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 COEA2020032615801Skin Panel · corrodedWO 209330 NR 100063 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE R/H LOWER PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 23D-24 BETWEEN STRINGERS 16R-17R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0113811_01...15875 ISSUE A, DATED 3/20/2020.SDR COEA2020032012801Skin Splice · damagedWO 209330 NR 200208 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE SKIN SPLICE IS DAMAGED AT FRAME 42 STRINGER 4-5R. CORRECTIVE ACTION: REPLACED SPLICE WITH FABRICATION.SDR COEA2020032011801Skin Panel · corrodedWO 209330 NR 200130 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE R/H UPPER PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 40-41, STRINGERS 7R-8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0113648_01...15859 ISSUE A, DATED 3/16/2020.SDR COEA2020032010801Skin Panel · corrodedWO 209330 NR 200123 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE R/H UPPER PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 41-42, STRINGERS 8R-9R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0113648_01...15859 ISSUE A, DATED 3/16/2020.SDR COEA2020031306801Skin Panel · corrodedWO 209330 NR 200164 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE R/H UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION AFT OF FRAME 23C BETWEEN STRINGERS 5AR-6R. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-806-A01.SDR COEA2020032414801Fitting · corrodedWO 209330 NR 300030 HEAVY CHECK COE/MINOR REPAIR: L/H ELEVATOR HORN TIP FITTING ATTACH FLANGE FOR PANEL 334AL HAS LEVEL 2 CORROSION ON MATING SURFACE AND INNER SURFACE UNDER NUTPLATES. CORRECTIVE ACTION: REPLACED WITH OEM.SDR COEA2020033118Frame · corrodedWO 209330 NR 100045 HEAVY CHECK COE/MAJOR REPAIR: FRAME 39 HAS LEVEL 2 CORROSION LOWER SURFACE WHERE IT PASSES THROUGH THE FLOOR WEB. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0115582_01...16012 ISSUE A, DATED 3/18/2020.SDR COEA2020032013801Frame · corrodedWO 209330 NR 300015 HEAVY CHECK COE/MAJOR REPAIR: FRAME 47 AFT SIDE HAS LEVEL 2 CORROSION AT UPPER L/H BONDING POINTS. CORRECTIVE ACTION: REPAIRED PER SRM 538140-300-804-A01.SDR COEA2020032007801Skin · distortedWO 209330 NR 100052 HEAVY CHECK COE/MAJOR REPAIR: NOSE FUSELAGE LOWER L/H AFT SKIN IS DISTORTED AT DME2 ANTENNA FASTENER LOCATIONS, FRAMES 8-9. CORRECTIVE ACTION: REPAIRED PER SRM 531129-300-802-B01.SDR COEA2020030403801Frame · corrodedWO 209330 NR 100031 HEAVY CHECK COE/MINOR REPAIR: FRAME 28A HAS LEVEL 2 CORROSION BETWEEN STRINGERS 20L-21L. CORRECTIVE ACTION: REPLACED WITH OEM PART.SDR COEA202002202801Spar · delaminatedWO 209330 NR 500022 HEAVY CHECK COE/MAJOR REPAIR: L/H WING FRONT SPAR LOWER FLANGE DELAMINATING IN MULTIPLE AREAS ON THE LOWER SURFACE BETWEEN RIBS 13-19. CORRECTIVE ACTION: REPAIRED PER SRAS ES_112901_01...15927 ISSUE A, DATED 2/12/2020.SDR COEA202002201801Spar · delaminatedWO 209330 NR 500021 HEAVY CHECK COE/MAJOR REPAIR: L/H WING FRONT SPAR UPPER FLANGE HAS DELAMINATION ON THE UPPER SURFACE BETWEEN RIBS 13-19. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112901_01...15927 ISSUE A, DATED 2/12/2020.SDR COEA2020032000001Skin · corrodedWO 209330 NR 100014 HEAVY CHECK COE/MAJOR REPAIR: FRAME 14 SKIN FLANGE IS EXFOLIATED BETWEEN STRINGERS 20R-21R LEVEL 2 CORROSION CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-828-A01.SDR COEA2020032000000Failsafe · corrodedWO 209330 NR 100010 HEAVY CHECK COE/MAJOR REPAIR: FRAME 14 FAIL SAFE HAS LEVEL 2 CORROSION, STRINGER 16R-18R. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-817-A01.SDR COEA2020031302801Stringer Clip · corrodedWO 209330 NR 200023 HEAVY CHECK COE/MINOR REPAIR: STRINGER 13L CLIP AT FRAME 32 HAS LEVEL 2 CORROSION ON TOP AND BOTTOM SIDES. CORRECTIVE ACTION: REPLACED CLIP WITH OEM PART.SDR COEA2020030401801Stringer · corrodedWO 209330 NR 200038 HEAVY CHECK COE/MAJOR REPAIR: STRINGER 6L HAS LEVEL 2 CORROSION BETWEEN FRAMES 19-20. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-824-A01.SDR COEA2018011801801Floorbeam · preloadedFLOORBEAM 38 EXCESSIVELY PRELOADED AGAINST FRAME AND INTERCOSTAL. REPAIR IAW SRM 53-00-00-300-856-A01.SDR COEA2017123009801Access Panel · corrodedFRETTING DAMAGE ON THE LT WING REMOVABLE PANEL LANDING FOR ACCESS PANEL 522CT CORRODED. REPAIRED IAW DO/TS-4809/07.4337, ISSUE E.SDR COEA2017123008801Access Panel · damagedHEAVY CHECK COE/MAJOR REPAIR: FRETTING DAMAGE ON RT WING REMOVABLE PANEL LANDING FOR ACCESS PANEL 622CT. LEVEL 2 CORROSION. REPAIR PER SRAS DO/TS-4809/07...4337 ISSUE E DATED 1/30/2018.SDR COEA2018020607801Access Panel · damagedHEAVY CHECK COE/MAJOR REPAIR: FRETTING DAMAGE ON LT WING REMOVABLE PANEL LANDING FOR ACCESS PANEL 521DT. LEVEL 2 CORROSION. REPAIR PER SRAS DO/TS-4809/07...4337 ISSUE E.SDR COEA2017122912801Frame · corrodedFRAME 38, AFT SIDE, BETWEEN STRINGERS 20L AND 21L, CORRODED UNDER THE FAIL SAFE. REPAIRED THE FRAME IAW SRM 536140-300-814-A01.SDR COEA2017122911801Skin · corrodedINTERNAL FUSELAGE SKIN HAD CORROSION UNDER THE BLANKET STANDOFF, FRAMES 14 - 15, STRINGERS 6R - 7R. REPAIRED IAW ES-533/16.984, ISSUE B.SDR COEA2017122910801Skin · corrodedINTERNAL FUSELAGE SKIN HAS CORROSION UNDER THE BLANKET STANDOFF, FRAMES 14 - 15, STRINGERS 8R - 9R. REPAIRED IAWES-533/16.9984, ISSUE B.SDR COEA2018020606801Seat Track · gougedHEAVY CHECK COE/MAJOR REPAIR: LT OUTBOARD SEAT TRACK BETWEEN FRAMES 24-25 IS GOUGED. REPAIR PER SRM 530000-300-853-A01.SDR COEA2018020605Stringer · crackedSTRINGER 1AL CRACKED AT FRAME 15 DRAIN HOLE. REPAIRED THE STRINGER IAW SRM 53-00-00-300-824-A01.SDR COEA2018020604Stringer · crackedWO 179311 NR 200023 HEAVY CHECK COE/MAJOR REPAIR: L/H STRINGER 1 CRACKED AT FRAME 15 DRAIN HOLE. CORRECTIVE ACTION: REPAIR IAW ATR72 SRM 530000-300-824-A01.SDR COEA2017122813801Skin · corrodedINTERNAL FUSELAGE SKIN HAD CORROSION UNDER THE STANDOFF, AFT OF FRAME 31, BETWEEN STRINGERS 10R-11R. REPAIRED SRAS ES-531/16.9972, ISSUE B.SDR COEA2017122803801Stringer · crackedSTRINGER 2AR CRACKED AFT OF FRAME 20. THE STRINGER WAS REPAIR IAW SRM 53-00-00-300-824-A01.SDR COEA2017122802801Strap · corrodedINTERNAL FUSELAGE SKIN STRAP HAS LEVEL 2 CORROSION FWD AND AFT OF FRAME 33, BETWEEN STRINGERS 12 - 13R. REPAIRED IAW ES-121/18.12361.SDR COEA2017122801801Skin · corrodedINTERNAL FUSELAGE SKIN HAS LEVEL 2 CORROSION AT FRAMES 33 - 34, STRINGERS 12 - 13R. REPAIRED IAW SRAS ES-121/18.12361.SDR COEA2016120553801Ovrspeed Limiter · failedDURING CLIMB, THE CREW NOTICED THE NR 1 ENGINE WAS HAVING TORQUE FLUCTUATIONS AND SURGES. THE CREW ELECTED TO RETURN TO DEPARTURE. THE AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED PROPELLER OVERSPEED GOVERNOR. OPS CHECKED GOOD.SDR COEA2016072552801Adc · failedPASSING THROUGH APPROX. 7000FT, THE NR 1 ENGINE SURGED THROUGH APPROX. 95%. CREW ELECTED TO RETURN TO ANC, NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: COULD NOT DUPLICATE DURING ENGINE RUNS. OCF PERFORMED TO MONITOR ALL ENGINE PARAMETERSSDR COEA2016012950801Splice Plate · damagedHEAVY CHECK COE & MAJOR REPAIR. DAMAGE TO FWD PRESS BULKHEAD SPLICE PLATE AT STIFFENER 3LT. REPAIRED IAW SRAS CE 437 16 10002 DATED 2 25 16.SDR COEA2016011726801Doubler · corrodedHEAVY CHECK COE & MAJOR REPAIR. LEVEL 2 CORROSION UNDER AFT AVIONICS COMPARTMENT DOOR SEAL RETAINER AFT INTERNAL & EXTERNAL SIDE OF FLANGE. REPAIR IAW SRAS CE 443 16 9954 DATED 2 17 16.SDR COEA2016011649801Skin · damagedHEAVY CHECK COE & MAJOR REPAIR. FUSELAGE CROWN HAS TWO CREASES, BETWEEN FRAMES 37 - 38, ABOVE AFT CARGO DOOR RAIN TROUGH. REPAIR IAW SRAS S536R0259 10017 DATED 2 26 16.SDR COEA2016011648801Skin · corrodedDURING HEAVY CHECK, FUSELAGE LT LATERAL UPPER SKIN PANEL HAS TWO CREASES, BETWEEN FRAMES 37 - 38, ABOVE AFT CARGO DOOR RAIN TROUGH. REPAIRED IAW SRAS S536R0259 10017. MAJOR REPAIR.SDR COEA2016010747801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL, BETWEEN FRAMES 15 - 16, STRINGER 7 - 8 FWD SIDE. REPAIR IAW SRAS ES 533 16 9984 DATED 2 25 16.SDR COEA2016010746801Strap · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL STRAP, BETWEEN FRAMES 15 - 16, STRINGER 8 - 9 AFT SIDE. REPAIR IAW SRAS ES 533 16 9984 DATED 2 25 2016.SDR COEA2016010745801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL, BETWEEN FRAMES 15 - 16, STRINGER 8 - 9. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 16.SDR COEA2016010744801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL, BETWEEN FRAMES 15 - 16, STRINGER 10 - 11. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 201.SDR COEA2016010735801Fitting · wornHEAVY CHECK COE & MAJOR REPAIR. LT ENG CTR COWL, FWD ATTACH POINT WORN ON OTBD LUG. REPAIR IAW SRAS CE 364 16 9961 DATED 2 8 2016.SDR COEA2016010734801Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL AFT OF FRAME 22, BETWEEN STRINGER 10 - 10A. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 2016.SDR COEA2016010733801Strap · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE, RT UPPER SKIN PANEL STRAP, BETWEEN FRAMES 15 - 16, STRINGER 7 - 8. REPAIR IAW SRAS ES-533 16 9984 DATED 2 25 16.SDR COEA2016010730801Skin · corrodedWO 155295 NR 200123 HEAVY CHECK COE & MAJOR REPAIR. LEVEL 2 CORROSION ON INTERNAL SKIN, BETWEEN RT FRAMES 31 - 32, STRINGERS 8 - 10, AFT OF WINDOW CUT OUT. REPAIR IAW SRAS ES 531 16 9972 DATED 2 23 16.SDR COEA2016010729801Skin · corrodedHEAVY CHECK COE & MAJOR REPAIR. LEVEL 2 CORROSION ON INTERNAL SKIN, BETWEEN RT FRAMES 31 - 32, STRINGERS 8 - 10, FWD OF WINDOW CUT OUT. REPAIRED IAW SRAS ES 531 16 9972 DATED 2 23 2016.SDR COEA2016010706801Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE RT UPPER PANEL, FRAME 15 - 16, STRINGER 9 - 10. DOUBLER REPAIR IAW SRM 533124-300-807-A01.SDR COEA2016010705801Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING FWD FUSELAGE RT UPPER PANEL, FRAME 16 - 17, STRINGER 10A - 11. DOUBLER REPAIR IAW SRM 530000-300-803-A01.SDR COEA2016010638801Floor Panel · corrodedHEAVY CHECK COE & MINOR REPAIR. COCKPIT FLOOR PANEL 211FF HAS AREAS OF SURFACE CORROSION, LEVEL 2. REPLACED WITH OEM PANEL.SDR COEA2016010628801Intake · corrodedHEAVY CHECK COE & MINOR REPAIR. AREAS OF LEVEL 2 CORROSION ON RT WING AIR INTAKE ASSEMBLY 623DB. REPLACED WITH OEM ASSEMBLY.SDR COEA2016010551801Bulkhead · dentedHEAVY CHECK COE & MAJOR REPAIR. FWD SIDE OF FWD PRESS BULKHEAD IS DENTED AT UPPER LT PORTION OF BULKHEAD NEAR RADOME LATCH. REPAIR IAW SRAS CE 437 16 10002 DATED 2 25 16.
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