N655FE

Service difficulty reports · 219

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 = 'N655FE' 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 04FDEA00284Target · wornPASSING 1500 FT ON DEPARTURE. AFT CARGO DOOR WARNING PRESENTED ON ECAM. NO PRESSURIZATION ABNORMALITY NOTED. RAN ECAM/QRH PROCEDURE. RETURNED TO JFK. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 11FEB04 MEL 52-71-01: AFT CARGO Feb 2, 2004 · N655FE · Airbus A300F4605R · Door Warning SystemSDR 04FDEA00094Switch · damagedAIR TURNBACK AFT CARGO DOOR ILLUMINATED AT 1000 ON TAKEOFF. RETURNED TO MEM AND LANDED, NO PRESSURIZATION. RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 20JAN04. REMOVED AND REPLACED AFT CARGO DOOR WARNING SWITCH 34WS IAW M/M 52-71-11-4Jan 10, 2004 · N655FE · Airbus A300F4605R · Door Warning SystemSDR 03FDEA01740Cooling Fan · failedON BLOCKOUT BETWEEN STARTING NR 1 AND NR 2 ENGINES SMOKE STARTED COMING IN TO THE COCKPIT FROM THE EQUIPMENT BAY. PERFORMED VISUAL INSPECTION OF AVIONICS COMPARTMENT, CHECKED ALL BOXES FOR EVIDENCE OF ODOR, REMOVED RELAY PANEL COVERS LOOKING FOR EVIDENCE OF Oct 15, 2003 · N655FE · Airbus A300B4605R · Air Distribution FanSDR 03FDEA00948Intercostal · crackedTHE INTERCOSTAL IS CRACKED AND DEFORMED BETWEEN FRAME 85 AND 86 AT STR 33R IN THIS COMPARTMENT. REPAIRED BY REPLACING CRACKED INTERCOSTAL FLANGE IAW A300-600 SRM 51-40-20 WORK DOCUMENTED ON M-1805 N00242.Jun 21, 2003 · N655FE · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR 03FDEA00947Skin · delaminatedNR 1 ENGINE RT TRANSLATING COWL IS DELAMINATED, FWD UPPER CORNER AT THE 2 O'CLOCK POSITION OF THE INNER BARREL 2 X 4 INCHES. REPAIRED BY T/R REPLACEMENT PER EA 6-7830-66985 WORK DOCUMENTED ON M-1805, S00029.Jun 21, 2003 · N655FE · Airbus A300F4605R · Nacelle/Pylon, Plate/SkinSDR 03FDEA00946Crossbeam · crackedAFT CARGO CROSSBEAM AT FRAME 59 IS CRACKED APPROX 1 INCH, 4 INCHES RIGHT OF CENTER. REAIRED CROSSBEAM IAW A300-600 SRM 53-10-15 BY CUTTING AND SPLICING IN A NEW SECTION OF BEAM. WORK DOCUMENTED ON M-1805 NR N00080Jun 21, 2003 · N655FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 03FDEA00944Intercostal · damagedTHE INTERCOSTAL IS DAMAGED AND DEFORMED BETWEEN FRAME 86 AND 87 AT STR 40R. REMOVED DEFORMED SUPPORT ANGLE AND FABRICATED NEW SUPPORT ANGLE AND INSTALLED IAW A300-600 SRM 51-40-20. WORK DOCUMENTED ON M-1805 NR N00245Jun 21, 2003 · N655FE · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR 03FDEA00912Floorbeam · crackedFWD CARGO FLOORBEAM (27) RIGHT SIDE 24 INCHES FROM CENTERLINE HAS CRACK IN UPPER SECTION. REPAIRED FLOORBEAM (27) IAW A300-600 SRM 53-10-15.Jun 19, 2003 · N655FE · Airbus A300B4605R · Fuselage Main, Floor BeamSDR 03FDEA00913Floorbeam · crackedFWD CARGO -CROSS BEAM AT FRAME 28 IS CRACKED APPROX 1 INCH LONG 18 INCHES RIGHT OF CENTER. REPAIRED IAW SRM 53-10-15 FIGURE 208 SHEET 3.Jun 19, 2003 · N655FE · Airbus A300B4605R · Fuselage Main, Floor BeamSDR 03FDEA00915Floorbeam · crackedFWD CARGO CROSS BEAM AT FRAME (30) IS CRACKED APPROX 1.5 INCH LONG, 18 INCHES RIGHT OF CENTER. REPAIRED IAW SRM 53-10-15 FIGURE 208 SHEET 2.Jun 19, 2003 · N655FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 03FDEA00887Skin · dentedON WALKAROUND UPON A/C ARRIVAL FOUND DENT ON LT HORIZONTAL STABILIZER LEADING EDGE LOWER SURFACE. THIS WILL BE C/W IN C-CHECK. FOUND DENT TO BE IN V-SHAPE 4 X 3 X .0265 INCH DEEP. LOCATION IS 5FT FROM WING TIP, APPROX STA 750 LOWER LEADING EDGE. C/W EA 6-5Jun 16, 2003 · N655FE · Airbus A300B4605R · Horizontal Stabilizer, Plate/SkinSDR 03FDEA00119Thrust Reverser · deployedNR 2 ENGINE THRUST REVERSER PRESSURIZED ON TAKEOFF ROLL, REJECTED TAKEOFF AT 70KTS. WHILE DEACTIVATING THE NR 2 ENGINE THRUST REVERSER, WE WERE UNABLE TO LOCK OUT THE SLEEVE DUE TO THE HOLE NOT LINEING UP TO INSTALL BOLTS. DIRECTIONAL PILOT VALVE HAS BFeb 12, 2003 · N655FE · Airbus A300F4605R · Engine Thrust ReverserSDR 02FDEA00982Anti-Ice Valve · failedEN ROUTE, DESTINATION ICING CONDITIONS EXISTED. NR 1 ENGINE NACELLE ANTI-ICE VALVE FAILED TO OPEN WHEN SELECTED. RELEASED FOR SERVICE IAW MEL/CDL. NR 1 ANTI-ICE INOPERATIVE ENGINE NACELLE. VALVES SECURED OPEN. REMOVED AND REPLACED NR 1 ENGINE NACELLE ANTDec 31, 2002 · N655FE · Airbus A300F4605R · Air Intake Anti/De-Ice SystemSDR 02FDEA00348Connector · contaminatedON TAKEOFF ECAM WARN NR 1 REVERSER PRESS FOLLOWED ECAM INSTRUCTIONS TO BRING NR 1 THROTTLE TO IDLE. FOUND CANNON PLUG GOING TO DIRECTIONAL PILOT VALVE WITH MOISTURE. CLEANED PLUG AND RAN NR 1 ENG. OK FOR SERVICE.May 17, 2002 · N655FE · Airbus A300F4605R · Engine Thrust ReverserSDR 01FDEA00302Landing Gear · malfunctionedON FINAL APPR NOSE GEAR DID NOT SHOW DOWN ON SYS 1 & 2, SYS 3 IND GEAR DOWN. AFT GO AROUND GEAR RECYCLED AND ALL ID WERE GREEN.Apr 25, 2001 · N655FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 00FDEA00087Fire Detector · malfunctionedMAIN CARGO LOOP DETECTION FAULT ILLUM ON ECAM. TEST MAIN CARGO DECK SMOKE DETECTION SYSTEM PER AMM 26-19-00-5. OPS CK GOOD. SUSPECT FAULT CAME FROM DRY ICE SHIPMENT ON CARGO DECK.Feb 17, 2000 · N655FE · Airbus A300F4605R · Fire DetectionSDR 98FDEA00515Switch · dirtyREJECTED T/O ATL DUE TO AFT CARGO DOOR WARN. TAXI BACK FOR VISUAL. CK GOOD LIGHT OUT, CAME ON AGAIN DURING LAND IN MEM. CLEAN SWITCH 32WS AND INSP SWITCH 34WS, SWITCH CKS GOOD. CARGO DOOR IND GOOD. PRESS ACFT WITH NO DOOR IND PROBLEM.Aug 16, 1998 · N655FE · Airbus A300* · Door Warning SystemSDR 98FDEA00419Controller · malfunctionCABIN PRESSURE CONTROLLER NR 2 FAULTED AFTER T/O. UNABLE TO CONTROL IN MANUAL. REMOVED AND REPLACED FWD OUTFLOW VALVE.Jun 28, 1998 · N655FE · Airbus A300* · Cabin Pressure ControllerSDR 97FDEA00154Wire · failedCLEARING RUNWAY AFTER LANDING, NR 2 GEN DROPPED OFF AT 90 KNOTS ON RUNWAY AND FWC ECAM APPEARED. STARTED APU AND IT TOOK GEN NR 1 OFF LINE AS WELL. *S/D* FOUND SEVERAL MELTED WIRES IN GEN 2 AND EXT POWER BAYS AND STRUCTURAL DAMAGE REQUIRING S/M REPAIR. STRMar 12, 1997 · N655FE · Airbus A300B21A · Electrical Power System Wiring
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