N11060
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
100 reports on file, 1995-04-30 – 2009-06-01.
Part: FLEX LINE — DEFECTIVE (HYDRAULIC SYS) · airframe 54,955 hrs · 21,395 cycles
MIA - AIRCRAFT HAD YELLOW HYDRAULIC SYSTEM LOSS DURING TAKEOFF. EMERGENCY DECLARED, RETURNED TO MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT GENERATOR YELLOW PRESSURE FLEX LINE. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: INDICATOR — INOPERATIVE (FUEL QTY) · airframe 54,843 hrs · 21,348 cycles
LOST FUEL QUANTITY INDICATION ILLUMINATED WHILE IN FLIGHT. EMERGENCY DECLARED RETURNED MIA WITHOUT INCIDENT. REPLACED TRIM TANK HARNESS AND PROBES. REPLACED FUEL QUANTITY PROCESSOR AND INDICATOR. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)
Part: PUMP — INOPERATIVE (HYDRAULIC SYSTEM) · airframe 54,794 hrs · 21,328 cycles
JFK - THE CREW REPORTED THAT THE AIRCRAFT HAD LOST THE YELLOW HYDRAULIC SYSTEM. EMERGENCY DECLARED LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED YELLOW HYDRAULIC SYSTEM ENGINE DRIVEN PUMP ON NUMBER TWO ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION.
Earlier reports · 1995–2008 · 97 reports
2008
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 54,058 hrs
MIA - EMERGENCY LIGHT AT SEAT 32C INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 32C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE — BROKEN (SLAT SYSTEM) · airframe 53,707 hrs
GYE - CREW REPORTED SLAT LOCKOUT AT 5 DEGREES. NO ECAM OR WARNINGS OR FAULT INDICATIONS. LANDED GYE WITHOUT INCIDENT. FOUND BROKEN WIRES ON CONNECTOR TO POSITION PICK OFF UNIT 4CN. REPLACED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,702 hrs
MIA - EMERGENCY LIGHT AT SEAT 33G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,702 hrs
MIA - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 52,702 hrs
MIA - EMERGENCY LIGHT AT SEAT 12G INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 12G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — BROKEN (CABIN) · airframe 52,702 hrs
MIA - EMERGENCY LIGHT AT SEAT 10G LIGHT BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 10G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 52,702 hrs
MIA - EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. FOUND PIN PUSHED BACK AT CONNECTOR. SECURED CONNECTOR FOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,702 hrs
MIA - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,702 hrs
MIA - EMERGENCY LIGHT AT SEAT ROWS 6G TO 18G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROWS 6G TO 18G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,702 hrs
MIA - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,702 hrs
MIA - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,702 hrs
MIA - EMERGENCY LIGHT AT SEAT 6C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 6C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,519 hrs
JFK - EMERGENCY LIGHT AT SEAT 3D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 3D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LINE — LEAKING (HYDRAULIC SYS)
SJU INFLIGHT T1692/29JAN - CREW REPORTED HYDRAULIC ODOR IN CABIN AROUND SEAT ROW 17AB. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. FOUND HYDRAULIC LEAK AT SEAT ROW 16AB. REPAIRED HYDRAULIC LINE AT SEAT ROW 16AB AND CLEANED AREA. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: GCU — FAULTED (LT GENERATOR)
JFK - LEFT GENERATOR FAILED IN FLIGHT. AUXILLIARY POWER UNIT WOULD NOT START. LANDED JFK WITHOUT INCIDENT. FLIGHT WAS OVERWEIGHT. REPLACED GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CYLINDER — FROZEN (MLG DOOR)
MIA INFLIGHT T639/28MAY - REPEATER RETURNED TO MIA DUE TO BOTH NOSE LANDING GEAR DOOR INDICATORS ILLUMINATED. LANDED MIA WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. FOUND DOOR ACTUATOR CYLINDER EYEBOLT END FROZEN. REPLACED DOOR ACTUATOR CYLINDER AS REQ PER 32-31-16. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: NUT — LOOSE (DOOR ROD END)
MIA INFLIGHT T639/28MAY - RETURNED TO MIA DUE TO BOTH NOSE LANDING GEAR DOOR INDICATORS ILLUMINATED. LANDED WITHOUT INCIDENT. FOUND LEFT LANDING GEAR DOOR ACTUATOR ROD END JAM NUT LOOSE. RESECURED LANDING GEAR DOOR ACTUATOR ROD END JAM NUT. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: LIGHT — INOPERATIVE (CABIN)
MIA - EMERGENCY LIGHT AT SEAT 7G INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 7G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN)
MIA - EMERGENCY LIGHTS AT SEATS 1G TO 3G DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 1G TO 3G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: ACTUATOR — INOPERATIVE (FUEL CROSSFEED)
MIA - ON CLIMBOUT CREW NOTICED FUEL IMBALANCE BETWEEN RIGHT INNER TANK AND LEFT INNER TANK OF 7000 POUNDS. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED CROSSFEED VALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (CABIN)
MIA - EMERGENCY LIGHTS FROM SEATS 6G TO 18G AND SEAT 23G INOPERATIVE. SECURED CONNECTION AT SEATS 6G TO 18G AND RESECURED PLUG 23G. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
EMERGENCY LIGHTS IN FORWARD RT ZONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD RT ZONE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
JFK - EMERGENCY LIGHTS IN AFT LEFT AND RIGHT ZONE INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS IN AFT LEFT AND RIGHT ZONE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (CABIN)
MIA - EMERGENCY EXIT LIGHTING AT LEFT FIRST CLASS SEAT INOPERATIVE. REPLACED BATTERY PACK AT 110WL1 FOR EMERGENCY EXIT LIGHTING AT LEFT FIRST CLASS SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: APU — LEAKING (APU BAY)
LIR - AIR INTERRUPT INTO LIR DUE TO SMOKE IN CABIN. LANDED LIR WITHOUT INCIDENT. REPLACED WATER SEPARATOR BAGS AND ACCOMPLISHED PACK BURN. PLACARD APU. MIA FOUND OIL IN APU COMPARTMENT. AIRCRAFT OUT OF SERVICE FOR REPAIRS.
Part: LOCK — INOPERATIVE (CONTAINER ROLLER)
AFT CARGO COMPARTMENT SMOKE WARNING RIGHT AFTER TAKEOFF. FIRED BOTH BOTTLES ALTHOUGH DID NOT GET AGENT 2 DISCHARGE LIGHT. AFTER LANDING GOT CARGO LOOP B. FOUND LEFT AFT CONTAINER ROLLER RUNS CONTINUOUSLY. REPAIRED JAMMED LOCK 511MY. REPAIRED JOYSTICK AND CARGO CONTROL BOX. REPLACED BOTH FIRE BOTTLES. REPLACED CED 44WH AND 8WH AS PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LINE — LEAKING (HYD SYSTEM)
YELLOW SYSTEM HYDRAULIC QUANTITY LOST ON CLIMB-OUT. FOUND HYDRAULIC LINE IN LT WHEEL WELL LEAKING. REPLACED HYDRAULIC LINE IN LT WHEEL WELL. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
JFK - EMERGENCY LIGHT EXIT SIGN AT DOOR 3L INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGN AT DOOR 3L. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: SMOKE DETECTOR — INOPERATIVE (E/E COMPT)
EN ROUTE MIA-BOS, AVIONICS SMOKE WARNING ON ECAM. NO SMOKE OR HEAT NOTED IN AVIONICS COMPARTMENT. LANDED IN RDU WITHOUT INCIDENT. TROUBLESHOT AND REPLACED SMOKE DETECTOR 11WA. SYSTEM ROUND CHECKED NORMAL OPERATION. (M)
2002
Part: SKIN — CORRODED (WING)
FOUND BOTTOM SKIN (WING) CORRODED TOP SURFACE JUST INBOARD OF NR 5 JACKSCREW. FLAP PEENED BLENDED AREA PER SRM 51-29-00-2 ALODINED AND PRIMED PER ESO 30595 DATED 9-23-2002. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
TUL - FOUND LEFT SEAT TRACK C IS CORRODED. INSTALLED SERVICEABLE TRACK PER SRM 51-72-10. (M)
2001
Part: SKIN — CORRODED (LT WING)
TUL - FOUND CORROSION IN THE FORM OF A HOLE THROUGH SKIN ON LEFT WING LOWER SKIN L/E JUST INBOARD OF RIB 20. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO30595 DATED 10 AUG 01. (M)
2000
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
TUL - FOUND LATERAL SUPPORT TRACK AFT OF FRAME 74 CORRODED BETWEEN TRACKS D/E RIGHT. REMOVED AND REPLACED LATERAL SUPPORT TRACK PER SRM 51-72-10-0. (M)
Part: TRACK — CORRODED (LAVATORY)
TUL - FOUND LAV L TRACK C LEFT IS CORRODED ON TOP. REMOVED CORROSION PER SRM, BEYOND LIMITS. INSTALLED REPAIR STRAP PER AARD 53-20-00-2. (M)
Part: LIGHT — INOPERATIVE (ROW 24)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FORWARD SEAT ROW 24B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — DAMAGED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS BETWEEN SEAT ROW 12B TO 15B INOPERATIVE. REPLACED EMERGENCY EXIT SPLICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM SEAT ROWS 12B AND 15B INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: COALESCER BAG — DIRTY (ACM BAY)
MIA - FLT 596 - AFTER TAKEOFF, WHOLE AIRPLANE HAD PLASTIC BURNING SMELL. RETURNED AND LANDED MIA WITHOUT INCIDENT. ACCOMPLISHED ENGINE RUN UP AT DIFFERENT POWER SETTINGS, ACCOMPLISHED PACK BURNOUT AND CHANGED COALESCER BAGS ON BOTH PACKS. NO ODOR NOTICED. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: CONNECTOR — DISCONNECTED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, L2 EMERGENCY EXIT SIGN INOPERATIVE. RECONNECTED L2 EMERGENCY EXIT SIGN CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: SENSOR — FAILED (LT MLG)
MIA - FLT 881 - ON FINAL MIA, UNABLE TO EXTEND LANDING GEAR HYDRAULICALLY. EXTENDED LANDING GEAR MANUALLY AND LANDED MIA WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: ANGLE — DAMAGED (RT WING)
TUL - ACCOMPLISH PERMANENT REPAIR TO RIGHT WING ROOT PICK UP ANGLE. MADE REPAIR TO RT WING ROOT PER ESO 3095, DATED 7-6-99. (M)
Part: ANGLE — DAMAGED (LT WING)
TUL - ACCOMPLISH PERMANENT REPAIR TO LEFT WING ROOT PICK UP ANGLE. INSTALLED PERMANENT REPAIR TO LT WING ROOT PICK UP ANGLE PER ESO 3095, DATED 7-6-99. (M)
Part: CONNECTOR — LOOSE (ROW 15-25)
JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEAT ROWS 15B THROUGH 25B WERE INOPERATIVE. RESEATED EMERGENCY FLOOR PATH LIGHT WIRE CONNECTOR AT SIDEWALL SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: FITTING — CORRODED (BS 0200)
TUL - CORRODED FITTING. REMOVED AND REPLACED CORRODED PART. TST: 27,050.02 HOURS. CYCLES: 10,790. (X)
Part: ROLLER TRAY — CORRODED (FORWARD CARGO)
TUL - NR 3 ROLLER TRAY CORRODED AT FRAME 38.2. INSTALLED TRACK PER SRM 51-72-10. TST: 27,050.02 HOURS. CYCLES: 10,790. (X)
Part: FITTING — CORRODED (FORWARD CARGO)
TUL - TWO EACH PALLET GUIDE FITTINGS CORRODED. REMOVED AND REPLACED 2 EACH PALLET GUIDE FITTINGS PER SRM 53-10-15. TST: 27,050.02 HOURS. CYCLES: 10,790. (X)
Part: STRINGER — CORRODED (BULK CARGO)
TUL - CORROSION BETWEEN FRAMES 64 AND 65 AT STR 51L. REMOVED CORROSION ON STR 51L PER SRM 51-74-10. REPLACED STRINGER SPLICE PER SRM 51-72-10. TST: 27,050.02 HOURS. CYCLES: 10,790. (X)
Part: ROLLER TRAY — CORRODED (FORWARD CARGO)
TUL - NR 6 ROLLER TRAY CORRODED. REMOVED AND REPLACED ROLLER TRAY PER SRM 53-10-15. TST: 27,050.02 HOURS. CYCLES: 10,790. (X)
Part: PANEL — CORRODED (NR 2 PYLON)
TUL - MILD CORROSION ON PANEL LANDING. REPLACED PANEL PER SRM 51-72-10-0. TST: 27,050.02 HOURS. CYCLES: 10,790. (X)
Part: SUPPORT — CORRODED (FORWARD CARGO)
TUL - CORROSION ON SLANT PANEL SUPPORT. REMOVED AND REPLACED SLANT PANEL SUPPORT PER SRM 53-10-15. TST: 27,050.02 HOURS. CYCLES: 10,790. (X)
Part: STRINGER — CORRODED (BULK CARGO)
TUL - CORROSION ON STR 57 FROM FRAMES 65 TO 70. REMOVED AND REPLACED STR 57 FROM FRAMES 65 TO FRAME 70 PER SRM 51-72-10. TST: 27,050.02 HOURS. CYCLES: 10,790. (X)
Part: STRINGER — CORRODED (BULK CARGO)
TUL - CORROSION ON STRINGER SPLICE 54L AT FRAME 65 IN BULK CARGO. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-72-10. TST: 27,050.02 HOURS. CYCLES: 10,790. (X)
Part: ROLLER TRAY — CORRODED (FORWARD CARGO)
TUL - NR 1 ROLLER TRAY CORRODED SEVERAL PLACES BETWEEN FRAMES 32 AND 37. INSTALLED NEW SECTION OF TRACK PER SRM 51-72-10-2. TST: 27,050.02 HOURS. CYCLES: 10,790. (X)
Part: SEAT TRACK — CORRODED (FRAME 31)
TUL - FOUND CORROSION ON SEAT TRACK NR 8 BETWEEN FRAME 29 AND 33. REMOVED CORRODED SECTION OF TRACK NR 8 AND FABRICATED NEW SECTION AND INSTALLED DOUBLERS PER SRM 51-72-10-0 AND ESO 30595 DATED 3/25/98. (M)
Part: STRINGER — CORRODED (FRAME 69)
TUL - FOUND STRINGER 49L HAS CORROSION AT FRAME 69. REMOVED CORRODED SECTION OF STRINGER. INSTALLED NEW SECTION AND DOUBLER TO STRINGER 49L PER SRM 53-10-14. (M)
Part: CROSS FRAME — CORRODED (CABIN)
TUL - FOUND CORROSION ON CABIN CROSS FRAME. INSTALLED DOUBLER ANGLE PER ESO 30595 DATED 3-20-98. (M)
Part: SEAT TRACK — CORRODED (FRAME 28)
TUL - FOUND CORROSION ON TRACK NR 10, 4 INCHES FORWARD OF FRAME 28. INSTALLED TRACK NR 10 FROM FRAME 26-30 PER SRM 51-72-10-0. (M)
Part: FRAME — CORRODED (FRAME 28)
TUL - FOUND CORROSION ON TOP OF FRAME 28 BETWEEN SEAT TRACK NR 9 AND NR 10. INSTALLED DOUBLER ANGLE PER SRM 51-71-50, ALODINED, PRIMED AND PAINTED, BLENDED AREA AND DOUBLER PER SRM 51-22-00. (M)
Part: SEAT TRACK — CORRODED (FRAME 21-26)
TUL - FOUND TWO AREAS OF CORROSION AND MECHANICAL DAMAGE ON NR 10 TRACK. INSTALLED TRACK NR 10 BETWEEN FRAMES 21-26 PER SRM 51-72-10-0, ALODINED, PRIMED AND PAINTED TRACK PER SRM 51-21-00-0. (M)
Part: SUPPORT — CORRODED (FRAME 74)
TUL - FLOOR SUPPORT CORRODED FWD FRAME 74 BETWEEN TRACKS 6 AND 7. BLENDED OUT CORROSION AND REPAIRED DAMAGE ON FRAME 74 BETWEEN TRACKS 6 AND 7 PER SRM 53-20-00-2. (M)
Part: TRACK — CORRODED (FRAME 31)
TUL - TRACK 3A LAV SUPPORT TRACK HAS CORROSION IN AROUND 3 LAVATORY BOLT HOLES AND ON TOP OF TRACK. REMOVED CORRODED TRACK AND LAVATORY SUPPORT BOLT HOLE BLOCKS AND REPLACED WITH NEW PER SRM 51-72-10-0 AND 51-21-00-0. (M)
Part: SEAT TRACK — CORRODED (FRAME 78)
TUL - FOUND CORROSION AROUND FLOORBOARD MOUNT HOLE ON NR 7 TRACK JUST AFT OF FRAME 78. BLENDED OUT CORROSION AND INSTALLED STRAP DOUBLER PER AARD 53-20-00-02. (M)
Part: SEAT TRACK — CORRODED (FRAME 14-18)
TUL - FOUND CORRODED SEAT TRACK NR 6. REMOVED AND REPLACED THE SECTION OF SEAT TRACK NR 6 PER SRM 51-72-10-0. (M)
Part: SUPPORT — CORRODED (FRAME 71-72)
TUL - FLOORBOARD SUPPORT IS CORRODED BETWEEN FRAME 71 AND 72 AT TRACK NR 7. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP PER AARD 53-20-00-02. (M)
Part: SEAT TRACK — CORRODED (FRAME 73-74)
TUL - THE SMALL SEAT TRACK INBOARD OF R-4 DOOR IS CORRODED BETWEEN 73 FRAME AND 74 FRAME TRACK 9. REMOVED AND REPLACED SEAT TRACK LOCATED AT TRACK 9 BETWEEN FRAME 73 AND 74 PER SRM 51-77-10-0. (M)
Part: FLOORBEAM — CORRODED (FRAME 66-69)
TUL - LARGE AREAS OF CORROSION BETWEEN FRAME 66 AND FRAME 69 LEFT SIDE OF BULK CARGO FLOORBEAM. REMOVED AND REPLACED BULK CARGO FLOORBEAM BETWEEN FRAME 66 AND 69 LEFT SIDE PER SRM 53-10-15. (M)
Part: SUPPORT — CORRODED (FRAME 72-73)
TUL - FLOOR SUPPORT CORRODED AT TRACK NR 6 BETWEEN FRAME 72 AND 73. BLENDED OUT CORROSION AND INSTALLED STRAP REPAIR PER AARD 53-20-00-02. (M)
Part: FLOORBEAM — CORRODED (FRAME 67)
TUL - FOUND CORROSION ON FLOORBEAM AT FRAME 67 BETWEEN TRAYS NR 1 AND NR 2. REMOVED AND REPLACED FLOORBEAM AT FRAME 67 BULK CARGO FLOOR BETWEEN TRAYS 1 AND 2 PER SRM 53-10-15. (M)
Part: SUPPORT — CORRODED (FRAME 72)
TUL - FLOOR SUPPORT CORRODED AT FRAME 72 BY TRACK NR 7. FABRICATED AND INSTALLED STRAP REPAIR PER AARD 53-20-00-02. (M)
Part: SUPPORT — CORRODED (FRAME 15)
TUL - FOUND CORROSION OF LAST 19 INCHES OF SECTION. INSTALLED STRAP ON FLOORBOARD SUPPORT PER AARD 53-20-00-2 PAGE 1. (M)
Part: SUPPORT — CORRODED (CABIN)
TUL - FOUND CORRODED FLOORBOARD SUPPORT IN CABIN. REMOVED AND REPLACED FLOORBOARD SUPPORT FROM FRAME 71 TO 73 PER SRM 51-72-10-0. (M)
1997
Part: WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN 12B AND 18B INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRES. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: CONNECTOR — BROKEN (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT LEFT AISLE BETWEEN PAX SEAT ROWS 12 AND 18 INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT LEFT AISLE BY PAX SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE OF FIRST CLASS CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTORS AT LEFT AISLE OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — BROKEN (CABIN)
JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 21B AND 23B INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: WIRE — BROKEN (CABIN)
JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 20AB TO 23AB INOPERATIVE. REPLACED BROKEN POWER FEED WIRE FROM CABIN SIDEWALL CONNECTOR TO LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CASTING — CORRODED (BS 2490-2505)
TUL - FOUND TWO AREAS OF CORROSION ON AFT LEFT SIDE OF AFT MANHOLE. INSTALLED DOUBLER PER ESO 30595, DATED 4-12-96. (M)
Part: ANGLE — CORRODED (FRAME 76-78)
TUL - FOUND ATTACH ANGLE CORRODED ALONG LENGTH AT N/P HOLES. REPLACED ATTACH ANGLE PER SRM 51-72-10. (M)
Part: ANGLE — CORRODED (FRAME 74-76)
TUL - FOUND ATTACH ANGLE CORRODED ALONG ENTIRE LENGTH AT N/P HOLES. REPLACED ATTACH ANGLE PER SRM 51-72-10. (M)
Part: SEAT TRACK — CORRODED (CABIN)
TUL - FOUND NR 8 SEAT TRACK CORRODED IN SEVERAL AREAS BETWEEN FRAME 26-31 IN FRONT OF LAV M AND RIGHT SERVICE CTR. INSTALLED SEAT TRACK NR 8 FROM FRAME 25.5 TO 33.5. PER AARD 51-10-00-3 AND SRM 51-72-10-0. (M)
Part: PIN — CORRODED (TE FLAPS)
TUL - FOUND FAIL/SAFE PINS FOR NR 3 AND NR 5 FLAP TRACK FRONT TO REAR G CARRIAGE PIN HAS CORROSION. REPLACED PINS. (M)
Part: SEAT TRACK — CORRODED (CABIN)
TUL - FOUND SEAT TRACK NR 3 IS HEAVILY CORRODED AT THRESHOLD TO LAV L BETWEEN FRAME 31L AND 33L. INSTALLED MANUFACTURED SEAT TRACK IAW SRM 51-71 50 PG 201-206. (M)
Part: PIN — CORRODED (NR 6 TE FLAP)
TUL - FOUND CORROSION ON FAIL/SAFE PIN FOR NR 6 FLAP TRACK FRONT TO REAR CARRIAGE PIN. REPLACED PIN. (M)
Part: PIN — CORRODED (NR 3 FLAP TRACK)
TUL - FOUND CORROSION ON HOLLOW PIN FOR NR 3 FLAP TRACK FRONT TO REAR CARRIAGE ATTACHMENT. REPLACED PINS. (M)
Part: ANGLE — CORRODED (FS NR 13)
TUL - FOUND Z-ANGLE CORRODED. DUPLICATED Z-ANGLE PER SAMPLE FROM 2024-T3. (M)
Part: SEAT TRACK — CORRODED (FRAME 73/74)
TUL - FOUND CORROSION ON SEAT TRACK SECTION JUST INSIDE R4 DOOR BETWEEN FRAMES 73 AND 74. REPLACED SEAT TRACK SECTION JUST INSIDE R4 DOOR BETWEEN FRAMES 73 AND 74 AARD 51-10-00 AND INSTALLED SUPPORT PER SRM 51-72-10-0. (M)
Part: CHANNEL — CORRODED (CABIN)
TUL - FOUND CORROSION ON J-CHANNEL AT FRAME 73 UNDER LAV U. REMOVED AND REPLACED J-CHANNEL PER SRM 51-72-10, PRIMED AND PAINTED AND ALODINED PER SRM 51-21-00. (M)
Part: SUPPORT — CORRODED (FRAME 72-73)
TUL - FOUND FLOORBOARD SUPPORT FLANGE IS HEAVILY CORRODED BETWEEN FRAMES 72 AND 73 AT FLANGE NR 4 FROM LEFT. REPLACED FLOORBOARD SUPPORT NR 4 FROM LEFT AT FRAME 71-5-74-5 PER AARD 51-10-00-3 AND INSTALLED SUPPORT PER SRM 51-72-10. (M)
Part: CHANNEL — CORRODED (FRAME 72-73)
TUL - FOUND CORROSION ON J-CHANNEL BETWEEN FRAME 72 AND 73. REMOVED AND REPLACED J-CHANNEL PER SRM 51-72-10 AND ALODINED, PRIMED, PAINTED. (M)
Part: CHANNEL — CORRODED (BS 71.5-74.5)
TUL - FOUND CORROSION ON J-CHANNEL BETWEEN FRAME 72 AND 73. REPLACED FLOORBOARD SUPPORT J-CHANNEL UNDER LAV-L FROM FRAME 71.5 TO 74.5 PER AARD 51-10-00-3 AND INSTALLED SUPPORT PER SRM 51-72-10-0. (M)
Part: ANGLE — CORRODED (LT PYLON)
TUL - FOUND T-ANGLE AT TOP OF PYLON HAS CORROSION AT WEB ATTACH AREA. REPLACED ANGLE PER SRM 51-72-10. (M)
Part: EVACUATION SLIDE — DEFECTIVE (R3 DOOR)
JFK - FLT 0587 - AFTER PUSH BACK FROM THE GATE WHEN NR 2 ENGINE STARTED, SMOKE NOTED IN COCKPIT. AIRCRAFT WAS EVACUATED USING SLIDES AND DOOR 3R EMERGENCY EVACUATION SLIDE CAME OUT OF THE CONTAINER AND PARTIALLY UNFOLDED, BUT DID NOT INFLATE. REPLACED EMERGENCY EVACUATION SLIDE AT DOOR 3R. SLIDE ROUTED TO VENDOR FOR EVALUATION. FINDINGS: ENGINEERING AND NTSB INVESTIGATIONS WERE UNABLE TO ESTABLISH CAUSE FOR SLIDE NON-DEPLOYMENT DUE TO SLIDE DAMAGE SUSTAINED DURING REMOVAL FROM AIRCRAFT. (X)
Part: LIGHT STRIP — DEFECTIVE (CABIN)
JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT CROSS AISLE BETWEEN 3L AND 3R, FOUND DOORS INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT CROSS AISLE BETWEEN 2L AND 3R DOORS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1995
Part: FILTER ASSY — DEFECTIVE (TAIL SECTION)
SJU - FLT 1170 - AFTER TAKEOFF, AIRCRAFT FILLED WITH SMOKE AND HYDRAULIC ODOR. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED HIGH PRESSURE FILTER ASSEMBLY FOR THE BLUE HYDRAULIC SYSTEM AND YELLOW HYDRAULIC SYSTEM RESERVOIR PRESSURE RELIEF VALVE. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT AND BURNED OFF REMAINING ODOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)
Part: HYD RESERVOIR — DEFECTIVE (YELLOW SYS)
SDQ - FLT 1266 - AFTER T/O SDQ, SMOKE NOTED IN CABIN AND COCKPIT AND YELLOW HYD SYSTEM QUANTITY NOTED TO HAVE DECREASED. A/C RETURNED TO SDQ AND LANDED WITHOUT INCIDENT, CHECKED WHEEL WELLS FOR HYDRAULIC LEAKS W/NO DEFECTS FOUND. SERVICED YELLOW HYD SYSTEM AND ACCOMPLISHED GROUND ENG RUN WITH NO DEFECTS FOUND. A/C REDEPARTED AND SMOKE AGAIN NOTED IN CABIN AND COCKPIT, BUT NO HYDRAULIC QUANTITY DECREASE. AIRCRAFT RETURNED SDQ AND LANDED WITHOUT INCIDENT. REPLACED YELLOW HYDRAULIC SYSTEM RESERVOIR, REPLACED SMOKE DETECTOR IN LOWER AVIONICS COMPARTMENT AND REPLACED COALESCER BAGS ON BOTH AIR CYCLE MACHINES. AIRCRAFT FUNCTIONAL CHECK FLT AND MX FERRY SDQ/MIA WITH NO DEFECTS FOUND. SYS OPS CHECKED NORMAL. (M)
Part: EEL CONDUCTOR — DEFECTIVE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 12H TO 15H INOPERATIVE. REPLACED FLAT CONDUCTOR WIRE BY PASSENGER SEAT ROW 12H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL WIRE — BROKEN (CABIN)
JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT 4L/4R CROSS AISLE INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED EMERGENCY FLOOR LIGHTS AT 4L/4R CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)