N189AN
Registered owner: WYATT AEROSPACE LLC, AZ (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.
74 reports on file, 2004-02-18 – 2019-09-20.
Part: SLIDING WINDOW — OPEN (COCKPIT) · airframe 63,818 hrs · 16,005 cycles
AIRCRAFT WAS GROUNDED: PILOT REJECTED TAKEOFF AT 120 KNOTS DUE TO THE CAPTAINS WINDOW HAD OPENED. MAINTENANCE ACCOMPLISHED HIGH ENERGY STOP INSPECTION IAW JOB CARD 19L00005024, NO FAULTS NOTED. A/C OK FOR SERVICE.
Part: GOVERNOR — UNRELIABLE (RT ENGINE) · airframe 63,585 hrs · 15,942 cycles
AIRCRAFT WAS GROUNDED: PILOT REPORTS ON INITIAL ROLL, HAD A LAG ON THE RIGHT ENGINE AND DECIDED TO ABORT TAKEOFF. TAXIED OFF ACTIVE RUNWAY AND DID A RUNUP AND ALL ENGINES WERE PERFORMING AS NORMAL, CREW DECIDED TO ATTEMPT ANOTHER TAKEOFF. TAKEOFF WAS NORMAL UNTIL V1 AND THE RIGHT ENGINE STARTED TO LAG AGAIN, THE CREW TOOK OFF AND IMMEDIATELY WENT INTO HOLD. THE RIGHT ENGINE ON TAKEOFF AND CLIMB WAS OPERATING AT 30% LESS POWER THAN THE LEFT ENGINE. THE CREW DECIDED TO RETURN TO SNN AFTER DETERMINING THAT THE POSSIBILITY OF ENGINE PROBLEMS ON AN ATLANTIC CROSSING WAS PROBABLE. NO EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE FUEL FLOW GOVERNOR IAW JOBCARD 73-94-01 / 19L40073001. ENGINE OPS AND LEAK CHECK GOOD.
Part: PACKING — CUT (FUEL SYSTEM) · airframe 63,564 hrs · 15,937 cycles
AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO DFW ON ACCOUNT OF LEFT ENGINE FUEL LEAK. EMERGENCY WAS DECLARED. MAINTENANCE FOUND LOWER FP PUMP TO FFG LINE PACKING CUT. REMOVED AND REPLACED IAW AMM 73-11-06-004-015-R00. LEAK CHECK GOOD AT TAKEOFF TEST #2. OK FOR SERVICE.
Part: GOVERNOR — UNRELIABLE (NR 1 FUEL FLOW) · airframe 63,525 hrs · 15,926 cycles
AIRCRAFT WAS GROUNDED: PILOT REPORTS L ENG WOULD NOT SHUTDOWN WITH FUEL CONTROL-FIRE HANDLE PULLED. MAINTENANCE REMOVED AND REPLACED # 1 ENG. FUEL FLOW GOVERNOR IAW JOB CARD 73-94-01. OPS CHECKED NORMAL.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 63,205 hrs · 15,846 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS RED CONFIG LIGHT ON CENTER PANEL ACCOMPANIED BY GEAR NOT DOWN EICAS DURING DECENT. MAINTENANCE ACCOMPLISHED TSM 31-51-00. SYSTEM OPS CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,547 hrs · 15,374 cycles
RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-00. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,547 hrs · 15,374 cycles
AIRCRAFT WAS GROUNDED: LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERABLE. MAINTENANCE RELAMPED OVERWING LIGHT AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.
Earlier reports · 2004–2018 · 67 reports
2018
Part: TRANSMITTER — FAULTY (FLAP POSITION) · airframe 61,229 hrs · 15,273 cycles
DURING CLIMBOUT, THE CREW RECIEVED A FLAP ASYMMETRY MESSAGE. AN EMERGENCY WAS DELCARED, THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. THE RIGHT FLAP POSITION TRANSMITTER WAS FOUND FAULTY IAW FIM 27-51-00. REPLACED THE TRANSMITTER IAW AMM 27-58-03.
Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 60,934 hrs · 15,181 cycles
DURING CLIMB, LT ENGINE RAPIDLY EXCEDED EGT LIMITS. A/T ARM SWITCH TURNED OFF, AND LT THROTTLE REDUCED FOR EGT TO STAY WITHIN LIMITS. EGT DID TURN AMBER & EGT REDUCED 795* BEFORE RETURNING TO NORMAL AT CRUISE. ENGINE PERFORMS NORMALLY. LT ENGINE FR WAS .7 HIGHER THAN RT IN CLIMB. N1 WAS 3% HIGHER IN CLIMB. BVCU BITE ACCOMPLISHED, NO FAULTS IAW AMM 75-32-00 AND TPU BITE, NO FAULTS. REPLACED THE LEFT ENGINE EPR TRANSMITTER IAW AMM 77-11-01. LEAK CHECKED. FFG RIG CHECKED OK IAW AMM 76-11-00. THRUST LEVER ANGLE CHECK, ACCELERATION AND DECCELERATION TESTED OK. TAKEOFF POWER CHECKED OK ALL IAW AMM 71-00-00.
Part: ANGLE — CORRODED (BS 992-996) · corrosion level 2 · airframe 60,907 hrs · 15,173 cycles
CORROSION ON THE RIGHT CREASE ANGLE BETWEEN BS 992 TO 996. REPAIRED THE ANGLE IAW SRM 53-00-13-2R.
Part: SKIN — CORRODED (BS 1690) · corrosion level 2 · airframe 60,907 hrs · 15,173 cycles
CORROSION FOUND ON THE FUSELAGE SKIN, AROUND DRAIN HOLE AT BS 1690, STRINGERS 29L AND 29R. REPAIRED THE SKIN IAW EA 284151.
Part: PRESSURE DECK — CORRODED (BS 1713) · corrosion level 2 · airframe 60,907 hrs · 15,173 cycles
CORROSION FOUND ON THE AFT GALLEY DECK DOUBLER AT BS 1713, RBL 7 TO RBL 42. REPAIRED THE DECK WEB IAW SRM 53-60-51-2R-18.
Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 60,907 hrs · 15,173 cycles
CORROSION FOUND ON THE FLOORBEAM AT BS 1640, RBL 3. REPAIRED THE FLOORBEAM IAW SRM 53-00-51-2R-3.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 60,824 hrs · 15,149 cycles
R2 DOOR FLIGHT ATTENDANT FLASHLIGHT BATTERY INOPERATIVE. REPLACED THE BATTERY IAW AMM 33-00-00.
Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 60,493 hrs · 15,070 cycles
R1 DOOR ESCAPE SLIDE BOTTLE HAD LOW PRESSURE. REPLACED THE SLIDE IAW WORK CARD 25-94-34, AND AMM 25-66-01.
Part: PROXIMITY SENSOR — MALFUNCTIONED (L2 DOOR SLIDE) · airframe 60,394 hrs · 15,049 cycles
L2 DOOR SLIDE LIGHT REMAINED ILLUMINATED AFTER SLIDE WAS DISARMED. RELACED THE GIRT BAR PROXIMITY SWITCHES IAW AMM 25-66-11
2017
Part: LIGHT — MISSING (CABIN) · airframe 58,672 hrs · 14,560 cycles
AIRCRAFT WAS NOT GROUNDED. DOOR EMERGENCY EXIT LIGHT MISSING. INSTALLED NEW EMERGENCY LIGHT COVER ENTRY/SERVICE DOOR. OPERATIONAL CHECK NORMAL PER AMM 33-51-00.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 58,330 hrs · 14,466 cycles
AFT GALLEY LEFT HAND FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT WAS INOPERATIVE. REPLACED THE AFT GALLEY LEFT HAND FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00.
Part: LIGHT — BROKEN (CABIN) · airframe 58,124 hrs · 14,416 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT ASSEMBLY BY THE R4 DOOR IS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-51-00. OPERATIONAL CHECK GOOD.
Part: LIGHT — BROKEN (CABIN) · airframe 58,124 hrs · 14,416 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT ASSEMBLY BY THE L4 DOOR IS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-51-00. OPERATIONAL CHECK GOOD.
Part: ARMING LEVER — LACK OF LUBE (L1 DOOR) · airframe 57,856 hrs · 14,353 cycles
AIRCRAFT WAS NOT GROUNDED. L1 DOOR HAS A FAULTY RED ARM TAB, STAYS ON AFTER BEING ARMED. LUBED RETRACTABLE DOOR SLIDE ARM/DISARM OPERATION PER AMM 52-11-00. OPERATIONAL CHECK GOOD.
Part: COMPUTER — FAULTY (ZONE 100) · airframe 57,646 hrs · 14,301 cycles
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. MIA-JFK FLIGHT RETURNED TO MIA ACCOUNT FLIGHT INSTRUMENTATION. OVERWEIGHT LANDING UNEVENTFUL. FLIGHT DIRECTOR AND AUTOPILOT WOULD NOT FOLLOW COMMANDS (NOT REPORTING) ON HEADING AND ALTITUDE, LATERAL AND VERTICAL ALTITUDE (NO FLAGS) ON ALL THREE AUTOPILOTS. REMOVED AND REPLACED FLIGHT CONTROL COMPUTER PER AMM 22-11-01. OPERATIONAL CHECK GOOD.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 57,230 hrs · 14,189 cycles
EMERGENCY EXIT LIGHTS AT ROW 3EF FORWARD AND AFT ARE INOPERATIVE. SECURED LOOSE LIGHT CONNECTOR IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.
Part: RESERVOIR — LOW PRESSURE (R2 DOOR) · airframe 57,173 hrs · 14,175 cycles
R2 DOOR EMERGENCY POWER RESERVOIR IS LOW. REMOVED AND REPLACED RESERVOIR IAW AMM 52-11-30. OPERATIONAL CHECKED GOOD.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,752 hrs · 14,062 cycles
EMERGENCY EXIT SIGN AT R4 DOOR HAS A MISSING LENS COVER. REINSTALLED THE LENS COVER. OPERATIONAL CHECKED GOOD.
Part: LENS — BROKEN (EXIT SIGN) · airframe 56,546 hrs · 14,007 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN OVER R1 DOOR HAS A BROKEN LENS COVER. REMOVED AND REPLACED LENS COVER IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 56,335 hrs · 13,949 cycles
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. LANDING UNEVENTFUL. TRAILING EDGE FLAP DISAGREE INDICATION WHILE SELECTING FLAP LEVER FROM 15 DEGREES TO 20 DEGREES. ACCOMPLISHED FIM 27-51-01 AND FLAP/SLAT ELECTRONICS UNIT TEST IAW AMM 27-51-01-722-005. OPERATIONAL CHECK GOOD.
2016
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 56,120 hrs · 13,894 cycles
DURING APPROACHED FLAPS 20 DEGREES SELECTED. RECEIVED "TE FLAP DISAGREE" EICAS MESSAGE. FLAPS STOPPED AT 17 DEGREES. EMERGENCY DECLARED. AIRCRAFT WAS GROUNDED. MAIANTENANCED CHECKED EICAS PAGES WITH NO MESSAGES NOTED. PERFORMED OPERATIONAL TEST OF FLAPS, ACCOMPLSIHED FSEU CHECK IAW AMM 27-51-00 AND CYCLED TRAILING EDGE FLAPS 0 THROUGH 30 SIX TIMES WITH NO FAULTS FOUND. COULD NOT DUPLICATE. SYSTEM CHECKS NORMAL.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,887 hrs · 13,831 cycles
EMERGENCY LIGHT LENS COVER MISSING AT L1 DOOR. REPLACED LENS COVER IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.
Part: CONTROL MODULE — INOPERATIVE (CABIN) · airframe 53,711 hrs · 13,335 cycles
AIRCRAFT WAS NOT GNDED. EMER EXIT LIGHT BETWEEN ROWS 29 DEF & 36 DEF ARE INOPERATIVE. R & R BATTERY PACK & CONTROL MODULE IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA 20160426008.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,711 hrs · 13,335 cycles
AIRCRAFT WAS NOT GNDED. EMER EXIT LIGHT BETWEEN ROWS 29 DEF & 36 DEF ARE INOPERATIVE. R & R BATTERY PACK & CONTROL MODULE IAW AMM 33-51-07. SYS CHECKS NORMAL. SEE ALSO AALA 20160426002.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,711 hrs · 13,335 cycles
AIRCRAFT WAS NOT GNDED. EMER EXIT LIGHT BETWEEN ROWS 9 DEF & 14 DEF ARE DIM. R & R BATTERY PACK & CONTROL MODULE IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA 20160426003.
Part: CONTROL MODULE — INOPERATIVE (CABIN) · airframe 53,711 hrs · 13,335 cycles
AIRCRAFT WAS NOT GNDED. EMER EXIT LIGHT BETWEEN ROWS 9 DEF & 14 DEF ARE DIM. R & R BATTERY PACK & CONTROL MODULE IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA 20160426009.
2015
Part: SKIN — CRACKED (L4 DOOR) · airframe 51,727 hrs · 12,868 cycles
L4 DOOR HAS A CRACK ON INNER DOOR SKIN AT UPPER HINGE AREA. INSTALLED REPAIR DOUBLER & FILLER IAW EA 252597.
Part: BATTERY — DISCHARGED (CABIN) · airframe 50,604 hrs · 12,629 cycles
SEAT MOUNTED EMER LIGHTS FROM ROW 26 TO 36 INOPERATIVE. REPLACED EMER LIGHT BATTERY WITH GOOD OPERATIONS CHECK IAW AMM 33-51-00.
Part: MODULE — INOPERATIVE (CABIN) · airframe 50,604 hrs · 12,629 cycles
FIRST CLASS EMER LIGHTS SEAT MOUNT INOPERATIVE. REPLACED LIGHT MODULE IAW AMM 33-51-00 WITH GOOD OPERATIONAL CHECKS.
2014
Part: COVER — MISSING (EXIT SIGN) · airframe 48,306 hrs · 12,092 cycles
RIGHT NR 1 DOOR FWD EMER EXIT SIGN COVER MISSING. REPLACED FWD EMER EXIT SIGN COVER. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,715 hrs · 11,938 cycles
EMERGENCY LIGHT AT SEAT ROW 26DEF INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT ROW 26DEF. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,715 hrs · 11,938 cycles
EMERGENCY LIGHT AT SEAT ROW 35DEF INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT ROW 35DEF. OPERATIONS CHECKED NORMAL.
Part: CONNECTOR — LOOSE (CABIN) · airframe 47,588 hrs · 11,904 cycles
EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. SECURED CONNECTOR UNDER SEAT 25D. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,588 hrs · 11,904 cycles
EMERGENCY LIGHT AT SEAT 35D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35D. OPERATIONS CHECKED NORMAL.
Part: GATE — OUT OF RIG (L4 DOOR) · airframe 46,967 hrs · 11,760 cycles
DFW CREW REPORTED LT AFT ENTRY DOOR EICAS MSG & ENTRY DOORS OVERHEAD LIGHT ILLUMINATED ALONG WITH LOSS OF PRESSURIZATION. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND LOWER GATE OUT OF RIG. RE-RIGGED LT NR 4 DOOR LOWER GATE. SYS GND CHECKED NORMAL, OPERATION CLOSED.
2013
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 44,523 hrs · 11,179 cycles
LT AFT JUMPSEAT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED LT AFT JUMPSEAT EMERGENCY FLASHLIGHT BATTERY. OPERATIONS CHECKED NORMAL.
Part: OVEN — DIRTY (GALLEY) · airframe 44,348 hrs · 11,142 cycles
SMOKE IN FIRST CLASS GALLEY. EMERGENCY DECLARED FLIGHT RETURNED TO CCS LANDED WITHOUT INCIDENT. FOUND FIRST CLASS GALLEY AREA OVEN WITH DEBRIS INSIDE OF GALLEY GRILLS. PLACARDED BOTH FIRST CLASS GALLEY OVEN IAW NEF 25-33A AUTH 6-967NEF-C. REPLACED FIRST CLASS GALLEY OVEN AT JFK ON 06/24/2013. SYSTEM GROUND CHECKED NORMAL.
2012
Part: WIRE — CRUSHED (CABIN) · airframe 41,457 hrs · 10,490 cycles
SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 26 TO AFT OF AIRCRAFT ARE INOPERATIVE. FOUND CRUSHED WIRING AT L760S. REPLACED WIRES. OPS CHECK NORMAL.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,443 hrs · 10,483 cycles
CORROSION ON FLOORBOARD SUPPORT AT STATION 1675. REPLACED FLOORBOARD SUPPORT PER AARD 51-00-05.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,443 hrs · 10,483 cycles
CORROSION ON AFT DECK AT STATION 1715 RIGHT BUTTLINE 13. INSTALLED REPAIR DOUBLER FROM RIGHT BUTTLINES 7 TO 42 AND STATIONS 1711 TO 1720 PER SRM 53-60-51-2R-2.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,443 hrs · 10,483 cycles
LAVATORY MOUNT AT STATION 1638 LEFT BUTTLINE 25 CORRODED. REPLACED LAVATORY MOUNT PER AARD 51-00-05.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,443 hrs · 10,483 cycles
AFT GALLEY HAT CHANNEL AT STATION 1715 CORRODED. REPLACED HAT CHANNEL PER AARD 51-00-05-1.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,443 hrs · 10,483 cycles
INTERCOSTAL TOP L-ANGLE CRACKED. REMOVED AND REPLACED TOP INTERCOSTAL L-ANGLE PER AARD 51-00-05.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,443 hrs · 10,483 cycles
GALLEY MOUNT AT STATION 1712 LEFT BUTTLINE 52 CORRODED. REPLACED GALLEY MOUNT PER AARD 51-00-05.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,445 hrs · 10,032 cycles
EXIT EMERGENCY LIGHT AT LEFT NUMBER 3 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,445 hrs · 10,032 cycles
EMERGENCY LIGHTS AT AISLE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL.
2011
Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 39,191 hrs · 9,971 cycles
CORROSION ON RIGHT LOWER INBOARD MAIN LANDING GEAR FORWARD TRUNNION BEARING AND TRUNION SUPPORT. FABRICATED AND INSTALLED NEW BUSHING PER EA B757-57-020831.
Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 39,191 hrs · 9,971 cycles
CORROSION ON RIGHT LOWER OUTBOARD MAIN LANDING GEAR FORWARD TRUNNION BEARING AND TRUNNION SUPPORT. FABRICATED AND INSTALLED NEW BUSHING PER EA B757-57-020831.
Part: BEARING — CORRODED (LT MLG TRUNNION) · corrosion level 2 · airframe 39,191 hrs · 9,971 cycles
CORROSION ON LEFT LOWER OUTBOARD MAIN LANDING GEAR FORWARD TRUNNION BEARING AND TRUNNION SUPPORT. FABRICATED AND INSTALLED NEW BUSHING PER EA B757-57-020831.
Part: TRUNNION — CORRODED (LT MLG) · corrosion level 2 · airframe 39,191 hrs · 9,971 cycles
CORROSION ON LEFT LOWER INBOARD MAIN LANDING GEAR FORWARD TRUNNION BEARING AND TRUNNION SUPPORT. FABRICATED AND INSTALLED NEW BUSHING PER EA B757-57-020831.
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 38,687 hrs · 9,874 cycles
LEFT NUMBER 1 DOOR EXTERNAL EMERGENCY PATH LIGHT INOPERATIVE. REPLACED M731 EMERGENCY LIGHT POWER SUPPLY. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,687 hrs · 9,874 cycles
LEFT NUMBER 1 DOOR EXTERNAL EMERGENCY PATH LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EXTERNAL EMERGENCY PATH LIGHT. OPS CHECK NORMAL.
Part: CONTROL MODULE — FAULTED (SPOILER) · airframe 38,196 hrs · 9,786 cycles
BOS - CREW REPORTED DURING CLIMBOUT SPOILER LIGHT ON OVERHEAD AND EICAS MESSAGE. NO ROLL CONTROL PROBLEMS OR FLIGHT CONTROL ISSUES REPORTED. FLIGHT RETURNED BOS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 2 SPOILER POWER CONTROL MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: OXYGEN BOTTLE — DISCHARGED (CREW O2) · airframe 34,468 hrs · 8,982 cycles
LHR - DURING CLIMBOUT FOUND CREW OXYGEN BOTTLE EMPTY. FLIGHT RETURNED LHR LANDED WITHOUT INCIDENT. REPLENISHED CREW OXYGEN BOTTLE AND REPLACED CAPTAINS MASK. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: PANEL — BROKEN (EMERGENCY LIGHT) · airframe 33,153 hrs · 8,713 cycles
GUARDED SWITCH ON EMERGENCY LIGHT PANEL BROKEN. REPLACED PANEL. OPS CHECKED NORMAL.
2009
Part: LENS — WRONG PART (CABIN)
DFW - FIRST CLASS GALLEY BIDIRECTIONAL FLOODLIGHT HAS INCORRECT LENS. REPLACED FIRST CLASS GALLEY BIDIRECTIONAL FLOODLIGHT WITH CORRECT LENS.
Part: MODULE — INOPERATIVE (CABIN)
DFW - MID COACH SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER SECTION AFT MODULE FOR MID COACH SEAT MOUNTED EMERGENCY LIGHTS.
Part: MODULE — INOPERATIVE (CABIN)
DFW - FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD SECTION MODULE FOR FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS.
Part: WIRE — DAMAGED (CABIN)
DFW - FIRST CLASS GALLEY BIDIRECTIONAL FLOOD LIGHT INOPERATIVE. REPLACED WIRE FOR FIRST CLASS GALLEY BIDIRECTIONAL FLOOD LIGHT.
Part: LENS — MISSING (CABIN)
DFW - AFT CARGO COMPARTMENT LIGHT MISSING LENS. REPLACED LENS FOR AFT CARGO COMPARTMENT LIGHT.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)
DFW - FORWARD GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD GALLEY.
2008
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,853 hrs
SFO - EMERGENCY LIGHTS FROM SEAT ROW 9D TO 15D INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · 28,015 cycles
DFW EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 9 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 9. SYSTEM GROUND CHECKED NORMAL OPS.
2007
Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 25,337 hrs
LAX - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 35D INOPERATIVE. SECURED WIRES AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 35D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
DFW - EMERGENCY EXTERIOR LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. RELAMPED EMERGENCY EXTERIOR LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE — DAMAGED (CABIN)
LAX - EMERGENCY LIGHTS ON SEATS 16D THROUGH 25D INOPERATIVE. FOUND BROKEN AND SHORTED WIRE AT SEAT 19D. REPAIRED WIRING AND REPLACED BATTERY PACK M10953 FOR INOPERATIVE EMERGENCY LIGHTS ON SEATS 16D THROUGH 25D. SYSTEM GROUND OPERATIONS NORMAL.
2004
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)
BULL NOSE EMERGENCY LIGHTS AT ROWS 11 THROUGH 14 AND R2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR EMERGENCY LIGHTS AT ROWS 11 THROUGH 14 AND R2 DOOR EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--