N661FE

Service difficulty reports · 318

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 = 'N661FE' 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 08FDEA01469Shear Web · crackedMAIN DECK CARGO DOOR RIGHT SIDE SHEAR WEB IS CRACKED BETWEEN FRAME 76 AND FRAME 77. REMOVED WEB IAW SRM 51-40-21. FABRICATED WEB IAW SRM 51-26-00 & MARKED IAW GMM 7-0-1001. HEAT TREATED IAW TPS 1003, REV A. ALODINED; PRIMED & PAINTED IAW SRM 51-21-10; Apr 22, 2008 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA01466Wire Harness · chafedRIGHT WING ABOVE THE NR 2 ENGINE PYLON INSIDE THE WING FIXED L/E; A WIRE BUNDLE HAS SEVERAL WIRES WITH THE INSULATION CHAFED THROUGH EXPOSING INDIVIDUAL WIRES. PREVIOUS REPAIR IS CHAFED THROUGH & TORN. INSTALLED A PROTECTIVE SLEEVE ON THE WIRES REF ESPM 20-5Apr 21, 2008 · N661FE · Airbus A300F4605R · Wing System WiringSDR 08FDEA01465Shear Plate · crackedTHE SHEAR PLATE IS CRACKED AT FR 79, STRINGER 16R - STRINGER 17R. REMOVED AND REPLACED THE SHEAR WEB IAW A300-600 SRM 51-40-21; PARAGRAPH 7.Apr 21, 2008 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 07FDEA05093Proximity Sensor · failedAFTER T/O GEAR WOULD NOT RETRACT. SELECTED SYSTEM NR 2 STILL NO RETRACTION. HANDLE WOULD NOT GO PAST NEUTRAL POSITION. JACKED A/C REF A300-600 M/M 07-11-00-0, PERFORMED GEAR SWING AND RETRACTION REF 32-30-00-6. FOUND FAULT ON PROX BOX. REMOVED AND REPLACEDec 18, 2007 · N661FE · Airbus A300F4605R · Landing Gear Position and WarningSDR 07FDEA04796Oil System · leakingDURING TAXI OUT MAIN DECK CARGO SMOKE DETECTOR "B" LOOP INDICATED SMOKE. ECAM INDICATED SMOKE IN AFT COMPARTMENT. STOPPED AIRCRAFT AND COMPLIED WITH ECAM. WARNING EXTINGUISHED WHEN NR 2 PACK VALVE TURNED OFF. RETURNED TO GATE. MAIN DECK CARGO DETECTOR AFTNov 15, 2007 · N661FE · Airbus A300F4605R · APU Oil SystemSDR 07FDEA04559Rib · crackedDURING COMPLIANCE WITH EO NR 6-5750-7-5000 P2, RIB 7 FLANGE WAS FOUND TO BE CRACKED COMPLIANCE WITH EO NR 6-5750-7-5000 P4. REPLACEMENT OF DAMAGED RIB 7.Oct 10, 2007 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 07FDEA04558Rib · crackedDURING COMPLIANCE WITH EO NR 6-5750-7-5000 P2, RT INBD FLAP RIB 25 WAS FOUND TO BE CRACKED IN UPPER RADIUS REPLACEMENT OF DAMAGED PART.Oct 10, 2007 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 07FDEA04557Rib · crackedDURING COMPLIANCE WITH EO NR 6-5750-7-5000 P2, RT INBD FLAP RIB 25 WAS FOUND TO BE CRACKED IN UPPER RADIUS REPLACEMENT OF DAMAGED PART.Oct 10, 2007 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 07FDEA04555Rib · crackedDURING COMPLIANCE WITH EO NR 6-5750-7-5000 P1, LT INBOARD FLAP RIB NR 25 WAS FOUND TO BE CRACKED. REPLACEMENT OF DAMAGED RIB NR 25.Oct 10, 2007 · N661FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR 06FDEA2553Unknown · unknownF/O'S ND AND PFD FAILED MOMENTARILY AT BEGINNING OF TAKEOFF ROLL- REJECTED TAKEOFF RETURNED FOR IMMEDIATE TAKEOFF WITH ALL SYSTEMS NORMAL. A/C DID NOT RETURN TO GATE MEM (FAULT CLEARED). NO HISTORY. 12JUL06 DEN R FLT CREW REPORTED FAILED LESS THEN 3 SEC'S,Jul 12, 2006 · N661FE · Airbus A300F4605R · Standard Practices/StructuresSDR 04FDEA02344Damper · failedAFTER TAKEOFF, GEAR WOULD NOT RETRACT, RETURNED. REMOVED AND REPLACED LT LANDING GEAR PITCH DAMPER REF MM 32-11-15-4 RII:233985, ENT BY: 274911 RPT BY: 274911, R/I 02AUG04 04:39 IAH R, FACT 02AUG04 10:38 IAH U GEAR SWING REQUIRED, JACKED A/C FOR GEAR SWING Aug 2, 2004 · N661FE · Airbus A300* · Landing Gear Retraction/Extension SystemSDR 04FDEA00771Proximity Sensor · failedON TAKEOFF AT BDL GEAR WOULD NOT RETRACT, COMPLIED WITH ECAM AND QRH PROCEDURES RETURNED TO KBDL UNEVENTFULL APPROACH AND LANDING. PERFORMED BITE CHECK ON PROX BOX PER TSM 32-61-00, FOUND BOX FAULT LIGHT ON. SENSORS ALL CHECK GOOD. CHECKED BOOGIE PITCH DAMPMar 30, 2004 · N661FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 04FDEA00314Proximity Sensor · malfunctionedCOULD NOT RAISE HANDLE GEAR LEVER. NO LANDING GEAR RETRACTION. PERFORM ECAM PROC 2ND ATTEMP NR 2 SYSTEM TO RAISE GEAR FAILED. AFTER FURTHER T/S REPLACED PROX DETECTION UNIT PER AMM 32-31-71-4. ALSO REPLACED LANDING GEAR MICRO SWITCH PER AMM 32-31-11-4. PEFeb 5, 2004 · N661FE · Airbus A300B4605R · Landing Gear Position and WarningSDR 03FDEA01830Crossbeam · crackedCROSSBEAM AT FR29 HAS 1 INCH CRACK BETWEEN RT SEAT TRACKS R1 & R2. REPAIRED CROSSBEAM AS PER A300-600 SRM 53-10-15 FIG 206.Oct 29, 2003 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 03FDEA00328Structure · vibrationON TAKE OFF, A LOUD THUMP WAS HEARD AND THE AC PULLED LT. GEAR WAS LEFT DOWN & RETURN TO LAND. ON LAND EVERYTHING SEEMED NORMAL AIRCRAFT STEERED STRAIGHT AND WITH NO PULL. NO VIBRATION OF ANY SORT. NO TIRES BLOWN. AC IN WORK FOR FUTHER TROUBLESHOOTING Mar 14, 2003 · N661FE · Airbus A300B4605R · Fuselage Main, StructureSDR 02FDEA00700Hmu · faultyNR 2 ENGINE FF 2500-5000 LB FLUCTUATION- ON CLIMB OUT, NOTICED FLUCTUATING FUEL FLOW EFFECTING A SPIKE IN N1 (5-10 PERCENT) EGT TEMP VARY 3-5 DEGREES ALONG WITH A SLIGHT N2 SPIKE (2 PERCENT) NOTIFIED MECHANIC, RETURNED TO LANDING RWY 36R. TAXI IN, INSTRUMESep 27, 2002 · N661FE · Airbus A300F4605R · Fuel Controlling SystemSDR 02FDEA00095Switch · faultyDURING CLIMB 7,000 FT RIGHT FWD CABIN DOOR NOT CLOSED WARNING ILLUM. REMOVED AND REPLACED DOOR WARNING SWITCH 8WS.Feb 8, 2002 · N661FE · Airbus A300F4605R · Door Warning SystemSDR 00FDEA00005Engine · malfunctioned00-5 - NR 2 ENGINE COMPRESSOR STALLED AFT CLIMB PWR SEL FOLLOW FLEX PWR T/O ON A NON PROFILE T/O. ENG RETARD TO IDLE AND NO FURTHER ADVERSE CONDITION NOTED. AC LAND WITH NR 2 IDLE, ENG SHUTDOWN AFT LAND.Jan 4, 2000 · N661FE · Airbus A300F4605R · Engine (Turbine/Turboprop)
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