N663FE

Service difficulty reports · 264

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N663FE' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 05FDEA00989Computer · malfunctionedON TAKEOFF, AFTER TOGA, ENGINES STABLE AT APPROX 98 PERCENT N1 PASSING 60 KTS: ECAM SINGLE CHIMED WITH "ENGINE 1 SHUTDOWN PROCEDURE". RTO COMPLIED WITH. ALL ENGINE ANALOG INDICATIONS WERE NORMAL. REMOVED AND REPLACED NR 1 FWC PER 31-53-34-4. OPS NORMALApr 13, 2005 · N663FE · Airbus A300F4605R · Central WarningSDR 04FDEA02557Seat Track · corrodedMAIN DECK SEAT TRACK L3 AT FRAME 38 HAS A SCREW HOLE ON FLANGE TORN OUT. REMOVED DAMAGED SEAT TRACK IAW A300-600 FREIGHTER SRM 53-10-16 FIG 201, INSTALLED NEW SEAT TRACK IAW A300-600 FREIGHTER SRM 53-10-16, FIG 201.Aug 24, 2004 · N663FE · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02542Seat Track · corrodedN00468 MAIN CABIN SEAT TRACK CORRODED FROM FR47 TO 50, TRACK 3R. REPAIRED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16.Aug 21, 2004 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02541Seat Track · corrodedN00466 MAIN CABIN SEAT TRACK (0) AT APPROX FRAME 78 HAS CORROSION ON TOP OF LUGS AND IN BOTTOM OF SCALLOPS. REMOVED CORROSION ON MAIN CARGO TRACK (0) FR 78 IAW SRM 51-74-10. MATERIAL LOSS WAS 0.050 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 PG 105. REPAAug 21, 2004 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02540Cargo Track · corrodedN00509 MDCC SIDE TRACK AT FR 37 BETWEEN R1 AND R2 HAS LEVEL 1 CORROSION APPROX. 1 INCH. REMOVED AND REPLACED SIDE TRACK ADAPTER TRACK IAW A300 SRM 51-40-20.Aug 21, 2004 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02539Cargo Track · corrodedMDCC SIDE TRACK AT FR 35 BETWEEN R1 AND R2 HAS LEVEL 1 CORROSION APPROX 1 INCH. REMOVED AND REPLACED SIDE TRACK IAW SRM 51-40-21Aug 21, 2004 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA01869Fitting · leakingIN LEVEL FLT, CRUISE AT FL310, GREEN HYD SYS LOW LEVEL OCCURRED. BOTH OVERHEAD QTY AND ECAM INDICATED RED DOT. QRH ACTIONS DIRECTED MANUAL LANDING GEAR EXTENSION. NORMAL LANDING. GEAR PINNED FOR TOW-IN AFTER LANDING. GREEN PUMPS TURNED OFF AT 3250 PSI. Jun 28, 2004 · N663FE · Airbus A300F4605R · Hydraulic System, MainSDR 04FDEA01866Fitting · leakingIN LEVEL FLIGHT, CRUISE AT FL310, GREEN HYD SYS LOW LEVEL OCCURRED. BOTH OVERHEAD QTY AND ECAM INDICATED RED DOT. QRH ACTIONS DIRECTED MANUAL LANDING GEAR EXTENSION. NORMAL LANDING. GEAR PINNED FOR TOW-IN AFTER LANDING. GREEN PUMPS TURNED OFF AT 3250 PSIJun 27, 2004 · N663FE · Airbus A300B4605R · Hydraulic System, MainSDR 04FDEA00298Switch · malfunctionedREJECTED TAKEOFF AT 50 KNOTS FOR SPOILER FAULTS 3 & 2, 5 ON ECAM. REMOVED AND REPLACED YELLOW SYS SERVO PRESSURE SWITCH PER A300 MM 27-14-18-4, OPS CHECK GOOD OK FOR SERVICE.Feb 3, 2004 · N663FE · Airbus A300F4605R · Drag Control SystemSDR 01FDEA00137Detector · malfunctionedON T/O ROLL, ABORTED FOR AVIONICS SMOKE ECAM. RAN CK LIST AND NO SMOKE DETECTED ON SNIFFER. REMOVED AND REPLACED SMOKE DET PER IAW A300-600 MM 26-15-12-4. SYS OPS CK GOOD.Feb 16, 2001 · N663FE · Airbus A300F4605R · Smoke DetectionSDR 00FDEA00725Thrust Reverser · activatedDURING CLIMBOUT, NR 2 ENG THRUST REVERSER PRESSURIZED, NO ADVERSE YAW NOTED. DEFERRED PER MEL/CDL.Oct 19, 2000 · N663FE · Airbus A300F4605R · Engine Thrust ReverserSDR 98FDEA00761Switch · failed98-308 - ECAM WARNING FOR NR 1 T/R PRESSURIZED ANNUNCIATED, NO REV OR REV UNLOCK LIGHTS ILLUM. ABORT TAKEOFF. REMOVED AND REPLACED DIRECTIONAL PILOT VALVE/PRESS SWITCH PER MM 78-31-06-2. RAN ENG NO FAULTS FND.Dec 23, 1998 · N663FE · Airbus A300F4605R · Engine Thrust ReverserSDR 98FDEA00758Connector · dirty98-306 NR 1 ENG REVERSER PRESS ECAM WARN ILLUM AT T/O ROLL. ABORT T/O CYCLED REVERSER LEVER. LIGHT ECAM REILLUM ON 2ND T/O ATTEMPT. ABORT AGAIN AND RETURN TO RAMP. CLEANED CANNON PLUG ON DIRECTIONAL PILOT VALVE AND SWITCH. HEATED VALVE AT NR 1 ENGINE. RDec 23, 1998 · N663FE · Airbus A300F4605R · Engine Thrust ReverserSDR 97FDEA00239Tr Unit · malfunctionECAM ANNUNCIATED NR 2 ENG REVERSER PRESSURIZED. REMOVED AND REPLACED NR 2 RT CDU PER M/M 78-31-01-4 PG 401-515. REMOVED AND REPLACED NR 2 PILOT DIRECTIONAL CONTROL VALVE PER M/M 78-31-0602, ALL OPS CK GOOD. REMOVED NR 2 MAIN OIL TANK TO FACILITATE REPLACINGApr 22, 1997 · N663FE · Airbus A300* · Engine Thrust Reverser
Back to N663FE