N430FE
Service difficulty reports · 110
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 = 'N430FE' 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 = 'N430FE' 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 FDEA201102080495Floor Panel · damagedMAIN CABIN FLOOR PANEL FROM FRAME 40- FRAME 41; LBL 85. FABRICATED NEW FLOOR PANEL 241 VJ IAW DWG SRZ 25-005, REV "H".SDR FDEA201102080494Floorboard · delaminatedAFT CARGO COMPARTMENT FLOORBOARD 152 BF TOP SKIN IS DELAMINATED. FABRICATED NEW FLOORBOARD 152 BF IAW DWG SRZ 25-005, REV "H".SDR FDEA201102080493Skin · crackedAFT CARGO COMPARTMENT FLOORBOARD 152 AF TOP SKIN IS CRACKED. FABRICATED NEW FLOORBOARD 152 AF IAW DWG SRZ 25-005, REV "H".SDR FDEA201102080492Floorboard · damagedAFT CARGO COMPARTMENT FLOORBOARD 151EF TOP SKIN IS TORN AND THE CORNER IS CRUSHED. FABRICATED NEW FLOORBOARD 151 EF IAW DWG SRZ 25-005, REV "H".SDR FDEA201102080491Skin · damagedAFT CARGO COMPARTMENT FLOORBOARD 151 CF FASTENER HOLE IS BROKEN AND THE BOTTOM SKIN IS TORN. FABRICATED NEW FLOORBOARD 151 CF IAW DWG SRZ 25-005, REV "H".SDR FDEA201102080490Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 132 RF, MULTIPLE CORNERS ARE BROKEN, THE EDGES ARE DAMAGED AND MISSING EDGE FILLER. FABRICATED NEW FLOORBOARD 132 RF IAW DWG SRZ 25-005, REV "H".SDR FDEA201102080489Floorboard · crackedFWD CARGO COMPARTMENT FLOORBOARD 131 RF IS CRACKED ON AND THE CORNERS ARE DAMAGED. FABRICATED NEW FLOOR BOARD 131 RF IAW DWG SRZ 25-005, REV "H".SDR FDEA201102080488Floorboard · crackedFWD CARGO COMPARTMENT FLOORBOARD 131 HG IS CRACKED ON THE BACK AND THE EDGE IS BROKEN. FABRICATED NEW 131 HG IAW DWG SRZ 25-005, REV "H".SDR FDEA201102030462Floorbeam · corrodedAFT CARGO COMPARTMENT RT FLOORBEAM STRUCTURE HAS DOUBLE DRILLED HOLES AND IS CORRODED AT THE NUTPLATES. CROSSBEAM WAS REMOVED PER SRM 51-40-21, PARA 6 & 7. DRILLED AND INSTALLED NEW PART PER SRM 51-72-10, PG 2SDR FDEA201102030461Floorbeam · damagedBULK CARGO COMPARTMENT FLOORBEAM T-CAP HAS 2 DRILL STARTS ON THE UPPER SURFACE AT FRAME 66, LBL 3". DAMAGE REMOVED PER SRM 51-40-21 AND NEW T-CAP WAS FITTED AND DRILLED PER SRM 51-40-44 AND INSTALLED PER SRM 51-40-21; PARA 6 & 7.SDR FDEA201102020450Plate · crackedAFT CARGO COMPARTMENT DOOR CUTOUT CEILING STRUCTURE SEAL PLATE IS CRACKED BETWEEN FRAME 60 AND FRAME 61. TRIMMED OUT DAMAGED AREA IAW SRM 51-71-40, PG 202. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 51-71-40. DRILLED IAW SRM 51-40-44. ALODINED FILLER AND SDR FDEA201102020449Retainer · crackedAFT CARGO COMPARTMENT DOOR CEILING PANEL RETAINER IS CRACKED BETWEEN FRAME 60 AND FRAME 61; STRINGER 21R TO STRINGER 23R. REMOVED AFT CARGO COMPARTMENT DOOR CEILING PROFILE IAW SRM 51-40-21, PARA 5. LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED CEILING PASDR FDEA201010073975Brake · smokeAFTER LANDING, TOWER REPORTED SMOKE COMING FROM RT MAIN GEAR. TAXIED CLEAR, STOPPED AND HAD FIRE DEPT CHECK ORIGIN. THEY REPORTED FLUID DRIPPING ONTO GEAR. SHUTDOWN AND TOWED BACK TO RAMP. BRAKE TEMPS APPROX 280 DEG MAX (NR3, 150 DEG) IDENTIFIED SMOKE COMSDR FDEA201010053936Lug · corrodedDURING RIB 5 INSPECTION, CORROSION WAS FOUND IN L/H MAIN LANDING GEAR RIB 5, FORWARD LUG. CORROSION WAS REMOVED BY OVERSIZING THE BORE DIAMETER TO 5.015" AND REWORKING THE LUG TO THICHNESS OF 2.237". THE LUG WAS CONFIRMED FREE OF CORROSION BY NDT INSPECTSDR FDEA201010053934Lug · corrodedFOUND CORROSION IN RT MAIN LANDING GEAR FORWARD LUG AT RIB 5 DURING RIB 5 INSPECTION. REMOVED CORROSION BY OVERSIZING THE BORE AND SPOTFACING THE SURFACES, PERFORMING FINISHING CUTS, (FINAL BORE DIAMETER 5.341", FINAL LUG THICKNESS 2.220"), PERFORMING ASDR 08FDEA03454Floorbeam · crackedBULK CARGO DOOR ENTRY FLOOR T-CAP ON INTERCOSTAL HAS 4 IN CRACK BEGINNING AT FR 68 REMOVED DAMAGED T-CAP AND SPLICE STRIPS AND INSTALLED NEW PARTS AT BULK CARGO DOOR FLOOR ENTRY BETWEEN FR 67 AND FR 69 IAW A310-200 SRM 51-40-21 AND 51-72-10.SDR 08FDEA03453Skin · damagedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP LOWER MAIN SKIN AT MAIN SPAR TO REAR SPAR AND FROM THE INBD EDGE TO BETWEEN RIB 2 AND TRACK NR 3, MEASURING 47.7 IN BY 19.9 IN. REMOVED EXISTING REPAIR AND REPAIRED IAW SRM 57-53-12,FIG 210, PG 25SDR 08FDEA03452Skin · dentedRT AFT CREW DOOR LOWER AFT CORNER HAS DENT 1.5 IN LONG BY 2 IN W BY .033 IN DEEP CUT OUT DAMAGE AND INSTALLED SKIN REPAIR ON RT AFT DOOR LOWER AFT CORNER IAW A310-200 SRM 52-10-00, FIG 204, PG 217/218.SDR 08FDEA03450Skin · damagedSKIN AFT OF REAR SPAR LT AT RIB 11 HAS PREVIOUS .5 IN CRACK REPAIR REMOVED PREVIOUS DOUBLER AND RE-INSTALLED IAW FEDEX EA 6-5710-73485, REV NO B, POS PT, RELEASE DATE 11/14/03.SDR 08FDEA03408Seat Track · crackedMD CARGO COMPT CLS ADAPTER AT FR 43 BETWEEN SEAT TRACK 2RT AND 3 RT HAS 2 INCH CRACK. REMOVED AND REPLACED MDCC CLS ADAPTER AT FR 43 BETWEEN SEAT TRACK 2RT AND 3RT IAW A310-200 SRM 21-72-10.SDR 08FDEA03376Skin · dentedDENT ON FUSELAGE SKIN LOCATED AT FR 68 ABOVE LT STRINGER 44 MEASURING 4 IN BY 1.5 IN BY .025 DEEP CUT OUT DAMAGED AREA AND INSTALLED SKIN REPAIR AT LONGITUDINAL LAP JOINT BETWEEN FR 68 AND FR 69, STR 44 LT IAW A310-200 SRM 53-10-12, FIG 216 SHT 1.SDR 08FDEA03220Adapter · wornMDCC BETWEEN SEAT TRACK 2R AND 3R FRAME 38 CARGO LOADING SYSTEM ADAPTER HAS 2 EACH AREAS OF WORN SCALLOPS. REMOVED WORN CLS ADAPTER AND INSTALLED NEW CLS ADAPTER BETWEEN SEAT TRACK 2R AND 3R FRAME 38 IAW A310-200 SRM 51-40-21 AND SRM 51-72-10.SDR 08FDEA03219Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT SIDE FUSELAGE SKIN BETWEEN FRAMES 80/82 TO 84 AND BETWEEN STRINGERS 29 TO 32 LT, THE REPAIR DOUBLER MEASURES 10.1 INCHES BY 12 INCHES WITH A SKIN CUTOUT MEASURING 2.5 INCHES BY 2.1 INCHES. REPAIR NOT IAW SRM RESDR 08FDEA03218Fitting · misrepairedPREVIOUS REPAIR LOCATED ON FUSELAGE CUTOUT AT L-1 FORWARD PAX DOOR FAILSAFE RING LOWER SECTION HAS 2 EACH EXTERNAL REPAIR DOUBLERS, AT FRAMES 14 AND 16A BETWEEN BEAMS 2 AND 5, EACH REPAIR DOUBLER MEASURES 16.1" INCHES LONG AND 3.1" INCHES WIDE. REPAIR NOT IAWSDR 08FDEA03217Stringer · misrepairedPREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 52 LT BETWEEN FRAMES 59 TO 60 HAS 1 EACH REPAIR SECTION MEASURING 29 INCHES LONG AND 1 EACH REPAIR SPLICE MEASURING 7.3 INCHES LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS STRINGER REPAIRSDR 08FDEA03216Skin · misrepairedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LT WING OUTBOARD FLAP UPPER MAIN SKIN UNDER RUB STRIP AREA BETWEEN RIBS 7 TO 8 MEASURES 4" BY 5.6" INCHES. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT EXTERNAL REPAIR DOUBLER LOCASDR 08FDEA03039Skin · failedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING AILERON LOWER SKIN BETWEEN RIBS 12 TO 16 MEASURES 18.5 X 11.3 INCHES REPAIR NOT IAW SRM REQUIREMENTS. REMOVED 3 EACH FASTENERS FROM PREVIOUS REPAIR DOULBLER AND INSTALLED 3EACH CORRECT FASTENERS ON LEFSDR 07FDEA04577Seal · crackedDURING SCHEDULED B CHECK INSPECTION NR 1 LT THRUST REVERSER LIP SEAL WAS FOUND TO BE CRACKED. REPLACEMENT OF DAMAGED REVERSER.SDR 07FDEA04478Unknown · multiple failAFTER TAKEOFF CLIMBING OUT OF 3000' ECAM ALERTED AVIONICS SMOKE. NO SNIFFER FAN SMOKE OBSERVED, ECAM CLEANED THE WARNING, AND A FEW SECONDS LATER. ADVISED AGAIN AVIONICS SMOKE. THIS SECOND ECAM ALERT PROMPTED EMERGENCY RETURN AND LANDED SAFELY 26L CYVR. INSSDR 06FDEA1834Battery · overheatedNR 2 BATTERY OVERHEAT IN FLIGHT. RESET WITH SECOND OVERHEAT. KEPT BATT NR 2 OFF. REMOVED AND REPLACED NR 2 BATTERY PER A300 AMM 24-31-11-4 AND PERFORMED TEST PER AMM 24-31-00-5. OPS CK GOOD. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 33082-001SDR 06FDEA0650Seat Track · crackedCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. CRACK FOUND ON RT WING LOADING EDGE NEAR SLAT RAILS NR 5 AND NR 6 POSITIONS. REPAIRED PER SRM 57-41-12.SDR 06FDEA0648Fitting · crackedCOMPLY WITH AGING 9-AGING-INSP, FWD MDCC UTILITY AREA SUSPECTED OF CRACK AT FLOORBEAM CONNECTION FITTING AT FRAME 12A RT.SDR 06FDEA0649Failsafe · corrodedFWD PASS CREW DOOR RING RT FAILSAFE RING CORRODED AT UPPER FWD CORNER AT CENTRAL UPPER AREA AND AT AFT LOWER CORNER. REPLACED FAILSAFE RING PER DWG. R53610899 AND FEDEX EA 6-5340-95697 AND AIRBUS T.D. REF. 942-042678/03/2006 AND SRM 51-72-10 AND SRM 51-40-21 SDR 06FDEA0647Fitting · crackedFWD MDCC UTILITY AREA SUSPECT A CRACK AT FLOORBEAM CONNECTION FITTING AT FRAME 12A LT.SDR 06FDEA0642Repair · noneFOUND REPAIR LOCATED LT PAX DOOR L1. EXTERNAL DOUBLER LWR AFT CORNER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR WAS PREVIOUSLY ACCOMPLISHED RAS/AS/027/2006 REPAIR EVALUATED SDR 06FDEA0641Skin Panel · unknownFOUND REPAIR LOCATED LT AILERON WS 513-538. LOWER SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0534Repair · misinstalledFOUND REPAIR LOCATED ON RT OUTBD FLAP, RT WS 935-950. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPSDR 06FDEA0530Repair · misinstalledFOUND REPAIR LOCATED ON LT INBD FLAP, LT WS 277 - WS 289. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOSDR 06FDEA0521Repair · misinstalledCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. FOUND REPAIR LOCATED RT FS 1534 - FS 1554, FR22 ON THE LOWER CARGO DOOR EXT DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING RESDR 06FDEA0524Repair · noneCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. FOUND REPAIR LOCATED RT FS 2982 - FS 2294, FR38-FR40 FLUSH REPAIR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PERMANENT REPAIR PERFORMED BYSDR 06FDEA0523Repair · noneCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. FOUND REPAIR LOCATED LT FS 1305, FR16A ON THE AFT L1 DOOR FRAME EXT DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVASDR 06FDEA0522Repair · noneCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. FOUND REPAIR LOCATED LT FS 1184, FR14 ON THE FWD L1 DOOR FRAME EXT DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALSDR 06FDEA0520Repair · noneCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. FOUND REPAIR LOCATED RT FS 3567 - FS 3587, FR66, STR 32 - STR 33 EXT DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVSDR 06FDEA0518Repair · noneCOMPLY WITH AGING 9-AGING-INSP REV POS PT1. FOUND REPAIR LOCATED RT FS 766 - FS 794, FR 1 - FR 2 EXT DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND SDR 06FDEA0533Repair · misinstalledFOUND REPAIR LOCATED ON RT INBD FLAP, RT WS 347-349. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX E:A: 6-5710-95695 REPAIR EVALUASDR 06FDEA0532Repair · misinstalledFOUND REPAIR LOCATED ON RT INBD FLAP, RT WS 110-119. REPAIR REQUIRES EVALUATION FOR MAJOR OR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX E:A: 6-5710-95695 REPAIR EVALUSDR 06FDEA0531Repair · unknownFOUND REPAIR LOCATED ON RT INBD FLAP, RT WS 359-409. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 AND RAS/DABRE/700SDR 06FDEA0529Repair · misinstalledFOUND REPAIR LOCATED ON LT INBD FLAP, LT WS 134-182. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 REPAIR EVALUATSDR 06FDEA0528Repair · misinstalledFOUND REPAIR LOCATED ON LT INBD FLAP, LT WS 346-400. REPAIR REQUIRES EVALUATION FOR MAJOR OR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 REPAIR EVALUATSDR 06FDEA0527Repair · misinstalledFOUND REPAIR LOCATED ON LT INBD FLAP, LT WS 236-276. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED TRAILING EDGE ASSY PER SRM 51-72-10 AND FEDEX EA 6-5710-95695 REPAIR EVALUATED
Back to N430FE