N659FE

Service difficulty reports · 213

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 = 'N659FE' 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 04FDEA02561Hydraulic System · malfunctionedREJECTED T/O AT APPROXIMATLEY 80 KIAS STANDARD POWER SET AT 109 N1 ON BOTH ENGINES. ECAM WARNING OF LOW HYDRAULIC PRESSURE ON NR 2 PUMP. RETURNED TO RAMP FOR INSPECTION. INSPECTED ALL AIRCRAFT EXTERIOR FOR OBVIOUS LEAKS, NONE FOUND. SUSPECT RIGHT HAND SIDEAug 25, 2004 · N659FE · Airbus A300B4605R · Hydraulic System, MainSDR 04FDEA02559O-Ring · tornAT 100 NM FROM GDL, LOST GREEN HYDRAULIC SYSTEM, GRAVITY GEAR EXTENSION AND LANDING NORMAL. PUMPS OFF AT 2300 PSI. FOUND EVIDENCE OF LEAKAGE ON ENGINE NR 1 PYLON. AFTER CLEANANCE AND INSPECTION FOUND GREEN PRESSURE SW LEAKING HYD DUE TO O-RING FAILURE, REPAug 24, 2004 · N659FE · Airbus A300B4605R · Hydraulic System, MainSDR 04FDEA02361Fire Loop · malfunctionedON CLIMBOUT PASSING APPROX 3,000 FT MSL RECEIVED ECAM ALERT FOR B-LOOP FAULT ON NR 1 ENGINE. CONTINUED CLIMB TO 11,000 MSL AND SLOWED A/C TO TROUBLESHOOT, DURING CLIMB FAULT LIGHT FLICKERED A COUPLE OF TIMES AND THEN REMAINED STEADY. ACCOMPLISHED ECAM PROC, Aug 4, 2004 · N659FE · Airbus A300F4605R · Fire DetectionSDR 03FDEA01913Connector · looseDURING CLIMB NR 1 ENG ANTI-ICE FAULT LIGHT ON / ECAM IND FAULT. DEPART ICING WX IN 30 SEC, SHUT OFF ENG A/I, FAULT LIGHT OUT. A/I VALVE DEACT'D, LOCKED OPEN FOR TROUBLESHOOTING. OPENED ENG FAN & REV COWLS FOR T/S. CW HARNESS SHAKE TEST AT CONNECTOR DV220,Nov 11, 2003 · N659FE · Airbus A300F4605R · Air Intake Anti/De-Ice SystemSDR 03FDEA01124Seat Track · wornDURING OFFLOAD, HUB ADVISED BROKEN YZ LATCH LOCK IN POS 11RT. CLOSE INSP NOTED SEAT TRACK DAMAGED. REPLACED LATCH IAW A300-600 AMM 25-58-00 AND SEAT TRACK ADAPTER REPLACED IAW EA 6-5310-71945 PT 2.Jul 22, 2003 · N659FE · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR 03FDEA01122Frame · damagedTEMPORARY REPAIR ON FRAME20A. PERMANENT REPAIR INSTALLED IAW EA 6-5310-60187 A AND DWG SR30-53-001.Jul 21, 2003 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR 03FDEA01097Floorbeam · crackedFLOORBEAM CRACKED ON BEAM 27 FWD LOWER CARGO PIT 17 INCHES OF CENTRLINE. REPAIRED FLOORBEAM IAW A300-600 IAW ENG DISPO PAGE 2 AND 3. FAB 2 EA ANGLES IAW SRM 53-10-15,HFEC INSPECT IAW SRM 51-10-08. PENETRANT INSPECTION IAW SRM 51-90-00,PART ID PMS 01-06-08.Jul 14, 2003 · N659FE · Airbus A300B4605R · Fuselage Main, Floor BeamSDR 03FDEA01056Seat Track · damagedMAIN CARGO COMPT FLOOR SEAT TRACK DAMAGED A 6 INCH CRACK IN SEAT TRACK ADAPTER AT 12R, FR 59 AND Y1456. REMOVED AND REPLACED SEAT TRACK ADAPTER IAW EA. (6-2550-71920) REV PT 2.Jul 7, 2003 · N659FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 02FDEA00575Uplock · brokenNOSE LANDING GEAR UNSAFE INDICATIONS ON TAKEOFF. DECLARED EMERGENCY RETURN TO KMEM. FOUND THE RIGHT NLG DOOR UPLOCK HOOK BROKEN. REMOVED AND REPLACED NLG DOOR UPLOCK ASSY, LEAK CK C/W. OP CHECKS NORMAL.Aug 12, 2002 · N659FE · Airbus A300F4605R · Landing Gear Door Retract SectionSDR 00FDEA00876Thrust Reverser · inoperative00-357 ON TO ROLL NR 1 ENGINE THRUST REVERSER PRESSURIZED. ECAM ALERT CAME ON. AC RELEASE FOR MEL 78-1.Dec 14, 2000 · N659FE · Airbus A300F4605R · Engine Thrust ReverserSDR 00FDEA00663Landing Gear · lack of lubeLOWERED GEAR AND MLG UNSAFE IND (SYS 2) ON BOTH FWD AND OVHD PNLS AND ECAM WARNING. LUBRICATED BOTH MLG IAW MM 12-22-32-0 LOC PG 9 VIEW C & PG 10 VIEW G. OK FOR SERVICE.Sep 15, 2000 · N659FE · Airbus A300F4605R · Landing Gear SystemSDR 99FDEA00100Proximity Switch · malfunctionedON T/O, ROTATION FELT VIBRATION IN YOKE. GEAR HANDLE UP BUT GEAR DID NOT RETRACT. ECAM L/G WOULD NOT RET, AT DROPPED OFF AND WOULD NOT RESET. GPWS FAULT LIGHT ON. REMOVED AND REPLACED PROXIMITY DETECTOR UNIT PER MM 32-31-71-4 PG 401. NO FAULTS ON BITE.Mar 11, 1999 · N659FE · Airbus A300F4605R · Landing Gear Position and WarningSDR 97FDEA00873Fire Det Contl · failed97-024 - STA-IND - T/O AT FL 310, NR 1 FIRE LT ILLUMINATED BOTTLES WERE BLOWN, LT REMAINED ON, DIVERTED TO IND AND LANDED UNEVENTFULLY. OPEN UP NR 1 ENG AND INSP FOR FIRE OR OVERHEAT CONDITION. ENG APPEAR NORMAL WITH AIRDUCTS TIGHT AND INTACT. REMOVED AND RDec 2, 1997 · N659FE · Airbus A300F4605R · Fire Detection
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