N801FX
Service difficulty reports · 223
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 = 'N801FX' 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 = 'N801FX' 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 COEA2016010432801Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. LT WING PANEL 521DT FOIL & CUT OUT HAS FRETTING, LEVEL 2. REPAIRED IAW SRAS DO TS 4809 07 4337 ISSUE D DATED 2 11 2016.SDR COEA2016010427801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. LT WING PANEL 522CT FOIL & CUT OUT HAS FRETTING. REPAIRED IAW SRAS DOTS 4809 07 4337 ISSUE D DATED 2 11 16.SDR COEA2016010419801Fitting · damagedHEAVY CHECK COE & MAJOR REPAIR. RT WING RIB 4 FLAP BEAM, UPPER INBD FITTING DAMAGED FROM CONTACT WITH PANEL 296CR SCREW. REPAIR IAW SRAS ES 562 16 9979 DATED 2 16 16.SDR COEA2016010403801Landing · corrodedWO 155295 NR 400021, HEAVY CHECK COE & MAJOR REPAIR. RT ENG NACELLE OTBD AFT LANDING FOR PANEL 484AR HAS CHAFING DAMAGE & LEVEL 2 CORROSION. REPAIR IAW SRAS CE219 16 9939 2 2 2016.SDR COEA2016010343801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL AFT OF FRAME 21, STRINGER 5A - 6. REPAIRED IAW SRAS ES-533 16 9984 DATED 2 25 16.SDR COEA2016010342801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL FWD OF FRAME 21, BETWEEN STRINGER 8 - 10. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 16.SDR COEA2016010341801Strap · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL STRAP, BETWEEN FRAMES 15-16, STRINGER 11 - 12. REPAIR IAW SRAS ES 533 16 9984 DATED 2 25 16.SDR COEA2016010340801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL, BETWEEN FRAMES 16 - 17, STRINGER 8 - 9. REPAIR IAW ES 533 16 9984 DATED 2 25 2016.SDR COEA2016010339801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL, BETWEEN FRAMES 16-17, STRINGER 4 - 5. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 16.SDR COEA2016010336801Stringer · corrodedHEAVY CHECK COE & MAJOR REPAIR. LEVEL 2 CORROSION ON STRINGER 6R FWD OF FRAME 18. STRINGER SPLICE, FRAME 16 - 21 IAW SRM 530000-300-824-A01.SDR COEA2016010225801Doubler · corrodedWO 155295 NR 100048 HEAVY CHECK COE & MINOR REPAIR. PANEL 193AL BEACON LIGHT DOUBLER HAS LEVEL 2 CORROSION. REPLACED DOUBLER WITH OEM PART.SDR COEA2016010322801Doubler · corrodedWO 155295 NR 200040 HEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING CTR FUSELAGE, FWD CROWN PANEL & DOUBLER, FRAME 23D - 24, STRINGER 3 - 3A RT. REPAIR IAW SRAS ES 367 16 9947 DATED 2 12 16.SDR COEA2016010317801Skin · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING CTR FUSELAGE FWD CROWN PANEL & DOUBLER, FRAME 23D - 24, STRINGER 3 - 4 LT. REPAIR IAW SRAS ES 367 16 9947 DATED 2 12 16.SDR COEA2016010314801Hinge Fitting · damagedWO 155295 NR 600009 HEAVY CHECK COE & MAJOR REPAIR. RT WING OTBD FLAP RIB 13 HINGE ARM DAMAGE AT THE HINGE POINT. REPAIR IAW SRAS CE 349 16 9922 DATED 1 26 16.SDR COEA2016010312801Fitting · damagedHEAVY CHECK COE & MAJOR REPAIR. RT WING RIB 13 FLAP BEAM, LOWER OTBD FITTING DAMAGED FROM CONTACT WITH BONDING STRAP. REPAIR IAW SRAS CE-332 16 9921 DATED 1 26 16.SDR COEA2016010311801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING CTR FUSELAGE, LT LOWER SKIN PANEL, BETWEEN FRAMES 23A - 23B, STRINGER 12 - 12A. REPAIR IAW SRAS CE-361 16 9926 DATED 1 29 16.SDR COEA2016010302801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING CTR FUSELAGE RT UPPER SKIN PANEL, BETWEEN FRAMES 23B - 23C, STRINGER 10 - 10A. REPAIR IAW SRAS CE 363 16 9925 DATED 1 29 2016.SDR COEA2016010237801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING REAR CTR FUSELAGE, LT UPPER PANEL, AFT OF FRAME 33 & FWD OF FRAME 34, STRINGER 8 - 10. REPAIR IAW SRAS ES 532 16 9964 DATED 2 24 16.SDR COEA2016010231801Floorbeam · corrodedHEAVY CHECK COE & MAJOR REPAIR. FRAME 25 FLOORBEAM TOP SURFACE HAS LEVEL 2 CORROSION, LT & RT OF BL 0. REPAIR IAW SRAS CE 276 16 9908 DATED 2 24 16.SDR COEA2016010224801Web · corrodedHEAVY CHECK COE & MINOR REPAIR. FWD CARGO DOOR DRAIN CHANNEL MOUNT, WEB HAS LEVEL 2 CORROSION. REPLACED WEB WITH OEM PART.SDR COEA2016010223801Web · corrodedHEAVY CHECK COE & MAJOR REPAIR. FWD CARGO DOOR LOWER SURROUND VERTICAL WEB HAS AREAS OF LEVEL 2 CORROSION. REPAIRED IAW SRAS CE 477 16 9957 DATED 2 17 16.SDR COEA2016010221801Seat Track · corrodedHEAVY CHECK COE & MINOR REPAIR. RT OTBD SEAT TRACK HAS LEVEL 2 CORROSION, FRAME 22 - 23. REPLACED SECTION OF EXISTING SEAT TRACK REPAIR IAW SRM 530000-300-832-A01.SDR COEA2016010220801Seat Track · corrodedHEAVY CHECK COE & MINOR REPAIR. LT OTBD SEAT TRACK HAS LEVEL 2 CORROSION AT FRAME 13 - 18. REPLACED SECTION OF EXISTING SEAT TRACK REPAIR IAW SRM 530000-300-832-A01.SDR COEA2016010218801Stringer · corrodedHEAVY CHECK COE & MAJOR REPAIR. STRINGER 21R, FWD OF FRAME 25, HAS LEVEL 2 CORROSION. REPAIR IAW SRM 530000-300-826-A01.SDR COEA2016010216801Seat Track · gougedHEAVY CHECK COE & MAJOR REPAIR. CTR FUSELAGE RT OTBD SEAT TRACK GOUGED, BETWEEN FRAMES 28A - 28B. SEAT TRACK SPLICE, FRAME 28A IAW SRM 530000-300-853-A01.SDR COEA2016010215801Seat Track · corrodedHEAVY CHECK COE & MAJOR REPAIR. CTR FUSELAGE RT INBD SEAT TRACK HAS LEVEL 2 CORROSION, BETWEEN FRAMES 23 - 23A. SEAT TRACK SPLICE, FRAME 23 - 23A IAW SRM 530000-300-853-A01.SDR COEA2016010213801Floorbeam · corrodedHEAVY CHECK COE & MAJOR REPAIR. FRAME 13 FLOORBEAM, TOP SURFACE HAS LEVEL 2 CORROSION, BETWEEN THE LT & RT INBD SEAT TRACKS. REPLACED FLOORBEAM BY FABRICATION.SDR COEA2016010210801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING REAR FUSELAGE, LT LATERAL UPPER PANEL, FRAMES 40 - 41, STRINGER 8 - 9 LT. SMALL DAMAGE EXTERNAL REPAIR SRM 530000-300-801-A01.SDR COEA2016010209801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING CTR FUSELAGE, LT UPPER SKIN PANEL, BETWEEN FRAMES 24 - 25, STRINGER 4 - 5. REPAIR IAW SRAS CE-339 16 9919 DATED 1 29 16.SDR COEA2016010208801Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING REAR FUSELAGE RT LATERAL UPPER PANEL, FRAME 34 - 35, STRINGER 10 - 11 RT. BETWEEN STRINGERS EXTERNAL DOUBLER REPAIR IAW SRM 530000-300-803-A01.SDR COEA2016010207801Reinforcement · corrodedHEAVY CHECK COE & MINOR REPAIR. FLOORBEAM 13 UPPER FLANGE REINFORCEMENT, AT THE 90 VU PILLAR, HAS LEVEL 2 CORROSION. REPLACED WITH OEM PART.SDR COEA2016010204801Frame · corrodedWO 155295 NR 100012 HEAVY CHECK COE & MINOR REPAIR. INT FUSELAGE, AFT SIDE OF FRAME 29 HAS LEVEL 2 CORROSION, BETWEEN STRINGER 19 - 20 RT. REPLACED FRAME 29 BOTTOM SEGMENT STRINGER 17L - 17R WITH OEM.SDR COEA2016010201801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING REAR FUSELAGE RT LATERAL UPPER SKIN PANEL, FRAMES 40 - 41, STRINGER 5 - 6 RT. EXTERNAL DOUBLER REPAIR, SRM 530000-300-803-A01.SDR COEA2015123105801Landing · corrodedHEAVY CHECK COE & MAJOR REPAIR. LT ENG NACELLE OTBD AFT LANDING FOR PANEL 473AL, HAS CHAFING DAMAGE, LEVEL 2 CORROSION. REPAIRED IAW SRAS CE 219 16 9938 DATED 2 2 2016.SDR COEA2015123104801Landing · corrodedHEAVY CHECK COE & MAJOR REPAIR. LT ENG NACELLE INBD AFT LANDING FOR PANEL 474AR, HAS CHAFING DAMAGE, LEVEL 2 CORROSION. REPAIR IAW SRAS CE 219 16 9937 DATED 2 2 2016.SDR COEA2015123103801Stringer · corrodedHEAVY CHECK COE & MINOR REPAIR. LEVEL 2 CORROSION AROUND FASTENER BUCK TAILS ON STRINGER 19, BETWEEN FRAMES 44 & 45. REPLACED STRINGER WITH NEW.SDR COEA2015030502801Block · faultyAIR TURN BACK DISCREPANCY, AFTER GEAR RETRACTION, THE FLAP UNLOCK WARNING ILLUMINATED & DID SO DURING CLIMB OUT. THE CREW ELECTED TO RETURN BACK. NO EMER WAS DECLARED. REPLACED THE FLAP VLV BLOCK. OPERATIONS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR COEA2015011401801Controller · faultyON CLIMB OUT, APPROACHING 11000FT, THE ACFT EXPERIENCED A LOSS IN CABIN PRESSURE. THE CREW SWITCHED TO MANUAL MODE & WAS UNABLE TO PRESSURIZE THE ACFT. AN EMER DESCENT WAS COMPLETED TO 10000 FT & A RETURN INITIATED DUE TO THE DEPRESSURIZATION. NO EMER WAS DSDR COEA2014111307801Switch · failedAIR TURN BACK. ON REACHING CRUISE ALTITUDE, THE ACFT LOST PRESSURIZATION. ELECTED TO RETURN. NO EMERGENCY WAS DECLARED. ACFT LANDED WITHOUT INCIDENT. AFTER TROUBLESHOOTING, IT WAS DETERMINED THAT THE CABIN PRESSURIZATION WORKED NORMALLY WHEN NR 1 ENGINE SDR COEA2014013005801Stiffener · crackedRIGHT TRUNION FITTING UPPER SURFACE STIFFENER HAS A CRACK AT THE UPPER FASTENER FOR THE FRAME 26 FAIRING SUPPORT. REPAIR IAW SRAS S535R0199 2982 ISSUE B 1/29/2014.SDR COEA2014013004801Skin · dentedFUSELAGE TAIL SECTION HAS A DENT ON THE LT SIDE BETWEEN FRAMES 46 - 47 & STRINGERS 11 - 12. REPAIR IAW SRM 53-00-00 FIG 403 & SRAS DT S-428-14 8194 DATED 1/30/2014.SDR COEA2014013003801Skin · damagedRIGHT WING CUTOUT FOR PANEL 622CT HAS LEVEL 1 FRETTING. REPAIR IAW SRAS DO TS-4809 07 4337 ISSUE C.SDR COEA2014013002801Skin · damagedLEFT WING CUTOUT FOR PANEL 522CT HAS LEVEL 1 FRETTING. REPAIR IAW SRAS DO TS-4809 07 4337 ISSUE C DATED 1/27/2014.SDR COEA2014013001801Skin · damagedLEFT WING CUTOUT FOR PANEL 521DT HAS FRETTING. REPAIR IAW SRAS DO TS-4809 07 4337 ISSUE C DATED 1/27/2014.SDR COEA2013121804801Bolt · shearedFLIGHT 7250 YVR TO OAK DISCREPANCY. DURING FLIGHT, FWD CARGO DOOR LEAKS AIR THROUGH A GAP IN LOWER FWD SECTION OF DOOR. AFTER ARRIVAL INTO OAK, MX FOUND MULTIPLE SHEARED BOLTS IN FWD LOWER DOOR FITTING. REMOVED FITTING, INSPECTED & INSTALLED NEW BOLTS IAW ASDR COEA2013050102801Fairing · missingON ARRIVAL OF FLIGHT 7663, DISCOVERED INSIDE FLAP ON THE LEFT WING WAS MISSING LEFT INBOARD FLAP OUTER HINGE FAIRING AND THE FLAP WAS DAMAGED. REPAIRED IAW SRM 57-52-10, REPAIR B4 AND B6. MAJOR REPAIR.SDR COEA2013040401801Mount Bolt · crackedFSR FOUND A CRACK IN THE RIGHT MLG FWD TRUNNION MOUNTING PIN, P/N D60999. THIS WAS A SCHEDULED INSPECTION FOR THE PURPOSE OF EXTENDING THE TBO FOR THE LANDING GEAR COMPONENTS. THE PART IS TO BE REPLACED WITH SERVICEABLE PART PRIOR TO AIRCRAFT OPERATION.SDR COEA2012033021801Unknown · malfunctionedAIR TURNBACK SEA FLIGHT 7202: DURING CLIMBOUT THE AIRCRAFT WOULD NOT PRESSURIZE. LEAK APPEARED TO BE AT THE DOCUMENT DOOR. CREW ELECTED TO RETURN TO SEA. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED DETAILED VISUAL INSPECTION OF DOCUMENT DOOR. SDR COEA2012022320801Intercostal · corrodedHEAVY CK / LEVEL 2 CORROSION: FOUND GOUGES WITH CORROSION ON INTERCOSTAL AT STR 16L FRA 15 - 16 (LENGTH 2", WIDTH 1", DEPTH .013"). REMOVED GOUGES AND CORROSION, REMOVED AND REPLACED INTERCOSTAL WITH OEM PART.SDR COEA2012022019801Skin · damagedNR 4 HEAVY CHECK, MAJOR REPAIR: IMPACT DAMAGE FROM GROUND SUPPORT STAND ON OUTER SKIN COMMON TO FRAME 8 AT DOCUMENT DOOR. FABRICATED AND INSTALLED NEW PART PER DRAWING, DOCUMNET DOOR LT SIDE OF COCKPIT AT FRAME 8 AND STRINGER 9.
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