N363AA
Registered owner: ANDURIL INDUSTRIES INC, CA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
88 reports on file, 1995-01-30 – 2015-06-29.
Part: SHROUD — MISSING (CABIN) · airframe 110,736 hrs · 18,003 cycles
SEAT MOUNTED EMER EXIT LIGHT SHROUD AT 11B IS MISSING. INSTALLED SHROUD ON 11B EMER EXIT LIGHT & PERFORMED TEST IAW AMM 33-60-00. SYS CHECKED NORMAL.
Part: LENS — MISSING (CABIN) · airframe 110,736 hrs · 18,003 cycles
EXIT SIGN AT LT FWD OVERWING EXIT HAS LENS MISSING. R & R LT FWD OVERWING EXIT SIGN ASSEMBLY. PERFORMED OPERATIONAL CHECK IAW AMM 33-60-00.
Part: SHROUD — MISSING (CABIN) · airframe 110,736 hrs · 18,003 cycles
SEAT MOUNTED EMER EXIT LIGHT SHROUD AT 33B IS MISSING. INSTALLED SHROUD ON 33B EMER EXIT LIGHT. PERFORMED TEST IAW MM 33-60-0. SYS CHECKED GOOD.
Part: BATTERY — DISCHARGED (EXIT SIGN) · airframe 109,449 hrs · 17,752 cycles
EMERGENCY EXIT SIGN ABOVE FLIGHT DECK DOOR HAS LOW BATTERY. R & R EMER SIGN IAW AMM 33-51-02. SYS CHECKED NORMAL.
Earlier reports · 1995–2014 · 84 reports
2014
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 106,457 hrs · 17,230 cycles
LEFT AFT OVERWING EXIT, LOWER SIGN INOPERATIVE. REPLACED LAMP FOR LT AFT OVERWING EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 106,457 hrs · 17,230 cycles
RIGHT NR 4 DOOR AFT UPPER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR RT NR 4 DOOR AFT UPPER EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 106,457 hrs · 17,230 cycles
EMERGENCY EXIT SIGN AT FIRST CLASS GALLEY FLOOR INOPERATIVE. REPLACED LAMP FOR EMER EXIT SIGN AT FIRST CLASS GALLEY FLOOR. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 106,457 hrs · 17,230 cycles
RIGHT NR 1 DOOR FWD UPPER EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR FWD UPPER EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 106,457 hrs · 17,230 cycles
LEFT FWD OVERWING EXIT, LOWER SIGN INOPERATIVE. REPLACED LAMP FOR LT FWD OVERWING EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,457 hrs · 17,230 cycles
SEAT 41H EMER LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 41H EMER LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 106,457 hrs · 17,230 cycles
LOWER EMER SIGN AT A5 LAVATORY INOPERATIVE & HAS TRIM DAMAGE. REPLACED LAMP FOR LOWER EMER SIGN & REPAIRED TRIM. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 106,457 hrs · 17,230 cycles
LEFT NR 4 DOOR LOWER EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR LOWER EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: CHECK VALVE — WORN (FUEL SYSTEM) · airframe 106,114 hrs · 17,176 cycles
SJU INFLIGHT GIG JFK. CREW REPORTED UNCONTROLLED TRANSFER OF FUEL FROM RT MAIN TANK TO CTR TANK. EMERGENCY DECLARED FLIGHT DIVERTED SJU & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT CTR AUXILIARY LEAK DISCHARGE CHECK VLV & RT OVERRIDE PUMP MPN 5006286G. SYS GND CHECKED NORMAL, OPERATION CLOSED.
Part: WIRE — DAMAGED (NR 4 SLIDE) · airframe 105,998 hrs · 17,159 cycles
LEFT NR 4 SLIDE FAILED CHECK. FOUND WIRE W784-106-20 DAMAGED. REPAIRED WIRE IAW SWPM 20-10-11.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 105,998 hrs · 17,159 cycles
ESCAPE PATH LIGHT ON SEAT 34H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR ESCAPE PATH LIGHT ON SEAT 34H. OPERATIONS CHECKED NORMAL.
Part: BEACON — INOPERATIVE (CVR) · airframe 105,998 hrs · 17,159 cycles
COCKPIT VOICE RECORDER UNDERWATER LOCATOR BEACON INOPERATIVE DURING OPERATIONS CHECK. R & R UNDERWATER LOCATOR BEACON.
Part: SHUTOFF VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 105,520 hrs · 17,077 cycles
LAX INFLIGHT DFW-HNL CREW REPORTED LOSS RT ENG HPSOV & EICAS MESSAGE. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. PLACARDED RT HPSOV INOPERATIVE & LOCKED OUT RT THRUST REVERSER. REPLACED RT HPSOV & PRESS CONTROLLER. SYS GND CHECKED NORMAL OPERATION CLOSED.
2013
Part: LIGHT — DEFECTIVE (CABIN) · airframe 102,846 hrs · 16,667 cycles
LAVATORY FS3 EMERGENCY LIGHT DIM. REPLACED LAMP FOR FLOOR EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — DEFECTIVE (CABIN) · airframe 102,846 hrs · 16,667 cycles
LT AND RT CENTER AFT SEAT AFT GALLEY EMERGENCY LIGHT VERY DIM. REPLACED LAMPS FOR FLOOR EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 102,846 hrs · 16,667 cycles
ROW 37ABC, CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR ROW 37ABC CEILING LIGHT. OPS CHECK NORMAL.
Part: ENGINE — FAULTY (RIGHT) · airframe 102,712 hrs · 16,645 cycles
CREW REPORTED ODOR THROUGH OUT CABIN AND FLIGHT DECK WITH M2 LAVATORY SMOKE DETECTOR SOUNDING. EMERGENCY DECLARED FLIGHT RETURNED LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ENGINE DUE TO OIL THROUGH OUT COMPRESSOR SECTION. SYS GROUND CHECK NORMAL OPERATION. (OPEN)
2012
Part: SKIN — PUNCTURED (TE FLAP) · airframe 100,102 hrs · 16,229 cycles
PUNCTURE IN THE UPPER SURFACE OF THE LEFT INBOARD AFT FLAP. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10-2R.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 98,367 hrs · 15,947 cycles
FORWARD GALLEY CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR FORWARD GALLEY CEILING EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 97,912 hrs · 15,869 cycles
EMERGENCY LIGHT OUT AT SEAT 30AB. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT 30AB. OPS CHECK NORMAL.
Part: WIRE — DISCONNECTED (CABIN) · airframe 97,912 hrs · 15,869 cycles
EMERGENCY LIGHT WIRING DISCONNECTED AND HANGING DOWN BY WALL OF SEAT 34J. CONNECTED AND SECURED WIRING FOR SEAT 34J EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,912 hrs · 15,869 cycles
EMERGENCY LIGHT ON SEAT 28HJ INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ON SEAT 28HJ. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,912 hrs · 15,869 cycles
EMERGENCY LIGHT ON SEAT 20AB INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT 20 AB. OPS CHECK NORMAL.
2011
Part: FAN — INOPERATIVE (E&E BAY) · airframe 95,661 hrs · 15,501 cycles
LAX - INFLIGHT HNL-DFW. CREW REPORTED STRONG BURNING SMELL DETECTED IN COCKPIT ACCOMPANIED BY STATUS MESSAGE FORWARD EQUIPMENT EXHAUST FAN. EQUIPMENT COOLING SWITCH MOVED TO STANDBY AND SMELL SEEMED TO DISSIPATE. UTILITY BUSES TURNED OFF AS A PRECAUTION. FORWARD EXHAUST EQUIPMENT COOLING FAN CIRCUIT BREAKER POPPED. REPLACED FORWARD RACK EXHAUST FAN. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: CONNECTOR — LOOSE (CABIN) · airframe 95,546 hrs · 15,484 cycles
SEAT MOUNTED EMERGENCY LIGHT ON 21 AB INOPERATIVE. SECURED CONNECTION ON SEAT MOUNTED EMERGENCY LIGHT 21AB. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 95,546 hrs · 15,484 cycles
LEFT NUMBER 1 DOOR EMERGENCY EXIT SIGN IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT LEFT NUMBER 1 DOOR. OPS CHECK NORMAL.
Part: FITTING — DAMAGED (AILERON) · airframe 95,108 hrs · 15,418 cycles
LEFT WING INBOARD AILERON INBOARD FAIL SAFE HINGE FITTING. DAMAGE APPEARS TO BE DUE TO HTE AILERON INBOARD FAIL SAFE WEARING INTO THE RIB FORGING. WING FAIL SAFE RIB DOUBLER REPAIR PER MAJOR EA B767-57-016371.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,108 hrs · 15,418 cycles
CORROSION WAS FOUND AT STATION 325 FLOORBEAM AT RIGHT BUTTLINES 13 TO 17. THE CORROSION WAS BLENDED SMOOTH AND DOUBLER INSTALLED PER EA B767-53-01607.
Part: FITTING — CRACKED (FUSELAGE) · airframe 95,108 hrs · 15,418 cycles
FOUND CRACK TO RIGHT SIDE STATION 1809.5 TENSION FITTING PER SB 767-53A0078. BOTH HOLES WERE OVERSIZED TO 0.2755 INCH IN ORDER TO REMOVE CRACK INDICATIONS PER MAJOR EA B767-53-016071.
Part: SPAR — CRACKED (LT PYLON) · airframe 95,108 hrs · 15,418 cycles
FOUND CRACK ON THE LEFT PYLON STRUT TORQUE BOX MID SPAR WEB FORWARD INBOARD. REPAIRED WITH DOUBLER AND TRIPLER PER EA B767-54-016000.
Part: WEB — CRACKED (RT PLYON) · airframe 95,108 hrs · 15,418 cycles
CRACKS AROUND THE RIGHT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CABLE CUTOUT. ACCOMPLISHED DOUBLER REPAIR PER EA B767-54-015989.
Part: WEB — CRACKED (LT PYLON) · airframe 95,108 hrs · 15,418 cycles
CRACKS AROUND THE LEFT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CABLE CUTOUT. ACCOMPLISHED REPAIRS PER EA B767-54-015990.
2010
Part: SHUTOFF VALVE — FAILED (HYDRAULIC SYS) · airframe 94,101 hrs · 15,231 cycles
DFW - RIGHT YAW DAMPER MESSAGE ALONG WITH TAIL HYDRAULIC VALVE MESSAGE DISPLAYED ON EICAS. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. REPLACED LEFT TAIL HYDRAULIC SHUTOFF VALVE AND GEN FIELD AND HYDRAULIC CONTROL PANEL. SYSTEM GROUND CHECKS NORMAL OPERATION.
Part: STRAP — BROKEN (FLASHLIGHT) · airframe 91,920 hrs · 14,870 cycles
EMERGENCY FLASHLIGHT FOR FLIGHT ATTENDANT SEAT BY 17B HAS BROKEN STRAP. REPLACED STRAP FOR FLIGHT ATTENDANT EMERGENCY FLASHLIGHT. OPS CHECKED NORMAL.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,546 hrs · 14,633 cycles
MID FLIGHT ATTENDANT (AFT) EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT.
Part: ANTENNA — FAILED (WEATHER RADAR) · airframe 89,017 hrs · 14,373 cycles
WX RADAR FAILED IN FLIGHT AIRCRAFT DIVERTED TO MIA. REPLACED WX RADAR ANTENNA. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)
Part: CONTROLLER — FAULTY (FUEL SYSTEM) · airframe 88,981 hrs · 14,365 cycles
JFK - IN-FLIGHT DFW-MAD. CREW REPORTED CROSS FEED VALVE WOULD NOT OPEN. EMERGENCY DECLARED, LANDED AT JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CROSS FEED VALVE CONTROLLER. SYSTEM GROUND CHECK NORMAL OPERATION.
2008
Part: INVERTER — ODOR · airframe 85,338 hrs
POS INFLIGHT T1668/25JUL. CREW REPORTED STANBY INVERTER STATUS MSG AND HEAVY ELECTRICAL SMOKE SMELL IN COCKPIT. RETURNED TO POS AND LANDED WITHOUT INCIDENT. REPLACED STATIC INVERTER. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,756 hrs
SFO - EMERGENCY LIGHT AT SEAT 20H TO 21H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 20H TO 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 84,756 hrs
SFO - EMERGENCY LIGHTS AT SEAT 20H TO 21H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 20H TO 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT OVERHEAD LEFT FORWARD GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD LEFT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 83,597 hrs
SFO - EMERGENCY FLASHLIGHT AT AFT RIGHT FLIGHT ATTENDANT STATION INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT AFT RIGHT FLIGHT ATTENDANT STATION. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: BEZEL — LOOSE (EMERGENCY LIGHT)
ORD EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. RESEATED LAMP HOLDER FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHT AT SEAT ROW 11HJ INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT ROW 11HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHT AT SEAT ROW 12HJ INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT ROW 12HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHTS AT BULKHEAD FORWARD OF SEAT ROW 20CEG INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHTS AT BULKHEAD FORWARD OF SEAT ROW 20CEG. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHT AT SEAT ROW 13HJ INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT ROW 13HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHT AT SEAT ROW 10HJ INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT ROW 10HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHT AT SEAT ROW 17HJ INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT ROW 17HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: COFFEEMAKER — MALFUNCTIONED (GALLEY)
FLIGHT ATTENDANT SAW FLASH AND HEARD POP FROM COFFEEMAKER NUMBER ONE AND TWO IN FORWARD GALLEY FOLLOWED BY SMELL OF ELECTRICAL SMOKE FOR A COUPLE OF MINUTES. PULLED BOTH CIRCUIT BREAKERS ON COFFEE MAKER. REPLACED COFFEE MAKER NUMBER ONE AND INSPECTED WIRING WITH NO DAMAGE FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: CONNECTOR — BROKEN (CABIN)
SFO - EMERGENCY LIGHT AT SEAT 22B INOPERATIVE. REPAIRED BROKEN CONNECTOR AT SIDEWALL FOR EMERGENCY LIGHT AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SKIN — DAMAGED (BS 566 S36L)
AFW - FUSELAGE HAS LIGHTNING STRIKE SKIN BLENDS AT STATION 566 AT STRINGER 36 LEFT. REPAIRED LIGHTENING STRIKE PER STANDARD STRUCTURAL REPAIR MANUAL WITH EXCEPTION TO ALLOW THE BLEND TO BE 15.25 PERCENT OF THE THICKNESS. ENTERED DAMAGE IN THE AIRCRAFT DAMAGE LOG.
Part: SKIN — DAMAGED (BS 610-569)
AFW - FUSELAGE HAS LIGHTNING STRIKES WITHIN 22 INCHES OF A DENT AND PREVIOUS REPAIRS. REPAIR LIGHTNING STRIKES PER STANDARD STRUCTURAL REPAIR MANUALS WITH EXCEPTION TO ALLOW THE PREVIOUS DENT REPAIR AND BLENDS WITHIN 22 INCHES OF EACH OTHER. ENTERED IN AIRCRAFT DAMAGE LOG.
Part: CONNECTOR — LOOSE (CABIN)
DFW - EMERGENCY LIGHT AT SEAT 34H INOPERATIVE. SECURED LOOSE PLUG ON SEAT 34H FOR INOPERATIVE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN)
JFK - EMERGENCY EXIT AND THRESHOLD LIGHTS AT LEFT AND RIGHT HAND NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK M1208 FOR EMERGENCY EXIT AND THRESHOLD LIGHTS AT LEFT AND RIGHT HAND NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: LIGHT — INOPERATIVE (EXTERIOR)
DFW - LOWER AFT EMERGENCY LIGHT ON FUSELAGE INOPERATIVE. REPLACED LIGHT FOR LOWER AFT EMERGENCY LIGHT ON LEFT FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (SEAT 34B)
GRU - EMERGENCY ESCAPE PATH LIGHT AT 34B INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT 34B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: BATTERY PACK — FAILED (CABIN)
SFO - EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 21H. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED LIGHT ASSEMBLY BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: INTERCOSTAL — DAMAGED (FUSELAGE)
INTERCOSTAL ASSEMBLY HAS DAMAGE AS SHOWN ON SKETCH INTERCOSTAL CRACKED IN TWO LOCATIONS, BS 1112 AND 1128. CLEAN UP DAMAGE, ROUTE OUT CRACK, REMOVED ALL SHARP EDGES, VERIFY CRACKS COMPLETELY REMOVED. FABRICATE REPAIR PARTS FROM 301 .5 HARD, .050 INCH. FINISH WITH TWO COATS B195 10-11 PRIMER. APPLY ALODINE AND PRIMER TO ALL BARE ALUMINUM SURFACES. INSTALL ALL FASTENERS AND REPAIR PARTS WET WITH BMS 5-95 SEALANT. REFER TO FIGURE FOR REPAIRS CONFIGURATION AND FASTENER TYPES. (M)
Part: GENERATOR — FAILED (LEFT ENGINE)
LEVEL AT 310 LT GEN DRIVE LIGHT FLICKERED AND THEN CAME ON STEADY. ROAR HEARD AND VIBRATION FLET. DISCONNECTED THE IDG AND RETURNED TO SCL. PLACARDED INOPERATIVE LEFT ENGINE IDG PER MEL 24-1 AUTH 6-49DC-A, ENTERED IN MIC SHEET AND MPM 24-1 ACCOMPLISHED SERVICING LT/RT AND APU IDGS, CHECKED HISTORY NONE FOUND. REPLACED LEFT ENGINE IDG AS PER AMM 24-11-01-4. RUNUP LEFT ENGINE AND CHECKED IDG FOUND TO BE OK. NO VIBRATION ON LEFT ENGINE DURING POWER RUNUP PER AMM. CLEARED MEL AND MIC. AIRCRAFT OK FOR SERVICE. (M)
Part: CONNECTOR — INOPERATIVE (CABIN)
DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 12 AB AND 24 HJ INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: TRU — FAILED (ELECTRICAL SYS)
PIK - STANDBY INVERTER MESSAGE ON LOWER EICAS. ELECTRICAL FUMES OBSERVED THROUGHOUT CABIN AND FLIGHT DECK. PUNGENT ELECTRICAL BURNING ODOR. FOUND STANDBY INVERTER OVERHEATED, REPLACED TRU AND ALL OPS AND INDICATIONS NORMAL RAISED MRR. (M)
Part: WIRE — DAMAGED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHT AT SEAT 34B INOPERATIVE. REPAIRED WIRE ON EMERGENCY ESCAPE LIGHT SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: INVERTER — FAILED (CABIN)
PIK - FLT 37 - EN ROUTE ZRH-DFW, SMOKE IN COCKPIT DURING CRUISE WITH ASSOCIATED EICAS MESSAGE. STANDBY INVERTER FAILED. DIVERTED TO PIK LANDED WITHOUT INCIDENT. REPLACED STANDBY INVERTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: PRESSURE SWITCH — FAILED (SMOKE DETECTION)
CARGO DET AIR STATUS MSD ILLUMINATED. RESET CBS AS PER QRH. STATUS MSG REMAINED, DIVERTED. TROUBLESHOT SYSTEM, REMOVED AND REPLACED SMOKE DETECTOR PRESS SWITCH. ALSO FOUND NR 2 BLOWER WAS EXTREMELY HOT TO TOUCH. REMOVED AND REPLACED BOTH NR 1 AND NR 2 FORWARD CARGO BLOWERS AS A PRECAUTION, PERFORMED OPS CHECK IAW MM. ALL OPS CHECK GOOD.
2001
Part: CONNECTOR — INOPERATIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31AB INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — INOPERATIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17HJ INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: POWER SUPPLY — DISCHARGED (CABIN)
JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 20AB THROUGH 24 AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: FAN — INOPERATIVE (ACM BAY)
CDG - FLT 49 - EN ROUTE DFW-CDG, A STRONG ELECTRICAL BURNING SMELL WAS DETECTED IN THE COCKPIT AND CABIN. RIGHT RECIRCULATING FAN INOPERATIVE. LANDED CDG WITHOUT INCIDENT. REPLACED RIGHT RECIRCULATING FAN PER MM. NO FURTHER SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 17 AND 37 INOPERATIVE. SECURED CONNECTORS AT SEAT 17 AND 37. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1999
Part: RELAY — DEFECTIVE (E/E COMPT)
MSY - FLT 207 - EN ROUTE MIA-LAX, LEFT FORWARD FUEL BOOST PUMP CAUTION LIGHT ILLUMINATED AND CIRCUIT BREAKER POPPED. CABIN SIDEWALL LIGHTS AND FLIGHT ATTENDANT JUMP SEAT WORK LIGHTS INOPERATIVE. ALSO, RECEIVED CARGO DETECTION AIR ADVISORY MESSAGE AND SYSTEM 1, 2 AND 3 HYDRAULIC FLUID QTY INDICATORS WENT TO .02. AIRCRAFT AIR INTERRUPTED TO MSY AND LANDED WITHOUT INCIDENT. REPLACED ELECTRICAL RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — FAILED (ROW 31B)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH MARKER LIGHT INOPERABLE AT SEAT 31B. REPLACED CONNECTOR AT SEAT 31B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: CONNECTOR — FAILED (ROW 28B)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH MARKER LIGHT INOPERABLE AT SEAT 28B. REPLACED CONNECTOR AT SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)
1998
Part: VALVE — MALFUNCTIONED (HYDRAULIC SYSTEM)
LHR - FLT 67 - AFTER TAKEOFF LHR EN ROUTE TO ORD WITH GEAR HANDLE UP, CENTER PRESSURE DROPPED TO 690 PSI. GEAR WOULD NOT RETRACT, GOT GEAR DOORS AND TAIL SKID LIGHTS. RETUREND AND LANDED LHR OVERWEIGHT AT 346,000 LBS. LANDED WITHOTU INCIDENT. FOUND HYDRAULC DRIVE GENERATOR SHUTOFF VALVE IN OPEN POSITION. POSITIONED AND LOCKED VALVE IN CLOSED POSITION PER MM AND ACCOMPLISHED CENTER HYDRAULC SYSTEM CHECK PER MM. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, RIGHT EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED WIRE IN EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: LAMP — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, FIRST CLASS CABIN EMERGENCY ESCAPE MARKING LAMP FOUND BROKEN AND INOPERATIVE. REPLACED FIRST CLASS CABIN EMERGENCY ESCAPE MARKING LAMP ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: WIRE — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 39H INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
EZE - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 38HJ INOPERATIVE. REPAIRED BROKEN/SHORTED EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 38HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: SWITCH — DEFECTIVE (LT LE SLAT)
DFW - FLT 1998 - DURING APPROACH DFW, WHILE EXTENDING FLAPS TO 5 DEGREES A EICAS LEADING EDGE SLAT ASYMMETRIC AND LEADING EDGE LIGHT CAME ON. DECLARED EMERGENCY, ACCOMPLISHED PCDR AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT OUTBOARD SLAT NR 2 INBOARD PROX SWITCH. ACCOMPLISHED SENSOR TARGET TEST, SENSOR TEST NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: MOUNT — CORRODED (GALLEY)
AFW - FOUND G-6 GALLEY MOUNT HAS CORROSION ON VERTICAL FLANGE. FABRICATE AND INSTALL DOUBLER PER ENGINEERING MRB 767-1272. (M)
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 36H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: EEL WIRE — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING ON RIGHT SIDE OF BUSINESS CLASS FOUND INOPERATIVE. REPAIRED WIRING AT 11H. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)
Part: EEL CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD GALLEY INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FOUND INOPERATIVE AT MID-GALLEY, AFT OF SEAT ROW 42H AND AFT GALLEY BELOW MID-JUMP SEATS. SECURED CONNECTORS AT SAME LOCATIONS. SYSTEM GROUND CHECKS NORMAL OPERATION. (X)