N304FE
Service difficulty reports · 283
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 = 'N304FE' 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 = 'N304FE' 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 05FDEA00248Hinge · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE CORRODED. REMOVED CORROSION, FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED BUSHING TO FINAL INSIDE DIAMETER OF 0.8745-0.8755 IAW DAC CMM 57-52-02 AND FEDEX EA 8-5710-83967, PRIMED BORE IAW DC10-3SDR 05FDEA00247Hinge · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION, FABRICATED, INSTALLED AND HONED BUSHING TO FINAL DIAMETER OF .8745 - .8755 INCHES IAW DAC CMM 57-52-02, PRIMED BORE IAW DC10-30 SRM 51-21-01 VOL II, AND FESDR 05FDEA00246Life Vest · brokenBOTH COURIER SEATS LIFE VEST POUCH RETAINING STRAPS MISSING/BROKEN. ACCOMPLISHED FEDEX EA 8-2560-83856, EQUIPMENT/FURNISHING- COURIER SEAT LIFE VEST POUCH RETAINING STRAP-REPAIR.SDR 04FDEA00477Seal · failedCLIMBOUT AT APPROXIMATELY FL 210, AIRCRAFT ALTITUDE WAS CLIMBING AT 1000 FPM. SECOND PACK BROUGHT ON LINE AND CABIN STILL CLIMBING AT 500 FPM, LEVELED AT FL 330. UNABLE TO STOP CABIN ALTITUDE FROM INCREASING TOWARD 10,000 FEET, RETURNED LAX AND LANDED WITHOUSDR 03FDEA01918Fuse · trippedLANDING GEAR HANDLE WOULD NOT MOVE TO LANDING GEAR POSITION. RAN RED TABS AND THAT (DEPRESS THE HANDLE RELEASE BUTTON & RAISE - ENSURE NOSE GEAR STEER CENTERED) DID NOT HELP. RETURNED FOR NORMAL LANDING. FOUND THE MAIN GEAR TRIM INTERLOCK FUSE HAD TRIPPED ISDR 03FDEA01104Bolt · looseNR 1 ENGINE EXHAUST NOZZLE HAS LOOSE AND MISSING HARDWARE AROUND THE ATTACH POINT TO CASE. CLOSING ACTION ON 06/16/03. ON N/R S00104. REPLACED LOOSE AND MISSING BOLT'S AND TORQUED IAW M/M 78-11-02-2.SDR 03FDEA00982Bushing · damagedNR S-20 COMPLY WITH EA 8-5750-70945, FOR LT INBD FLAP OUTBD HINGE SUPPORT. ON 06/24/03. RECEVIED BUSHINGS IAW MAE TRAVELERS T2/343779@T2/343901.INSTALLED BUSHINGS IAW CMM 57-52-01. COMPLIED WITH EA 8-5750-70954.SDR 03FDEA00983Hinge · damagedS 16 COMPLY WITH EA 8-5740-70941.WINGS-RT INBD FLAP HINGE ATTACH LUG REWORK. COMPLIED WITH EA 8-5740-70941.WINGS-RT INBD FLAP HINGE ASSY ATTACH REWORK.SDR 03FDEA00984Bushing · wornNR S 21 COMPLY WITH EA 8-5750-70954, FOR RT INBD FLAP OUTBD SUPPORT. RECEIVED BUSHINGS IAW MAE TRAVELERS T2/343953 @ T2/343780. INSTALLED BUSHINGS IAW CMM 57-44-09.COMPLIED WITH EA 8-5750-70954 FOR RT INBD FLAP OUTBD HINGE SUPPORT.SDR 03FDEA00985Clip · crackedN 1137 AFT FUSELAGE ZONE 312. FS 2140 AFT CANT BULKHEAD TOP FUSELAGE FRAME CLIP ANGLE SKIN ATTACHMENT SUPPORT HAS 2 INCH CRACK ON LT SIDE. REMOVED FRAME CLIP IAW SRM 51-35-01. FAB NEW CLIP ON MAE TRAVLER T2/343533. INSTALLED NEW CLIP IAW SRM 51-35-01 AND 51SDR 03FDEA00943Bracket · gougedNR S 22 LT INBD FLAP BRACKET ASSY, GOUGED COMPLY WITH E.A.8-5750-70945. CLOSING ACTION ON 06/20/03. COMPLIED WITH E.A.8-5750-70945.WINGS-LT INBD FLAP-BRACKET ASSY GOUGE REPAIR P/N ARC2761.SDR 03FDEA00855Bolt · looseREF EO 8-5410-7-3321 ITEM A 1 AND 2 GAIN ACCESS TO NR 1 PYLON AFT BULKHEAD REAR BOLTS, 5 OF THEM FOUND LOOSE. EO 8-5410-7-3321 BOLTS WERE INSPECTED AND HOLES CHECKED BY NDT DEPT. BOLTS RETORQUED AND AREA PREP FOR CLOSING.SDR 01FDEA00347Longeron · corrodedINNER GRANULAR CORROSION DEVELOPING INSIDE LONGERON 44L APPROX 7 STA 1126 AS VIEWED INSIDE CTR ASSY COMPT BELOW WORK STEPS ON LT SIDE OF CAC ACCESS DOOR. *S/D* CLEAN AND TREATED 44L PER SRM 51-21-01. INSTALL NEW LONGERON SPLICE PER EA 8-5311-53297.SDR 01FDEA00339Fitting · crackedREF EO 8-5740-7-4312 RT MLG RETRACT CYLINDER SUPPORT FRAME HAS A CRACK IND AT FWD FLANGE FROM TOP TO RADIUS. *S/D* REMOVED AND REPLACED RT MLG RETRACT CYLINDER SUPPORT PER EO 8-5740-7-4312 PART 3.SDR 00FDEA00884Throttle · stuck00-363 PRIOR TO TOP OF DESCENT NR 1 THROTTLE BECAME STUCK AT 95 PERCENT NL. ** S/D ** R&R NR 1 ENGINE THROTTLE DRUM AND FUEL SHUTOFF SECTOR RAN ENGINE CK GOOD PER JRH.SDR 00FDEA00081Warning Light · illuminated00-46 - CAB PRESS RELIEF OPEN LIGHT ILLUMINATED. RAN RED TABS. REMOVED INSULATION MATERIAL FROM UPPER FWD POSITIVE VALVE. PERF ADJUST TEST PER DC10-30 MM 21-34-01-2, CK GOOD. OK FOR SERVICE.SDR 00FDEA00075Switch · failedALL 4 GEAR IND STAY RED ON BOTH PNLS. RAN RED TAB PROC WITH NO RESULTS. REMOVED AND REPLACED NR 3 SUBPEDESTAL THROTTLE SWITCH ASSY PER DC10 MM 76-11-04-2. OPS CHECK GOOD.SDR 00FDEA00074Prox Sensor · malfunctioned00-41 - IMMEDIATELY AFTER T/O, LG HORN SOUNDED WITH GEAR HANDLE RAISED. REMOVED AND REPLACED PROX ELECTRONIC UNIT PER MM 32-61-01-2 BOX CK GOOD.SDR 98FDEA00342Spar Cap · crackedFOUND .5 INCH CRACK IN UPPER REAR SPAR CAP OUTER SECTION SKIN PANEL (RIGHT HAND SIDE). REF: EO 8-5510-7-3310 PART 4. REPAIRED PER EA 8-5510-38504- HORIZONTAL STAB RT UPPER AFT SKIN PANEL REPAIR.SDR 98FDEA00341Bolt · looseSNRM N 00874, A/C 304, FOUND 9 EA BOLTS LOOSE AT BOTTOM OF PYLON FWD MOUNT. REMOVE, INSPECTED AND INSTALLED 9 EA BOLTS PER M/M 20-50-0212.SDR 98FDEA00230Fire Bottle · blownDURING B CHECK, FOUND NUMBER 2 LEFT ENGINE FIRE BOTTLE NUMBER 2 CARTRIDGE BLOWN DURING REMOVAL AND REPLACEMENT OF EXPIRED CARTRIDGE. REMOVED AND REPLACED NR 2 ENGINE LEFT FIRE BOTTLE AND CARTRIDGES PER M/M 26-21-02 AND M/M 26-21-01.SDR 96FDEA00998Stringer · crackedRIGHT WING STR 41 OUTBOARD HOLE HAS VERTICAL CRACK AT 2 O/C POSITION INTO UPPER STR RADIUS APPROX .3125 INCH LONG. REF: EO 8-5710-7-4310.SDR 96FDEA00975Spar Chord · shearedSNRM 4358, NR 3 PYLON UPPER LT SPAR CHORD AFT AREA EXHIBITS TWO SHEARED HOCK BOLTS HEADS INSIDE PYLON.SDR 96FDEA00974Spar Chord · shearedSNRM 4145, NR 1 PYLON UPPER SPAR WEB STA 363, 1 FASTENER HEAD HAS SHEARED OFF.SDR 96FDEA00942Flap Track · grooveSNRM 6030, RT I/B FLAP I/B TRACK VERTICAL FACE UPPER AND LWR BEARING SURFACES DAMAGED WITH GROOVES AND GOUGED METAL APPROX .020 INCHES DEEP DUE TO I/B FLAP CARRIAGE SIDE LOAD BEARING FAILURE. *S/D REMOVED AND REPLACED RT I/B FLAP TRACK PER GMM 57-52-01, ISDR 96FDEA00941Thrust Link · looseSNRM 4361, NR 3 PYLON FWD ENG MOUNT AREA LOWER THRUST LINK LT SIDE OF PYLON HORIZONTAL ROW OF .3125 BOLTS ARE LOOSE, AS VIEWED FWD LOWER LT SIDE OF PYLON AT APPROX YN222 TO 226, 3 BOLTS LOOSE. *S/D* REPLACED NUTS WITH NEW AND RETORQUED PER EO 8-5410-7-4319.SDR 96FDEA00940Thrust Link · looseSNRM 4360, NR 3 PYLON FWD ENG MOUNT, LWR THRUST LINK RT SIDE OF PYLON HAS VERTICAL ROW OF .25 BOLTS AND HORIZONTAL ROW OF .3125 IN BOLTS LOOSE, TOTAL OF 18 BOLTS LOOSE AT APPROX PYLON STA YN 222 TO 226. *S/D* REPLACED NUTS WITH NEW AND RETORQUED PER EO 8-541SDR 96FDEA00939Thrust Links · looseSNRM 4359, NR 3 PYLON FWD ENG MOUNT LOWER THRUST LINKS, 7 MOUNTING BOLTS ARE LOOSE ON PYLON BOTTOM LT AND RT SIDES APPROXIMATE PYLON STA YN 222. *S/D* RT SIDE TORQUED PER MM 20-50-02, REMOVED AND REPLACED NUTS ON BOTTOM OF FWD THRUST LINK LT AND RT AND RETORSDR 96FDEA00938Fasteners · looseSNRM 4353, NR 3 PYLON INSIDE ACCESS PANEL 488 BL PYLON FWD BULKHEAD AT STA YN 342, BOTTOM ROW OF FASTENERS ARE ALL LOOSE.SDR 96FDEA00935Screws · looseSNRM 4342, NR 3 PYLON HAD 8 TRI-WING SCREWS LOOSE ON PYLON AFT MOUNT BULKHEAD, STA YN420 RT SIDE OF PYLON.SDR 96FDEA00934Screws · looseSNRM 4343, NR 3 PYLON HAD 5 TRI-WING SCREWS LOOSE ON LT SIDE OF PYLON AT AFT MOUNT BULKHEAD, STA YN 420.SDR 96FDEA00933Bolt · shearedSNRM 4126. NR 1 PYLON FORWARD ENGINE MOUNT TRUSS FITTINGS HAVE NUMEROUS LOOSE BOLTS AT BOTTOM, TOP, AND SIDES. APPROXIMATELY 50 PERCENT OF THE FASTENERS ARE LOOSE. ONE BOLT IN THE BOTTOM RIGHT IS SHEARED. YN222 STA. S/D: TORQUED BOLTS PER E.O. 8-5410-7-4SDR 96FDEA00968Bolt · shear offDURING ACCOMPLISHMENT OF EO 8-5410-7-3321 PART 1, FOUND FLATHEAD BOLT SHEAR OFF ON NR 1 PYLON AFT SUPPORT BULKHEAD.
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