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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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; SDR 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 20-5SDR 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.SDR 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 REPLACESDR 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 AFTSDR 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.SDR 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.SDR 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.SDR 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.SDR 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,SDR 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 SDR 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 DAMPSDR 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. PESDR 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.SDR 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 SDR 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, INSTRUMESDR 02FDEA00095Switch · faultyDURING CLIMB 7,000 FT RIGHT FWD CABIN DOOR NOT CLOSED WARNING ILLUM. REMOVED AND REPLACED DOOR WARNING SWITCH 8WS.SDR 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.
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