N70072
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERICAN AIRLINES, INC. (AALA) | Operator | on 1998-07-09 | Operator named in NTSB report |
Accident & incident history
Operated by AMERICAN AIRLINES, INC (per NTSB report)
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.
59 reports on file, 1995-11-20 – 2008-04-27.
Part: DRAIN LINE — LEAKING (RT ENGINE) · airframe 51,588 hrs
SJU INFLIGHT T1845/27APR - DURING CRUISE, GREEN HYDRAULIC QUANTITY DROPPED TO ZERO. LANDING GEAR LOWERED MANUALLY. CREW DECLARED AN EMERGENCY AND LANDED SJU WITHOUT INCIDENT. FOUND NUMBER TWO ENGINE HYDRAULIC PUMP CASE DRAIN LINE LEAKING AT B NUT. TIGHTENED CASE DRAIN LINE AND REPLACED ENGINE DRIVEN PUMP AND CASE DRAIN FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: MODULE — FAILED (RUDDER TRIM) · airframe 51,372 hrs
AUA INFLIGHT T2106/22MAR CCS TO MIA - CREW REPORTED SMOKE IN COCKPIT. LANDED AUA WITHOUT INCIDENT. FOUND RUDDER TRIM MODULE FAILED DURING FLIGHT. REPLACED RUDDER TRIM MODULE AND INSPECTED WIRING HARNESSES AND COCKPIT SYSTEMS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,234 hrs
JFK EMERGENCY LIGHT AT SEAT 29G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 29G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 51,234 hrs
JFK - EMERGENCY LIGHT AT SEAT 19G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 19G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 51,234 hrs
JFK - EMERGENCY LIGHT AT SEAT 23G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Earlier reports · 1995–2007 · 54 reports
2007
Part: FIXTURE — INOPERATIVE (EMERGENCY LIGHTS)
JFK - EMERGENCY LIGHT AT SEAT ROW 10G INOPERATIVE. REPLACED LIGHT ASSEBMLY FOR EMERGENCY LIGHT AT SEAT ROW 10G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: HYDRAULIC LINE — CHAFED (LT PYLON)
SJU INFLIGHT T1845/17APR GREEN HYDRAULIC SYSTEM FLUID LOSS. MANUALLY LOWERED LANDING GEAR. LANDED SJU WITHOUT INCIDENT. LOST NOSE WHEEL STEERING. FOUND LEFT ENGINE PYLON FLEXIBLE HOSE CHAFED AGAINST PIPE AND LEAKING FLUID THROUGH PIN HOLE. REPLACED HYDRAULIC LINE ON NUMBER ONE ENGINE PYLON AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - EMERGENCY LIGHT AT SEAT 34G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 34G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS)
MIA - FOUND EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - FOUND EMERGENCY LIGHT AT SEAT 34C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 34C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - FOUND EMERGENCY LIGHT AT SEAT 11C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — BROKEN (CABIN)
MIA - FOUND EMERGENCY LIGHT ASSEMBLY AT SEAT 13G IS BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 13G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — BROKEN (CABIN)
MIA - FOUND EMERGENCY LIGHT ASSEMBLY AT SEAT 25G IS BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 25G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - FOUND EMERGENCY LIGHT AT SEAT 37C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 37C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - FOUND EMERGENCY LIGHT AT SEAT 10G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 10G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - FOUND EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - FOUND EMERGENCY LIGHT AT SEAT 11G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - FOUND EMERGENCY LIGHT AT SEAT 5C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 5C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS)
MIA - FOUND EMERGENCY LIGHT AT SEAT 30C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 30C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: ACTUATOR — INOPERATIVE (ZONE 100)
MIA INFLIGHT T1845/06JAN - AFTER TAKEOFF AT FLAP RETRACTION BOTH RUDDER TRAVEL SYSTEMS ONE AND TWO FAULTED. RESET AND FAULTED AGAIN. LANDED MIA WITHOUT INCIDENT. REPLACED THE VARIABLE STOP TRANSDUCER UNIT AND THE VARIABLE STOP ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BULB — BROKEN (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT SEAT 36G IS BROKEN. RELAMPED EMERGENCY LIGHT AT SEAT 36G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
MIA - EMERGENCY LIGHT AT SEAT 11C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
MIA - EMERGENCY LIGHT AT SEAT 11C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — BROKEN (CABIN)
MIA - EMERGENCY LIGHT AT SEAT 36G HAS BROKEN LAMP. RELAMPED EMERGENCY LIGHT AT SEAT 36G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)
JFK - EMERGENCY LIGHT EXIT SIGN AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY CHARGER FOR EMERGENCY LIGHT EXIT SIGN AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)
JFK - SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS LEFT SIDE INOPERATIVE. REPLACED BATTERY CHARGER UNIT FOR SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: FUEL FILTER — CONTAMINATED (NR 1 ENGINE)
NR 1 ENGINE FUEL CLOG LIGHT CAME ON MOMENTARILY WITH CLIMB-OUT. INSPECTED ENGINE. REPLACED MAIN ENGINE FUEL FILTER ASSEMBLY AND DIFFERENTIAL PRESSURE SWITCH. OPERATIONAL CHECK NORMAL AND NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: TRANSMITTER — MALFUNCTIONED (HYDRAULIC SYS)
MIA - GREEN HYDRAULIC SYSTEM QUANTITY LOSS DURING DESCENT. ECAM AND GAUGE ON OVERHEAD PANEL BOTH SHOWED HYDRAULIC LEVEL IN YELLOW BAND. PERFORMED MANUAL GEAR EXTENSION AND LANDED MIA WITHOUT INCIDENT. REPLACED GREEN SYSTEM RESERVOIR QUANTITY TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: HYDRAULIC LINE — CRACKED (HYDRAULIC SYS)
MIA - GREEN SYSTEM QUANTITY SHOWED AT RED DOT. MANUALLY EXTENDED GEAR. FOUND PRESSURE LINE IN CENTER GEAR WELL CRACKED. REPLACED PRESSURE LINE IN CENTER GEAR WELL. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: LIGHT — INOPERATIVE (SEAT 36G)
JFK - EMERGENCY LIGHT INOPERATIVE AT SEAT 36G. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 36G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: PIN — BACKED OUT (CONNECTOR)
MIA - FORWARD ENTRY EMERGENCY LIGHT AT DOOR 3R INOPERATIVE. REPLACED PUSH BACK PIN AT CONNECTION FOR FORWARD ENTRY EMERGENCY LIGHT AT DOOR 3R. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: RECEPTACLE — DISCONNECTED (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT RECEPTACAL PULLED OUT FROM SEAT 19G AND IS INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY FOR SEAT 19G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SCHRADER VALVE — LEAKING (RT MLG ACTUATOR)
BOS T2087/5 UNABLE TO RETRACT MAIN LANDING GEAR. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND MAIN LANDING GEAR TILT ACTUATOR SHRADER VALVE AND SERVICED ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: WINDOW — CRACKED (COCKPIT)
CAPTAIN'S L1 WINDSCREEN DEVELOPED ARCING IN THE OUTER PAIN. WINDOW CRACKED SEVERELY. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED CAPTAINS WINDSHIELD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: GROUND WIRE — BROKEN (ELECTRICAL SYS)
FLT 93 - APU FAULTED IN FLIGHT AND WOULD NOT RESTART. NO FAULTS WERE FOUND ON THE ECB. REPLACED THE ECB AS PRECAUTIONARY. PROBLEM FOUND TO BE A BROKEN GROUND WIRE TO THE STANDBY GENERATOR CONTROL VALVE. WIRE WAS REPAIRED AND STANDBY GENERATOR TEST WAS PERFORMED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT APU WAS RETURNED TO SERVICE. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
TUL - FOUND CORROSION. INSTALLED STRAP REPAIR PER ESO 30595 DATED 5/15/01 TRACK TO BE REPLACED AT MBU 8. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - FOUND CORROSION ON FRAME 11A AT BOTTOM SECTION OF FRAME 11 AND STRINGER 49L, CORROSION ON LEFT LOWER NWW TORQUE BOX CHORD ANGLE AT FRAME 11 AND STRINGER 49L. COMPLETED REPAIR PER ESO 30595 D=05-18-01. (M)
Part: SUPPORT — CORRODED (FUSELAGE)
TUL - FOUND CORROSION FS 75-80, BEYOND LIMITS. REPLACED GALLEY SUPPORT FROM FS 75-80 PER SRM 51-72-10-01. (M)
2000
Part: PCU — MALFUNCTIONED (SLATS)
JFK - FLT 0092 - ON INITIAL CLIMB-OUT, GOT SLATS SYSTEM 2 FAULT. CONCURRENT WITH F/O SPEED LIMIT WARNING WHEN SLATS RETRACTED, GOT CGCC FAULT (TRIM TANK ISOL VALVES SLOW TO OPEN). NO OTHER FAULTS OR ANOMALIES (SUCH AS RUDDER TRAVEL OR PITCH FEEL). F/O ADC INSTRUMENT SWITCHING NORMAL CLIMBING THROUGH MODERATE CHOP SLAT FAULT LIGHT ON SFPI ILLUMINATED. EN ROUTE TO JFK, DIVERSION SLATS EXTENDED NORMALLY. NORMAL SLAT/FLAPS 30/40 LANDING AT 350.000 POUNDS SINK RATE 200 FPM, SMOOTH TOUCH DOWN. REPLACED YELLOW FLAP SYSTEM SWITCH ON PCU RIGHT HAND AFT CLEAR BOX OF FAULTS. OPS CHECKS OK OF FLAP SYSTEM. NO FAULT NOTED, LEAK CHECKS OK. (X)
1999
Part: WIRE — LOOSE (E/E COMPT)
JFK - FLT 1540 - EN ROUTE JFK-PAP - DURING CRUISE LEFT INNER FUEL QTY DROPPED BY 10,000 LBS AND REMAINED LOW THE REMAINEDER OF THE FLIGHT. WHEN LEFT INNER FUEL TANK REACHED ZERO, XX'S WERE DISPLAYED FOR REMAINDER OF FLIGHT. LANDED JFK WITHOUT INCIDENT. RESECURED LOOSE HI-Z TERMINAL ON NR 4 PROBE. CAPACITY TEST CHECKS NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: COMPUTER — DEFECTIVE (E/E COMPT)
MIA - FLT 657 - EN ROUTE JFK-PAP, DURING CRUISE, LEFT INNER FUEL QTY INDICATION RAPIDLY DECREASED FROM ABOUT 28,000 TO 11,500 LBS. NO FUEL LEAK INDICATION. AIR INTERRUPTED AND LANDED MIA WITHOUT INCIDENT. REPLACED FUEL QTY COMPUTER. PERFORMED ALL REQUIRED TEST CHECKS ACCORDING TO MAINTENANCE MANUAL. SUMPED ALL TANK OF WATER. TRANSFERRED ALL FUEL OUT OF LEFT INNER TANK, HAD FUELER METER FUEL BACK INTO TANK. USED FUEL TANK STICK FOR FUEL VERIFICATION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (L3 DOOR)
JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SELF TEST AT L3 DOOR INOPERATIVE. SECURED LOOSE CONNECTOR ON OVERHEAD CEILING LIGHT AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (ROW 17A)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17H INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 17H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: MOUNT — CORRODED (LAVATORY)
TUL - FOUND OUTBOARD FORWARD MOUNT CORRODED LEV U. REPAIRED IN SHOP ON SHOP ORDER NR YFT4. (M)
Part: MOUNT — CORRODED (LAVATORY)
TUL - MOUNTING FOOT FORWARD OF LAV V DOOR IS CORRODED. REPLACED IN SHOP ON SHOP ORDER NR YFT6. (M)
Part: SEAT TRACK — CORRODED (BS 1764-1817)
TUL - NR 9 SEAT TRACK IN 'A' ZONE CABIN CORRODED. INSTALLED NEW SEAT TRACK NR 9 BETWEEN FRAME 26 - FRME 30. INSTALLED 1ST OVER SIZE .25 HLT 4268 AND 4266, SEALED TRACK WITH 870 SEALANT. REF SRM 51-72-10-0. (M)
Part: SUPPORT — CORRODED (FRAM 71-74)
TUL - FOUND CORROSION ON TOP OF FLOORBOARD SUPPORT TRACK NR 6. REPLACED FLOORBOARD SUPPORT FRAME 71-74 PER SRM 51-71-10. (M)
Part: SEAT TRACK — CORRODED (FRAME 27-30)
FOUND CORROSION IN SEAT TRACK NR 10 FRME 27 TO FRAME 30 AND TIE DOWN FOR LAV 'M'. REMOVED AND REPLACED SECTION OF SEAT TRACK NR 10 PER SRM 51-72-10-0 FROM FRAME 26 TO 30. (M)
Part: SUPPORT — CORRODED (FRAME 74)
TUL - FOUND CORROSION ON TOP OF FLOORBOARD SUPPORT AFT OF FRAME 74, BETWEEN FLOORBOARD SUPPORT 5A AND TRACK NR 6. REPLACED FLOORBOARD SUPPORT ANGLE PER SRM 51-71-10. (M)
1998
Part: SWITCH — FAILED (RT ENGINE)
LHR - FLT 109 - AFTER T/O, THE FWD INSTRUMENT PNL RT ENG OIL CLOG LAMP ILLUMINATED, FOLLOWED A SHORT TIME LATER BY THE ECAM PROCEDURE FOR OIL CLOG DIPICTED. RT THROTTLE RETARDED TO IDLE. AFTER 3 MINS WITH THE OIL CLOG LAMP BRIGHTLY LIT. THE ENG WAS SHUT DOWN WITH THE RT FUEL SHUTOFF VALVE. A SINGLE ENG APPROACH WAS FLOWN AND A LANDING MADE AT 36,800 LBS. RT SIDE BRAKES INDICATED 700 DEGREES. THE RT 4 TIRES DEFLATED AFTER APPROX 30 MIN CREW WAS CLEARED TO DEPART. REPLACED DIFF PRESS SW, ACCOMP NR 2 ENG POWER RUN. NO ABNORMAL IND'S. OK FOR SERV REF MX CHECK CARD AE059214. VISUAL INSPECTION ACCOMP OF A/C WITH REF TO LANDING WT AND SINK RATE. ALL CHECKS OK. REPLACED ALL RT MLG WHEELS AND BRAKES. ALSO,
Part: ENGINE — FAILED (NR 2)
JFK - FLT 141 - N2 ENGINE VIBRATION ECAM, NR 2 ENGINE INDICATION FLASHING. VARIED FROM 4.6 AT CRUISE POWER INCREASING TO 6.0 -6.4 WHEN THROTTLE REDUCED TO IDLE. POSSIBLE SLIGHT BUZZ LEFT IN NR 2 THROTTLE. N1 VIB AND ALL OTHER INDICATIONS NORMAL. NOTICEABLE HARMONIC VIBRATION WHEN ENGINE WINDING DOWN AT GATE. REMOVED AND REPLACED NR 2 ENGINE AS PER MCM WORKCARD NR AE719307 AND ACCOMPLISHED ENGINE RUN UP. ENGINE OPS AND LEAK CHECKS NORMAL. (M)
1997
Part: RELAY — DEFECTIVE (CABIN)
JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS ILLUMINATED WITH SWITCH IN DISARM POSITION. REPLACED EMERGENCY FLOOR LIGHT RELAY 38WJ AND DIODE MODUEL5VD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: STRIP — DEFECTIVE (CABIN)
JFK - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS AT 12HJ TO 14HJ INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT ASSEMBLY BETWEEN 12HJ AND 14HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: COALESCER — DIRTY (ACM BAY)
SDQ - FLT 1728 - AFTER TAKEOFF SDQ DURING CLIMB-OUT, ELECTRICAL TYPE ODOR NOTED IN CABIN WITH NO VISIBLE SMOKE. AIRCRAFT RETURNED SDQ AND LANDED WITHOUT INCIDENT. CHECKED CABIN AREA WITH NO DEFECTS FOUND. ACCOMPLISHED PACK BURNOUT PROCEDURE AND PRECAUTIONARY REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION AND UNABLE TO DUPLICATE ODOR. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — DEFECTIVE (CABIN FLOOR)
JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY R4 DOOR INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY R4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (CABIN FLOOR)
JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 23H AND 32H INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 23H AND 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DAMAGED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AT ROW 14-16 A AND B DAMAGED. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: STRIP — MISSING (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP MISSING AT RIGHT AISLE FROM PAX SEAT ROW 29H AFT. REPLACED EMERGENCY FLOOR LIGHT STRIP AT RIGHT AISLE FROM PAX SEAT ROW 29H AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: CONNECTOR — LOOSE (CABIN)
JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 18HJ AND 22HJ INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 18HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)