N552AA
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.
84 reports on file, 1999-03-18 – 2014-11-28.
Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 66,274 hrs · 34,475 cycles
PORTABLE EMER LIGHT FAILS OPERATIONAL TEST. R & R PORTABLE EMER LIGHT. SYS CHECKED NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 66,274 hrs · 34,475 cycles
MID CABIN OVERHEAD EMER LIGHTS FAIL OPERATIONAL TEST. R & R MID CABIN POWER SUPPLY. SYS CHECKED NORMAL.
Earlier reports · 1999–2013 · 82 reports
2013
Part: A/C PACK — SEIZED (AC BAY) · airframe 63,088 hrs · 32,610 cycles
DFW CREW REPORTED UNABLE TO PRESSURIZE WITH RT PACK WITH LT PACK ON PLACARD. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT PACK THAT HAD SEIZED. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.
Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 62,753 hrs · 32,404 cycles
LT NR 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED LT NR 1 DOOR PORTABLE LIGHT. OPERATIONS CHECKED NORMAL.
Part: SIGN — BROKEN (CABIN) · airframe 62,753 hrs · 32,404 cycles
RT NR 1 GALLEY DOOR EGRESS LIGHT FOUND BROKEN. REPLACED RT NR 1 GALLEY DOOR EGRESS SIGN. OPERATIONS CHECKED NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 62,753 hrs · 32,404 cycles
CEILING EMERGENCY LIGHTS AT ROWS 28 & 29 INOPERATIVE. REPLACED POWER SUPPLY AT ROW 29. OPERATIONS CHECKED NORMAL.
Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 62,627 hrs · 32,336 cycles
VERTICAL STABILIZER HAS DAMAGED HOLES, L/E DORSAL SKIN AND SPAR. ACCOMPLISHED REPAIR IAW EA MD 80-55-030222.
Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 62,627 hrs · 32,336 cycles
DORSAL L/E DAMAGED. INSTALLED DOUBLER REPAIR IAW SRM 55-03-00, PARA 27, FIG 30.
Part: COALESCER BAG — DIRTY (AC BAY) · airframe 61,945 hrs · 31,931 cycles
CLT - CREW REPORTED ELECTRICAL ODOR IN CABIN AREA. EMERGENCY DECLARED FLIGHT RETURNED CLT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED CABIN ODOR CARD 21-96-01 AND REPLACED BOTH WATER SEPARATOR BAGS. SYSTEM GROUND CHECK NORMAL OPERATION.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,451 hrs · 31,106 cycles
FORWARD GALLEY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP FOR FORWARD GALLEY EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: CONTROL VALVE — LEAKING (LANDING GEAR) · airframe 59,271 hrs · 30,433 cycles
DFW - CREW REPORTED DURING CLIMB AUTO SPOILER DO NOT USE LIGHT ILLUMINATED FOLLOWED BY LEFT MAIN GEAR RED LIGHT. SEVERAL MINUTES LATER GEAR DOOR OPEN AMBER LIGHT CAME ON. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LANDING GEAR CONTROL VALVE THAT WAS LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: PROXIMITY SENSOR — INOPERATIVE (LT MLG) · airframe 59,266 hrs · 30,429 cycles
ELP - REW REPORTED LEFT MAIN LANDING GEAR UNSAFE LIGHT DID NOT EXTINGUISH WHEN GEAR HANDLE WAS UP. FLIGHT RETURNED ELP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PROXIMITY SENSOR AND PROXIMITY BOX. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: FRAME — CRACKED (FUSELAGE) · airframe 59,264 hrs · 30,426 cycles
STATION 1418, FRAME CRACKED AT LONGERON 2 LEFT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-03-00 FIGURE 31A.
2011
Part: BATTERY PACK — OUT OF POSITION (CABIN) · airframe 58,785 hrs · 30,147 cycles
EMERGENCY LIGHT AT SEATS 29DEF AND 30DEF INOPERATIVE. REPOSITIONED BATTERY PACK AT EMERGENCY POWER SUPPLY. OPS CHECK NORMAL.
Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 58,785 hrs · 30,147 cycles
BATTERY PACK FOR CABIN EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK AT EMERGENCY POWER SUPPLY. OPS CHECK NORMAL.
Part: LIGHT — MISSING (CABIN) · airframe 58,125 hrs · 29,751 cycles
EMERGENCY PATH LIGHT AT SEAT 5E MISSING LAMP. REPLACED LAMP FOR EMERGENCY PATH LIGHT AT SEAT 5E. OPS CHECK NORMAL.
Part: LENS — MISSING (CABIN) · airframe 58,125 hrs · 29,751 cycles
EMERGENCY PATH LIGHT AT SEAT 5E MISSING LENS. REPLACED LENS FOR EMERGENCY PATH LIGHT AT SEAT 5E. OPS CHECK NORMAL.
Part: DUCT — CRACKED (LT ENGINE) · airframe 57,539 hrs · 29,416 cycles
LIT - INFLIGHT DFW-IAD. CREW REPORTED LEFT ENGINE FIRE WARNING INDICATION. EMERGENCY DECLARED FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. NO EVIDENCE OF FIRE WAS FOUND. REPLACED LOWER STARTER DUCT AT T-FITTING THAT WAS CRACKED. FOUND LOWER BURN THROUGH BARRIER LOOP ON LEFT ENGINE OPEN. REPLACED LOOP. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: BEAM — CRACKED (ENTRY DOOR) · airframe 55,615 hrs · 28,339 cycles
FORWARD ENTRY DOOR NUMBER 7 BEAM AFT SIDE CRACKED. STOP DRILLED BEAM CRACK AND INSTALLED DOUBLER PER SRM 52-05-00.
Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
HEAVY CARGO/AFT- CORROSION ON DOOR CUTOUT BEAM, SEVERAL PLACES STA 1155-1212. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3 AND EA MD80-53-012185.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
HEAVY CORROSION ON CUSP RIGHT SIDE 1309 BOTTOM SURFACE. COMPLETE CUSP INSTALLATION PER AARD 53-20-00-16 RIGHT SIDE STATION 1250 TO 1309 ALSO WIP NUMBER 8 INSTALLED PER ATTACHED EAMD 80-51-012071.
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 55,615 hrs · 28,339 cycles
DAMAGED ON STRINGER 2 STATION 1418. INSTALLED SPLICE PER AARD 53-30-00-2.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 55,615 hrs · 28,339 cycles
DAMAGED FRAME FORWARD SIDE OF STATION 1418 AT STRINGER 2 RIGHT. INSTALLED DOUBLER PER SMR 53-03-00.
Part: SKIN — CRACKED (FUSELAGE) · airframe 55,615 hrs · 28,339 cycles
SKIN CRACK STATION 1380 LONGERON 15. INSTALLED DOUBLER PER SRM53-01-00 AND AARD 53-30-00-02.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
HEAVY CABIN CORROSION BELOW GIRT BAR FITTING AT AFT SERVICE FORWARD FITTING. REMOVED CORRODED MATERIAL AT AFT SERVICE DOOR FORWARD GIRT BAR FITTING. REPAIRED BY INSTALLING DOUBLER AND NEW GIRT BAR FITTING PER AARD 53-20-00-16.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
MID CARGO STATION 579 TO 598 RIGHT SIDE CORROSION ON BOTTOM SIDE OF CUSP. REPAIRED CUSP/DIAPHRAGM IN ACCORDANCE WITH AARD 53-20-00-16.
Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
CORROSION ON FORWARD CARGO DOOR BEAM. INSTALLED DOUBLER PER SRM 53-05-00.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
CORROSION ON BOTTOM SIDE OF RIGHT CUSP STATION 1183. INSTALLED DOUBLER PER AARD 53-20-00-16.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
CORROSION ON SUBFLOOR STATION 207 TO 210 FORWARD OF NUMBER 6 SEAT TRACK. REPLACED SUBFLOOR CUSP SHEET AT RIGHT STATION 200 TO 218 PER AARD 53-20-00-16 AND SRM 51-30-02.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
CORROSION ON SHEAR TIE. REMOVED AND REPLACED SHEAR-TIE PER SRM 53-03-00.
Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 55,615 hrs · 28,339 cycles
DAMAGE TO CUSP SHEET RIGHT STATION 699. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
CORROSION ON AFT SERVICE DOOR CUSP UNDER FORWARD GIRT BAR FITTING. INSTALLED DOUBLER ON CUSP UNDER FORWARD GIRT BAR FITTING PER AARD 53-20-00-16.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
HEAVY CABIN CORROSION ON LEFT CUSP FORWARD OF STATION 1309 ON CUSP BETWEEN NUMBER 10 SEAT TRACKS TOP AND BOTTOM OF CUSP. INSTALLED CUSP SHEET AT STATIONS 1250 TO 1309 PER AARD 53-20-00-16.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
HEAVY CABIN - LIGHT CORROSION ON SUBFLOOR DOUBLER STATIONS 200 TO 207 OUTBOARD OF NUMBER 5 SEAT TRACK. INSTALLED DOUBLER AT STATION 200 TO 218 PER AARD 53-20-00-16.
Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 55,615 hrs · 28,339 cycles
CORROSION ON RIGHT CUSP, STATION 237 UNDER FORWARD END OF NUMBER 6 SEAT TRACK. REPLACED CUSP SHEET RIGHT STATION 218 TO 237 PER AARD 53-20-00-16.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
HEAVY CABIN - CORROSION ON GALLEY TIE-DOWN FITTING NUMBER 1 INBOARD STATION 160 (MARKED). REMOVED DAMAGED FITTING AND INSTALLED NEW FITTING PER SRM 51-01-00.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
CORROSION ON RIGHT CUSP SHEET STATION 218-237 IS OUT OF LIMITS. REPLACED CUSP SHEET AT RIGHT SIDE AT STATION 218 TO 237 PER AARD 53-20-00-16.
Part: PAN — CRACKED (WINDOW) · airframe 55,615 hrs · 28,339 cycles
RIGHT WINDOW PAN AT STATION 845 IS CRACKED AT FORWARD UPPER CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.
Part: CASTING — CRACKED (FUSELAGE) · airframe 55,615 hrs · 28,339 cycles
CABIN AFT ENTRY DOOR RIGHT LOWER STOP PAD CASTING IS CRACKED AT LOWER ATTACH FASTENER. REMOVED AND REPLACED STOP PAD CASTING PER SRM 51-01-00.
Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 55,615 hrs · 28,339 cycles
RIGHT CUSP CRACKED AT STATION 846. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,615 hrs · 28,339 cycles
SEAT TRACK BLEND OUT FOR CORROSION REMOVAL IS BEYOND LIMITS AT STATION 1197 TO 1202 ON SEAT TRACK NUMBER 3. INSTALLED SEAT TRACK REPAIR PLUG AT STATION 1198.5 TO 1202 PER AARD 53-20-00-10.
Part: PAN — CRACKED (WINDOW) · airframe 55,615 hrs · 28,339 cycles
WINDOW PAN CRACKED AT UPPER FORWARD CORNER BETWEEN STATION 750-769 LEFT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.
Part: PAN — CRACKED (WINDOW) · airframe 55,615 hrs · 28,339 cycles
RIGHT WINDOW PAN AT STATION 845 IS CRACKED AT UPPER FORWARD CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.
Part: PAN — CRACKED (WINDOW) · airframe 55,615 hrs · 28,339 cycles
RIGHT WINDOW PAN AT 1079 CRACKED AT AFT UPPER CORNER. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
Part: PAN — CRACKED (WINDOW) · airframe 55,615 hrs · 28,339 cycles
RIGHT WINDOW PAN CRACKED STATION 1117 AT AFT UPPER CORNER. REMOVED CRACK AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.
Part: PAN — CRACKED (WINDOW) · airframe 55,615 hrs · 28,339 cycles
RIGHT WINDOW PAN CRACKED AT FORWARD LOWER CORNER STATION 1041. REMOVED CRACK AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.
Part: PAN — CRACKED (WINDOW) · airframe 55,615 hrs · 28,339 cycles
RIGHT WINDOW PAN CRACKED AT STATION 1136 AT AFT UPPER CORNER. REMOVED CRACK AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.
Part: PAN — CRACKED (WINDOW) · airframe 55,615 hrs · 28,339 cycles
RIGHT WINDOW PAN CRACKED AT FORWARD LOWER CORNER STATION 1060. REMOVED CRACK AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.
2009
Part: GENERATOR — INOPERATIVE (NR 2) · airframe 52,543 hrs · 26,655 cycles
SLC - DURING FLIGHT RIGHT GENERATOR KICKED OFF AND AUXILIARY POWER UNIT WOULD NOT COME ON. RETURNED SLC WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 2 ENGINE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: PAN — CORRODED (ZONE 100) · airframe 52,461 hrs · 26,609 cycles
SKIN BULGING IN AREA OF AFT LAV SERVICE PANEL, FORWARD LOWER CORNER. REPAIRED PER EA MD80-53-005988 DATED 04/14/09. FOUND TO BE LEVEL 1 CORROSION.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,417 hrs · 26,584 cycles
EMERGENCY BATTERY PACK FOR EPL DEAD AND WILL NOT CHARGE. REPLACED EMERGENCY BATTERY PACK WITH SERVICEABLE UNIT AND PERFORMED OPERATIONAL CHECK PER WORK CARD 4854.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,450 hrs · 2,658 cycles
FORWARD AISLE BATTERY PACK HAS LOW OUTPUT. REPLACED BATTERY PACK WITH SERVICEABLE UNIT AND PERFORMED OPERATIONAL CHECK PER WORK CARD 4854.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,417 hrs · 26,584 cycles
AFT AISLE BATTERY PACK HAS VERY LOW OUTPUT. INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED OPERATIONAL CHECK PER WORK CARD 4854.
Part: SKIN — CRACKED (FUSELAGE) · airframe 52,417 hrs · 26,584 cycles
FUSELAGE SKIN CRACKED AT STATION 1380 LONGERON 14R. INSTALLED DOUBLER PER SRM 53-30-00-02.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,417 hrs · 26,584 cycles
FORWARD AISLE BATTERY PACK HAS LOW OUTPUT. REPLACED BATTERY PACK WITH SERVICEABLE UNIT AND PERFORMED OPERATIONAL CHECK PER WORK CARD 4854.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,417 hrs · 26,584 cycles
EMERGENCY LIGHT BATTERY INOPERATIVE. INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED OPERATIONAL CHECK PER WORK CARD 4289.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,417 hrs · 26,584 cycles
EMERGENCY LIGHT BATTERY INOPERATIVE. INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED OPERATIONAL CHECK PER WORK CARD 4289.
2008
Part: PLATE — MISSING (EMERGENCY LIGHT) · airframe 51,617 hrs
SFO - EMERGENCY LIGHT AT SEAT 13D MISSING BACK PLATE. REPLACED BACK PLATE AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 51,617 hrs
SFO - EMERGENCY LIGHT AT SEAT 13D MISSING LENS. REPLACED LENS AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — DAMAGED (EMERGENCY LIGHT) · airframe 51,617 hrs
SFO - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED LAMP AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: SEAL — INOPERATIVE (NLG STRUT) · airframe 49,027 hrs
MSP INFLIGHT T1085/06DEC - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR SHOCK STRUT SEALS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHTS AT OVERWING COME ON WHEN SWITCH IS MOVED TO OFF POSITION. REPLACED BATTERY PACKS AT B549 AND B103 FOR INOPERATIVE EMERGENCY LIGHTS AT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHTS IN CABIN COME ON WITH EMERGENCY LIGHT SWITCH IS MOVED TO OFF. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
LGA - SEAT MOUNTED EMERGENCY LIGHTS WILL NOT EXTINGUISH WITH EMERGENCY LIGHT SWITCH IN OFF. REPLACED BATTERY PACK AND RESEATED CONNECTOR AND RESET SYSTEM FOR SEAT MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
SAT - FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)
DFW - CEILING EMERGENCY PATH LIGHT AT ROWS 23, 24, AND 26 INOPERATIVE. RESEATED BATTERY IN BATTERY PACK FOR ROWS 23, 24 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DFW - OVERHEAD EMERGENCY LIGHT AT TAIL COMPARTMENT WALKWAY INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD TAIL COMPARTMENT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY — DISCHARGED (CABIN)
DFW - CEILING EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)
ORD) OVERHEAD EMERGENCY LIGHTS AT SEAT 15A INOPERATIVE. REPLACED BATTERY INSIDE BIN 14DEF FOR EMERGENCY LIGHTS ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--
2002
Part: BATTERY — DISCHARGED (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-175/155-152 DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
SEAT TRACK, CORROSION IN NR 2 SEAT TRACK AT STATION 1200. CUT OUT CORROSION, INSTALLED SEAT TRACK PLUG PER SRM. (2002-1090/ AMC 4)
Part: ACM — LEAKING (A/C BAY)
JFK - FLT 1567 - AFTER TAKEOFF, EN ROUTE LGA-MIA - AT 6000 FEET, FLIGHT ATTENDANT NOTIFIED COCKPIT OF SMOKE IN THE CABIN. SMELLED LIKE ELECTRICAL IN NATURE. AIR INTERRUPTED AND LANDED FJK WITHOUT INCIDENT. REPLACED AIR CONDITIONING DUCT AFT OF WATER SEPARATOR DUE TO RIGHT ACM INTERNAL OIL LEAK. REPLACED RIGHT ACM AND ASSOCIATED DUCTS AND LINES. PRECAUTIONARY REPLACED COALESCER BAG AFTER RUN UP ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: WIRE — DAMAGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: PUMP — LEAKING (NR 2 ENGINE)
DFW - FLT 320 - EN ROUTE DFW-DEN, DETECTED RIGHT SIDE HYDRAULIC PUMP FAILURE DURING CLIMB-OUT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE HYDRAULIC PUMP. SERVICED HYRAULIC SYSTEM. RAN ENGINES. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: LIGHT — BROKEN (AFT AIRSTAIR)
DFW DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT AT AFT AIR STAIR BROKEN. REPLACED EMERGENCY EXIT LIGHT AT AFT AIR STAIR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE — DAMAGED (EXIT LIGHT)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON CATWALK INOPERATIVE. REPINNED EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: STRUT — DISCHARGED (NLG)
DFW - FLT 594 - AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT COMPLETELY. RED LIGHT REMAINED ILLUMINATED AND LOUD AIR NOISE REPORTED BY CREW. AIRCRAFT RETURNED AND LANDED DFW WITHOUT INCIDENT. SERVICED NOSE GEAR STRUT WITH FLUID AND NITROGEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: APU — LEAKING (APU BAY)
ELP - FLT 750 - AFTER TAKEOFF FLIGHT CREW REPORTED SMOKE IN COCKPIT. RETURNED AND LANDED ELP WITHOUT INCIDENT. SEAL LEAKING ON AUXILIARY POWER UNIT. REPLACED AUXILIARY POWER UNIT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS IN AFT HALF OF CABIN INOPERATIVE. RECONNECTED LOOSE CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AFT HALF OF CABIN INOPERATIVE. RESEATED CONNECTOR IN AFT SECTION OF CABIN. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: CONNECTOR — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, AFT DOOR TO STAIRWAY EMERGENCY EXIT MARKER LIGHT INOPERATIVE. REPLACED CONNECTOR TO AFT DOOR TO STAIRWAY EMERGENCY EXIT MARKER LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTS STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS CABIN WERE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)