N335JS
Registered owner: AMERICAN AIRLINES INC, TX (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.
11 reports on file, 1995-02-13 – 2025-03-16.
Part: SENSOR — FAILED (MAU2- MOD NOSE W) · airframe 24,354 hrs · 16,743 cycles
STEERING FAIL ON APPROACH WHEN GEAR LOCKED DOWN. EMERGENCY DECLARED TOWED IN. "TRANSFERRED FROM AML PAGE 110600387 - ITEM 1" REFERENCE ITEM 2 AND 3 THIS NRWC FOR THE RAR OF THE NWSCM AND THE STEERING FEEDBACK SENSOR 1. THEN THE STEERING SYSTEM OPC GOOD IAW AMM 32-52-00-710=801
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,815 hrs · 16,394 cycles
FORWARD GALLEY RH SEAT TRACK FLOOR BEAM BETWEEN FRAME 13-14 GALLEY FLOOR BOLT HOLE IS CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION) PERFORMED PERMANENT REPAIR TO FORWARD GALLEY RH SEAT TRACK FLOOR BEAM BETWEEN FRAME 13-14 GALLEY FLOOR BOLT HOLE IAW ERS-EJ-53MR-5111
Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,815 hrs · 16,394 cycles
SSI 53-10-027 FWD GALLEY CROSSBEAM AT FR 16 INBD OF LH FLOOR SILL AFT END IS CORRODED (MAJOR REPAIR) (LEVEL 2 CORROSION) ACCOMPLISHED REPAIR ON FWD GALLEY CROSSBEAM AFT END AT FR16 INBD OF LH FLOOR SILL IAW ERS-EJ-53MR-5110
Part: DOUBLER — CORRODED (ZONE 800) · corrosion level 2 · airframe 23,815 hrs · 16,394 cycles
LH FLOOR DOUBLER CORRODED AT FR 16. (LEVEL 2 CORROSION) REMOVED AND REPLACED LH FLOOR DOUBLER AT FR 16 IAW EMB 175 SRM 51-40-08..
Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,815 hrs · 16,394 cycles
AFT GALLEY FLOOR RH SHEAR PANEL LOCATED BETWEEN FR 87 AND 88 IS CORRODED. (LEVEL 2 CORROSION) REMOVED AND REPLACED AFT GALLEY FLOOR RH SHEAR PANEL BETWEEN FR 87 AND 88 IAW EMB 175 SRM 51-40-08.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,815 hrs · 16,394 cycles
FORWARD GALLEY RH SEAT TRACK FLOOR BEAM BETWEEN FRAME 13-14 GALLEY FLOOR BOLT HOLE IS CORRODED. (LEVEL 2 CORROSION) (MAJOR REPAIR). COMPLETE:PERFORMED PERMANENT REPAIR TO FORWARD GALLEY RH SEAT TRACK FLOOR BEAM BETWEEN FRAME 13-14 GALLEY FLOOR BOLT HOLE IAW ERS-EJ-53MR-5111
Part: SENSOR — FAILED (NR 1 SLAT) · airframe 23,571 hrs · 16,210 cycles
SLAT FAIL DURING CRUISE EMERGENCY DECLARED. REMOVED AND REPLACED LH INBOARD SLAT SKEW SENSORS FOR TRACKS #1 AND #3 AND RH INBOARD SLAT SKEW SENSOR #3 IAW EMB 175 AMM 27-83-02. OPERATIONAL CHECK GOOD.
Part: SENSOR — FAILED (ZONE 600 SLAT) · airframe 23,551 hrs · 16,192 cycles
SLAT FAIL ON DESCENT EMERGENCY DECLARED FOUND FAULT CODE 27833017ACE TRAK 1 R/H IB SKEW CH2. RAR R/H INBD SKEW SENSOR PER AMM 27-83-02 AND OPS CHECKED PER AMM 27-80-00 OPS CHECK GOOD. NO ACTIVE FAULTS
Part: AHRS COMPUTER — MALFUNCTION (AVIONICS COMP)
PIT - FLT 4162 - DURING CLIMB-OUT PHASE OF FLIGHT, CAPTAIN NOTICED A DISCREPANCY IN HEADING INDICATION. AIRCRAFT RETURNED TO PIT GATE, WHERE MAINTENANCE RE-RACKED AND INITIALIZED BOTH NR 1 AND NR 2 AHRS COMPUTERS IAW MM 34-21-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE.
Part: ACCUMULATOR — DEFECTIVE (HYD SYST)
FLT 4262 - CREW NOTED ON TAKEOFF, LANDING GEAR TOOK 45 SECONDS TO FULLY RETRACT. AIRCRAFT WAS FERRIED TO CAK WHERE MAINTENANCE REPLACED LANDING GEAR SYSTEM ACCUMULATOR - 32-50-00. CONDUCTED GEAR SWING, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: OIL PRESS TRANS — DEFECTIVE (RT ENGINE)
FLT 4262 - AFTER TAKEOFF, CREW RECEIVED LOW OIL PRESSURE WARNING, BOTH AURAL AND VISUAL NR 2 ENGINE. AIRCRAFT RETURNED TO GATE, OUTSIDE MAINTENANCE INSPECTED NR 2 ENGINE, SERVICED OIL LEVEL. AIRCRAFT WAS FERRIED TO CAK WHERE MAINTENANCE REPLACED OIL PRESSURE TRANSMITTER, GROUND RUNS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.