N1612T

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,613 hrs · 10,357 cycles

EMERGENCY EXIT LIGHTS AT SEAT 17GF, AND 33GF-41GF INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER M733. SYSTEM OPERATION IS NORMAL.

Part: MODULE — DEFECTIVE (TE FLAP) · airframe 81,278 hrs · 10,321 cycles

SHIP 1612 FLIGHT 230 RDU-CDG - ATO AT 70 -75 KNOTS DUE TO FLAP EICAS MESSAGE AND TONE. CORRECTIVE ACTION: REPLACED THE FSPM, RELAY K730 AND NUMBER 4 FLAP POSITION SENSOR.

Part: COMPRESSOR — OVERHEATED (POTABLE WATER) · airframe 81,038 hrs · 10,295 cycles

ELECTRICAL FUMES DETECTED AFT OF ROW 40 AFTER PASSENGERS DISEMBARKED. FOUND POTABLE WATER COMPRESSOR OVERHEATED AND EMANATING ELECTRICAL FUMES. PULLED AND SECURED POTABLE WATER COMPRESSOR C/ B AND FWD TO MEL 38-10-01A. REPLACED POTABLE WATER COMPRESSOR. SYSTEM OPERATION IS NORMAL.

Part: HMU — MALFUNCTIONED (LT ENGINE) · airframe 78,863 hrs · 10,073 cycles

SHIP 1612-DIVERSION INTO SYA DUE TO LEFT ENGINE STUCK AT FLIGHT IDLE WITH NO THROTTLE RESPONSE. ENGINE NOT SHUT DOWN. CORRECTIVE ACTION: THE HMU, HMU SOLENOID AND EEC WERE REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING HORN — NO TEST (APU FIRE) · airframe 76,467 hrs · 9,835 cycles

APU FIRE WARNING HORN WON'T SOUND DURING FIRE, OVERHEAT TEST. REPLACED APU FIRE WARNING HORN AT APU REMOTE CONTROL PANEL.

Part: LATCH — OUT OF ADJUST (SLIDE DOOR) · airframe 75,116 hrs · 9,697 cycles

4 LATCH JAWS DO NOT REMAIN OPEN WHEN TURNING THE CAM OF THE INTEGRATOR TO THE UNLOCK POSITION AT THE RIGHT WING SLICE COMPARTMENT DOOR. CHECKED AND ADJUSTED LATCHES.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 75,116 hrs · 9,697 cycles

DURING ET/UT INSPECTION FOUND RIGHT STA 955 FAIL STRAP WITH CRACK INDICATION. REPAIRED FAIL SAFE STRAP.

Part: BATTERY — FAILED (ESCAPE SLIDE) · airframe 74,521 hrs · 9,627 cycles

RIGHT EMERGENCY SLIDE TEST 1 AND SPOILER TEST 2 LIGHT NOT ILLUMINATING. FOUND THE RT OVERWING SLIDEE SYS EMERGENCY BATTERY FAILED. REPLACED THE BATTERY, AND THE SYSTEM OPS NORMAL.

Part: CIRCUIT BREAKER — TRIPPED · airframe 74,182 hrs · 9,594 cycles

EMERGENCY ESCAPE SQUID TEST LIGHT IS INOPERATIVE. RESET C/B P36 ONP11 PANEL. SYSTEM OPERATIONS IS NORMAL.

Part: LIGHT — UNSECURE (SEAT 29B) · airframe 74,078 hrs · 9,584 cycles

EMERGENCY LIGHTS AT SEAT 29B ARE INOPERATIVE. SECURED LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 71,720 hrs · 9,304 cycles

EMERGENCY LIGHTS AT SEAT 36G ARE INOPERATIVE. SECURED OTBD CONNECTOR. SYSTEM OPS NORMAL.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 69,614 hrs · 9,055 cycles

OVEN EXPERIENCED AN ELECTRICAL FIRE AND BLEW A FUSE. PER FLIGHT ATTENDANT HE TURNED OVEN ON AND THE C/B TRIPPED. FOUND LEFT C/B OPEN. NO MENTION OF FIRE. INSPECTED OVEN AND FWD TO NEF 25-34-02. OVEN REPLACED. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (LT WING) · airframe 79,111 hrs · 10,096 cycles

MAINTENANCE FOUND CRACKS ON LOWER INSPAR SKIN OF LH WING FROMA FASTENER COMMON TO STR L-9.5. DAMAGE OB OF RIB 31 AT WSTA 990.2. CRACK AND REPAIRED PER ERA 532083-14. (LP 1783285)

Part: BATTERY PACK — NO TEST (ESCAPE SLIDE) · airframe 57,195 hrs · 7,555 cycles

LEFT AND RIGHT ESCAPE SLIDES WILL NOT TEST. REPLACED ESCAPE SLIDE BATTERIES . SQUIB TESTED GOOD.

Part: STRUCTURE — CRACKED (BS 903) · airframe 56,621 hrs · 7,492 cycles

CABIN LT BELOW DOOR FRAME BS 903.5 LOWER CORNER FOUND CRACKED, REPAIRED.

Part: SQUIB — NO TEST (ESCAPE SLIDE) · airframe 56,311 hrs · 7,454 cycles

ON PDC, FOUND OVERWING LT AND RT EMERGENCY ESCAPE SQUIBS WILL NOT TEST. TROUBLESHOT IAW SSM 25-65-01. REPLACED M962 RT OVERWING POWER SUPPLY TEST. OK IAW AMM 25-65-17.

Part: BATTERY PACK — FAILED (SLIDE) · airframe 54,762 hrs · 7,280 cycles

ON S/C, FOUND SLIDE/SPOILER SQUIB LIGHTS FAIL. R & R BOTH BATTERY PACKS, CHECKED GOOD.

Part: LIGHT — INOPERATIVE (LT WING SLIDE) · airframe 54,536 hrs · 7,254 cycles

LEFT WING SLIDE GROUND LIGHT L396 INOPERATIVE. REPLACED LIGHT ASSY IAW WDM 33-51-21 AND AMM 33-51-06. TESTED OK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,148 hrs · 7,211 cycles

DURING CHECK, FOUND OFF WING ESCAPE EMERGENCY TEST OF SQUIB NOT SUCCEED. R & R BOTH LT AND RT BATTERYS OF ESC SYS OFF WING IAW AMM 25-65 AND OPS CHECKED OK.

Part: BATTERY — INOPERATIVE (ESCAPE SLIDE) · airframe 54,097 hrs · 7,206 cycles

EMERGENCY ESCAPE SQUIB WILL NOT TEST. REPLACED RT EMERGENCY ESCAPE SLIDE BATTERY, PN AD 2013-1A IAW AMM, OPS NORMAL.

Part: BATTERY — INOPERATIVE (ESCAPE SLIDE) · airframe 53,379 hrs · 7,122 cycles

EMERGENCY ESCAPE SQUIB TEST 1 AND 2 TEST LIGHTS WILL NOT TEST T/S IAW FIM 25-65. FOUND BATTERIES INOPERATIVE AT M961 AND M962. R & R BATTERIES AT M961 AND M962 IAW AMM 25-65. SQUIB TEST, GOOD TEST 1 AND 2.

Part: COMPRESSOR — SMOKE (POTABLE WATER) · airframe 52,875 hrs · 7,068 cycles

FOUND SMOKE AND ELECTRICAL SMOKE IN THE AFT PAX COMPARTMENT. FOUND THE SMOKE COMING FROM THE POTABLE WATER COMPRESSOR AND CONFIRMED THE SMOKE DISAPPEARED AFTER THE COMPRESSOR CIRCUIT BREAKER WAS PULLED. OPEN

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 52,516 hrs · 7,022 cycles

23AB EMERGENCY LIGHT INOPERATIVE. RECONNECTED QUICK DISCONNECT, OPS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (SLIDE) · airframe 51,287 hrs · 6,881 cycles

DURING PDC FOUND RT EMERGENCY SQUIB NOT WORKING. CHANGED BATTERY CHARGER. OPS CHECKED NORMAL IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,973 hrs · 6,457 cycles

EMERGENCY SEAT MOUNTED LIGHTING AT SEAT 39F IS INOPERATIVE. MAINTENANCE SECURED LIGHT BASE. SYSTEM OPERATION IS NORMAL.

Part: BATTERY — INOPERATIVE (ESCAPE SLIDE) · airframe 47,489 hrs · 6,392 cycles

RT EMERGENCY ESCAPE SLIDE FAILS TEST 1 AND TEST 2 C/A T/S IAW FIM 25-65-00 RT EMERG BATT. REPLACED IAW AMM 25-65-17. OPS CK GOOD. RII TASK C/W PINS VERIFIED REMOVED AND STOWED.

Part: WIRE — BROKEN (CABIN) · airframe 45,902 hrs · 6,198 cycles

DURING DRC FOUND EMERGENCY PATH LIGHTS INOPERATIVE AT SEATS 16G-20G. MAINTENANCE REPAIRED BROKEN WIRE AND REPLACED THE POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 44,439 hrs · 6,006 cycles

EMERGENCY LIGHTS AT SEAT 29FG ARE INOPERATIVE. WIRE AT WALL IS BROKEN. MX FOUND A CONNECTOR UNDER SEAT 29FG LOOSE AND RECONNECTED.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 43,822 hrs · 5,912 cycles

EMERGENCY LIGHTS AT ROW 22FG INOPERATIVE. MX RECONNECTED PLUG. SYS OPS IS NORMAL.

Part: IDG — MALFUNCTIONED (LEFT) · airframe 43,082 hrs · 5,815 cycles

AFTER DEPARTING JFK, THE LEFT ENGINE GENERATOR FAILED FOLLOWED BY AN ACRID SMELL IN THE CABIN AND LAVATORY SMOKE DETECTORS SOUNDING. FLIGHT RETURNED TO JFK WHERE MAINTENANCE PERFORMED BITE ON BPCU AND FAULTED THE DP TRIP GENERATOR AND FDR. THE LEFT IDG WAS REPLACED AND THE SYSTEM OPERATION RETURNED TO NORMAL. (2010-D1303)(DL76G103021)

Part: LIGHT — INOPERATIVE (SEAT 19FG) · airframe 41,959 hrs · 5,687 cycles

RED SEAT MOUNTED EMERGENCY LIGHTS ARE INOPERATIVE AT SEAT 19FG. MX REPLACED LIGHT ASSY AND THE SYS. OPS RETURNED TO NORMAL.

Part: UNKNOWN — FUMES (CABIN) · airframe 41,314 hrs · 5,618 cycles

ELECTRICAL FUMES IN CRUISE. STOPPED WITH RT UTIL BUSS SWITCH OFF. NO ADDITIONAL STATUS OR EICAS MESSAGES. NO SPECIFIC EVIDENCE REPORTED BY F/A EXCEPT THE FUMES MID GALLEY AREA REPROTED TO MX. CKD ROWS 6-16 FWD AND AFT OF MID GALLEY. NO EVIDENCE OF DAMAGE FROM SMOKE. CHECKED OVENS/CHILLERS/COFFEE MAKERS. INSP LT/RT RECIRC FANS/LOGO LIGHTS/WATER HEATERS AND ALL IFE VIDEO SCREEN BEHIND THE MID GALLEY AND F/C SEATS AND IFE PANELS UNDER SEATS. CHECKED ALL GALLEY COMPONENTS WITH RT UTILITY BUSS OFF/ON. ALL CHECKS NORMAL. NO FUMES NOTICED.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 40,347 hrs · 5,520 cycles

EMERGENCY ESCAPE PATH SEAT LIGHTS INOP AT ROWS 21 TO 23A/B FOUND NUMEROUS BREAKS IN WIRING IN AFFECTED AREA. ALSO DAMAGED LIGHT ASSY AT SEAT 22AB BLOWN FUSE IN POWER SUPPLY M737. REPAIRED WIRING/ REPLACED LIGHT ASSY REPLACED BLOWN FUSE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 39,830 hrs · 5,473 cycles

SEAT 37GF EMERGENCY PATH LIGHT DOES NOT ILLUMINATE. FOUND POWER WIRE AT BASE OF SEAT AT WALL BROKEN OFF. TERMINATED BROKEN WIRES IAW SWPM AT SAME LOCATION - EMERGENCY PATH LIGHT CHECKS NORMAL.

Part: PROCESSOR — MALFUNCTIONED (TCAS) · airframe 39,398 hrs · 5,433 cycles

ON PUSHBACK TCAS PROCESSOR ERROR ON RADAR SCREEN. REMOVED AND REPLACED TCAS PROCESSOR PER AMM. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: IDG — MALFUNCTIONED (NR 2 ENGINE) · airframe 38,603 hrs · 5,355 cycles

RT GEN OFF AND RT AC BUS OFF LIGHT ILLUMINATED AFTER ENG START. FWD TO MCO AND PLACARD IAW 24-00-01. PLACARD INSTALLED DISPATCH BY MCC. REPETITIVE CHECK REQ ONCE EACH FLIGHT DAY. SWAPPED LT AND RT GCU, NO HELP. REINSTALLED TO ORIG POSITION. REMOVED AND REPLACED IDG PER AMM, OPS CHECKS OK NOW. MALF-4P0 POS-RT CTL-947297001.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,001 hrs · 5,297 cycles

ELECTRICAL ODOR IN REAR BUSINESS CLASS LAV. INSPECTED WATER HEATER AND LAV FLUSH MOTOR. NO ODOR DETECTED. INSTALLED LAV SEALS, ALL OK.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 37,958 hrs · 5,293 cycles

E-PATH LIGHT INOP AT SEATS 1GF THRU 3GF. FOUND CHARGER M730 AT FAULT. REPLACED SAME PER WDM. CHECKS NORMAL PER AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 37,048 hrs · 5,198 cycles

SEAT ROW 17GF HAS A BURNT OUT EMERGENCY LIGHT. RELAMPED SEAT ROW 17GF EMERGENCY LIGHT IAW B767 MM 33-51-10-962-105. OPS CHECK GOOD IAW B767MM 33-51-10-962-105.

Part: HEAT EXCHANGER — DAMAGED (NR 1 ENGINE) · airframe 37,047 hrs · 5,197 cycles

DURING TAKEOFF ROLL AT APPROX 40 KTS FELT SHUTTER AND ACFT VEERED TO THE LEFT. THROTTLES PULLED BACK AND TAKEOFF ABORTED. LT ENG LEAKING FUEL FROM COWLING. LT ENG SHUT ITSELF DOWN. MAINTENANCE FOUND FOHE BAD. AFT SECTION OF HEAT EXCH WELD FAILED/5IN DIA DISC BLOWN OFF BACK. MAINTENANCE IN PROGRESS. FOUND LT ENG FUEL/OIL HEAT EXCHANGER LEAKING. REMOVED AND REPLACED HEAT EXCHANGER PER M/M NEEDS LEAK CK 475905. PERFORMED ENG STALL SURGE INSP PER FIM 71-05-00 THRU BLOCK 3 631428. PERFORMED LEAK CK AND ENGINE RUN.

Part: START VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 36,657 hrs · 5,153 cycles

L START VALVE LIGHT REMAINS ILLUMINATED, NO AIR DROP NO ROTATION, RETURN TO GATE. START VALVE INOP FWD TO MCO AND PLACARD IAW MEL 80-00-02. REMOVED AND REPLACED LEFT ENG START VALVE PER AMM, OPS CHECK OK.

Part: BLADES — DAMAGED (ENGINE FAN) · airframe 35,347 hrs · 5,008 cycles

RIGHT ENGINE BIRD INGESTION, ENGINE VIBS, DIVERTED TO DKR 3 FAN BLADES ARE DAMAGED BORO WAS GOOD. REPLACED FANBLADE SETS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,070 hrs · 4,635 cycles

RIGHT SIDE AFT 3 EXTERIOR EMERGENCY LIGHTS INOP. CHARGED BATTERY PACKS, OPS CHECK GOOD IAW B767-300 MM 33-51-07 WDM 33-51-00.

Part: LENS — MISSING (EMERGENCY SIGN) · airframe 32,070 hrs · 4,635 cycles

RT OVERHEAD AISLE EMERGENCY EXIT SIGN MISSING LENS. REMOVED AND REPLACED EMERGENCY EXIT SIGN LENS IAW DAL B767-300 AMM 33-51-01,TIMCO HMV CARD 41147

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,070 hrs · 4,635 cycles

SEAT EMERGENCY LIGHTS AT 1A, 2A, 4A, 3G, 17G ARE INOP. RELAMPED SEAT EMERGENCY LIGHTS AT SEATS 1A, 2A, 4A, 3G, AND 17G, NO FAULTS NOTED ON OPS CHECK IAW B767-300 AMM 33-51-10.

Part: WIRE — DAMAGED (DOOR ACTUATOR) · airframe 32,070 hrs · 4,635 cycles

OXYGEN MASK AT FWD MID LAV AND 28AB DID NOT DEPLOY. RECONNECTED CONNECTOR FOR FWD MID LAV DOOR ACTUATOR IAW B767-300 AMM 35-21-16. REPAIRED WIRES FOR 28AB DOOR ACTUATOR IAW SWPM 20-10-13. MANUAL DEPLOY GOOD IAW B767-300 AMM 35-21-00.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 32,070 hrs · 4,635 cycles

LT AND RT EMERGENCY EXIT SQUIB TEST DOES NOT WORK ON TEST 1 OR TEST 2. DISARMED OFFWING ZSCOPE SYSTEM IAW B767-300 AMM 25-65-00. REMOVED AND REPLACED M961 BATTERY CHARGER IAW B767-300 AMM 25-65-17. RE-ARMED OFFWING ESCAPE SYSTEM IAW B767-300 AMM 25-65-00. OFFWING ESCAPE SYSTEM SQUIB TEST OK IAW B767-300 AMM 25-65-00-442-010-001 SUB TASK 732-017-001.

Part: FUSE — BLOWN (CABIN) · airframe 32,070 hrs · 4,635 cycles

EMERGENCY LIGHTS L979, L9700, L975, L9699, L308, L333 ARE INOP. TROUBLESHOT SYSTEM AND DETERMINED PICO FUSE BLOWN. REMOVED AND REPLACED FUSE IAW DAL B767-300 MM 33-51-07. OPS CHECK GOOD IAW B767-300 AMM 33-51-07.

Part: WIRE — BROKEN (CABIN) · airframe 32,070 hrs · 4,635 cycles

OVERHEAD LT AISLE EMERGENCY LIGHTS HAS BROKEN WIRE AT STA 1197+132. SPLICED REPAIRED BROKEN WIRE AT LT AISLE EMERGENCY LIGHT STA 1197+132 IAW B767-300 SWPM 20-30-12. NO FAULTS NOTED ON OPS CHECK IAW B767-300 AMM 33-57-05.

Part: PIN — LOOSE (EVAC SLIDE) · airframe 32,070 hrs · 4,635 cycles

L2 SLIDE LOCK BALL PINS ARE LOOSE. REMOVED AND REPLACED L2 DOOR SLIDE/RAFT.

Part: POWER SUPPLY — FAILED (ROW 4AB) · airframe 31,792 hrs · 4,599 cycles

EMERGENCY LIGHTS IN AFT SECTION OF BUSINESS CLASS INOP. REPLACED BATTERY POWER SUPPLY PACK M11558, LIGHTS NOW CHECK GOOD PER AMM.

Part: UNKNOWN — ODOR (MID CABIN) · airframe 29,974 hrs · 4,378 cycles

INFLIGHT FLIGHT ATTENDANT REPORTS AN ELECTRICAL/BALLAST ODOR IN MID CABIN ON LEFT SIDE. CAN NOT DUPLICATE FAULT. RAN ALL ELECTRICAL EQUIPMENT IN MID GALLEY AND CHECKED FOR ANY LIGHT THAT WERE OUT OR FLICKERING. NO FAULT NOTED. DID NOT DETECT ANY ODOR.

Part: APU — LEAKING · airframe 28,751 hrs · 4,225 cycles

SMOKE REPORTED COMING FROM APU. FOUND EXCESSIVE OIL IN TAIL PIPE REMOVED AND REPLACED APU PER AJIC 7952. APU OPS NML NO LEAKS NOTED AIR AND GEN OPS OK.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 27,596 hrs · 4,076 cycles

STRONG ELEC SMELL IN AFT CABIN DURING CLIMB-OUT. INSPECTED A/C DURING VERIFICATION FLT. TURNED ON ALL OVENS/COFFEE MAKERS/AND CHILLERS IN AFT GALLEY. OPENED UP CEILING PANELS IN AFT GALLEY/CABIN. CHECKED DOOR HEATERS DUCTING/OXY/CANISTERS AND FANS. CHECKED ENTIRE CABIN/COCKPIT/LWR E/E AND FWD CARGO. CHECKED CHILLER VENTS, NO ODOR PRESENT. ONLY ODOR NOTICED WAS A BURNT SMELL FROM COFFEE MAKER 1/2. REMOVED COFFEE MAKER AND FOUND HEAVY CRUD NEAR HEAT ELEMENT. REMOVED ALL COFFEE MAKERS AND CLEANED UNDERBASES NR 1 AND 2 WERE REPLACED.

Part: TEAR STRAP — DAMAGED (BS 1417 S2R) · airframe 27,024 hrs · 4,004 cycles

WHILE ACCOMPLISHING A LAP JOINT REPAIR PER SRM AT STA 1417, S-2R, THE TEAR STRAP WAS INADVERTENTLY CUT. THE DAMAGED PART OF THE TEAR STRAP WAS CUT OUT AND A TRIPLER WAS INSTALLED AS PART OF THE LAP JOINT REPAIR.

Part: A/C PACK — ODOR · airframe 26,600 hrs · 3,948 cycles

MUSTY SMELL FROM PACKS BELOW 5000FT TO LANDING RUN PACKS FOR 15 MIN ALL IND NORMAL NO STRONG SMELL METIONED CABIN ANYMORE ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 26,543 hrs · 3,941 cycles

DURING T/O FROM ATL, NR 2 ENG HAD SURGE EVENT RETURNED TO ATL FOR INSPECTION. REMOVED HPC 1 - 2 - 3 AND 12 BORO PLUGS. PERFORMED BOROSCOPE INSP NR 2 ENG S/N 704750 HPC STAGES 1 AND 12 AND HPC STG 1 FOUND DAMAGE TO HPC STG 1 BLADES BEYOND AMM LIMITS, REF ITE 010 THIS LOG PAGE. REINSTALLED THE HPC 1 - 2 - 3 AND 12 BOROSCOPE PLUGS . REPLACED NR 2 ENG PER TRANSMITTAL NR 01T161.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,412 hrs · 3,925 cycles

ROWS 4 5 AND 6 INSEAT EMERGENCY LIGHT INOP FAIL TEST REPLACED PWR SUPPLY.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 25,528 hrs · 3,819 cycles

DURING TAXI, MASKS AT SEAT 19AB DROPPED. OXY MASKS AT SEAT 19AB RESTOWED OK. ETOPS CATEGORY (F): ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: ANTENNA — FAULTED (WX RADAR SYS) · airframe 25,363 hrs · 3,801 cycles

WX RADAR INOP SHOWS ANT FAULT. REPLACED WEATHER RADAR ANTENNA AND TRANSCEIVER IAW MM. ALL CKS NORMAL ETOPS CATEGORY (B): DIVERSION OR TURNBACK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,334 hrs · 3,558 cycles

RT WING CTR OVERWING EMERGENCY LIGHT HAS AFT BULB INOP. RELAMPED, CKS OK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,334 hrs · 3,558 cycles

EXT EMERGENCY LIGHT INOP ON LT SIDE, FIRST LIGHT AFT OF WING. RELAMPED OPS OK.

Part: MODULE — OUT OF POSITION (RUDDER) · airframe 21,390 hrs · 3,321 cycles

RUDDER RATIO EICAS MSG WITH RUDDER RATIO LIGHT ILLUMINATED ON OVERHEAD PANEL. FOUND RUDDER RATIO MODULE IN TEST. PUT SW TO NORM. MSG AND LIGHT EXT. T/S PER FIM RUDDER RATIO CHECKS GOOD.

Part: DISPLAY — FAILED (COCKPIT RT) · airframe 19,683 hrs · 3,099 cycles

CO-PILOTS CDU WENT BLANK DID NOT COME BACK ON. REPLACED WITH NEW CDU. OPS CKS OK.

Part: APU — CONTAMINATED (APU BAY) · airframe 19,480 hrs · 3,074 cycles

APU FAULT ON START OF LEFT ENGINE. APU WOULD NOT RESTART. REMOVED PLASTIC BAG FROM INLET AND REPLACED SURGE VALVE.

Part: INDICATOR — FAILED (COCKPIT) · airframe 17,880 hrs · 2,857 cycles

AFTER TAKEOFF CAPTS VSI WAS INTERMITTENT AND ON THEN OFF. APPROX 15 MIN AFTER T/O CREW SMELLED ELECTRIC SMELL AND PULLED THE P-6-E5 CB FOR CAPT VSI SMELL THEN DISSIPATED. REPLACED CAPT VSI, CHECKS OK.

Part: ENGINE — LEAKING (NR 2) · airframe 17,417 hrs · 2,797 cycles

ENGINE SHUTDOWN BY CREW AT CRUISE DUE TO OIL QTY DROPPED TO 0 AND OIL PRESSURE STARTED FLICKERING. REPLACED ENGINE.

Part: ENGINE — LEAKING (NR 1) · airframe 16,750 hrs · 2,708 cycles

DURING L/O CHECK OIL LEAK IN D-SUMP AREA BEYOND M/M LIMITS. REPLACED ENGINE.

Part: SENSOR — MALFUNCTIONED (NR 1 SLAT) · airframe 14,034 hrs · 2,320 cycles

LEADING EDGE SLAT ASYM ON TAKEOFF OUT OF EHAM. LIGHT CAME ON GOING FROM FLAPS 1 WITH FLAP HANDLE UP. PSEU LEFT SLAT 1 INBD SENSOR 282 PER AMM REPLACED SENSOR PER AMM. OPS OK PSEU NO FAULTS ALL NEAR/FAR INDICATIONS GOOD FOR DIFFERENT SLAT POSITIONS. OK FOR SERVICE. SLATS CHECKED, NO ACTUAL ASYMMETRY.

Part: WHEEL — DAMAGED (NR 1MLG) · airframe 11,437 hrs · 1,944 cycles

LEFT SHEARED ON MAIN WHEEL. REPLACED NR 1 MAIN WHEEL AS PER MM REF 32-45-004-001.

Part: PROXIMITY SENSOR — FAULTY (LE FLAPS) · airframe 9,122 hrs · 1,575 cycles

EN ROUTE TO LGW SLAT ASSY LIGHT ILLUMINATED AND FLAP POSITION INDICATOR BEGAN BOUNCING BETWEEN 0 AND .5 DEGREE. A/C HAS EXTENSIVE HISTORY OF THIS PROBLEM. A/C DIVERTED TO JFK AS A PRECAUTION. FAULTS 276285 CARD 10 CARD AND SW PREV REPLACED. REPLACED PS BITE CK OK. INSPECTED CONNECTOR P4434J FOUND SILVER PINS INSTALLED. PINS FREE AND CLEAR OF CORROSION AND CLEAN. REINSTALLED CONNECTOR.

Part: PSEU — LOOSE (E/E BAY) · airframe 5,689 hrs · 986 cycles

DURING CLIMB AT FL140 AND 340 KNOTS THE FLAP IND MOVED TO 1/2 WITH ROLL MOTION L/E FLAP CAUTION LIGHT/EICAS MSG L/E FLAP ASYMMETRY MSG AS A/C SLOWED TO 250 KNOTS THE FLAP IN CYCLED UP AND BACK 1/2 4 TIMES/C PER FIM 27-81-00 FIG 107. FOUND FAULT AT PSEU 276 THEN PSEU BLANKED. FOUND PSEU LOOSE IN RACK. REMOVED AND REPLACED PSEU AND ALL OPS OK.

Part: LINE — CRACKED (#7 SPOILER) · airframe 783 hrs · 125 cycles

RT HYD SYSTEM FLUID LOSS.REPLACED NO.7 SPOILER ACTUATOR LINE WITH TEMP LINE.FWD TO MCO. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 783 hrs · 125 cycles

NR 7 SPOILER CONTROL ACTUATOR PRESSURE LINE AT ACTUATOR PULLED OUT OF B-NUT BREAKING LINE AND CAUSING COMPLETE LOSS OF RIGHT HYDRAULIC SYSTEM FLUID. REPLACED LINE.

Part: HYDRAULIC LINE — SEPARATED (HYDRAULIC SYS) · airframe 492 hrs · 83 cycles

RT HYDRAULIC SYSTEM QUANTITY AND PRESSURE WENT TO ZERO DURING DESCENT AND APPROACH. ACCOMPANIED BY A SPOILERS EICAS MESSAGE. NO ABNORMAL CONTROL INPUTS WERE FELT. ACCOMPLISHED PROCEDURES PER POM. FOUND HYD PRESSURE LINE TO NR 7 SPOILER PCA SEPARATED FROM PCA. LINE FAILED AT SWAGE. REPLACED SAME.