRAME — BENT (FUSELAGE) · airframe 56,638 hrs · 20,767 cycles

AFT CARGO FRAME BENT STA 1400, STR 26L TO 27L. ACCOMPLISHED MAJOR REPAIR AT GSO-RPR DAMAGE FRAME IAW SRM 53-00-07 REPAIR 5 DETAIL I. THIS REPAIR IS A CAT B REPAIR IN ZONE 3 AND REQUIRES SUPPLEMENTA L INSPECTIONS STARTING IN 12,000 FLT CYCLES AND 11,000FC THEREAFTER THIS INSP CONSISTS OF BOTH DETAIL VISUAL AND NDT. CURRENT P TC IS 20618.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,638 hrs · 20,767 cycles

AFT CARGO FRAME DENTED STA 1420, STR 27L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA OF FRAME INBOARD FLANGE. FORMED AND INSTALLED A REPAIR ANGLE.

Part: CABLE — BINDING (EVAC SLIDE) · airframe 56,638 hrs · 20,767 cycles

RT OVERWING SLIDE BACK UP CABLE IS BINDING. CABLE OUT OF POSITION. PROPERLY RE-ROUTED CABLE TO PRESSURE BOTTLE SUPPORT SHROUD AND OPS CHECK GOOD AND REINSTALLED CLEVIS PIN TO MASTER CONTROL VALVE.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,638 hrs · 20,767 cycles

AFT CARGO FRAME DENTED STA 1540, STR 26L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF INBOARD FLANGE. FORMED & INSTALLED REPAIR ANGLE.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,638 hrs · 20,767 cycles

CABIN, JUST FWD OF L-2 DOOR CUTOUT, STR 12 CHORD SHOWS EVIDENCE OF CRACK JUST BELOW RADIUS BLOCK. MAJOR REPAIR ACCOMPLISHED: REMOVED INTERCOSTAL WEB. FORMED & INSTALLED NEW INTERCOSTAL WEB (P/N 143N8334-27).

Part: FRAME — DENTED (FUSELAGE) · airframe 56,638 hrs · 20,767 cycles

AFT CARGO FRAME DENTED STA 1520, STR 26L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR.

Part: STRUCTURE — CORRODED (L4 DOOR) · airframe 56,638 hrs · 20,767 cycles

L4 DOOR HANDLE BOX HAS CORRODED INSERTS ON TOP OF BOX. INSTALLED NEW HANDLE BOX PER UAL SM 50-52-11-06-JD.

Part: DOOR FRAME — DAMAGED (L2 DOOR) · airframe 56,638 hrs · 20,767 cycles

L2 DOOR REQUIRES REPAIR DOUBLER AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 56,638 hrs · 20,767 cycles

R2 DOOR UPPER HINGE CUTOUT CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED FRAME REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,638 hrs · 20,767 cycles

AFT PIT FRAME TOP CHORD BENT OVER STA 1440, STR 27L. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE. INSTALLED FRAME REPAIR.

Part: WIRE — CORRODED (NR 2 PYLON) · airframe 56,638 hrs · 20,767 cycles

NR 2 PYLON HAS SEVERAL CORRODED WIRES AT GROUND STUD LOCATION SHEARED FROM GROUND. RE-TERMINATED WIRES IAW BSW PM 20-30-11.

Part: GIRT BAR — BENT (L1 DOOR) · airframe 56,162 hrs · 20,589 cycles

DOOR 1L DOES NOT DISARM. FOUND GIRT BAR ASSY BENT/DAMAGED. REPLACED GIRT BAR ASSY AND DOOR ARMS/DISARMS NORMALLY.

Part: LIGHT — INOPERATIVE (ROW 23) · airframe 54,861 hrs · 20,109 cycles

EEL LIGHT INOP AT ROW 23. INSTALLED NEW EMERGENCY LIGHT SECTION.

Part: ASPIRATOR — CRACKED (ESCAPE SLIDE)

ASPIRATOR CRACKED. REPLACED ASPIRATOR.

Part: OVERHEAT SYS — NO TEST (COCKPIT) · airframe 54,555 hrs · 20,002 cycles

RIGHT ENGINE OVERHEAT DOES NOT TEST.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 53,922 hrs · 19,786 cycles

EEL LIGHT RIGHT WING EXIT DOOR INOP. REPLACED LIGHT ASSY.

Part: BEARING — LEAKING (ENGINE) · airframe 53,882 hrs · 19,772 cycles

OIL ODOR IN CABIN. ON TROUBLE SHOOTING FOUND ODOR COMING FROM RT PACK WITH NR 2 ENGINE BLEED ON. SUSPECTED SKYDROL SMELL IN CABIN AFTER FINDING LEFT HYDRAULIC SYSTEM OVER SERVICED., NO OIL FOUND IN DUCTS. AFTER FURTHER TROUBLE SHOOTING, CONFIRMED NR 2 ENGINE HAD SMALL AMOUNT OF OIL SEEPAGE FROM NR 3 BEARING COMPARTMENT. ENGINE REMOVED AND ROUTED TO ENGINE SHOP FOR REPAIR. RAN ENGINES AT POWER. ACCOMPLISHED A/C PACK BURNOUT, NO ODOR NOTED AFTER PACK BURNOUT, REPLACED BOTH RECIRCULATION FILTERS.

Part: IDG — MALFUNCTIONED (NR 1) · airframe 53,750 hrs · 19,717 cycles

EICAS MSG LT GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONNECTED. [08-08-07] RED DPI POPPED ON IDG. APU OIL SVC'D TO FULL. REPLACED NR 1 ENG IDG.

Part: BEARING — FAILED (NR 1 GEARBOX) · airframe 53,027 hrs · 19,432 cycles

FLIGHT DIVERTED DUE TO IFSD OF NR 1 ENGINE. [SUP 05-24-07] THIS OCCURRENCE WAS DUE TO ANGLE GEARBOX BEARING FAILURE CAUSED BY EXCESSIVE VIBRATORY STRESS. THIS IS BELIEVED TO HAVE BEEN THE RESULT OF AN IMPROPER BALANCING OF THE LOWER TOWER SHAFT WHICH COULD HAVE OCCURRED DURING INITIAL STAGE OF MANUFACTURE BY THE OEM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,996 hrs · 19,061 cycles

SIDEWALL EMERGENCY EXIT LIGHTS AT DOOR 2L, 2R AND OVERDOOR EMERGENCY LIGHT AT DOOR 2L INOP. REPLACED BATTERY PACK AT M733.

Part: SLIDE — UNSERVICEABLE (BOTTOM TUBE) · airframe 49,228 hrs · 18,210 cycles

BOTTOM INFLATION TUBE HAS A HOLE IN EXCESS OF 1 INCH WHICH WOULD NOT PASS AR TEST. SLIDE WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. SLIDE FAILED AIR RETENTION TEST DUE TO HOLE IN INFLATABLE LOWER TUBE. IT WAS OBSERVED THAT SLIDE HAD BEEN PACKED CORRECTLY. EXACT CAUSE OF THE WEAR DAMAGE COULD NOT BE DETERMINED. DAMAGE WAS REPAIRED BY PATCHING PER AIR CRUISERS CMM 25-60-46.

Part: SLIDE — UNSERVICEABLE (ASPIRATOR) · airframe 49,228 hrs · 18,210 cycles

ASPIRATOR VALVES LEAKING. SLIDE WAS REMOVED FROM AIRCRAFT AT NORMAL MAINTENANCE INTERVAL. ASPIRATOR FLAPPER VALVE WAS OBSERVED LEAKING DURING SLIDE OVERHAUL AIR RETENTION TEST. SPECIFIC CAUSE OF LEAK WAS NOT DETERMINED. ASPIRATOR WAS REPLACED.

Part: TOILET — INOPERATIVE (LAVATORY) · airframe 45,253 hrs · 16,601 cycles

DIVERTED DUE TO LAVATORY FLUSH SYSTEM INOPERATIVE. CAUSED BY CLOG / BLOCKAGE IN PLUMBING. SERVICED LAVATORIES, ALL OPS NORMAL. NO FLUID SPILLAGE NOTED.

Part: SKIN — DENTED · airframe 37,639 hrs · 13,842 cycles

EXTERNAL FUSELAGE SKIN DENTED AT LOWER EDGE OF AFT CARGO PIT DOOR CUTOUT STATION 1427 SKIN LAYERS ALSO DISBONDED. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TRIPLER REPAIR INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,639 hrs · 13,842 cycles

CABIN FLOORBEAM STA 365 RBL 18 MATERIAL REMOVED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. CABIN FLOORBEAM UPPER CAP REPLACED.

Part: CREASE BEAM — CORRODED · airframe 37,639 hrs · 13,842 cycles

RIGHT HAND CREASE BEAM IN FLOOR BELOW SUPPORT ANGLE AT BODY STATION 837 RBL 63 UPPER SURFACE CORRODED AT NUT PLATE HOLE. MAJOR REPAIR ACCOMPLISHED. CREASE BEAM DOUBLER REPAIR INSTALLED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,639 hrs · 13,842 cycles

CABIN FLOOR SUPPORT AT STATION 395-418, BL 0, WL 208 CORRODED. MAJOR REPAIR ACCOMPLISHED. CABIN FLOOR SUPPORT REPLACED.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,639 hrs · 13,842 cycles

LEFT HAND FUSELAGE HAS SEVERAL DENTS BETWEEN STATION 600 AND 620 ON AND BELOW STRINGER 16L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: FLOOR SUPPORT — WORN (FUSELAGE) · airframe 37,639 hrs · 13,842 cycles

CABIN FLOOR SUPPORT IS WORN AT STATION 365 RBL 46. MAJOR REPAIR ACCOMPLISHED. CABIN FLOOR SUPPORT AT STATION 365 RBL 46 WAS REPAIRED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,639 hrs · 13,842 cycles

CABIN FLOOR SUPPORT IS CORRODED AT STATION 365 RBL 26. MAJOR REPAIR ACCOMPLISHED. CABIN FLOOR SUPPORT AT STATION 365 RBL 26 WAS REPAIRED.

Part: STRINGER — DENTED · airframe 37,639 hrs · 13,842 cycles

LEFT HAND FUSELAGE STRINGER 16L AT STATION 600 TO 620 DENT OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. STRINGER SPLICED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,639 hrs · 13,842 cycles

CABIN FLOORBEAM STATION 1640, RBL15-53R, WL208 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED T-CAP.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 37,639 hrs · 13,842 cycles

AFT FUSE STATION 1830 AT STRINGER 20R WAS PUNCTURED. STRINGER 20R WAS ALSO CRACKED. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN DOUBLER INSTALLED. STRINGER SPLICED WAS INSTALLED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,639 hrs · 13,842 cycles

CABIN FLOOR CREASE BEAM AT STATION 410, LBL 72, WL 208 CORRODED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,265 hrs · 12,286 cycles

EXTERNAL FUSELAGE DENTED-CREASED AT FUSELAGE STATION 560 BETWEEN STRINGER 26LT AND STRINGER 26. SUPPLEMENTAL DATA UPDATE DAMAGE WAS CUTOUT IN THE LOWER SKIN MEASURING 5.5 LONGITUDINALLY BY 14.25 CIRCUMFRENTIALLY, SPANNING FROM THE S-26L LAP SEAM TO ONE FASTENER ROW INBOARD OF S-28L. DAMAGE REMOVAL TO THE UPPER SKIN RESULTED IN A CUTOUT MEASURING 2.75 LONGITUDINALLY BY 1.75 CIRCUMFRENTIALLY. THE REPAIR INCLUDED A STRUCTURAL FILLER/DOUBLER BUTT AGAINST THE LOWER SKIN, AND A TRIPLER OVER THE UPPER AND LOWER SKIN. THE TRIPLER EXTENDS THREE ROWS BEYOND CUTOUT IN THE LOWER SKIN. THE DOUBLER EXTENDS ONE ROW BEYOND THE TRIPLER ON THE FORWARD, AFT, AND LOWER EDGE.

airframe 32,839 hrs · 12,128 cycles

DOOR 1L OPENED WITH SLIDE ARMED, DOOR STOPPED LESS THAN HALF WAY OPEN. CHAINS ON BOTTOM OF SLIDE RESTRAINED DOOR FROM OPENING FURTHER.

Part: ENGINE — FAILED (NR 2)

RETURNED TO LAX DUE TO A NR 2 ENGINE VIBRATION. FOUND METAL IN THE TAIL PIPE AND THE ENGINE WAS REPLACED. SHOP FINDINGS WERE A FAILED 4TH STAGE LPT VANE. CAUSE WAS HEAVY SULFIDATION, AND PARTS WERE RETURNED TO PWA FOR INVESTIGATION.

Part: ENGINE — BIRD STRIKE (LEFT)

RETURNED TO FIELD DUE TO A BIRD STRIKE IN THE LEFT ENGINE.