N863DA
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| DELTA AIR LINES, INC. (DALA) | Operator | 2013-07-12 – 2013-07-12 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2013-07-12 – 2013-07-12 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EMERGENCY EXIT LIGHTS/SIGNS AT 3L/4L DOORS FAIL DURING LIGHTS TEST REPLACED BATTERY PACKS AT 3L/4L DOORS PER B777 AMM 33-51 ALL LIGHTS NOW CK GOOD
(AIRCRAFT 7004, L/P 1479043) DURING MONITOR INSPECTION FOR LOG 7152450 FOUND T/R DAMAGE AT APPROX. 10 O'CLOCK POSITION ON #1 ENGINE CRACK IS APPROX. 15 1/2" LONG RUNNING FWD FROM TRAILING EDGE. CORRECTIVE ACTION: STARTED CURE CYCLE FOR PERMANENT REPAIR IAW BOEING 777-200 SRM 54-32-01-2R AND 51-70-05-2R PROCEDURE 12.
DOOR FLIGHT LOCK 1R STATUS MESSAGE. ADJUSTED THE TARGET. OPS CHECKED GOOD.
R1 DOOR FLIGHT LOCK FAULT. INSPECTED FLIGHT LOCK PROXIMITY SENSORS. FOUND THE TARGET GAP ON HIGH SIDE. ADJUSTED IAW MM 52-71-01.
DOOR FLIGHT LOCK 1R MESSAGE REOCURRING ISSUE. TIGHTENED DOOR LOCK SWITCH CONNECTOR .
(AIRCRAFT 7004, L/P 1406821) WHILE CLOSING #1 FAN FOUND VISABLE DAMAGE TO LT OUTBD UPPER FAN COWL. CORRECTIVE ACTION: APPLIED PERMANENT REPAIR WITH REFERENCE TO B777 SRM 51-70-04-2R.
DOOR FLIGHT LOCK 1R MESSAGE. ERASED MESSAGE IAW FIM 52-11.
(AIRCRAFT 7004, L/P 1351578) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. CORRECTIVE ACTION: FOUND EMERGENCY FLOOR LIGHT COVER DAMAGED. R&R COVER.
(AIRCRAFT 7004, L/P 1351575) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. CORRECTIVE ACTION: FOUND EMERGENCY FLOOR LIGHT COVER DAMAGED. R/R COVER.
(AIRCRAFT 7004, L/P 1351580) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / INTERIOR. CORRECTIVE ACTION: FOUND COVER BROKEN. REPLACED COVER.
(AIRCRAFT 7004, L/P 1351577) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / INTERIOR. CORRECTIVE ACTION: FOUND FLOOR LIGHT COVER DAMAGED AT 205 AND R/R COVER.
(AIRCRAFT 7004, L/P 1351585) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / INTERIOR. CORRECTIVE ACTION: FOUND EMERGENCY LIGHT COVER BROKEN. REPLACED COVER.
(AIRCRAFT 7004, L/P 1351579) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / INTERIOR. CORRECTIVE ACTION: FOUND EMERGENCY FLOOR LIGHT COVER DAMAGED R/R COVER.
SHIP 7004 -FIRE- FWD GALLEY OVEN FIRE DUE TO MELTED AND SPILLED CHOCOLATE DURING OPERATION. EXTINGUISHER USED (REFERENCE LOGPAGE 5656327) / FIRE EXTINGUISHED /C/B PULLED / FLIGHT CONTINUED. CORRECTIVE ACTION: REMOVED AND REPLACED OVEN LOCATION 401 PER B777 AMM 25-35. OK FOR SERVICE (REFERENCE LOGPAGE 1022470).
EMERGENCY EXIT COVER DIFFUSER LENS MISSING. REPLACED LENS COVER. LP 0972574
CHECK PED 4R RIGGING. DUE TO CONFIRMED REPORTS OF EMERGENCY LIGHTS ILLUMINATING AT 4R / PED WITH EMERGENCY LIGHT SW ON P5 ARMED AND 4R DOOR MODE SELECT HANDLE IN DISARMED POSITION AND DOOR HANDLE TO THE FULL OPEN POSITION. CORRECTIVE ACTION: WRANG OUT S52121 PINS 7, 8 REDS M OHMS. REMOVED MODE SELECT SW. PER B777 AMM 52-11-28-000-801 (269944). REINSTALLED NEW S52121 SWITCH IAW B777 AMM 52-11. TEST OK.
(AIRCRAFT 7004, L/P 0919748) WORKING INSPECTION OF EEPLS LENSES, FOUND EMERGENCY LOWER FLOOR PROXIMITY LIGHT ASSY DAMAGED, AFT OF FLIGHT ATTENDANT CREW REST DOOR. REMOVED AND REPLACED LOWER PROXIMITY LIGHT ASSY.
(AIRCRAFT 7004, L/P 5338782) 4L DOOR FLIGHT LOCK INOP. REMOVED BUSTLE TO MANUALLY UNLOCK FLIGHT LOCK IN ORDER TO OPEN DOOR REPLACED FLIGHT LOCK ACTUATOR PER B777 AMM 52-11-26, OPS CHECK GOOD.
(AIRCRAFT 7004, L/P 5338771) MTC RECEIVED VERBAC REPORT FROM CLEANING CREW THAT DOOR 4L/R EMERGENCY LTS WERE ON. UPON ENTERING DR4L/R LOCATION FOUND EMERGENCY LTS NOT ILLUMINATED. PERFORMED OPS TEST PER B777 AMM33-51. LTS AT DOOR 4 L/R CHECK OK.
(AIRCRAFT 7004, L/P 4683509) DOOR FLIGHT LOCK 2L STATUS MESSAGE IN CRUISE FLIGHT APPROXIMATELY 1 HOUR AFTER DEPARTURE. / REPLACED FLIGHT LOCK ACTUATOR IAW B777 AMM 52-11-26.
(AIRCRAFT 7004, L/P 4841186) EMERGENCY SIGN LIGHTS INOP AT DOORS 2R & 2L. REPLACED POWER BASE AT 2L AND BATTERY AT 2R PER AMM 33-51.
(AIRCRAFT 7004, L/P 4709426) WITH POWER CHANGES CLIMBS AND DESCENT ACRID ORDER THROUGHOUT AIRCRAFT. BOROSCOPE INSPECTION REQUIRED PER FIM TASK 71-05-20-810-822. REMOVED IPC AND HPC BOROSCOPE PLUGS IAW AMM 72-00-00 PERFORMED VISUAL INSPECTION FOR OIL LEAKS WITH BORESCOPE. FOUND LEAKS BETWEEN COMPOSER STAGES IP3 AND IP5. REINSTALLED BOROSCOPE PLUGS IAW AMM 72-00-00 WIP 813089 RAN BOTH ENGINES AND APU NO ODOR DELECTATED WITH PACK FULL HOT OR COLD.
UNIDENTIFIABLE ODOR OCCURRED THROUGH ENTIRE DESCENT, UNTIL LANDING. HORRIBLY STRONG ODOR. STRONG OIL, ORGANIC, MUSTY ODOR. FOLLOWED AMM 21-00-01-100-801, STEPS 15 TO 19, STEP 15 LT & RT ENGINE RUNNING, BOTH PACKS OFF & ON, NO OIL CONTAMINATION FROM LEFT & RIGHT, GROUND CONDITIONED AIR CONNECTOR, PERFORMED HIGH POWER RUN OF THE ENGINES, NO ODOR OF OIL NOTED. VISUALLY INSPECTED OZONE CONVERTERS AND RECIRCULATION FAN FILTERS, NO OIL CONTAMINATION. INSPECTED APU COMPARTMENT, NO EXTERNAL LEAK NOTED, OIL WAS FULL. REMOVED GROUND PNEUMATIC AIR CONNECTOR CHECK VALVE AND APU BLEED ON, NO CONTAMINATED OIL OR ODOR. INSPECTED BLEED DUCT, DOWN STREAM OF APU, NO OIL CONTAMINATED. OK FOR SERVICE.
ACRID ODOR, PERIODICALLY DETECTED IN THE FLT DECK. POSSIBLY OUTPUT FROM LT PACK OR DUCT SYSTEM. REMOVED APU SURGE VALVE, NO CONTAMINATION FOUND IN APU DUCTS. REMOVED LEFT ENG IP CHECK VALVE, NO CONTANMINATION FOUND IN DUCTS. R & R THE LT OZONE CONVERTER, OPS AND LEAK CHECKED GOOD IAW MM 21-73. REPLACED UPPER RECIRCULATION FILTERS IAW IAW AMM 21-25. RAN BOTH ENGINES AND REMOVED APU AIR. RAN PACKS WITH ENGINE BLEED, AIR WENT FULL TEMP RANGE WITH PACKS, NO ODOR DETECTED. REPLACED THE RT SIDE HEPA FILTERS IAW MM 21-25 SYSTEM CHECKED GOOD.
R3 DOOR FLIGHT LOCK STATUS MESSAGE. REMOVED AND REPLACED THE R3 DOOR FLIGHT LOCK ACTUATOR IAW AMM 52-11, OPS CHECKED GOOD IAW AMM 52-11-26, LOCK OPERATED OK.
STATUS MSG: DOOR FLIGHT LOCK 3L. REPLACED 3L FLIGHT LOCK ACTUATOR PER MM 52-11-26, LOCK TEST GOOD.
DURING PRE-FDA INSPECTION, GALLEY A-2 COMPARTMENT A719 FWD HOLD DOWN BRACKET EXHIBITING CORROSION ON UPPER SURFACE (ACTION ITEM REQUEST ITEM 1). GALLEY A-2 COMPT A719 FWD HOLD DOWN BRACKET REMOVED AND REPAIRED AS PER AMM 25-31-03.
CABIN SEAT TRACK AT BS 1455 TO 1505, RBL 74 CORRODED. ER/A 566931-14 PRI REV O AND REV 1 COMPARED WITH FINAL ER/A 566931 REV ORIGINAL AND FOUND COMPLIANCE.
CABIN SEAT TRACK, BS 1520 - 1640, RBL 108 FOUND CORRODED. REPAIRD IAW ER/A 566931-14, PRI REV 0, AND REV 1
MAIN CABIN SEAT TRACK, BS 1455 - 1497, RBL 108 FOUND CORRODED. REPAIRED IAW ER/A 566931-14, PRI REV 0, REV 1, AND REV ORIGINAL.
L3 DOOR FLIGHT LOCK STATUS MESSAGE AFTER TAKE OFF. R & R THE DOOR FLIGHT LOCK IAW MM 52-11-26. OPS CHECKED GOOD.
R4 DOOR FLIGHT LOCK STATUS MESSAGE IN FLIGHT . CARRIED OUT A FLIGHT LOCK GROUND TEST, ALL DOORS LOCKING UNLOCKING NORMAL. STATUS MESSAGE ERASED. OK FOR SERVICE.
AFT CROSSFEED VALVE IS INTERMITTENT IN OPERATION. THE VALVE FAILED TO OPEN WHEN COMMANDED. AFTER SEVERAL CYCLES OF AFT CROSSFEED VALVE SWITCH, THE AFT VALVE OPENED, EICAS AND STATUS MESSAGES WERE PRESENT, WHEN THE VALVE IS COMMANDED, THE VALVE FAILED TO CLOSED. AFTER SEVERAL CYCLES OF THE AFT CROSSFEED SWITCH, THE VALVE CLOSED. VALVE DISAGREEMENT LIGHT AND DISPLAY OF FUEL SYSTEM SCHEMATIC CONFIRM FAULT. FWD CROSSFEED VALVE OPS NORMAL. R & R THE AFT CROSSFEED VALVE IAW AMM 28-22. ALL CDCCL REQUIREMENTS COMPLIED IAW SFAR 88. OPS CHECKED NORMAL. OK FOR SERVICE.
TROUBLESHOT IAW FIM 32-53-00-810-810. COMPLETED MLG STEERING TEST, NO FDE'S PRESENT. R & R THE RT MLG STEERING PCA IAW AMM 32-53-03-000-801. PERFORMED MLG STEERING FAULT ISOLATION PROCEDURES 32-53-00-810-810. NO FAULTS PRESENT. OK FOR SERVICE.
DURING SVC CHK FOUND 2 CRACKS IN LT WING TO BODY FAIRING PN 191DL. REPAIRED MPN 149W1212-5 PANEL PER ERA 561376-14 PER SRM 53-00-70.
DURING WALK AROUND CHECK, FOUND THE LEFT WING PANEL 511AB DAMAGED. REMOVED AND REPLACED THE PANEL IAW SRM 57-41-01.
EMERGENCY LIGHT AT SEATS 1D TO 7D INOPERATIVE. R & R THE BATTERY AND CHARGER ASSY IAW AMM 33-51. OPS CHECKED GOOD.
L4 DOOR EXTREMELY LOUD NOISE COMING FROM LOWER HALF FRONT AND BACK OF DOOR SEALS. NEVER DISSIPATES THROUGHOUT FLIGHT. TROUBLESHOT IAW TSM 52-09-01. PERFORMED A FLASHLIGHT CHECK OF DOOR SEAL AND OPS CHECKED WITH NO DAMAGE FOUND. CLEANED THE SEAL AND VERIFIED SEAL IN GOOD CONDITION.
EMERGENCY LIGHT LENS DAMAGED. REPLACED THE LENS. CHECKED OK.
EMERGENCY LIGHT LENS DAMAGED. REPLACED THE LENS. CHECKED OK.
EMERGENCY LIGHT LENS DAMAGED. REPLACED THE LENS. CHECKED OK.
FLUORESCENT BULB SHORTED CAUSING FUMES IN F/A CREW REST AREA. REPLACED CREW REST NR 2 BUNK LIGHT ASSEMBLY.
EMERGENCY EXIT LIGHT AT SEAT 34D MISSING. REPLACED LIGHT ASSEMBLY.
L3 DOOR, LEFT OUTSIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS.
EMERGENCY FLOOR LIGHTING DAMAGED AT POSITION 405. REPLACED EMERGENCY LIGHTING LENS COVER.
FOUND EMERGENCY FLOOR LIGHT LENS MISSING NEAR THE SEAT 57. INSTALLED A NEW LENS. LIGHT CHECKED GOOD.
EMERGENCY EXIT SIGN COVER LOOSE LOCATIONS:01R. EMERGENCY EXIT COVER FIXED.
EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:407. ADJUSTED LIGHT OPS CHECK GOOD.
EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:405. ADJUSTED LIGHT OPS CHECK AND LENS OPS CHECK GOOD.
DURING PDC CHECK, L1 DOOR, AFT SIDE EMERGENCY EXIT SIGN MISSING LENS. INSTALLED MISSING EMERGENCY EXIT SIGN DOOR 1 LEFT.
ROW 43D EMERGENCY LIGHT MOUNT BROKEN. SECURED EMERGENCY LIGHT MOUNT IAW CMM 25-27-89.
FOUND EMERGENCY LIGHT AT R1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. SYSTEM OPERATION IS NORMAL.
PASSENGER CABIN BS 1444-1480, RBL 108 SEAT TRACK FOUND CORROSION AT MULTIPLE LOCATIONS. SEAT TRACK REPAIRED IAW SRM 53-00-52, REPAIR 4, SRM 51-40-02 AND ER/A 543546-14 PRI REV 0.
PASSENGER CABIN, BS 1444-1557, RBL 74 SEAT TRACK FOUND CORROSION AT MULTIPLE LOCATIONS. SEAT TRACK REPAIRED SRM 53-00-52, REPAIR 4, SRM 51-40-02 AND ER/A 543546-14, PRI REV 0.
PASSENGER CABIN BS 976, RBL 74, SEAT TRACK FOUND CHAFING. SEAT TRACK REPAIRED IAW SRM 53-00-52, REPAIR 3, SRM 51-40-02 AND ER/A 543546-14, PRI REV 0.
PASSENGER SEATS 10-12 LT AND RT FLOOR EMERGENCY LIGHTS INOPERATIVE. POWER SUPPLY M33098 FAILING. REMOVED IAW AMM 33-51-06. CEILING PANEL OPEN AT DOOR 2R. WIP 588392. REPLACED FUSE IAW AMM 33-51-06. OPS NORMAL, CLOSED ACCESS. OK FOR SERVICE. 1888895.
DURING A MAINTENANCE VISIT, THE 4L DOOR EMERGENCY LIGHT OF POWER SUPPLY WAS FOUND TO BE WEAK. MAINTENANCE REPLACED THE BATTERY PACK. SYSTEM OPERATION WAS NORMAL AFTER THE BATTERY PACK WAS REPLACED.
SEAT 5B EMERGENCY LIGHT MISSING LENS AND BULB. SEATS 10BC-1414BC EMERGENCY AISLE LIGHTS INOPERATIVE. RELAMPED SEAT 5B. REPLACED CHARGER AND BATTERY M33098. SEATS 10BC-14BC CK OK.
DURING A MAINTENANCE VISIT, THE EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 12B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE PROXIMITY LIGHT ASSEMBLY. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT WAS REPLACED.
DURING EMERGENCY LIGHT TEST FOUND LIGHTS INOPERATIVE, ROW 10 THROUGH 13. REPLACED POWER SUPPLY ABOVE DOOR 2R AND TESTS OK.
ODOR IN AFT CABIN FOUND RT LWR RECIRCULATION FAN FAILED. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.
F/A REPORTED BURNING RUBBER ODOR IN AFT GALLEY AREA. SHUTOFF OVENS, LIGHTS, IFE, RECIRC FANS. ODOR DISSAPATED. TURNED LIGHTS BACK ON AND STILL NO SMELL. T/S SYS. CHECKED LIGHTS OVENS IFE AND RECIRC FANS. FOUND LATCHED MSG FOR LOWER RT RECIRC FAN OVERHEATED. MX MSG 21-24700. DEACTIVATED LWR RT RECIRC FAN AND FWD TO MCO AND PLAC IAW MEL 21-25-01. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.
LEFT AFT BOOST PUMP LIGHT ON PUSHBACK RETURNED TO GATE. FOUND LEFT AFT FUEL BOOST PUMP AND ELECTRIC CONNECTOR PINS BURNED. REPLACED LEFT FUEL BOOST PUMP AND CONNECTOR DM28102 OPS CKS NORMAL.
LEFT AFT FUEL BOOST PUMP LIGHT ON PUSHBACK, RETURNED TO GATE. FOUND LEFT AFT FUEL BOOST PUMP AND ELECTRIC CONNECTOR PINS BURNED. REPLACED LEFT FUEL BOOST PUMP AND CONNECTOR DM28102. OPS CKS NORMAL.
NOTICED ELEC BURNED ODOR AND SMOKE IN AFT CABIN AREA, FOUND APU BATTERY THERMAL DISCHARGED. REPLACED APU BATTERY AND CHARGER. FOUND APU BATTERY WITH BURN SPOT ON BACK AND IN CONTACT WITH INSULATION REPLACED APU BATTERY AND CHARGER PER MM. REMOVED BUR INSULATION. POSITIONED INSULATION CORRECTLY
BORO NR 1 ENG HPC DUE TO PARAMETER SHIFT ON TRENDS AMM 72-00-00-200-802-R00. FOUND DAMAGE TO IPT NOZZLE GUIDE VANES BEYOND LIMITS REF M/M 72-000-00-200-810-R00-00 CHANGED ENGINE NR 1 PER TRANSMITTAL 11T00.
GALLEY 401 OVEN 2 AFTER COOKING 8 MINS MADE HIGH PITCH BUZZ THEN QUIT W/ASSOCIATED BURNT WIRE ODOR NO FAULT LIGHT.
NR 8 WHEEL ASSY MISSING ON ARRIVAL ATL. NOTIFIED BY TLV A WHEEL HUBCAP FOUND ON RUNWAY. C/W BURST TIRE INSPECTION ON LOG ITEM 030 INSTALLED TIRE ASS PER M/M. INSTALLED NEW NR BRAKE AND SLEEVE IAW 32-45-07. INSTALLED TRANSDUCER PER AMM 32-42-05, ALL CHECKS GOOD. REMOVED AND REPLACED CENTER AXLE RT MLG PER MM 32-11-26-400-802 AND 32-11-26-000-802.
TOWER REPORTED SMOKE COMING FROM AIRCRAFT MAIN GEAR AFTER VERY SMOOTH LANDING. FOUND RESIDUAL DEICING FLUID ON WHEELS AND BRAKES. CLEANED BRAKES. OK FOR SERVICE. NO DEFECTS NOTED.
ANTI-ICE ENG L EICAS MSG ON ENG SHUTDOWN. MTC MSG 30-10101 VLV FAILED IN CLOSED POSITION. NO ICE NOT AVIAL TRIED TO MEL PER 30-21-01B. MTC UNABLE TO C/W MEL ENG RUN. DEFERRED TO CREW PROCEDURE WHICH FAILED AFTER PUSH BACK. MTC REPLACED L ENG ANTI ICE VALVE AND REMOVED MCO.
NR 1 ENG SHOWED TREND SHIFT. C/W BORO OF HPC COMPRESSOR. FOUND 6TH STAGE PC COMPLETELY FO OUT. OUT OF LIMITS IAW MM. NR 1 ENG S/N 51177 ENG CHANGE REQUIRED. C/W ENG CHANGE IAW TRANS 11T003.
ELECTRICAL SMELL IN CABIN UPPER AFT FAN FWD TO MCO CB COLLARED REMOVED AND REPLACED FAN IAW MM OPS CK GOOD MCO AND PLACARD REMOVED ETOPS CATEGORY (F): ANY OTHER EVENT DETRIMENTAL TO ETOPS.
VIDEO SYSTEM IN CNTR SECTION 45-49 DID NOT WORK PROPERLY. FLICKERING ON AND OFF RESET NO HELP. UNFAMILIAR ODOR ASSOCIATED WITH THE FLICKERING. INSPECTED FOUND AVU UNDER SEAT 48 GHJ OVERHEATING CAUSING BURNING ODOR. REPLACED AVU LOADED SOFTWARE, CHECKS OK, ODOR GONE.
CREW REST SIDE LIGHT HAS BURNED END. REPLACED SAME.
EXCESSIVE OIL CONSUMPTION LEFT ENGINE DUE TO REPORT OF LEFT ENGINE HOC AND AT ROLLS ROYCE RECOMMENDATION, REPLACE THE LEFT ENGINE.
SMOKE COMING FROM VIDEO SCREEN OVERHEAD AT SEAT ROW 33G/32G ATL AMT'S. REMOVED AND REPLACED OVERHEAD MONITOR 32H AND VDU 5. OPS CHECK NORMAL.
AFTER HOOKING UP EXTERNAL POWER, NOTICED ARCING COMING FROM RECEPTICLE. DISCONNECTED CORD FROM A/C. RECEPTACLE HAD BURNED. REPLACED EXTERNAL POWER RECEPTACLE IAW M/M. OPS CHECK GOOD. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.
GALLEY FWD 2 DOOR CENTER OVEN OVERHEATS WHEN TURNED ON STRONG ELECT SMELL NOTICED BY FLT ATTEND. REPLACED OVEN IN MID GALLEY POS 1 OPS CHECK GOOD MCO AND PLACARD REMOVED ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS
ABORTED T/O DUE TO MAIN GEAR STEERING AND T/O WARN HORN. MTC MSGS 32-63010 AND 32-63020 ACTIVE. AUTO EVENT RT ACTUATOR FAILED. FWD TO MCO AND PLC. LT ACTUATOR WILL NOT LOCK. PERFORMED MDM BLOCK PROCEDURE TO ZE OUT AND LOCK.
CAPTS O2 MASK CAME APART WHEN TAKING FROM STOWAGE. CAPTS O2 MASK REPLACED LEAK CK CARRIED OUT
STRONG BURNING ODOR COMING FROM APPROXIMATE LOCATION OF ROW 44 FG FLOOR LEVEL. INSPECTED AREA AROUND 44 FG SUSPECT ROCKWELL COLLINS ENTERTAINMENT SYSTEM SEAT BOX CHECK ROCKWELL AVU - UPCUS AND WIRING. NO HEATING OR BURN SMELL ON COMPONENTSSYSTEM WORKS FINE. PERFORMED ROCKWELLCOLLINS CONFIDENCE CHECK. ALL NORMAL. UNABLE TO DUPLICATE PROBLEM. CONTINUE TO MONITOR SYSTEM.
LEFT ENG EEC C1 MAINT MSG 73-70211 - FMU. FOUND WIRE HARNESS W0816 CHAFING ON 1 OIL LINE APPROX 10 INCHES FROM CONNECTOR PM76001A ON FMU EVIDENCE OF ARCING EXIST. REPLACED WIRE W816-2001 R/R FROM DM73003A TO DM76001A PER WDM. CKS GOOD PER FIM 73-21-20-2 AND ENG RUN.
AIRCRAFT BEGAN A LOUD VIBRATION PASSING 15000 FT/305KNTS. LOUDEST ON LEFT SIDE OF AIRCRAFT AT ROW 12, OVERWING AREA. FOUND LEFT RAM AIR DOOR ACTUATOR CONTROL LINKS HAD SHEARED AND SEPARATED. REPLACED LT PACK RAM AIR DOOR AND MECHANISMS. RAN OPERATION CHECK, DOOR OPS NORMAL.