N803FX
Service difficulty reports · 262
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 = 'N803FX' 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 = 'N803FX' 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 COEA2026070713803Fitting · brokenDURING HEAVY CHECK, AFT AVIONICS BAY RUDDER SUPPORT QUADRANT FRWD DIAGONAL BRACE UPPER ATTACH POINT IS BROKEN. REPLACED IAW MP ATR-A-27-23-30-00001-720A-A REV.11.SDR COEA2026062501803Floorbeam · gougedFLOORBEAM 19 UPPER FLANGE LOWER SURFACE GOUGED. REPAIRED PER ATR72 SRM 533140-08-A01, 51-25-01 REV. 122.SDR COEA2026062505803Skin · dentedEXTERNAL FUSELAGE SKIN DENTED AT FRAME 11 STRINGER 13L. REPAIRED PER SRM 530000-300-808-A01 REV. 122.SDR COEA2026072331803Spar · corrodedRIGHT WING FRONT SPAR UPPER STRIP SLAT BETWEEN RIBS 3-5R HAS SCRATCHES. LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS-00026284-02 ISSUE A, DATED 6/8/2026.SDR COEA2026072327803Fitting · corrodedHORIZONTAL TO VERTICAL STAB AFT RT FITTING HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FITTING PER ATR72 SRM 51-25-04 REV. 122.SDR COEA2026072224803Fitting · corrodedHORIZONTAL TO VERICAL STAB AFT L/H FITTING HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FITTING PER ATR72 SRM 51-25-04 REV. 122.SDR COEA2026072223803Seat Track · corrodedWO 273091 NR 200099 HEAVY CHECK COE/MAJOR REPAIR: FIRST OFFICER SEAT FITTING HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS-00026373-01 ISSUE A, DATED 6/12/2026.SDR COEA2026072221803Seat Track · corrodedWO 273091 NR 200098 HEAVY CHECK COE/MAJOR REPAIR: CAPTAIN SEAT FITTING HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS-00026373-01 ISSUE A, DATED 6/12/2026.SDR COEA2026072328803Spar · corrodedUPPER WING AFT SPAR UPPER FLANGE LOWER SURFACE RIBS 0-4R HAS CHAFE DAMAGE AND LEVEL 2 CORROSION. REPAIRED PER SRAS-00026285-01 ISSUE B, DATED 6/17/2026.SDR COEA2026070716803Landing · corrodedWO 273091 NR 600048 HEAVY CHECK COE/MAJOR REPAIR: R/H WING 622CT PANEL LANDING HAS FRETTING DAMAGE. LEVEL 2 CORRECTIVE ACTION: REPAIRED PER SRAS 00026533-01 ISSUE A, DATED 6/3/2026.SDR COEA2026070715803Landing · corrodedWO 273091 NR 500061 HEAVY CHECK COE/MAJOR REPAIR: L/H WING PANEL 521DT LANDING HAS FRETTING. LEVEL 2 CORRECTIVE ACTION: REPAIRED PER SRAS 00026533-01 ISSUE A, DATED 6/3/2026.SDR COEA2026070714803Landing · corrodedDURING HEAVY CHECK, LT WING PANEL 522CT WING LANDING FRETTING. LEVEL 2. REPAIRED IAW SRAS 00026533-01 ISSUE A, DATED 6/3/2026.SDR COEA2026072330803Spar · chafedLEFT WING FWD SPAR UPPER STRIP SLAT RIB 4L-5L HAS CHAFING DAMAGE. CORRECTIVE ACTION: REPAIRED PER SRAS-00026284-01 ISSUE B, DATED7/17//2026.SDR COEA2026072219803Floorbeam · corrodedFLOORBEAM UPPER FLANGE ON R/H FRAME 25 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER U.S. TECHNICAL EO-26165-53-001 REV. NC 6/5/2026.SDR COEA2026070717803Door Frame · crackedDURING HEAVY CHECK, FWD CARGO DOOR FRAME AT BS 7065 WAS CRACKED, SKIN ATTACH FLANGE UPPER END. REPAIRED IAW SRM 523100-300-811-A01 REV. 122.SDR COEA2026070712803Frame · damagedDURING HEAVY CHECK, INTERNAL FUSELAGE FRAME 21 HAD TWO FLAWED HOLES, INBD & OTBD OF STRINGER 5L. REPLACED IAW SRM 51-25-01, 51-25-02 AND 51-25-04 REV. 122.SDR COEA2026062504803Stringer · crackedINTERNAL FUSELAGE, STRINGER 11R FRAMES 23-23D FLAW INDICATIONS FOUND TO BE CRACKS. REPAIRED PER ATR72 SRM 530000-300-826-A01 REV. 122.SDR COEA2026072226803Channel · corrodedRT AILERON, MOVEABLE TRIM TAB CLOSEOUT CHANNEL HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED CHANNEL PER ATR72 SRM 51-25-03 REV. 122.SDR COEA2026072222803Stiffener · corrodedRIGHT CREASE BEAM WEB LOWER SURFACE FRAME 23-23A HAS LEVEL 2 CORROSION. REPLACED STIFFENER PER ATR72 SRM 535150-01-A01, 51-25-01, 51-25-04 REV. 121.SDR COEA2026072220803Floorbeam · corrodedFLOORBEAM 15 HAS LEVEL 2 CORROSION UPPER SURFACE BETWEEN INBOARD SEAT TRACKS. REPAIRED PER ATR72 SRM 530000-300-849-A01 REV. 122.SDR COEA2026070710803Crease Beam · corrodedDURING HEAVY CHECK, RT CREASE BEAM HAD LEVEL 2 CORROSION FRAMES 23A-23B. REPLACED IAW SRM 51-25-01 REV. 122.SDR COEA2026062508803Angle · corrodedL/H INNER ANGLE NEAR FWD CARGO DOOR THRESHOLD HAS LEVEL 2 CORROSION. REPLACED PER SRM 51-25-01, 51-25-03, 51-25-04 REV. 122.SDR COEA2026062507803Floorbeam · corrodedFLOORBEAM 17 UPPER SURFACE HAS LEVEL 2 CORROSION. REPLACED FLOORBEAM PER SRM 533140-06-A01, 51-25-01, 51-25-04 REV. 122.SDR COEA2026062506803Seat Track · corrodedL/H OUTBOARD SEAT TRACK LOWER SURFACE HAS LEVEL 2 CORROSION. REPAIRED PER ATR72 SRM 530000-300-832-A01 REV. 122.SDR COEA2026062502803Stringer · crackedWO 273091 NR 100041 HEAVY CHECK COE/MAJOR REPAIR: STRINGER 21R IS CRACKED AFT OF FRAME 18. CORRECTIVE ACTION: REPAIRED PER ATR72 SRM 530000-300-826-A01 REV. 122.SDR COEA2026072329803Spar · corrodedWO 273091 NR 600013 HEAVY CHECK COE/MAJOR REPAIR: R/H WING REAR SPAR STRIP SLAT UPPER SURFACE BETWEEN RIBS 6-9 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS-00026285-01 ISSUE B, DATED 7/17/2026.SDR COEA2026072225803Strip · corrodedLEFT WING, REAR SPAR STRIP SLAT UPPER SURFACE BETWEEN RIBS 10-13 HAS LEVEL 2 CORROSION AROUND MULTIPLE FASTENER HOLES. CORRECTIVE ACTION: REPAIR PER SRAS-00026288-01 ISSUE A, DATED 6/8/2026.SDR COEA2026072218803Seat Track · corrodedRT SEAT TRACK HAS LEVEL 2 CORROSION. REPAIRED PER SRM 536300-01-A01, 51-25-02, 51-25-04 REV. 121.SDR COEA2026062509803Stringer · corrodedSTRINGER 11R HAS LEVEL 2 CORROSION BETWEEN FRAMES 30-34. REPAIRED PER SRM 530000-300-826-A01 REV. 122.SDR COEA2026070711803Skin · dentedDURING HEAVY CHECK, LT STATIC PORT AREA SKIN DENTED. REPAIRED IAW SRAS 00026106-01 ISSUE A, DATED 6/11/2026.SDR COEA2026062503803Skin · dentedEXTERNAL FUSELAGE CROWN SKIN IS DENTED BETWEEN FRAMES 28D-29 STRINGERS 2-3R. REPAIRED PER SRM 530000-300-803-A01 REV. 121.SDR COEA2025050102803Shield · corrodedWO 265739 NR 600006 BRIDGING COE/MINOR DISCREPANCY: R/H SPOILER THUNDER SHIELD BLADE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: SPOILER REPAIRED PER ATR72 SRM 5771-10-300-823-A01.SDR COEA2025050101803Shield · corrodedWO 265739 NR 500007 BRIDGING COE/MINOR DISCREPANCY: L/H SPOILER THUNDER SHIELD BLADE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: SPOILER REPAIRED PER ATR72 SRM 5771-10-300-823-A01.SDR MTNA20250221001Oxygen Bottle · failedSHORTLY AFTER LINE CHECK, CREW O2 PRESSURE WAS AGAIN BELOW 1500PSI AFTER BEING SERVICED JUST PRIOR. DURING INSPECTION FOUND OXGEN BOTTLE VALVE DAMAGED AND LEAKING. BOTTLE REQUIRES REPLACE. REMOVED AND REPLACED CREW OXYGEN BOTTLE (5101HT) W/ REF TO ATR-A-35-11-SDR MTNA20240228001Door · missingUPON POST FLIGHT INSPECTION IN CHS, THE FO DISCOVERED THAT THE LEFT HAND ENGINE COWLING ON THE NUMBER 2 ENGINE WAS MISSING. BOTH PRE FLIGHT INSPECTIONS BY BOTH CREW MEMBERS CONFIRMED THAT THE COWLING WAS ATTACHED PRIOR TO FLIGHT. THE COWLING APPEARS TO HAVE BESDR MTNA202312040341Unknown · unknownDURING THE CLIMB TO CRUISE ALTITUDE, AT APPROXIMATELY FL190, THE CREW RECEIVED AN EXCESS CABIN ALTITUDE ALERT. AFTER PERFORMING THE ASSOCIATED QRH ITEMS, THE CREW NOTIFIED ATC, DESCENDED TO 10,000 FT, AND THE FLIGHT RETURNED TO THE FIELD WITHOUT FURTHER INCIDSDR COEA2022102509803Fitting · corrodedWO 238881 NR 500029 HEAVY CHECK COE/MAJOR REPAIR: L/H WING INBOARD FLAP RIB 9 FITTING HAS LEVEL 2 CORROSION UNDER FAIRING SUPPORT BRACKET. CORRECTIVE ACTION: REPAIR PER ATR SRAS ES_00201503_01...19648 ISSUE A, DATED 10/20/2022.SDR COEA2022102510803Skin · corrodedWO 238881 NR 600018 HEAVY CHECK COE/MAJOR REPAIR: UPPER WING ACCESS DOOR CUTOUT FOR PANEL 622CT HAS FRETTING DAMAGE. CORRECTIVE ACTION: REPAIR PER ATR SRAS DO/TS-4828/10...6020 ISSUE F, DATED 10/20/2022.SDR COEA2022102508803Panel · corrodedWO 238881 NR 500023 HEAVY CHECK COE/MAJOR REPAIR: UPPER WING ACCESS DOOR CUTOUT FOR PANEL 522CT HAS FRETTING DAMAGE. CORRECTIVE ACTION: REPAIR PER ATR SRAS DO/TS-4828/10...6020 ISSUE F, DATED 10/20/2022.SDR COEA2022102507803Skin · corrodedWO 238881 NR 500022 HEAVY CHECK COE/MAJOR REPAIR: UPPER WING ACCESS DOOR CUTOUT FOR PANEL 521DT HAS FRETTING DAMAGE. CORRECTIVE ACTION: REPAIR PER ATR SRAS DO/TS-4828/10...6020 ISSUE F, DATED 10/20/2022.SDR COEA2022102506803Attach Angle · crackedWO 238881 NR 500014 HEAVY CHECK COE/MAJOR REPAIR: L/H AILERON LOWER MIDDLE ACCESS CUT-OUT FOR PANEL 544GB AT FRONT SPAR HAS BENT/CRACKED ATTACH ANGLE. CORRECTIVE ACTION: REPAIR PER ATR SRAS ES_00200735_01...19589 ISSUE A, DATED 10/22/2022.SDR COEA2022102105803Web · corrodedW/O 238881 NR 200018 HEAVY CHECK COE/MAJOR REPAIR: PAX DOOR THRESHOLD UPPER SURFACE BETWEEN FRAMES 36-39 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIR PER ATR72 536770-200-802-A01.SDR COEA2022080804803None · failedFLIGHT 8584 DISCREPANCY: UPON LANDING IN RAP, THE FO SIDE LEFT BRAKE FAILED WITH PRESSURE APPLIED TO BRAKE PEDAL. USED CAPTAIN'S BRAKE TO STOP THE AIRCRAFT. CORRECTIVE ACTION: MAINTENANCE SERVICED THE BRAKE RESEVOIR AND BLED THE BRAKE SYSTEM. TAXI CHECK FAILEDSDR COEA2022020403803Drain Line · failedFLIGHT 8663, ON CLIMB ANC - FAI AIR TURNBACK/DISCREPANCY: DURING CLIMB, THE CREW RECEIVED A DADC DATA INVALID MESSAGE, FOLLOWED BY AN ANTI - ICE FAULT, AMP FAULT AND THE FDAU LIGHT WAS FLASHING ON FEDEP PANEL. AIRCRAFT WAS RETURNED TO ANC, NO EMERGENCY SDR COEA2022011402803Cable · brokenFLIGHT 7663, ENROUTE FAI - ANC/DISCREPANCY: PITCH TRIM ASYMMETRY IN FLIGHT. AIRCRAFT LANDED SAFELY IN ANC. MAINTENANCE IS CURRENTLY TROUBLESHOOTING. A SUPPLEMENTAL SDR WILL FOLLOW WITH CORRECTIVE ACTION.SDR COEA2022011101803Relay · faultedFLIGHT 8663, ENROUTE ANC - FAI/AIR TURNBACK DISCREPANCY: IDLE GATE FAIL ON TAKEOFF. RESET BUT IDLE GATE CAP LIGHT STAYED ILLUMINATED. RETURNED AIRCRAFT TO ANC. NO EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE CLEANED IDSDR COEA2021020301803Spar · damagedDURING TAXI, THE AIRCRAFT STRUCK THE HANGAR. DAMAGE DESCRIPTION RT WING FRONT SPAR SUSTAINED COMPOSITE DELAMINATION, TORN MISSING PLIES AND BROKEN FIBERS AT RIB 31. CORRECTIVE ACTION REPAIRED PER SRAS ES_0131069_02...17181 ISSUE B, DATED 2/3/2021.SDR COEA2020081104803Stringer · damagedSTRINGER 2L DAMAGED BY BUCKING BAR BETWEEN FRAMES 17-18. REPAIRED PER SRM 530000-300-824-A01.SDR COEA2020082506803Spar · damagedWO 216494 NR 400013 HEAVY CHECK COE, MAJOR REPAIR. RIB 10R LOWER SPAR FLANGE OUTBOARD FASTENER HOLE HAS FLAW INDICATION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0122248_01.16593 ISSUE A, DATED 8/21/2020.SDR COEA2020081105803Panel · corrodedL/H WING NACA DUCT PANEL 523DB HAS LEVEL 2 CORROSION ON THE MATING SURFACE. CORRECTIVE ACTION: REPLACED WITH OEM PART.
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