N1609

Part: WIRE — BROKEN (CABIN) · airframe 85,533 hrs · 11,077 cycles

EMERGENCY LIGHTS INOPERATIVE AT 21AB TRIM, 3D CEILING AND SEAT 25GF SEAT LIGHT ASSEMBLY DAMAGED FOUND BROKEN WIRE AT 21AB SEAT TRIM. RETERMINATED WIRE. SYSTEM OPERATION IS NORMAL.

Part: WIRE — PULLED (EMERGENCY LIGHTS) · airframe 85,052 hrs · 11,028 cycles

FOUND SEAT EMERGENCY LIGHTS AT 29B AND 33F INOPERATIVE. MAINTENANCE FOUND WIRES PULLED FROM CONNECTOR AT SEAT 29B AND CONNECTOR BROKEN AT 33F. REPLACED CONNECTORS. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 84,305 hrs · 10,931 cycles

EMERGENCY LIGHTS AT SEAT 25B AND 33F ARE INOPERATIVE. FOUND MATE N LOCK CONNECTOR DISCONNECTED AND SIDEWALL FOR SEAT 33F AND RECONNECTED. REPLACED SEAT HARNESS MAT N LOCK CONNECTOR AT SEAT 25B SIDEWALL. SYSTEM OPERATION IS NORMAL.

Part: WIRE — DETACHED (EMERGENCY LIGHTS) · airframe 84,305 hrs · 10,931 cycles

ALL EMERGENCY EXIT LIGHTS INOP AT BOTH AFT DOORS. REINSTALLED WIRE 41H4300A10 TO GROUND STUD GD1888 AFT 2L AND 2R DOOR EMERGENCY EXIT SIGN LIGHTS TEST NORMAL.

Part: DOUBLER — CORRODED (BS 676-698) · airframe 83,527 hrs · 10,857 cycles

FWD CARGO AT STA 676 - STA 698 AND S-36L - S-35L FOUND DOUBLER CORROSION OUT OF LIMITS. DOUBLER REPLACED. (LP 1002059)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,492 hrs · 10,851 cycles

SEAT TRACK - CABIN SEAT TRACK AT RBL 88.5 FROM STA 1208 TO STA 1428 FOUND CORROSION OUT OF LIMITS AND REPLACED. (LP 1002048)

Part: STRAP — DAMAGED (FUSELAGE) · airframe 83,492 hrs · 10,851 cycles

RIGHT 955 FAILSAFE STRAP DAMAGED AND REPAIRED. (LP 1002034)

Part: STRAP — DAMAGED (FUSELAGE) · airframe 83,492 hrs · 10,851 cycles

LEFT FAIL SAFE STRAP DAMAGED AND REPAIRED. (LP 1002029)

Part: SKIN — DENTED (LE SLAT) · airframe 83,492 hrs · 10,851 cycles

NR 7 SLAT LOWER SURFACE HAS DENT FROM O/B EDGE 50.4 INCH CROSS T/E 2.4 INCH. REPAIRED PER SRM 57-43-02. (LP 1000838)

Part: FRAME — CRACKED (FUSELAGE) · airframe 83,490 hrs · 10,850 cycles

HFEC INSPECTION FOUND 01EA CRACK ON LT BS 883.5 FRAME INNER CHORD SURFACE AND TRANSITION RADIUS AND REPAIRED. (LP 0993356)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,490 hrs · 10,850 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT RBL 88.5 FROM STA 1098 TO STA 1208 FOUND CORRSION OUT OF LIMITS. PARTS REPAIRED AND NEW SPLICES INSTALLED. (LP 0990937)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,490 hrs · 10,850 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT RBL 88.5 FROM STA 841 TO STA 1098 FOUND CORRSION OUT OF LIMITS. REPAIRED PARS AND NEW SPLICES INSTALLED. (LP 0990925)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,490 hrs · 10,850 cycles

CORROSION LEVEL: 2 SEAT TRACK - CABIN SEAT TRACK AT LBL 88.5 FROM STA 1098 TO STA 1230 FOUND CORRSION FOUND OUT OF LIMITS. REPLACED. (LP 0982943)

Part: SKIN — CRACKED (WING) · airframe 83,490 hrs · 10,850 cycles

HFEC INSPECTION FOUND 01EA CRACK APPROX 0.100" IN LENGTH ON LT LOWER SKIN AT THE AFT SIDE OF NR 1 HOLE AT STRINGER L-6.5 REPAIRED PER ER/A 576037-14. (LP 0982758)

Part: CHARGER — INOPERATIVE (CABIN) · airframe 83,474 hrs · 10,848 cycles

EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED M733 BATTERY CHARGER. SYSTEM OPERATION IS NORMAL.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 79,438 hrs · 10,440 cycles

FOUND 1" CRACK AT STA 1659 STRINGER S-13AL REMOVED DAMAGED AREA PER SRM 53-80-01. DAMAGE AREA APPROX 2" LONG 1" HIGH. C/W SRM 53-80-01 AND ERA 567617-14.

Part: FUSE — BLOWN (CABIN) · airframe 79,438 hrs · 10,440 cycles

DURING SERVICE CHECK FOUND EMERGENCY LIGHTS AT SEATS 1-3D INOPERATIVE. MAINTENANCE REPLACED FUSE F1 ON POWER SUPPLY M730. SYSTEM OPERATION IS NORMAL.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 82,935 hrs · 10,797 cycles

THIS ERA PERFORMS A REPAIR TO A 1 INCH CRACK FOUND DURING INSPECTION AT STA 1654.5 COMMON TO S-13AL THE REPAIR WAS COMPLETED PER SRM 53-80-01 REPAIR 7 WITH A FASTENER SUB DEVIATION ASSOCIATED ER/A 567617-14.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,370 hrs · 10,335 cycles

FOUND THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE AT THE SIDE OF SEATS 1D, 2D AND 3D. REPLACED THE POWER SUPPLY UNIT. SYSTEM OPS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 78,094 hrs · 10,309 cycles

EMERGENCY LIGHTS AT SEAT 29F ARE INOPERATIVE. MAINTENANCE RECONNECTED ELECTRIC HARNESS CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 77,838 hrs · 10,284 cycles

EMERGENCY LIGHT HANGING DOWN AT SEAT 38A. SECURED LIGHT FIXTURE. SYSTEM OPERATION IS NORMAL.

Part: FUSE — BLOWN (CABIN) · airframe 77,838 hrs · 10,284 cycles

FOUND EMERGENCY LIGHTS AT SEATS 1, 2, AND 3 D CHARGER FUSE BLOWN AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,848 hrs · 10,172 cycles

SEAT 31GF AND 28GF EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS. CHECKED GOOD.

Part: SKIN — DAMAGED (BS 359) · airframe 71,522 hrs · 9,497 cycles

LIGHTNING STRIKE AT FS 359 JUST ABOVE STR 34R, DAMAGE IS OUT OF LIMITS, REPAIRED IAW SRM 53-00-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,311 hrs · 9,232 cycles

EMERGENCY LIGHTS AT SEAT 25FG ARE INOPERATIVE. MAINTENENACE REPLACED BATTERY M732. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (LT WING) · airframe 82,808 hrs · 10,784 cycles

INSPECTION OF LOWER WING SKIN FASTENER HOLES COMMON TO REPAIR DOUBLER INDICATES CRACKING AT 40EA FASTENER HOLES, ALSO LEFT WING SKIN DISHING JUST INBOARD OF RIB 32 AT STR 9.5. REPAIR PER ER/A 534150-14AD

Part: SKIN — CRACKED (LT WING) · airframe 82,808 hrs · 10,784 cycles

CRACKED HOLES 9EA WHILE COMPLETING MODIFICATION OF STRINGER L-6.5 ON THE LH WING PER AA 5724-01010 REV A SECTION 05, MAINTENANCE DETECTED CRACK INDICATIONS IN THE LOWER INSPAR SKIN AT THE INBOARD-MOST FASTENER HOLE COMMON TO THE STRINGER. INSPECTION REPORTS THE CRACK IS LOCATED IN THE SKIN ONLY, REPAIRED PER ER/A 534151-14

Part: SKIN — CRACKED (LT WING) · airframe 66,422 hrs · 8,870 cycles

WHILE PERFORMING BHEC, FOUND FASTENER HOLE NR 1 STILL CRACKED AT .282 OF GROUP "A" FASTENER HOLES, LT WING LOWER SKIN AT L 9.5. C/W 5724-01010-05.

Part: SKIN — CRACKED (RT WING) · airframe 66,422 hrs · 8,870 cycles

WHILE PERFORMING BHEC, FOUND FASTENER HOLE NR 1 STILL CRACKED AT .282 OF GROUP "A" FASTENER HOLES, RT WING LOWER SKIN AT L 9.5. C/W AMDS CARD 5724-01010-06.

Part: UNKNOWN — ODOR (CABIN) · airframe 64,129 hrs · 8,603 cycles

DURING DESCENT, F/A AND PAX DETECTED SMOKEY ODOR NEAR R3 DOOR. INSPECTED AND NO TROUBLE FOUND.

Part: DISPLAY — FAILED (WX RADAR SYS) · airframe 59,273 hrs · 8,040 cycles

CREW REPORT BURNING ODOR WITH ASSOCIATED SKEWED DISPLAY ON WEATHER RADAR ON TCAS. TURNING DISPLAY OFF CLEARED ODOR. MX REPLACED WEATHER RADAR DISPLAY AND SYSTEM, OPS CHECKED NORMAL.

Part: FRAME — CRACKED (BS 903) · airframe 57,321 hrs · 7,818 cycles

MAIN DECK STA 903 WL200 RT FRAME INNER CHORD TRANSITION RADIUS CRACKED AT RADIUS APPROX .2500"LONG. REPAIRED IAW ERA 511795-14AD REV O.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 57,320 hrs · 7,817 cycles

RT WING INBD MAIN FLAP L/E OTBD FAIRING FOUND DELAMINATED. REPAIRED IAW SRM 57-53-01, REPAIR 1. AND SRM 51-70-05, PARA 5A (1).

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 57,320 hrs · 7,817 cycles

LEFT WING INBD MAIN FLAP L/E OTBD FAIRING DELAMINATED. REPAIRED IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-05, PARA 5A (1).

Part: LATCH — BROKEN (EMERGENCY SLIDE) · airframe 55,241 hrs · 7,590 cycles

DURING PSV 10, RIGHT OVERWING SLIDE DOOR FAILED TORQUE CHECK. UNABLE TO OPEN OVERWING DOOR INITIALLY. APPLIED PRESSURE TO DOOR AND WORKED INTEGRATOR BACK AND FORTH, UNTIL THE DOOR UNLATCHED. ON INVESTIGATION, FOUND THE THIRD LATCH WAS BROKEN, SPRING WAS MISSING AND FOUND IN THE O/WING SLIDE COMPARTMENT.

Part: PIN — LOOSE (CONNECTOR) · airframe 52,737 hrs · 7,258 cycles

CREW FOUND PASSENGER SEAT 24A EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE SECURED LOOSE PIN IN CONNECTOR, OPERATIONAL CHECK OK.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 49,436 hrs · 6,832 cycles

RT WING INBD MAIN FLAP OTBD L/E NOSE FAIRING FOUND DELAMINATED. COMPOSITE PREPREG LAY UP HOT BOND REPAIR CARRIED OUT IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-05, FIG 5.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 49,436 hrs · 6,832 cycles

LT WING INBD MAIN FLAP OTBD L/E NOSE FAIRING FOUND DELAMINATED. COMPOSITE PREPREG LAY UP HOT BOND REPAIR CARRIED OUT IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-05, FIG 5.

Part: SKIN — DAMAGED (LT STABILIZER) · airframe 49,436 hrs · 6,832 cycles

DURING WALK CHECK FOUND 0.25" HOLE ON LT STABLIZER BOTTOM SURFACE 1' OF AUX SPAR STA 191. METAL HOT BOND REPAIR PERFORMED AT HOLE AREA IAW SRM 55-10-01, REPAIR 1 FIG 201 AND SRM 51-70-10, REPAIR 4, FIG 201.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,304 hrs · 6,582 cycles

THE COCKPIT EMERGENCY LIGHT ABOVE DOOR DOES NOT ILLUMINATE WITH TEST SWITCH OR LIGHT ON SWITCH. MX REPLACED THE LIGHT ASSY. SYS OPS IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,472 hrs · 6,488 cycles

MX FOUND THE EMERGENCY PATH LIGHTS BETWEEN 24F AND 32F INOPERATIVE AND REPLACED M732 POWER SUPPLY. SYS OPS IS NORMAL.

Part: CARD — FAULTY (AUTOTHRUST SYS) · airframe 43,664 hrs · 6,196 cycles

ON TAKEOFF A/C SPEED LIMITED TO 245 KTS WITH FLAP LIM MESSAGE ON BOTH ADI. DIV TO JFK FOR REPAIRS. T/S PER WDM FOUND NR 3 FLAP POSN TRANS STUCK AT 1 DEG DETENT, SUSPECT RIG OR TRANS. REPLACED M838 FLAP/STAB POSN CARD OP OK. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: CIRCUIT CARD — DEFECTIVE (STALL WARNING) · airframe 43,485 hrs · 6,171 cycles

WARN ELEC STATUS MSG WILL NOT CLEAR - RTB. MTC REPLACED BOTH WEU PWR SUPPLIES AND L AND R STALL WARN CARDS, ALL CHECKS NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: NOSE COWL — DAMAGED (NR1 ENGINE) · airframe 41,387 hrs · 5,951 cycles

BIRD STRIKE AFTER TAKEOFF CAN DETECT ODOR IN CABIN RETURNING TO JFK FOR REPAIRS. NR 1 ENG BIRDSTRIKE. PERFORMED BOROSCOPE, ALL NORMAL. REPLACED ENGINE NOSE COWL.

Part: TIRE — PUNCTURED (RT NLG) · airframe 41,194 hrs · 5,925 cycles

RT TIRE DEFLATED. REPLACED WHEEL ASSY SPACER INSTALLED. TIRE NOT DEFLATED-HAD FOD MFG B767-300ERN.

Part: TRANSMITTER — MALFUNCTIONED (NR 8 FLAP) · airframe 40,509 hrs · 5,849 cycles

FLAP/SLAT ELEC STATUS MESSAGE DISPLAYED DURING TAXI. HARD FAULT NR 8 RES 12/28/08 JFK 271703321. REMOVED AND REPLACED NR 8 FLAP POSITION TRANSMITTER PER AMM. OPS NORMAL.

Part: SWITCH — UNSERVICEABLE (APU) · airframe 40,443 hrs · 5,843 cycles

APU WON`T START REPOSITION FROM PAD TO GATE 6. T/S PER FIM AUTO SHUTDOWN GEN FILTER ON BITE. REMOVED AND REPLACED GEN DIFF PRESS SWITCH PER AMM. RAN APU, OPS NORMAL. T/S PER FIM AUTO SHUTDOWN GEN FILTER ON BITE. REMOVED AND REPLACED GEN DIFF PRESS SWITCH PER AMM. RAN APU, OPS NORMAL.

Part: PRESSURE SWITCH — FAILED (NR 2 FUEL FILTER) · airframe 40,028 hrs · 5,795 cycles

INTERMITTENT RIGHT ENGINE FUEL FILTER LIGHT. REMOVED AND REPLACED RT ENG FILTER PER M/M. INSPECTED NTF REMOVED AND REPLACED FUEL FILTER PRESSURE SW PER M/M RAN ENG MSG DID NOT RETURN.

Part: SKIN — GOUGED (FS 440-630 S32L) · airframe 36,934 hrs · 5,447 cycles

SKIN BLENDS AT FS 440 - 630 BETWEEN STRINGERS S-32L AND 35L.

Part: CONNECTOR — DIRTY (PRSOV) · airframe 36,255 hrs · 5,374 cycles

INBOUND RT ENG HPSOV EICAS MSG, MTC PLACED HPSOV ON MEL-THENON TAXI OUT NO PNEUMATIC AIR FROM RT ENGINE, RTB-MTC THEN CLEANED PRSOV CONNECTOR.

Part: VALVE — MALFUNCTIONED (E/E BAY) · airframe 32,839 hrs · 4,978 cycles

RTB DUE EQUIPMENT COOLING OVERBOARD VALVE LIGHT ILLUMINATED DID NO GO OUT IN STANDBY. NO DISPATCH ALLOWED BY FCP. LOCKED VALVE CLOSED AND RELEASED PER MEL. RE-ACTIVATED SYSTEM AND PUT BACK IN AUTO SYSTEM, OPS NML. NO HISTORY. MCO AND PLAC REM.

Part: PROCESSOR — FAILED (FUEL QTY) · airframe 32,716 hrs · 4,964 cycles

DURING FUELING RT FUEL QTY DISPLAY IN FLIGHT COMPARTMENT INOP. RESET C/B QTY 1 AND 2 ALSO READ OUT FUEL QTY PROCESSOR FAULTS INDICATED AL COMPENSATORS AFTER CLEARED MEMORY RERACKED PROCESSOR NO HELP IND BLANK. REPLACED F/Q PROCESSOR BORROWED FROM KLM AND OPS CK OK.

Part: DOOR LATCH — MISINSTALLED (RT OVERWING DOOR) · airframe 32,309 hrs · 4,908 cycles

RT OFF WING SLIDE COMPARTMENT DOOR LATCH 3RD FROM THE FRONT, FOUND INCORRECTLY INSTALLED. FOUND LATCH INSTALLED UPSIDE DOWN. REORIENTED LATCH.

Part: ENGINE — LEAKING (NR 2) · airframe 31,744 hrs · 4,839 cycles

ON WALKAROUND, FOUND OIL DRIPPING FROM BOTTOM AFT END OF THRUST REVERSER AND PUDDLING IN COR COWL NR 2 ENG ADDED 5 PINTS. UPON ARRIVAL REMOVED RECOUP DUCTS AT 6 O`CLOCK AND 8 O`CLOCK POS SEE ITEM 10 FOR T/S FINDINGS REQ ENG CHA REPLACED ENGINE IAW TRANSMITTAL 1T161.

Part: BATTERY — INOPERATIVE (MASTER) · airframe 29,844 hrs · 4,601 cycles

BATT CHARGER STATUS MSG. RESET BATTERY CHARGER C/B, NO HELP. RESEATED BATTERY CONNECTOR. OPS OK AND MSG CLEARED. REPLACED BATTERY CHARGER MSG CAME ON AGAIN. TEST OK AND MSG CLEARED.

Part: START VALVE — FAILED (LT ENGINE) · airframe 29,663 hrs · 4,578 cycles

NO ENGINE ROTATION DURING START OF LEFT ENG. REPLACED NR 1 ENG START VALVE.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 28,067 hrs · 4,383 cycles

APU PNEUMATICS QUIT AFTER LEFT ENGINE START. NO FAULTS LISTED ON ANY FLT LEG ON APU ECU. APU AIR OPS NORM SPUN ENGS TO 28 PERCENT AND OPERATED PACKS, ALL NORMAL. CLEARED MCO AND PLACARD REMOVED.

Part: COMPRESSOR — DAMAGED (NR 1) · airframe 26,633 hrs · 4,199 cycles

DURING ETOPS PDC FOUND PIECE OF 5TH STAGE VSV LEVER ARM IN COWLING. VSV LEVER AT 8 O`CLOCK POS VERIFIED BROKEN VANE SPINS FREELY IN CASE. BOROSCOPED HPC AND FOUND NUMEROUS BLADES DAMAGE 6TH STAGE. REPLACED ENGINE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 25,237 hrs · 4,003 cycles

AFTER STARTING RT ENGINE PRIOR TO TAKEOFF THE CABIN ALT DESCENDED RAPIDLY APPROX 1000 FPM. AUTO INOP LIGHT ILLUM SHORTLY THEREAFTER. T/S PER FIM. BIT CHECKED CABIN AUTO CONTROLLERS. CABIN AUTO 1 FAULTED SELECTOR PANEL AND AUTO 2 FAULTED ITSELF. PER FIM REPLACED NR 2 CABIN AUTO CONTROLLER AND CABIN ALT CONT PANEL PER MM. CABIN AUTO CONTROLLER 1 AND 2 BITE CHECK OK. NO FAULT. EICAS MSG CLEARED.

Part: IDG — FAILED (RT ENGINE) · airframe 22,336 hrs · 3,611 cycles

T/O ABORT AT 70 KTS FOR RT GEN DRIVE LIGHT EICAS MSG. REPLACED IDG.

Part: ENGINE — MAKING METAL (NR 1) · airframe 21,477 hrs · 3,480 cycles

DURING L/O FOUND METAL IN THE LT ENG MASTER CHIP DETECTOR. REPLACED ENGINE.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 19,388 hrs · 3,189 cycles

WX RADAR INOP. REPLACED WX RADAR XCVR AND INDICATOR. OPS CHECK OK.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 18,720 hrs · 3,093 cycles

THE RIGHT AND LEFT INBOARD ELEVATORS WERE FOUND WITH DAMAGE ON THE LOWER SKIN PANELS. THE DAMAGE EXTENDS THROUGH THE OUTER SKIN, INNER SKIN, AND HONEYCOMB CORE. REPAIRED PER ER/A 417308-14.

Part: TIE BOLT — SHEARED (WHEEL) · airframe 16,023 hrs · 2,684 cycles

SIX TIRE TIEBOLTS SHEARED. WHEEL ASSY 6 REPLACED PER MM.

Part: CONTROL MODULE — MALFUNCTIONED (HORIZ STAB) · airframe 12,703 hrs · 2,156 cycles

REJECTED TAKEOFF DUE UNSCHEDULED STAB TRIM. REPLACED THE LEFT AND RT STAB POS TRANSMITTER. MEGGED WIRING FROM RT STAB POS TRANSMITTER TO RT FSPM, ALL CHECK OK. REPLACED LEFT STCM. REPLACED RT SAM MODULE PER AMM. INSTALLATION TESTS OK. INCLUDING AUTOPILOT INTERFACE AND OUTBOARD AILERON LOCKOUT TESTS.

Part: MODULE — FAULTY (STABILIZER) · airframe 12,406 hrs · 2,096 cycles

UNSCHED STAB TRIM, EICAS CAUTION ON TAKEOFF ROLL. TAKEOFF ABORTED. T/S PER FIM ON UNSCH STAB TRIM EICAS MSG. LT SAM FAULTED `STCM` REPLACED LT SAM PER M/M. LT STAB TRIM OPS NORMAL.

Part: IDG — MALFUNCTIONED (NR 1 ENGINE) · airframe 11,750 hrs · 1,989 cycles

EN ROUTE TO STR RIGHT GENERATOR OFF LIGHT ILLUMINATED. BPCU BITE CHECK FAULTED, DP TRIP AND MAIN BUS/OVERLAP ZONE- ON RT GEN T/S FAULT MSG PER FIM FOUND IDG CT WIRING RESISTANCE O C-PHASE OUT OF TOLERANCE DURING STEP 2. REMOVED IDG RT GCU/BPC. REPLACED FOR T/S. INSTALLED ORIG RT GCU/BPCU PER AMM. INSTALLED IDG PER AMM. RQS R/U AND LEAK CHECK. R/U AND LEAK CHECK PERFORMED PER PFHB, NORMAL. DISC RESET.

Part: COMPUTER — FAILED (E/E BAY) · airframe 11,395 hrs · 1,928 cycles

AUTO THROTTLE FAILED TO ENGAGE. TMC AC CIRCUIT BREAKER POPPED. HINT OF ELECTRICAL SMOKE DISSIPATED QUICKLY. FWD TO MCO AND PLACARD PER MEL 22-30-01A.

Part: COFFEEMAKER — DIRTY (FWD GALLEY) · airframe 10,788 hrs · 1,821 cycles

ELECTRICAL SMELL IN FWD GALLEY. COULD NOT LOCATE. OPERATED ALL FWD GALLEY AND IFE EQUIPMENT, NO ELECTRICAL ODOR NOTED. ALSO CHECKED ALL LIGHTING IN FWD CABIN. ALL CHECKED GOOD. FOUND EVIDENCE OF BURNED COFFEE. CLEANED SAME, OK FOR SERVICE.

Part: EEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 4,502 hrs · 749 cycles

ON DESCENT OUT OF 10,000 FEET, THE CREW NOTICED THE RT ENGINE ROLLING BACK AND FLAMED OUT. CREW WAS ABLE TO RESTART THE ENGINE SUCCESSFULLY. NO WATER IN FUEL SUMPS. RAN ENG AND VERIFIED CONT AND ENGINE PARAMETERS NML EEC REPLACED. CHECKED WIRING AND POWER SPAR VALVE NTF VLV ACT REMOVED PRECAUTION.RPLD SPAR VLV RPL RT ENG FUEL T SW PER 76-11-00-2-N. REPLACED RT ENGINE EEC RESET PIMU PERFORMED ENG RUN.NO FAULTS RECORDED ALL ENG PARAMETERS ARE NORMAL.MCO AND PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 2,389 hrs · 401 cycles

AFTER LOWERING GEAR NOSE GEAR GREEN DID NOT COME ON. REPLACED INDICATOR LIGHT ASSY. ETOPS CATEGORY ''F'': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: WIRE — SHORTED (CABIN) · airframe 1,847 hrs · 301 cycles

EMERGENCY ESCAPE FLOOR MARKING LIGHT IN PARTITION BETWEEN F/C AND COACH CLASS SHORTING OUT LIGHTS ROWS 10 THROUGH 21 RIGHT SIDE OF AIRCRAFT. REPAIRED DEFECTIVE WIRING IN PARTITION.