N209UA

Part: ENGINE — BIRD INGESTION (NR2) · airframe 101,516 hrs · 12,191 cycles

BIRD STRIKE FOUND ON ENG #2. ACCOMPLISH BIRDSTRIKE INSPECTION AS PER AMM 72-00-00-210-808-N02 (601) AND CONDITIONAL INSPECTION AS PER AMM 05-51-18-210-801 (201). BIRDSTRIKE FOREIGN OBJECT DAMAGE INSPECTION CARRIED OUT PER AMM 72-00-210-808-NO2, BIRD REMAINS REMOVED FROM CORE AND BYPASS AREA. INSPECTED LP COMPRESSOR BLADES AND VANES AND FOUND BIRD DEBRIS BUT NO DAMAGE. BOROSCOPE INSPECTION CARRIED OUT OF HPC STAGES 5,6 AND 10 REF AMM 72-00-000-290-833-N02. NO DAMAGE OR DEBRIS NOTED. ENGINE RUN CARRIED OUT AND ALL PERAMETERS NORMAL WITH NO BIRD SMELL FROM ENGINE BLEED. BYPASS AND ACCESSABLE AREAS OF LP COMPRESSOR CLEANED, AND REQUEST PUT IN WITH TOMC TO SCHEDULE COMPR...

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 101,355 hrs · 12,170 cycles

DUE TO CAB LT MALF CYC CAB/UTIL SW AND EMER EXIT LTS ILLUM FOUND MX MSG 24-12045 "ELCU (UTIL BUS R) IN P200 IS NOT IN COMMANDED POSITION" LATCHED. FOLLOWED FIM 24-51 TASK 807. ACP'D ELMS POWER MANAGEMENT PANEL, P210 INITIATED EU SELF TEST PER AMM TASK 45-10-00-860-811. TEST PASSED. MSG NOT ACTIVE. VERIFED R UTILITY BUS POWERED, CABIN LIGHTS FUNCTIONS, EMERGENCY LIGHTS AND CACPS OPERATION OK FOR SERVICE.

Part: LOCK — FAULTED (ZONE 800) · airframe 100,939 hrs · 12,127 cycles

DOOR FLIGHT LOCK 1L EICAS STATUS #1 LEFT PASSENGER ENTRY DOOR FLIGHT LOCK COMMAND/FLT LK RLY/SENS OR DISAGREEMEN.DB PSEU 2 (R2) DB PSEU 2 (L2) STS MSG NOT ACTIVE,MAT DISPLAYS NO FAULT/MAINT MSG.DOOR OPENED AND CLOSED OK

Part: LENS — FAULTED (CALL LIGHT) · airframe 100,696 hrs · 12,103 cycles

EMERGENCY LIGHT 4R INOPERATIVE, EMERGENCY LIGHT AT DOOR 4R CHECKED NORMAL, ACTUAL DISCREPANCY WAS RJ DOOR LAVATORY CALL LIGHT STUCK, REPLACED CALL LIGHT LENS OPS CHECK NORMAL AT THIS TIME.

Part: SWITCH — OUT OF ADJUST (ZONE 800) · airframe 98,137 hrs · 11,813 cycles

DOOR FLIGHT LOCK 4R EICAS STATUS #4 RIGHT PASSENGER ENTRY DOOR FLIGHT LOCK COMMAND/FLT LK RLY/SEN SOR DISAGREEMENT. FIM TASK REF : FIM TASK REFERENCE NOT FOUND CMC MSG# 5211350 FLIGHT STATUS: I INTERMITTENCE CODE: I PH: CLIMB NARRATIVE: PSEU 2 (R2) CMC MSG# 5212290 FLIGHT STATUS: I INTERMITTENCE CODE: I PH: INITIAL CLIMB NARRATIVE: PSEU 2 (R2) FOUND A MIGRATED ROLL PIN IN THE FLIGHT LOCK PROXIMITY SENSOR MECHANISM CAUSING CONTACT WITH THE SENSOR SWITCH. ADJUST ROLL PIN POSITION TO CORRECT POSITION, CLOSED DOOR AND PRESSURIZED A/C TO 3.0 DIFFERENTIAL PRESSURE WITH NO EICAS MESSAGES. REF FIM 51-11 TASK 806.

Part: SWITCH — UNKNOWN (ZONE 200) · airframe 97,480 hrs · 11,738 cycles

CABIN EMER LTS CAME ON BY ITSELF 40 MIN OUT WENT OFF 10MIN LATER . PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS FLT DECK SWITCH REF MM TASK 33-51-00-720-801. ALL ADVISORY EICAS MSGS PRESENT AS REQUIRED. COULD NOT DUPLICATE AT THIS TIME. OK TO CONTINUE

Part: GIRT BAR — UNKNOWN (ZONE 800) · airframe 97,292 hrs · 11,715 cycles

GIRT BAR AT 4L WILL NOT ARM. CYCLED DOOR ARMING HANDLE AT 4L. OPERATES NORMALLY AND LOWER VIEWING INDICATOR WINDOWS ARE YELLOW WHEN ARMED.

Part: BATTERY — MALFUNCTIONED (L1 DOOR) · airframe 97,253 hrs · 11,709 cycles

L1 DOOR EMERGENCY LIGHT POWER PACK M33424 BATTERY FOUND MALFUNCTIONED. REPLACED L1 DO OR EMERGENCY LIGHT POWER PACK M33424 BATTERY AND C/O TEST OF THE NEW BATTERY PACK. THE RESULT FOUND NORMAL AS PER AMM 33-51-06-9 60-802 REV 102.

Part: BATTERY — MALFUNCTIONED (ZONE 200) · airframe 97,253 hrs · 11,709 cycles

R3 DOOR M33401 EMERGENCY POWER SUPPLY BATTERY FOUND MALFUNCTIONED. REPLACED R3 DO OR M33401 EMERGENCY POWER SUPPLY BATTERY AND C/O TEST OF THE NEW BATTERY PACK THE RESULT FOUND NORMAL AS PER AMM 33-51-06-960-80 2 REV 102.

Part: RELAY — FAILED (NR 2 ENG) · airframe 96,225 hrs · 11,598 cycles

ENG IGNITOR R2 STATUS MSG AWAITING TOMC APRVL TO DEF R ENG IGNITOR 2 PER MEL 7400D M-PROCEDURE C/W PLACARD INSTALLED TOMC APPROVES MEL 7400D DEF. RT ENG NBR 2 IGNITOR INOP PER MEL 7400D M-PROCEDURE C/W PLACARD INSTALLED *DM* REF. AIPC 74-11-21-02-01 ITEM 5 ADDING INGITER PLUG M&E 27-7421-3-0001 IN CASE NEEDED. ACPD MAT TEST ENGINE IGNITION TEST, NO AUDIBLE SPARK HEARD FROM R2 LOWER IGNITOR. RAN TEST AGAIN AND TAPPED ERU DURING TEST AND HAD INTERMITTANT SPARK, SUSPECT BAD ERU 27-7321-9-0002. PARTS ORDERING SHOWS NIS SFO, BUT 2 SERVICEABLE UNITS IN SFOPD PW4000 FLOWLINE. ENG 2 WIRES CHECKED GOOD FROM ERU CONNECTOR DM73005A TO IGN EXCITER 2 CONNECTOR DM74002. VERIFIED 115VAC AT PIN 9 AT DM 73005A WHEN START LEVER IN THE RUN POSITION. SUSPECT BAD ERU OR EEC. REF SSM 74-11-21-101.

Part: ENGINE — DAMAGED (NR 1) · airframe 94,795 hrs · 11,443 cycles

ENG 1 SURGED ON TAKEOFF, STARTED AT 1500FT, CLIMBED TO 3000 AND THROTTLED BACK, NOTED EGT WAS AT RED LINE, NO IFSD. CREW REPORTS 6-7 BANGS FELT AND HEARD AND AN EGT SPIKE, ENGINE STABLE AFTER ROLLING BACK THROTTLE. MAX EGT 673 FOR 7 SECS PER AHM. FOD OR EVIDENCE OF BIRD STRIKE FOUND. NO METAL PARTICLES OR MAINT MSG 75-41051. ALSO 2.9 STABILITY BLEED VALVE OUTLET SCREEN ALSO EGT COMPARISON CALCULATIONS INDICATE 2.9 STABILITY (LEFT THAN 60HOURS. EGT DEBRIS FOUND IN EXHAUST AND LP TURNS FREELY FOUND BROKEN. S VLV REPLACEMENT DUE TO SNAPSHOT VALVE SYSTEM DID NOT OPERATE CORRECTLY OVERTEMP VISUAL INSPS TO BE CARRIED OUT, DATA AND SCREEN DMG EGT SPIKE CONFIRMED TO BE WITHIN THE FIRST 5MINS OF TAKEOFF SNAPSHOTS SHOW ON EPCS L ENG, CH A, T2.95SB IND BLANK AND CH B AFTER CONSULTATION WITH TOMC AND REF TO POWERPLANT TEST ENG TEST NO.12 EGT PRINTOUTS FROM CH A..EPCS 1: 693. EPCS 2: PHASE AND REACHED 673 MAX, PER AMM 72-00-00-290-828-N02 FIG VERY HIGH . TCA T CH B ALSO BLANK. BOTH HAVE LONG REFERENCE TABLE, FIM 71-08 TASK 828 ENGINE CHECK NO. 12 - 2.9 517. EPCS 3: 514. EPCS 4: 475. EPCS 5: 646. DURING THIS TEST EGT 602/3, NO ACTION NECESSARY. AFTER CONSULTATION WITH TOMC AND THE HISTORY IN FAULT HISTORY ON MAT FOR MAINT MSGS 75-41061 AND BLEED VALVE SYSTEM CARRIED OUT. MAT TEST SHOWS EXCD RED TO ABOVE 690 FOR 7SECS. PER EGT OVERTEMP AMM FLIGHT CREW FEEDBACK FIM TASK 71-05 TASK 819.

Part: BATTERY PACK — FAILED (M33456) · airframe 92,923 hrs · 11,227 cycles

B777-33-3-7019 - DOOR 3L EMER LIGHT BATT PACK (M33406) FAILED CAPACITY CHECK TRANSFER REF HXWO 2448088 AND ORIGINATED BY EMP V920570 DOOR 3L EMER LIGHT BATT PACK (M33456) REPLACED AND TEST NORMAL AS PER AMM33-51-06 WORK ACCOMPLISHED BY MECHANIC V920571 INSPECTED BY V896963

Part: BATTERY PACK — FAILED (M33409) · airframe 92,923 hrs · 11,227 cycles

B777-33-3-7019 - DOOR 4R EMER LIGHT BATT PACK (M33409) FAILED CAPACITY CHECK TRANSFER REF HXWO 2448095 AND ORIGINATED BY EMP V920570 DOOR 4R EMER LIGHT BATT PACK (M33409) REPLACED AND TESTED NORMAL AS PER AMM 33-51-06 WORK ACCOMPLISHED BY MECHANIC V920569 AND INSPECTED BY V896963

Part: ENGINE — DAMAGED (NR 2) · airframe 92,120 hrs · 11,120 cycles

RIGHT ENGINE EXCEEDED TEMP LIMITS ON TAKEOFF AFTER ROTATION. ENG 2 SHOWS ENG R EGT RED WITH MM 77-62122 DURING TAXI OUT. REF FIM TASK 71-05-00-810-833-N00.THE SUBJECT ENGINE HAD AN EXCEEDANCE DURING TAKEOFF WITH A PEAK EGT OF 701 DEGREES CELSIUS PER AHM EXCEEDANCE REPORT SNAPSHOT. PERFORM AMM TASK 72-00-00-290-828-N02 PARAGRAPH H. STEPS (1) GVI OF EXHAUST AREA, (2) & (3) HOT SECTION BSI PER TABLE 603. INSPECTION PROCEDURES AFTER OVERTEMPERATURE OPERATION. EXCEEDENCE SNAPSHOT PHOTO ADDED. VISUAL EXAMINATION OF THE IGNITION PLUG HIGH TENSION LEADS ACCOMPLISHED AND VERIFIED IDT INSP REQUIREMENT FOR E2 BORESCOPE AP8, AP10, AP11, AP12 AND CRANK PAD COVER INSTALLATION WITH NO DEFECTS NOTED AT THIS TIME. REF: AMM 72-00-00-290-824-N02, AMM 72-00-00-290-825-N02 AND AMM 72-00-00-840-805-N00. LOCKED FOR FERRY. UNLOCKING FOR INSP. LOCKED FOR MX. FERRY TO SFO. LOCKED. UNLOCKINIG FOR MX. INSTALLED & SAFETY WIRED AP8, AP10, AP11 & AP12 REF AMM 72-00-00-290-824-N01,72-00-00-290-825-N01. REINSTALLED N2 CRANK PAD COVER REF AMM 72-00-00-840-805-N00. CRANK PAD LEAK CKS GOOD ACCOMPLISHED BORESCOPE INSP OF E2 COMBUSTION CHAMBER, FUEL NOZZLES, HPT STG.1 VANES (AMM 72-00-00-290-834-N02), HPT STG.1 BLADES (AMM 72-00-00-290-835-N02), HPT STG. 2 BLADES (AMM72-00-00-290-835-N02 AND HPT STG. 3 BLADES AND VANES. PERFORMED COMPLIED WITH INSP ON #2 ENG PER AMM 72-00-00-290-828-N02 STEP H(1)(2). NO DAMAGE FOUND IN LPT EXHAUST AREA OR ON IGNITER CABLELEADS AND TERMINAL ENDS. INSP WILL UPDATE STEP H (3) ON FINDING OF BORESCOPE INSP. REMOVED BORO PLUGS AP8, AP10, AP11 & AP12 REF AMM 72-00-00-290-824-N01 & 72-00-00-290-825-N01 ALSO REMOVED CRANK PAD COVER REF AMM 72-00-00-980-807-N00 72-00-00-290-837-N02). UNLOCKED FOR MAINT.ESN 222308 REMOVED FROM AC 2809 REF JC 97-7100-1-9801. E2 ESN 222308 EGT EXCEEDANCE. DURING BORESCOPE INSP FOUND HPT STG. 1 BLADE T/E WITH BURNING AND ERROSION IN AREA E ONLY. RECORDS UPDATE. HC REVIEWED INTERVAL OF 1000 HRS OR 300 CYCLES, WHICH EVER COMES FIRST. REF: AMM 72-00-00-290-835-N02 STEP H-4(G) TABLE 623. PICTURES UPLOADED TO RVI WEBSITE. ERROSION IS IN AREA (E) T/E ONLY WITHIN LIMITS OF (0.040" TO 0.180"). ENGINE CAN CONTINUE IN SERVICE WITH REDUCED INSP ENG2 SN. 222308 (TSI= 4741) HPT T1 BLADE BURNING AND EROSION AT T/E (AREA "E") IS OKAY TO PUT ON REDUCED INSPECTION INTERVALS TO RE-CHECK EVERY 1000 HRS OR 300 CYCLES (RIR) WHICH EVER COMES FIRST AS PER AMM 72-00-00-290-835-N02 AND TABLE 623. CURRENT PTT/PTC IS 92116/1119. WHQLM-EMC ARSHAD. 21AUG23. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED RIR: 1000 FH OR 300 FC. SCHEDULED PARTS CHANGE M&E P/N: 27-7200-9-0001. IF S/N FOUND, REMOVE AND REPLACE. IF THE PART REPLACED REQUIRES AN RII, FLAG THE INSPECTION FIELD OF THIS LOG PAGE. IF SCHEDULED S/N NOT FOUND, VERIFY & DOCUMENT S/N'S IN ALL OTHER POSITIONS & CONTACT PLANNING FOR REASSIGNMENT. ESN 222308 REMOVED INSTALLED REF JC 97-7100-1-9801.

Part: SCREW — MISSING (PANEL 149BL) · airframe 89,995 hrs · 10,831 cycles

PDA 3 ONE SCREW MISSING ON FAIRING PANEL 149BL.REPORTED BY JCAB. FOUND PANEL NO DAMAGE.INSTALLED SCREW,CONDITION OK FOR SERVICE.

Part: BATTERY — LOW (DOOR 2L) · airframe 88,474 hrs · 10,584 cycles

EMERGENCY LIGHTING BATTERY PACK CAPACITY FUNCTIONAL CHECK FOUND DR 2L M33096 EMERGENCY LIGHT BATTERY PACK LOW CAPACITY - ORIGINA TED BY EMP V905400 ON HAECO NR 9475112, SPEC NO.B777-33-3-7030. PERFORMED BY EMP V924363, REPLACED DR 2L M33096 EMERGENCY LIGHT BATTERY PACK, AND PERFORMED THE LIGHT TEST, THE RESULT FOUND NOR MAL, REF AMM 33-51-06-960-802 REV 94.

Part: CHARGER — MALFUNCTIONED (LLAR) · airframe 88,474 hrs · 10,584 cycles

LLAR BACK-UP LIGHTS BATTERY PACK FUNCTIONAL CHECK FOUND THE BACK UP LIGHTS AND EXI SIGN NOT ILLUMINATED - ORIGINATED BY EMP V9054 00 ON HAECO NR 9474072, SPEC NO.B777-33-3-7024. PERFORMED BY EMP V903232, REPLACED LLAR BACK UP LIGHTS POWER SUP PLY ASSY, AND PERFORMED THE LIGHTS TEST, THE RESULT FOUND NORMAL , REF AMM 33-29-01-960-809 REV 94.

Part: BATTERY — LOW (DOOR 1L.) · airframe 88,474 hrs · 10,584 cycles

EMERGENCY LIGHTING BATTERY PACK CAPACITY FUNCTIONAL CHECK FOUND DR 1L M33903 EMERGENCY LIGHT BATTERY PACK LOW CAPACITY - ORIGINA TED BY EMP V905400 ON HAECO NR 9475113, SPEC NO.B777-33-3-7030. PERFORMED BY EMP V924363, REPLACED DR 1L M33903 EMERGENCY LIGHT BATTERY PACK, AND PERFORMED THE LIGHT TEST, THE RESULT FOUND NOR MAL. REF AMM 33-51-06-960-802 REV 94.

Part: SKIN — PUNCTURED (RH ELEV) · airframe 88,474 hrs · 10,584 cycles

RT ELEV HAS PUNCTURE, 29" FROM TE, 139" FROM OTBD AND .75 DIA. REF SRM 55-20-01-1A-1, SEALED WITH SPEED TAPE. LOCKING FOR MAINTENANCE FERRY. UNLOCKED TO CLEAR LOGPAGE PERFORMED BY EMP V902560 ON HAECO NR 9473850,RIGHT ELEVATOR OTBD REWORK MOMENT(MR)=0.088*12.5= +1.1 IN.LB. BALANCE CONDITION WITH AREA UPPER SURFACE DAMAGED AREA PERMANENT REPAIRED AS PER SRM 5 IN LIMIT. RII BY TA636,EMP NO.V903313. 5-20-01-2R-1 REPAIR 1 TABLE 201 PARA4.D AND SRM 51-70-04-2R-2 RE PAIR 2 REV 88.ADDER WEIGHT=40 GRAM(0.088LB),MOMENT ARM=12.5INCH, RII BY TA636, EMP NO.V903313

Part: BATTERY PACK — INOPERATIVE (L3 DOOR) · airframe 88,455 hrs · 10,581 cycles

EMERGENCY LIGHT BATTERY PACK INOP LOCATED ABOVE L3 DOOR FWD REMOVED EMERGENCY LIGHT BATTERY PACK P/N D717-01-100 S/N 57468 AND REPLACED WITH S/N 241619 LOCATED ABOVE L3 DOOR FWD REF 777-200 AMM 35-51-06 REV 93

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 86,005 hrs · 10,325 cycles

EMERGENCY LIGHT CAPACITY TEST FND 2L-3L 2R-3R FLOOR EMER LIGHT ILLUMINATE TIME LESS THAN 15 MIN SPEC NR B777-33-3-7019 REF NON-ROUTINE NR 9483889. REPLACED R2 DOOR THE EMERGENCY LIGHT POWER SUPPLY BATTERY PACK, AND PERFORMED THE TEST, THE RESULT FOUND NORMAL REF AMM 33-51-06-960-802 REV 86.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 86,005 hrs · 10,325 cycles

EMERGENCY LIGHT CAPACITY TEST FND 3R-4R FLOOR, AND CEILING EMERGENCY LIGHT ILLUMINATE TIME LESS THAN 15 MIN SPEC NR B777-33-3-7019 REF NON-ROUTINE NR 9483892. R4 DOOR REPLACED EMERGENCY LIGHT POWER SUPPLY CHARGER AND PERFORMED THE TEST, THE RESULT FOUND NORMAL REF A MM 33-51-06-960-803 REV 86.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 86,005 hrs · 10,325 cycles

EMERGENCY LT CAPACITY TEST FND L4 CEILING EMERGENCY LIGHT ILLUMINATE TIME LESS THAN 15 MIN SPEC NR B777-33-3-7019 REF NON-ROUTINE N O.9483874. REPLACED DR L4 THE EMERGENCY LIGHT POWER SUPPLY CHARGER AND BATTERY PACK, AND PERFORMED THE TEST. THE RESU LIGHT FOUND NORMAL. REF AMM 33-51-06-960-802 REV 86 & AMM 33-51-06-9 60-803 REV 86.

Part: WIRE — SHORTED (FWD GALLEY) · airframe 78,631 hrs · 9,490 cycles

ELECTRIC SHOCK FROM FWD GALLEY. WHEN THE CHILLER IS TURNED OFF, IN THE FIRST CLASS GALLEY SHOCK GOES AWAY. EMERGENCY DECLARED. FOUND WIRE INSULATION FOUR INCHES FROM COUNTER LIGHT SWITCH CAUSING SHORT TO STRUCTURE. REPAIRED THE WIRE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,536 hrs · 9,479 cycles

R4 DOOR BATTERY PACK M33408 CAPACITY LOW. R4 DOOR BATTERY PACK M33408 REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,536 hrs · 9,479 cycles

DOOR R1 M33094 BATTERY PACK CAPACITY LOW. DOOR R1 M33094 BATTERY PACK REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,536 hrs · 9,479 cycles

DOOR R3 M33401 BATTERY PACK CAPACITY LOW. DOOR R3 M33401 BATTERY PACK REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,536 hrs · 9,479 cycles

L4 DOOR BATTERY PACK M33407 CAPACITY LOW. L4 DOOR BATTERY PACK M33407 REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,536 hrs · 9,479 cycles

DOOR R4 BATTERY PACK M33409 CAPACITY LOW. DOOR R4 BATTERY PACK M33409 REPLACED AND TESTED NORMAL AS PER AMM 33-51-06.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 77,358 hrs · 9,355 cycles

A STRONG ODOR IN THE COCKPIT AFTER TAKEOFF TO 18,000 FT. SUSPECT AIR CONDITIONING CONTAMINATION. TROUBLESHOTING, NR 1 & 2 ENGINES RAN. C/O FIM 21 -00-00-810-808 STEP C. WITH APU AND ENGINES RUNNING, NO ODOR DETECTED DURING OPS ON GROUND. ACCOMPLISHED FIM, FOUND IT WAS AN INTERMITTENT FAULT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,585 hrs · 9,042 cycles

CEILING EMERGENCY LIGHT LOCATED NEAR SEAT ROW 39 IS NOT WORKING. REMOVED AND REPLACED LAMP - OPERATIONAL CHECKED NORMAL.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 70,496 hrs · 8,573 cycles

CABIN BS 1046 - 1200, LBL 11 SEAT TRACK OTBD FLANGE, FOUND SURFACE CHAFING. SURFACE CHAFING SMOOTHED OUT IAW SRM 51-10-02 & PROTECTED IAW SRM 51-20-01.

Part: POWERPACK — DEFECTIVE (CABIN) · airframe 61,464 hrs · 7,646 cycles

CABIN ZONE D EMERGENCY LIGHT FOUND DIM. RT NR 4 DOOR OVERHEAD POWER PACK M33409 REPLACED IAW AMM33-51-06.

Part: POWERPACK — WEAK (CABIN) · airframe 61,464 hrs · 7,646 cycles

CABIN R4 DOOR EMERGENCY LIGHT POWER PACK WEAK M33409. R4 DOOR EMERGENCY LIGHT POWER PACK M33409 REPLACED & OPERATIONS CHECKED CARRIED OUT IAW 33-51-06.

Part: FITTING — BENT (CARGO DOOR) · airframe 60,140 hrs · 7,512 cycles

AFT CARGO DOOR, LATCH RANGE PROXIMITY TARGET & FITTING IS BENT. REPLACED BENT DOOR SENSOR, TARGET BRACKET FITTING IAW IPC, 53-63-51-005, PG-10, ITEM-205 IN AFT PIT FWD, LOWER DOOR FRAME.

Part: CONNECTOR — LOOSE (NR 1 ENGINE) · airframe 59,866 hrs · 7,479 cycles

NR 1 ENG MEC CANNON PLUG DM76001 LOOSE AT BACK SHELL. REPLACED CANNON PLUG PCN 420-2120, J2 TO FMU IAW WDM 73-21-72. FOUND WIRES IDENT WITH NR S 1-17. OPERATIONS CHECKED OF THE FMU ENG NR 1 WILL BE OPERATIONS CHECKED ON ANOTHER WRITE UP.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 59,504 hrs · 7,442 cycles

EXTERNAL FUSELAGE SKIN HAS TWO DEEP SCRATCHES AT BS 437 ABOVE STRINGER 47L. AFTER BLENDING, THE SKIN THICKNESS WAS OUT OF LIMITS IAW SRM 53-00-01. REMOVED DAMAGE, MANUFACTURED DOUBLER & FILLERS & INSTALLED REPAIR IAW SRM 53-00-01 REPAIR 6. ALL FASTENER HOLES WERE NOT ZERO TIMED DUE TO EDGE MARGIN CONCERNS.

Part: PIN — DAMAGED (LT HORZ STAB) · airframe 59,504 hrs · 7,442 cycles

DURING LT HORIZONTAL STAB PIVOT PIN REPLACEMENT IAW COA 210 181, THE NEW PIVOT PIN WAS FOUND TO HAVE DAMAGED THREADS. REWORKED DAMAGED THREADS & MAG PARTICLE INSPECTED IAW ECRA 5510-02334. INSTALLED PIVOT PIN IAW COA 210181.

Part: MODULATING VALVE — FAULTY (FLIGHT DECK) · airframe 58,890 hrs · 7,371 cycles

FLIGHT DECK TRIM AIR VALVE DOES NOT MOVE IN AUTO OR MANUAL. REPLACED ZONE A, TRIM AIR MODULATING VALVE IAW AMM 21-61-02. TEST PASSED. PERFORMED LEAK CHECK. NO LEAKS DETECTED.

Part: IDG — FAULTED (NR 2) · airframe 58,890 hrs · 7,371 cycles

GENERATOR DRIVE RIGHT IDG FAULT (LOW INTERNAL OIL PRESSURE). ADVISORY MSG-2431552 LATCHED ER MODE REPLACED RT IDG.

Part: INSULATION — WORN (WIRE) · airframe 58,645 hrs · 7,341 cycles

NR 1 ENGINE IDG OIL IN LINE, TWO WIRES EXHIBIT INSULATION AND BRAIDED SHIELD WEAR AT TWO LOCATIONS ADJACENT TO OR AT EACH WIRE CLAMPS. CLAMPS WORN AS WELL. ACCCOMPISHED REPAIR IAW ECRA 2415 01009.

Part: INSULATION — DAMAGED (IDG WIRE) · airframe 58,645 hrs · 7,341 cycles

NR 1 ENGINE IDG WIRE BUNDLE EXHIBIT INSULATION DAMAGE. REPAIRED IAW ECRA 2415-01009.

Part: IGNITER — WARNING MESSAGE (LT ENGINE) · airframe 58,549 hrs · 7,331 cycles

DURING START, LT ENGINE SECOND START ATTEMPTED. ENGINE IGNITER L2 STATUS MESSAGE 74-61501. REPLACED EXCITOR, LEAD, AND IGNITOR, ENGINE STARTS NORMAL.

Part: RADIO — MALFUNCTIONED (COCKPIT) · airframe 58,434 hrs · 7,316 cycles

VHF RADIO TRANSMISSION PROBLEMS. CANNOT TRANSMIT ON LEFT BOOM MICROPHONE. HAND MICROPHONE OK. REPLACED CAPTAIN`S BOOM MICROPHONE, NO HELP. ASSOCIATED HAND MICROPHONE OPERATES NORMALLY. REPLACED CAPTAIN`S RADIO, OPS CHECKED NORMAL.

Part: IGNITER — INOPERATIVE (LT ENGINE) · airframe 58,468 hrs · 7,321 cycles

LEFT ENGINE FAILED TO IGNITE USING IGNITOR NR 2. STATUS MESSAGE 7461501 INACTIVE ES MODE. LOWER EICAS MESSAGE 74-6 1501. REPLACED EXCITER, CABLE AND IGNITER IAW MM 74-11-01,74-21-01,74-21-02, OPS TESTED OK.

Part: UNKNOWN — UNKNOWN (RT WINDSHIELD) · airframe 58,454 hrs · 7,318 cycles

EXPOSED METAL BOLT HEAD ELECTRIC CONNECTOR LOWER RT CORNER, RT WINDSHIELD. RIGHT WINDSHIELD LOWER RT CORNER BOLTHEAD COVER INSTALLED.

Part: LENS — BROKEN (CABIN) · airframe 57,941 hrs · 7,267 cycles

AFT GALLEY EMERGENCY LIGHT LENS BROKE LOWER RIGHT CORNER. REPLACED LIGHT ASSEMBLY, OPERATIONS NORMAL.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT ROW 9G) · airframe 57,873 hrs · 7,261 cycles

OXYGEN MASKS DROPPED 9G. MASKS STOWED AND SECURED CLOSE.

Part: WINDOW — CRACKED (CABIN) · airframe 57,777 hrs · 7,249 cycles

WINDOW INNER PANE HAS TWO CRACKS AT SEAT 35A. REPLACED INNER PANE ON WINDOW REVEAL ASSY AND OK.

Part: RADOME — ERODED (FUSELAGE NOSE) · airframe 57,484 hrs · 7,217 cycles

RADOME ERODED WITH POSSIBLE DELAMINATION. REPAIRED IAW SRM 53-10-72.

Part: MASK — UNKNOWN (CABIN) · airframe 56,989 hrs · 7,164 cycles

OXYGEN DEMO MASK AT 45C NEEDS REPLACING. REPLACED MASK-AY-DEMO OXYGEN.

Part: HOUSING — MISSING (AC PACK) · airframe 55,260 hrs · 6,972 cycles

LEFT PACK FAN INLET DIFFUSER HOUSING SUPPORT BRACKET EXITED PACK EXHAUST. REPLACED DIFFUSER HOUSING PER MM, OPS CHECK NORMAL AND LEAK CHECK OK.

Part: RIVET — LOOSE (ENGINE EXHAUST) · airframe 54,637 hrs · 6,901 cycles

LEFT ENGINE HAS LOOSE RIVET IN EXHAUST CONE AT 6 O'CLOCK POSITION ON DATA PLATE.

Part: PANEL — MALFUNCTIONED (ELECTRICAL SYS) · airframe 54,611 hrs · 6,898 cycles

ELMS P310 CHANNEL ONE, BUT NOT BOTH, OF THE ELECTRICAL LOAD MANAGEMENT SYSTEM (ELMS) 310 PANEL CHANNEL IS FAULTY. RPL- :GOT MSG 24-13092. REPLACED M24406A1 PER MM, OPS TEST NORMAL, NO STATUS MSG PRESENT.

Part: COUPLER — FAILED (HF SYSTEM) · airframe 54,504 hrs · 6,886 cycles

RT HF TUNING. DUE TO CHRONIC REPORTS OF RT HF RADIO WILL NOT TUNE, PERFORM THE FOLLOWING TASKS. COUPLER MR23167-10 WAS INSTALLED ON 8-26 AND HAD PREVIOUS HISTORY FOR SAME PROBLEM. PREVIOUS PROBLEM ON THIS AC WAS RECEPTION. TUNING PROBLEM ONLY APPEARED AFTER INSTALL OF THIS UNIT. REPLACED THE RT HF COUPLER IAW AMM 23-11-03. REPLACED RT HF COUPLER REF AMM23-11-03, OPS CHECKS NORMAL.

Part: TRANSCEIVER — FAULTY (HF COMM) · airframe 54,403 hrs · 6,874 cycles

HF SYSTEM FAILURE, RTFL HF COMM RT INOP. RADIO TUNES BUT NO VOX XMIT ORRCV. CYCLED C-B NO HELP. REPLACED RIGHT HF TRANSCEIVER PER MM. CONFIRMED REC-TRANSMIT FUNCTION RIGHT HF SYSTEM OPERATES NORMAL.

Part: TRANSCEIVER — FAULTY (HF COMM) · airframe 54,397 hrs · 6,873 cycles

HF COMM RT INOP. RADIO TUNES BUT NO VOX XMIT ORRCV. CYCLED C-B, NO HELP. REPLACED RIGHT HF TRANSCEIVER PER MM. CONFIRMED REC-TRANSMIT FUNCTION RIGHT HF SYSTEM OPERATES NORMAL.

Part: ENGINE — OVERTEMP (NR 1) · airframe 54,210 hrs · 6,848 cycles

LT ENGINE EGT EXCEEDANCE, IN AREA C, BEFORE NEXT FLIGHT ACCOMPLISH VISUAL CHECKS AND HOT SECTION BORESCOPE PER AMM 72-00-00. REPLACED NR 1 ENGINE.

Part: ENGINE — FAULTY (LEFT) · airframe 54,190 hrs · 6,845 cycles

REF L ENG EGT EXCEEDANCE. REPLACED NR 1 ENGINE IAW AMM 72-00-00 PAGE 623 CONFIG 2.

Part: CHARGER — FAULTY (APU) · airframe 52,866 hrs · 6,696 cycles

BATTERY CHARGER APU MESSAGE. REPLACED APU CHARGER AND BATTERY PER MM, CKS OKAY.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 52,656 hrs · 6,672 cycles

LLAR BACKUP LIGHT BATTERY FAILS CAPACITY CHECK. REF A CHECK JC 2-2018 ITEM 3 AND MM. REPLACED M023 BATTERY PACK POWER SUPPLY ASSY PER AMM. SYSTEM CHECKS NORMAL.

Part: CONNECTOR — FAULTY (CABIN) · airframe 52,132 hrs · 6,613 cycles

SIDE WALL LIGHTING CONNECTOR DM33084E LOCATED AT STA 1840 LBL 90, CONNECTOR IS NON COMPLIANT PER FCD 3321- 01019 REV C PG 32 STEP 8. REPLACED CONNECTOR DM33084E REF FCD 3321-01019. ACCOMPLISHED INSPECTION AS REQUIRED REF FCD 3321-01019.

Part: CONNECTOR — FAULTY (CABIN) · airframe 52,132 hrs · 6,613 cycles

LIGHTING HARNESS ON STR CLIP BETWEEN STA 1970 AND 1990 LT STR 12L CONNECTOR DM33036C INS NON-COMPLIANT PER FCD 3321-01019. NEED TO SEND OLD CONNECTOR TO SFOEG. REPLACED CONNECTOR DM33036C REF FCD 3321-01019.

Part: CONNECTOR — FAULTY (CABIN) · airframe 52,132 hrs · 6,613 cycles

LIGHTING HARNESS ON STR CLIP BETWEEN STA 1970 AND 1990 LT STR 12L CONNECTOR DM33036A IS NON COMPLIANT PER FCD 3321-01019 STEP 12 PG 34. REPLACED CONNECTOR DM33036A REF FCD 3321-01019. REPLACED CONNECTOR DM33036A REF FCD 3321-01019. ACCOMPLISHED INSPECTION AS REQUIRED REF FCD 3321-01019.

Part: CONNECTOR — FAULTY (CABIN) · airframe 52,132 hrs · 6,613 cycles

LIGHTING HARNESS LOCATED BETWEEN STA 1580 & 1601 STR 12R, CONNECTOR D5188P IS NON COMPLIANT PER FCD3321-0101 9 REV C PG 34 STEP 13. REPLACED CONNECTOR D5188P REF FCD3321-01019. ACCOMPLISHED INSPECTION AS REQUIRED REF FCD 3321-01019.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 52,132 hrs · 6,613 cycles

SIDEWALL LIGHT BALLAST CONNECTOR DM33084E WON'T LOCK AT 41ABC. REPLACED SIDEWALL LIGHT ASSY AT ROW 41ABC PER AMM, OPERATIONAL CHECK OK.

Part: CONNECTOR — FAULTY (CABIN) · airframe 52,132 hrs · 6,613 cycles

LIGHTING HARNESS LOCATED ON STR CLIP BETWEEN STA 1580 & 1601 STR 12R CONNECTOR D5188J IS NON COMPLIANT PER FCD 3321-01019 REV C PG 34 STEP 13. REPLACED CONNECTOR. ACCOMPLISHED INSPECTION AS REQUIRED REF FCD 3321-01019.

Part: CONNECTOR — IMPROPER PART (CABIN) · airframe 52,132 hrs · 6,613 cycles

LIGHTING HARNESS ON STR CLIP BETWEEN STA 1970 1990 LT STR 12L CONNECTOR DM33036B IS NON-COMPLIANT PER FCD 3321- 01019. NEED TO SEND OLD CONNECTOR TO SFOEG. REPLACED CONNECTOR DM33036B REF FCD 3321-01019.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 52,035 hrs · 6,599 cycles

F-O RT DISPLAY BLANK. SELECTOR PANEL INOP. REPLACED NR 2 AIMS DISPLAY UNIT PER MM.

Part: FUEL/OIL COOLER — LEAKING (NR 1 ENGINE) · airframe 51,238 hrs · 6,503 cycles

RETURN TO GATE DUE TO NR 1 ENGINE FUEL LEAK. FUEL OIL COOLER LEAKING FUEL FROM DRAIN MAST. TROUBLESHOT & RAN ENGINE 2X5 MIN IDLE TO INSPECT FOR LEAKS ON NR 11 DRAIN MAST NR 1 ENG. AFTER IDLE RUNS, CHECKED FOR LEAKAGE FOR OVER 5 MIN, AND NO DROPS NOTED ON NR 11 DRAIN MAST NR 1 ENGINE. PER MM OK FOR SERVICE.

Part: BATTERY — FAILED (CONTROLLER) · airframe 51,064 hrs · 6,480 cycles

ON ARRIVAL RECEIVED MESSAGE 24-50243, & STATUS MESSAGE FOR FLIGHT CONTROL SYS. PER FIM 24-35 TASK 802 CHK FOUND FCDC CENTER BATTERY IS BAD PER MM. REPLACED WITH NEW BATTERY, MSG GONE. OPERATION TEST FINE, NO FAULT FOUND.

Part: SEAL — DAMAGED (LT FLAPERON) · airframe 51,051 hrs · 6,479 cycles

LEFT FLAPERON SEAL DAMAGED AT T/E. FLAPERON REMOVED, REPLACED DAMAGED SEAL WITH NEW SEAL.

Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 51,051 hrs · 6,479 cycles

LEFT FLAP INBD TRAILING EDGE HAS DAMAGE. CUT OUT DAMAGE, POTTED IN REPLACEMENT CORE. REPAIRED WITH 250 DEGREE OVERLAY REPAIRS PER SRM.

Part: LINER — DELAMINATED (NR 2 NACELLE) · airframe 51,051 hrs · 6,479 cycles

NR 2 ENGINE EXIT LINER SEGMENT AT 7 O'CLOCK POSITION HAS WIRE MESH DELAMINATED FROM THE LEADING EDGE IN 2 LOCATIONS. REMOVED EXIT LINER AT 7 O'CLOCK POSITION PER MM. INSTALLED NEW SECTION OF LINER AND APPLIED SEALANT.

Part: SEAL — DAMAGED (BLEED AIR SYS) · airframe 50,805 hrs · 6,453 cycles

NR 2 ENGINE LT THERMAL INSULATION BLANKET DAMAGED FROM AIR LEAK. REPLACED DAMAGED BLANKET. REMOVED NR 2 ENGINE PRSOV. REPLACED SEALS AND RE-INSTALLED PRSOV, LEAK CHECKED GOOD.

Part: PRESSURE SWITCH — DAMAGED (NR 1 ENGINE) · airframe 50,805 hrs · 6,453 cycles

NR 1 ENGINE MAIN FUEL PUMP PRESS SWITCH ELECTRICAL CONNECTOR DAMAGED. REMOVED AND REPLACED NR 1 ENG FUEL PUMP DIFFERENTIAL SWITCH IAW MM. OPS AND LEAK NORMAL IAW MM.

Part: STARTER — DAMAGED (LT ENGINE) · airframe 50,643 hrs · 6,438 cycles

ENG START VALVE L LEFT STARTER AIR VALVE POSITION DISAGREES WITH COMMANDED POSITION OR STARTER AIR VALVE POSITION INDICATION IS LOST. STARTER ON LEFT ENGINE DAMAGED, METAL FOUND ON CHIP DETECTOR. REPLACED LEFT ENGINE STARTER PER AMM. MOTORED ENGINE. ALSO REPLACED LEFT ENGINE START VALVE. OPS NORMAL.

Part: LOCK — DEFECTIVE (CREW REST DOOR) · airframe 50,316 hrs · 6,402 cycles

CREW REST DOOR STUCK, UNABLE 2 OPEN. FCR DOOR LOCK IS DEACTIVATED IN UNLOCKED POSITION. DOOR OPENS & CLOSED NORMALLY. CAN BE USED. LOCK ASSY PART # 023-1394 OUT OF STOCK AT ORD.

Part: ELECTRICAL BOX — MALFUNCTIONED (REST SEAT) · airframe 50,193 hrs · 6,388 cycles

PILOT CREW REST SEAT INOPERATIVE. STUCK PARTIALLY RECLINED, RESET UNDERSEAT ELECTRONICS CONTROL BOX.

Part: STRUCTURE — LOOSE (DOOR FRAME) · airframe 50,064 hrs · 6,372 cycles

PILOT CREW REST AREA DOOR FRAME TRIM AT FWD BOTTOM IS STICKING OUT. SECURED TRIM WITH TAPE.

Part: FIRE LOOP — SHORTED (APU BAY) · airframe 50,024 hrs · 6,368 cycles

FIRE HANDLE WAS PULLED BY FLIGHT CREW DUE TO APU AUTO SHUT DOWN. BEFORE DEPARTURE APU AUTO SHUT DOWN, APU CONSIDERED INOPERATIVE. CREW PULLED HANDLE AND DISCHARGED FIRE EXTINGUISHER. REPLACED APU FIRE EXTINGUISHING BOTTLE AND SQUIB PER MM. BOTTLE PRESSURE SWITCH & BOTTLE SQUIB TESTS BOTH PASSED. REPLACED APU FIRE DET CARD PER MM. ALSO HAD MESSAGE 26-11230 (APU LOWER FIRE LOOP B SHORTED). REPLACED LOWER APU A&B LOOPS. MESSAGES CLEARED.

Part: PRECOOLER — CRACKED (NR 2) · airframe 49,772 hrs · 6,344 cycles

NR 2 ENGINE PRECOOLER CRACKED AT BOTTOM. COMPLETE INSTALLATION OF NR 2 PRECOOLER. INSTALLATION THRU ITEM G. NEED TO COMPLETE INSTALLATION FROM 3H TO END - ACCOMPLISHED.

Part: BATTERY — FAULTY (MAIN) · airframe 49,695 hrs · 6,335 cycles

MAIN BATT DISCHARGE EICAS ADVISORY MSG. EICAS MAINTENANCE PAGE INDICATES MAIN BATT VOLTAGE AT 24 VDC AND 11AMP DISCHARGE. REPLACED MAIN BATT AND MAIN BATT CHARGER.

Part: INTERFACE UNIT — FAULTY (LEFT) · airframe 49,694 hrs · 6,334 cycles

CREW REPORTS WITH NR 1 ENGINE OFF SITTING AT GATE N2 INDICATION FLUX'S BETWEEN 4.5 AND 5.5 PERCENT WITH EEC GRD POWER ON N2 READS 11.1 PERCENT. REST AIMS AND SWAPPED EDIU'S S/N 99080051 IS IN THE LT POSITION AND S/N 99076300 IS IN THE RT POSITION. WITH CREW ASSIST ENGINE HAS BEEN RUN, ALL INDICATION OPERATE - FUNCTION NORMAL. REVIEWED WITH SAMC & OPBLM.

Part: CHILLER — INOPERATIVE (GALLEY) · airframe 49,435 hrs · 6,304 cycles

CHILLER - INOPERATIVE 212. (LOCATION NOT DEFINED - CHK CABIN FORM FOR SPECIFIC LOCATIONS). CREW COMMENTS: FIRST CLASS CHILLER INOP MEALS WERE WARM. THE CHILLER DID NOT PRODUCE CHILLED AIR. NOTIFIED CATERING SERVICE TO PUT DRY ICE INTO FOOD CART. REPLACED FWD GAL OVERHEAD CHILLER PER MM. OPS CHECK OKAY.

Part: CONTROL UNIT — FAULTY (FUEL SYSTEM) · airframe 49,030 hrs · 6,259 cycles

FUEL QTY AND IMBALANCE GRIPE. ACPD DISCHARGE CHECK VLV. ND TO CONT TO ACP LOW LEVEL SCAVENGE SYSTEM, R&E'S ASSISTING. FUELED AC FOR HIGH LEVEL SCAVENGE CHECKS. CONT T-S. *DOR*. ACFT DROPPED OFF AT GATE WITH MSG FUEL PUMP CENTER RIGHT MSG, NO TIME SFO. REPLACED CENTER RIGHT OVERRIDE FUEL PUMP ECLU M28213 & CENTER RIGHT OVERRIDE FUEL PUMP PRESSURE SWITCH S28210. CHECKS GOOD. REPLACED FUEL QUANTITY PROCESSER UNIT (FQPU). ALL PART NUMBERS & FUEL QUANTITY INDICATIONS CHECK GOOD. NO FURTHER ACTION REQUIRED.

Part: STRIKER — MISSING (CREW REST DOOR) · airframe 48,889 hrs · 6,244 cycles

FLIGHT CREW REST DOOR LOWER STRIKER PLATE ROBBED. DOOR SECURED IN CLOSED POSITION PER MEL 2529B. REPLACED DOOR LOWER STRIKER.

Part: SWITCH — OUT OF POSITION (COCKPIT) · airframe 47,717 hrs · 6,118 cycles

EMERENCY LIGHTS ADVISORY ON EICAS. COCKPIT EMER SWX CONFIRMED OFF. FOUND ARMING DEVICE NOT IN THE CORRECT POSITION OF SWITCH IN FLIGHT DECK P5 OVERHEAD PANEL. SECURED ARMING DEVICE OVER TOGGLE SWITCH. EMERGENCY LIGHTS OPS CHECKED OKAY.

Part: IDG — FAILED (LT ENGINE) · airframe 47,463 hrs · 6,089 cycles

ELEC GEN DRIVE L LEFT IDG FAULT (LOW INTERNAL OIL PRESSURE). INSTALLED NEW IDG AT LT ENGINE. ACCOMPLISHED IDG TEST PER MM. OPS CHECK GOOD.

Part: SENSOR — FAULTY (RT TEMP) · airframe 47,441 hrs · 6,087 cycles

RIGHT ENG BLEED INOP, FLIGHT DIVERTED. REPLACED DUAL MAIN TEMP SENSOR AND MAT TEST PASSED. ACCOMPLISHED PNEU TEST AT ALL POWER SETTINGS, BLEEDS AND PACKS ON AND OFF AND NO OPERATIONAL PROBLEMS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,999 hrs · 6,041 cycles

DOOR 2R EXTERIOR EMERGENCY LIGHT INOP. RELAMPED, OPS GOOD.

Part: WINDOW — LEAKING (COCKPIT) · airframe 46,624 hrs · 5,986 cycles

CONTINUOUS LOUD AIR NOISE ON FIRST OFFICERS SIDE WINDOW. REPLACED RIGHT SIDE COCKPIT WINDOW SEAL PER MM. SEAL REPLACED. DUE TO REPEAT PILOT REPORTS OF WINDOW SQUEAL, AND SEAL WAS PREVIOUSLY REPLACED NEED TO REPLACE F/O SLIDING WINDOW. POSSIBLE ADJUSTMENT ISSUE, ADDED 5 CYCLES TO ITEM TO ALLOW OPS AFTER ADJUSTMENT. REPLACED RT SLIDING WINDOW. OPS AND INDICATIONS NORMAL.

Part: CONTROLLER — FAILED (ENG ANTI ICE) · airframe 46,534 hrs · 5,974 cycles

ON ACCT OF REPLACEMENT OF LT ENG ANTI-ICE VALVE, ACCOMPLISH A TEST (ENGINE RUNNING) OF THE ENGINE ANTI-ICE SYSTEM. ACCOMPLISHED ENGINE ANTI-ICE ENGINE RUNNING SYSTEM TEST. TEST FAILED MAINTENANCE MESSAGE 30-10-101. REPLACED EAI VALVE CONTROLLER HEATER. OPS NORMAL.

Part: CIRCUIT CARD — FAULTY (ANTI ICE SYS) · airframe 46,534 hrs · 5,974 cycles

CARD ASSY-AIRFOIL AND COWL ICE NEEDS REPLACEMENT. REPLACED CARD ASSY.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 46,522 hrs · 5,973 cycles

EAI VALVE LEFT ENGINE ANTI-ICE (EAI) VALVE FAILURE. STATUS MSG01- LATCHED DESCENT MODE DEPENDENT; ENGINE ANTI-ICE VALVE (LT) IS FAILED IN CLOSED POSITION. DB- ACIPS CONTROL CARD, LT (L EAI CARD) MSG-3010101 LATCHD DC MODE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,997 hrs · 5,911 cycles

EXTERIOR EMERGENCY LIGHT INOP AT DOOR 3L. RELAMPED. OPS GOOD.

Part: BUTTON — STUCK (CONTROL PANEL) · airframe 45,921 hrs · 5,901 cycles

FIRST OBSERVERS AUDIO PANEL MIC BUTTON STUCK. PANEL FOUND DEFECTIVE. REPLACED FIRST OBSERVER'S AUDIO CONTROL PANEL. OPS NORMAL.

Part: HEATER — INOPERATIVE (CREW REST AREA) · airframe 45,305 hrs · 5,842 cycles

LOWER F/A CREW REST AREA TEMPATURE CONTROL PANEL DOES NO RESPOND TO SELECTED TEMPERATURE. NR1 HEATER INOP. REPLACED NR1 HEATER IAW MM, OPS NORMAL.

Part: CONTROLLER — INOPERATIVE (WINDOW HEAT) · airframe 45,144 hrs · 5,826 cycles

AFTER T/O ECIAS MESSAGE, WINDOW HEAT LT FWD, FOLLOWED CHECKLIST. NO HELP. FOUND AFTER TEST OF WINDOW HEAT CONTROLLER INTERNAL FAULT CODE 304 011 41, 304 012 41 REPLACED CONTROLLER SWAPPED LT FOR RT, OPS CHECKS GOOD.

Part: WIRE HARNESS — FAULTY (EMERGENCY LIGHTS) · airframe 45,047 hrs · 5,818 cycles

EMERGENCY LIGHTS DO NOT OPERATE AT SEAT 3F. REPAIRED HARNESS IN AFT SEAT LIGHT. OPS CHECKS NORMAL.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 45,016 hrs · 5,814 cycles

TOP OF FLAP HAS SMALL GOUGES APPROX CENTER OF FLAP TOWARD LEADING EDGE RT OUTBOARD TRAILING FLAP. REPAIRED DAMAGE.

Part: TRANSCEIVER — FAILED (NR 2 RADIO) · airframe 44,627 hrs · 5,763 cycles

F-O RADIO ALL DASHES IN WINDOW. TRANSCEIVER FAILED TESTING. REPLACED TRANSCEIVER. OP CK'S OKAY.

Part: TERMINAL BLOCK — BROKEN (CABIN LIGHTS) · airframe 44,615 hrs · 5,762 cycles

TERMINAL BOARD ASSY BROKEN AT M2 GALLEY. TERMINAL BOARD ASSY IS FAULTY. REPLACED WITH NEW BOARD, TESTS OKAY.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 44,612 hrs · 5,761 cycles

EMERGENCY POWER SUPPLY M33400 DOES NOT KEEP EMER LIGHTS ILLUMINATED AT DOOR 3L. POWER SUPPLY IS NOT SUFFICIENT. REPLACED EMERGENCY POWER SUPPLY, TESTS OKAY.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 44,612 hrs · 5,761 cycles

EMERGENCY POWER SUPPLY M33409 DOES NOT KEEP EMERGENCY LIGHTS ILLUMINATED AT DOOR 4R. POWER SUPPLY IS UNRELIABLE. REPLACED POWER SUPPLY. OP ARE NORMAL.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 44,612 hrs · 5,761 cycles

EMERGENCY POWER SUPPLY M33099 DOES NOT KEEP EMERGENCY LIGHTS ILLUMINATED AT DOOR 2L. POWER SUPPLY DEFECTIVE. REPLACED EMERGENCY POWER SUPPLY. TESTS OKAY.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 44,612 hrs · 5,761 cycles

EMERGENCY POWER SUPPLY M33096 DOES NOT KEEP EMER LIGHTS ILLUMINATED AT DOOR 2L. POWER SUPPLY IS FAULTY. REPLACED EMERGENCY POWER SUPPLY. TESTS OKAY.

Part: GENERATOR — CORRODED (NR 1) · airframe 44,612 hrs · 5,761 cycles

APU GENERATOR HOUSING FWD SECTION CORROSION. REPLACED WITH NEW APU GENERATOR, TESTS OKAY.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,612 hrs · 5,761 cycles

SEAT 2EF, EMERGENCY LIGHT INOP. REPLACED INVERTER ASSY, OP CHECKS GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 44,612 hrs · 5,761 cycles

EMERGENCY LIGHTS BROKEN AT MID GALLEY. REPLACED LIGHTS. OP CHECKS GOOD PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 44,612 hrs · 5,761 cycles

EMERGENCY LIGHT BROKEN AT MID GALLEY. REPLACED WITH EMERGENCY LIGHT AND TESTS OKAY. THE WORK IS ACP BY AMECO.

Part: LIGHT — CRACKED (CABIN) · airframe 44,612 hrs · 5,761 cycles

TWO (2) EACH EMERGENCY EXIT LIGHTS CRACKED AT NR 4 LT DOOR. REPLACED LIGHTS IAW MM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 44,612 hrs · 5,761 cycles

EMERGENCY POWER SUPPLY M33094 DOES NOT KEEP EMERGENCY LIGHTS ILLUMINATED AT DOOR 1R. REPLACED POWER SUPPLY IAW MM. OP CHECK GOOD.

Part: RESERVOIR — LOOSE (L1 DOOR) · airframe 44,612 hrs · 5,761 cycles

DOOR 1L EPAS RESERVOIR PRESS GAUGE IS LOOSE. INSTALLED NEW EPAS RESERVOIR.

Part: TRANSDUCER — INOPERATIVE (THRUST REVERSER) · airframe 44,353 hrs · 5,737 cycles

ENG REV L EICAS. NR 1 REV INOPERATIVE. REPLACED RT SLEEVE RVDT(M7 8003) PER AMM. RT RVDT CHECKS GOOD. CONFIRMED LT SLEEVE RVDT (M78002) IS DEFECTIVE. NEW RVDT IS NOT AVAILABLE. REPLACED NR 1 ENG LT SLEEVE POS RVDT, OP TEST TR, NO FAULT.

Part: CHARGER — FAULTY (MASTER BATTERY) · airframe 44,232 hrs · 5,720 cycles

ENROUTE MAIN BATTERY CHARGER SHOWED 55AMP 29V FOR 1 HR THEN DROPPED TO 5 AMPS 28V. REPLACED MAIN BATTERY CHARGER.

Part: BATTERY — FAULTY (MASTER) · airframe 44,230 hrs · 5,719 cycles

MAIN ACFT BATTERY CHARGING AT 5-6AMPS-INDICATING 27V-NOT TAKING CHARGE. REPLACED MAIN BATTERY. CHECKS OK, NO MESSAGES.

Part: WIRE HARNESS — MISSING (CABIN) · airframe 43,799 hrs · 5,676 cycles

FOUND ARM HARNESS AT FORWARD LAMP ASSY CONNECTOR MISSING. NEEDS HARNESS AND 2 LAMPS. REPLACED HARNESS AND LIGHT ASSEMBLIES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,592 hrs · 5,657 cycles

EXTERIOR EMERGENCY LIGHT JUST AFT OF NR 3 LT ENTRY DOOR IS NOT WORKING. RELAMPED.

Part: TERMINAL BLOCK — BROKEN (EMERGENCY LIGHTS) · airframe 43,592 hrs · 5,657 cycles

TERMINAL BLOCK FOR EMERGENCY LIGHTS AT GALLEY AT DOOR 2R BROKEN. REPLACED TERMINAL BLOCK. OPS CHECKED EMERGENCY LIGHTS AT GALLEY. OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,294 hrs · 5,620 cycles

EMERGENCY LIGHT AT SEAT 39C IS INOPERATIVE. REPLACED LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,294 hrs · 5,620 cycles

FWD EMERGENCY LIGHT AT SEAT 11F IS INOP. REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,294 hrs · 5,620 cycles

EMERGENCY LIGHT AT SEAT 41G IS INOP. REPLACED LIGHT ASSY.

Part: PACKING — LEAKING (LT WING) · airframe 43,259 hrs · 5,616 cycles

FUEL LEAKING FROM WING PANEL 552HB. FOUND FUEL LEAKING FROM LT MAIN FUEL JET PUMP AROUND MATING SURFACE. RECOMMEND REPLACING PACKINGS. REPLACED PACKINGS, LEAK CHECK FAILED. RPLC'D SEALS. FUELED & STILL LEAKING. ORDERING PUMP AVAIL IN THE SYS. PUMP INSTLD. FUELED MAIN TANKS TO 62300K. RAN JETT PUMP FOR 15 MIN. NO LEAKS FOUND.

Part: VALVE — FAULTY (AC BAY) · airframe 43,259 hrs · 5,616 cycles

TRIM AIR VALVE ZONE B INOPERATIVE. DE-ACTIVATED ZONE B TRIM AIR VALVE IN CLOSED POSITION. REPLACED TRIM AIR VALVE AND OPS AND REVERSE MEL 2161P.

Part: CONTROLLER — FAULTY (APU) · airframe 42,765 hrs · 5,557 cycles

ON PREFLIGHT CHECK FOUND APU CONTROLLER FAULT. REPLACED APU CONTROLLER, ACP OP CHKS, NO DEFECTS. STATUS MSG CLEARED.

Part: WIRE — ILLUMINATED (FLAPS/SLATS) · airframe 42,719 hrs · 5,553 cycles

FLAP SLAT SKEW SENSORS STATIS MSG. L2A SENSOR FAILED AND REPLACEMENT OF UNIT NEEDED. FOUND L2A READS 1.75 AND ALL OTHER READS 8.35. CHECKED WIRING AT DM27325 AND NOW IT READS 0.05. SUSPECT DAMAGED CONNECTOR. PART ON ORDER 566-1452. REPLACED L2 SKEW SENSOR, NO HELP. FOUND WIRE W8875-2001B-20 DAMAGED APPROX 8 INCHES FROM CONN DM27325. REPAIRED WIRE, CHECKS GOOD.

Part: LENS — FAULTY (EMERGENCY LIGHT) · airframe 42,351 hrs · 5,507 cycles

EXIT SIGN MISSING AT DOOR 4L. MADE A INTERIM REPAIR WITH TAPE. TAPED LENS TO BASE. SIGN IS FULLY FUNCTIONAL AND IN VIEW. NEEDS NEW BASE. EXIT SIGN IS THE AFT EXIT SIGN AT DOOR 4L NEXT TO DOOR SLIDE. REPLACED LIGHT ASSY. REPLACED BASE. LIGHT OP CKS OK.

Part: CIRCUIT CARD — FAULTY (BLEED SYSTEM) · airframe 42,221 hrs · 5,467 cycles

BLEED ISOLATION VALVE C CENTER BLEED ISOLATION VALVE NOT IN COMMANDED POSITION. STATUS MSG-3610150 LATCHD CL MODE MSG-3610170 INACTV CL MODE. NEEDS ASCPC. REPLACED LEFT ASCPC, NO HELP. REINSTALLED OLD CONTROLLER. SUSPECT BAD VALVE. INSTALLED NEW VALVE, NO HELP. STILL TESTS WITH SOLENOID OR RVDT CIRCUIT OPEN SHORT. NEED TO CHECK RVDT. OLD VALVE REINSTALLED. FOUND NO WIRING DEFECTS. NEED CONTRPL SWITCH & OVERHEAD INTERFACE CARD TO CONTINUE. REPLACED LEFT A1 OVERHEAD PANEL INTERFACE CARD. C ISOLATION VALVE INDICATION RETURNED AND MESSAGE CLEARED. REACTIVATED VALVE AND SYSTEM TESTS OK IN MAT.

Part: LINE — LOOSE (ANTI ICE VALVE) · airframe 42,191 hrs · 5,464 cycles

R WING ANTI-ICE FAULT, FLT DIVERTED. REPLACED ENG ANTI ICE VALVE AND CONTROLLER (P/N 810503-7 (S/N 162). NO HELP, FOUND LOOSE LINE. SECURED LOOSE MUSCLE LINE. SYS OPS TEST GOOD. ACFT GOOD FOR SVC.

Part: TURBINE BLADES — BURNED (NR 1 ENGINE) · airframe 41,627 hrs · 5,392 cycles

NR 1 ENG FAILED STG 1 HPT BOROSCOPE. EXCESSIVE BURN THROUGH DAMAGE TO HPT STG 1 BLADE. BLADE BURN THROUGH JUST AFT OF LEADING EDGE. COMPLETELY THROUGH BLADE ALSO THE INNER AFT SIDE OF REMAINING LEADING EDGE HAS A CRACK AROUND MID SPAN. REPLACED ENGINE. NEW SERIAL NUMBER IS 222182. NR 1 ENGINE ACCOMPLISH ENGINE RUN IDLE LEAK CHECK OF GEAR BOX CRANK PAD COVER. ACP IDLE LEAK CHECK. NO LEAKS DETECTED.

Part: LENS — MISSING (SEAT 20G) · airframe 40,866 hrs · 5,315 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 20G MISSING LENS. REPLACED LIGHT HOUSING.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 40,866 hrs · 5,315 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 34G MISSING LENS. REPLACED LENS, CHECKS OK.

Part: INDICATION SYS — INACCURATE (FUEL QTY) · airframe 40,559 hrs · 5,286 cycles

FUEL QTY INDICATION FUEL TANK QUANTITY ACCURACY IS UNACCEPTABLE. STATUS MSG-2412250 ACTIVE ER MODE MSG-2411111 ACTIVE ER INTER MSG-2820150 ACTIVE ER INTER MSG-2820150 ACTIVE ER HARD. REPLACED FQPU AND LOADED SOFTWARE, OPS GOOD.

Part: STARTER — FAULTY (APU) · airframe 40,330 hrs · 5,262 cycles

APU CONTROL APUC DETECTED FAILURE OF REDUNDANT CONTROL FUNCTION OR LOSS OF ONE ARINC 629 CHANNEL. STATUS MSG01- ACTIVE TAXI IN HARD; ELECTRIC STARTER MOTOR HAS BRUSH WEAR. DB- APU CONTROLLER (APUC) MSG02- ACTIVE TAXI IN HARD; ELECTRIC STARTER MOTOR HAS BRUSH WEAR. MSG-4910760 ACTIVE TI HARD MSG-4910760 ACTIVE TI HARD. STARTER DRIVE (GEARBOX SIDE ) CLUTCH AND ADAPTER DAMAGED. STARTER DAMAGED ALSO. REPLACED APU ELECT STARTER & CLUTCH ASSY. REPLACED APUC, NO HELP. REPLACED APU STARTER (SERIAL NUMBER 34) OPS CHECKS GOOD.

Part: ENGINE — FAULTY (APU) · airframe 40,277 hrs · 5,256 cycles

APU APUC DETECTED FAULT THAT WOULD CAUSE AUTOMATIC SHUTDOWN OF APU IN UNATTENDED MODE OPERATION, OR COMPLETE LOSS OF APUC BUS ACTIVITY (BOTH L AND R 629) FOR 3 SECONDS AFTER THE APU MASTER CONTROL SWITCH HAS BEEN IN THE ON POSITION FOR TEN SECONDS. STATUS CREW COMMENTS: APU NO START. REPLACED ELECTRIC STARTER MOTOR. ACP'D TWO STARTS, BOTH NORMAL.

Part: SEAL — LEAKING (APU FUEL SYS) · airframe 40,131 hrs · 5,243 cycles

APU FUEL PUMP LEAKING FROM MATING SURFACE. REMOVED APU DC FUEL PUMP MOTOR, APPLIED NEW SEALS, AND REINSTALLED MOTOR, TORQUED ALL MOUNT BOLTS. LEAK CHECK OK, PUMP OPERATION OKAY. REINSTALLED ACCESS PLATE AFTER PUMP REPAIR.

Part: BATTERY — FAULTY (APU) · airframe 40,131 hrs · 5,243 cycles

BAT CHARGER APU APU BATTERY CHARGER FAILURE. CHARGER ALREADY REPLACED, SUSPECT APU BATTERY. REPLACED APU BATTERY. OPS CHECKS NORMAL.

Part: CHARGER — FAILED (APU BATTERY) · airframe 40,129 hrs · 5,242 cycles

ON DELIVERY FROM HGR TO GATE ACFT STATUS "APU BATT" & "APU BATT CHGR" MESSAGES. REPLACED APU BATTERY CHARGER. MSG'S CLEARED & OPS TEST OKAY.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,670 hrs · 4,997 cycles

DURING EMERGENCY LIGHTS CHECK, FOUND EMERGENCY SEAT AND CEILING LIGHTS INOP FROM ROWS 17 THRU 25. REPLACED BATTERY ASSY ON DOOR 3R. OP CK NORMAL.

Part: BATTERY PACK — INOPERATIVE (ROWS 17 - 25) · airframe 37,670 hrs · 4,997 cycles

DURING EMERGENCY LIGHTS CHECK FOUND EMERGENCY SEAT AND CEILING LIGHTS INOP FROM ROWS 17 THRU 25. REPLACED BATTERY ASSY ON DOOR 3R. OP CK NORMAL.

Part: OVEN — DIRTY (GALLEY) · airframe 36,891 hrs · 4,917 cycles

BURNING PLASTIC ODOR EVIDENT IN BUSINESS CLASS GALLEY PRIOR DEPT. FOUND EVIDENCE OF MELTED PLASTIC INSIDE WARMING OVEN. REMOVED AND CLEANED WARMING OVEN LINER. NOW OK. NO ODOR NOW EVIDENT.

Part: CONTROLLER — INOPERATIVE (WINDOW HEAT) · airframe 36,840 hrs · 4,910 cycles

STATUS MSG WINDOW HEAT LEFT. REPLACED WINDOW HEAT CONTROLLER. OP GOOD.

Part: CHECK VALVE — FAULTY (FUEL SYSTEM) · airframe 36,149 hrs · 4,836 cycles

FUEL APPEARS TO XFR TO THE RT TANK AT 600-HR OR MORE. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED LT AND RT WING BOOST PUMP DISCHARGE CHECK VALVES. OPS CHECK AND LEAK CHECK GOOD. LT FWD SERIAL NR RMV 172231-15 INST 1072645-42, AFT RMV 172231-18 INST 1066737-32, RT FWD RMV NR 133888-2 INST 1072645-47, RT AFT RMV 172231-18 INST 1066737-28.

Part: UNKNOWN — UNKNOWN (FUEL TRANSFER) · airframe 36,149 hrs · 4,836 cycles

CREW REPORT: FUEL APPEARS TO TRANSFER TO THE RT TANK AT 600-HR OR MORE.

Part: LIGHT — TRIPPED (APU FIRE DETECT) · airframe 35,493 hrs · 4,771 cycles

APU REMOTE FIRE IND-AUTO DISC ARM CIRCUIT BREAKER FOUND POPPED AND WILL NOT RESET. FOUND APU FIRE BOTTLE ARMED LIGHT SHORTED. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE.

Part: FILTER — DIRTY (CABIN AIR) · airframe 35,245 hrs · 4,745 cycles

EQUIPMENT COOLING FAN WARNING HORN KEEPS GOING OFF. *S/D* SUSPECT DIRTY FILTER. REPLACED FILTER, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: AIR FILTER — DIRTY · airframe 34,855 hrs · 4,699 cycles

EQUIPMENT COOLING HORN ON AND EQUIP COOLING EICAS. FOUND DIRTY AIR FILTER. REPLACED AIR FILTER PER MM -21-27-02. OP CHECK GOOD. AC OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,516 hrs · 4,666 cycles

FOUND DOOR 3L EXTERIOR EMERGENCY LIGHT INOP. FOUND FAULTY LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE.

Part: OIL FILTER — CLOGGED (NR 2 ENGINE) · airframe 34,253 hrs · 4,640 cycles

ENG OIL FILTER R RIGHT ENGINE PRIMARY OIL FILTER APPROACHES BYPASS (LARGE PRESSURE DIFFERENTIAL ACROSS NORMAL FILTER) WITH ENGINE RUNNING. REPLACED OIL FILTER & CHANGED OIL.

Part: EXTINGUISHER — FAULTY (LAVATORY) · airframe 34,176 hrs · 4,633 cycles

TRASH CAN EXTINGUISHER AT LAV 4R DISCHARGED WITH NO SIGN OF FIRE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,247 hrs · 4,535 cycles

EMERGENCY LIGHT OUT AT MID GALLEY NR 2 RIGHT SIDEWALL. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,247 hrs · 4,535 cycles

EEL(S) INOP AT FIRST CLASS SEAT 3E AFT & BUSINESS CLASS SEATS 11F & 13D. RELAMPED.

Part: OVEN — FUMES (GALLEY) · airframe 30,882 hrs · 4,256 cycles

FLIGHT DIVERTED DUE TO FUMES COMING FROM A BUSINESS CLASS OVEN. [07-27-07] FOUND ODOR TO BE STRONGEST IN MID GALLEY AREA. APPEARED TO BE ACIDY SMELL. WHEN WARMING OVEN W33 WAS OPENED, ODOR BECAME MUCH STRONGER. FOUND PAPER TOWEL AND RESIDUE OF MELTED PLASTIC ALONG WITH ROLL BAGS. REMOVED ALL MATERIAL AND INOPED WARMING OVEN. NO ODOR NOTED AFTER ITEMS REMOVED FROM AC. AFTER FURTHER TROUBLESHOOTING, REPLACED LEFT HAND GALLEY CEILING LIGHT BALLAST, DR 2 CROSS AISLE

Part: IDG — FAILED (APU) · airframe 30,201 hrs · 4,177 cycles

CREW REPORTS RIGHT GENERATOR FAILURE. APU BEING USED & APU INLET DOOR OPEN. APU AUTO SHUTDOWN AT 16500 FT 310K & AGAIN AT 14500 FT 250K IDLE POWER. [SUP 06-06-07] NR 2 ENGINE IDG WAS REPLACED, BUT CAUSE OF W-U WAS APU AUTO SHUTDOWN. AFTER TROUBLESHOOTING, APU DIFFERENTIAL PRESSURE SENSOR WAS CLEANED AND RESECURRED. FOLLOW-UP VERIFICATION FLIGHT CONFIRMED APU OP AT ALTITUDE. PLANE RETURNED TO ETOPS SERVICE.

Part: LIGHT — DAMAGED (SEAT 2F) · airframe 29,670 hrs · 4,113 cycles

SEAT 2F EVACUATION LIGHT IS DAMAGED. REPAIRED LIGHT. OP CHECKS OK.

Part: LAMP — BURNED OUT (DOOR 3L) · airframe 23,029 hrs · 3,258 cycles

NR 3 LT DOOR EMERGENCY SLIDE LIGHT INOP. REPLACED LAMP.

Part: SKIN — DENTED (R4 DOOR) · airframe 20,174 hrs · 2,895 cycles

DOOR 4R HAS 2 EA DENTS ON EXT SKIN AT BOTTOM EDGE. DOOR SKIN ON PASSENGER ENTRY DOOR (PED) WAS FOUND DAMAGED. THE DAMAGE CONSISTED OF TWO DENTS AT THE LOWER DOOR EDGE. THE DAMAGE WAS REPAIRED PER SRM. MAJOR REPAIR ACCOMPLISHED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 16,065 hrs · 2,374 cycles

STA 246 FLOORBEAM LBL 7.88 VERTICAL STIFFENER CRACKED. MAJOR REPAIR ACCOMPLISHED. STIFFENER REPLACED.

Part: FLAPERON — MALFUNCTIONED (LT & RT) · airframe 12,556 hrs · 1,871 cycles

AIRCRAFT EXPERIENCED FISHTAILING, LASTING 30 SECONDS. SYNOPTIC INDICATED INDEPENDENT CYCLING OF LT & RT FLAPERONS NEAR FULL UP DEFLECTION. AFTER 3-4 CYCLES OPS NORMAL. AUTOPILOT ENGAGED DURING ENCOUNTER, FL380. NO FMC DIRECTED TURNS.