N917FX
Service difficulty reports · 142
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 = 'N917FX' 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 = 'N917FX' 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 COEA2026032001917Warning Message · illuminatedFLIGHT 202, BZN - GEG, ABORTED TAKEOFF DUE TO STICK SHAKER ACTIVATED ON RUNWAY, MOMENTARY LOSS OF CPT'S BRAKES AND AIRCRAFT LISTING TO THE RIGHT. OPS TEST OF ANTISKID CHECKS GOOD. OPS TEST OF STALL WARNING SYSTEM AND STICK PUSHER GOOD. VISUAL INSPECTION OF THSDR COEA2024072610917Pan · dentedWO 254917 NR 800003 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: L/H AFT CARGO DOOR LOWER AFT CORNER OF PAN HAS A DENT. CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 521100-300-812-A01.SDR COEA2024072609917Skin · dentedWO 254917 NR 200105 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: R/H EXTERNAL FUSELAGE BETWEEN FRAMES 19-20 AT STRINGER 11R HAS A DENT. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00240251_01...23669 ISSUE A, DATED 6/28/2024.SDR COEA2024072608917Stiffener · corrodedWO 254917 NR 200093 HEAVY CHECK COE/MINOR REPAIR DISCREPANCY: FWD PRESSURE BULKHEAD FWD SURFACE MIDDLE STIFFENER HAS LEVEL 2 CORROSION AT UPPER END. CORRECTIVE ACTION: REPLACED STIFFENER PER ATR42 SRM 51-25-01 AND 51-25-04.SDR COEA2024072607917Seat Track · corrodedWO 254917 NR 200083 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: L/H OUTBOARD SEAT TRACK HAS LEVEL 2 CORROSION BETWEEN FRAMES 34-35. CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 530000-300-856-A01.SDR COEA2024072606917Skin · corrodedWO 254917 NR 200081 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: INTERNAL FUSELAGE HAS LEVEL 2 CORROSION AT STRINGER 10AL BETWEEN FRAMES 20-21 UNDER INSULATION STANDOFF. CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 530000-300-803-A01.SDR COEA2024072502917Web · corrodedWO 254917 NR 100014 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: FWD CARGO DOOR THRESHOLD VERTICLE WEB HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER ATR SRM 533780-300-803-A01.SDR COEA2024072501917Floorbeam · corrodedWO 254917 NR 100014 HEAVY CHECK COE/MINOR REPAIR DISCREPANCY: FRAME 14 FLOORBEAM HAS LEVEL 2 CORROSION ON THE AFT SIDE L/H OUTBOARD END. CORRECTIVE ACTION: REPAIRED PER SRAS ES-00241796_01...23805 ISSUE A, DATED 7/5/2024.SDR COEA2024072605917Skin · corrodedWO 254917 NR 200071 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: INTERNAL FUSELAGE ABOVE STRINGER 6R BETWEEN FRAMES 20-21 HAS LEVEL 2 CORROSION UNDER INSULATION STANDOFF. CORRECTIVE ACTION: REPAIR PER ATR42 SRM 530000-300-803-A01.SDR COEA2024072504917Stringer · corrodedWO 254917 NR 200068 HEAVY DUTY COE/MAJOR REPAIR: DISCREPANCY: INTERNAL FUSELAGE STRINGER 6R HAS LEVEL 2 CORROSION FROM FRAMES 14-23. CORRECTIVE ACTION: REPAIRED PER ATR42 SRM 530000-300-826- A01.SDR COEA2024072503917Window Frame · corrodedWO 254917 NR 200066 HEAVY CHECK COE/MINOR REPAIR DISCREPANCY: L/H FRAME 19-20 WINDOW FRAME HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FRAME PER ATR42 SRM 51-25-04 AND 51-21-27.SDR COEA2023081001917Gcu · faultedFLT 7826, ENROUTE FCA-GTF AIR TURNBACK/DISCREPANCY: ON CLIMB OUT, THE #1 DC GENERATOR FAULTED. THE AIRCRAFT WAS RETURNED TO FCA. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE TROUBLESHOT AND REPLACED THE #1 DC GENERATOR CONTROL UNIT.SDR COEA2022081817917Stringer · crackedWO 238445 NR 200070 HEAVY CHECK COE/MAJOR REPAIR: STRINGER 1L IS CRACKED AT FRAME 34. CORRECTIVE ACTION: REPAIR PER ATR42 SRM 53-00-00-300-826-A01.SDR COEA2022081614917Skin · corrodedWO 238445 NR 200063 HEAVY CHECK COE/MAJOR REPAIR: INNER SKIN HAS SPOTS OF INSULATIONS STANDOFF LEVEL 2 CORROSION FRAMES 28-29 STRINGER 2R-3R. CORRECTIVE ACTION: REPAIR PER SRAS ES_0161784_01...19268 ISSUE A, DATED 8/5/2022.SDR COEA202207150691Panel · corrodedWO 238445 NR 200059 HEAVY CHECK COE/MAJOR REPAIR: INNER SKIN HAS SPOTS OF INSULATIONS STANDOFF LEVEL 2 CORROSION FRAMES 28-29 STRINGER 1L-2L. CORRECTION ACTION: REPAIR PER ATR42 SRM 530000-300-864-A01.SDR COEA2022080911917Panel · corrodedWO 238445 NR 600016 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUTOUT BETWEEN RIBS 4R AND 5R PANEL 622CT FLANE AND FOIL HAVE FRETTING DAMAGE. CORRECTIVE ACTION: REPAIR PER SRAS DO/TS- 4504/08...4888 ISSUE F, DATED 8/3/2022.SDR COEA2022080910917Panel · corrodedWO 238445 NR 500016 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUTOUT BETWEEN RIBS 4L AND 5L PANEL 522CT FLANGE AND FOIL HAVE FRETTING DAMAGE. CORRECTIVE ACTION: REPAIR PER SRAS DO/TS-4504/08...4888 ISSUE F, DATED 8/3/2022.SDR COEA2022080909917Panel · corrodedWO 238445 NR 500015 HEAVY CHECK COE/MAJOR REPAIR: UPPER CENTER WING CUTOUT BETWEEN RIBS 1L AND 2L PANEL 521DT FLANGE AND FOIL HAVE FRETTING DAMAGE. CORRECTION ACTION: REPAIR PER SRAS DO/TS...4504/08...4888 ISSUE F.SDR COEA2022081616917Attach Bracket · bentWO 238445 NR 100032 HEAVY CHECK COE/MAJOR REPAIR: INTERIOR FUSELAGE AFT OF FRAME 24 L/H LONGITUDINAL FLOORBEAM ATTACHMENT BRACKET IS BENT AND BOWED. CORRECTIVE ACTION: REMOVED AND REPLACED ATTACH BRACKET IAW EMPIRE AIRLINES E.O. 5315-01.SDR COEA2022081615917Attach Bracket · bentWO 238445 NR 100032 HEAVY CHECK COE/MAJOR REPAIR: INTERIOR FUSELAGE AFT OF FRAME 24 L/H LONGITUDINAL FLOORBEAM ATTACHMENT BRACKET IS BENT AND BOWING. CORRECTIVE ACTION: REMOVED AND REPLACED ATTACH BRACKET IAW EMPIRE AIRLINES E.O. 5315-01.SDR COEA2022081012917Bulkhead · corrodedWO 238445 NR 200028 HEAVY CHECK COE/MAJOR REPAIR: FWD PRESSURE BULKHEAD HAS MULTIPLE AREAS OF FRETTING AT THE RADOME BONDING POINTS. LEVEL 2 CORROSION CORRECTIVE ACTION: REPAIR PER SRAS ES_0162057_01...19253 ISSUE A, DATED 8/5/2022.SDR COEA2022080908917Mount · chafedWO 238445 NR 400024 HEAVY CHECK COE/MAJOR REPAIR: R/H NACELLE FWD MOUNT TUBE 1 HAS CHAFE DAMAGE AFT OF THE FWD FITTING. CORRECTIVE ACTION: CORRECTIVE ACTION: REPAIR PER SRAS ES_0161869-01...19177 ISSUE A, DATED 8/4/2022.SDR COEA2022080907917Floorbeam · corrodedWO 238445 NR 100027 HEAVY CHECK COE/MAJOR REPAIR: INTERIOR FUSELAGE FLOORBEAM 15 UPPER SURFACE BETWEEN IB SEAT TRACKS HAVE LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIR PER ATR42 SRM 530000-300-846-A001.SDR COEA2022071506917Stringer · crackedWO 238445 NR 200019 HEAVY CHECK COE/MAJOR REPAIR: FRAME 26 SHEAR TIE STRINGER 12R-13R IS CRACKED. CORRECTIVE ACTION: REPLACED SHEAR TIE WITH NEW PER ATR42 SRM 51-25-01.SDR COEA2022071205917Stringer · dentedWO 238445 NR 200047 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE STRINGER 2L HAS A DENT BETWEEN FRAMES 22-23. CORRECTIVE ACTION: FABRICATION OF STRINGER IAW SRM 530000-300-826-A01.SDR COEA2022070604917Floorbeam · crackedWO 238445 NR 100033 HEAVY CHECK COE/MAJOR REPAIR: INTERIOR FUSELAGE AFT OF FRAME 21 R/H LONGITUDINAL FLOORBEAM CRACKED AT ATTACHMENT. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.SDR COEA2022070603917Floorbeam · crackedWO 238445 NR 100025 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM IS CRACKED FRAMES 26-27. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.SDR COEA2022070602917Floorbeam · crackedWO 238445 NR 100024 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM 33-34 IS CRACKED. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.SDR COEA2022070601917Floorbeam · crackedWO 238445 NR 100023 HEAVY CHECK COE/MAJOR REPAIR: R/H LONGITUDINAL FLOORBEAM 38-39 IS CRACKED. CORRECTIVE ACTION: REPAIRED PER EMPIRE AIRLINES E.O. 5315-01.SDR COEA2021052101917Adc · faultedFLIGHT 7771, BZN-GTF/AIR TURNBACK DISCREPANCY: CAPTAIN VMO FLAGGED ON TAKEOFF, 15KTS DIFFERENCE ON STANDBY ASI COMPARED TO PRIMARYS. TORQUE BUGS FELL TO 20%. TCAS FAIL ON CAPTAIN SIDE. AIRCRAFT WAS RETURNED TO BZN. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACSDR COEA2020062308917Floorbeam · corrodedFLOORBEAM 10 FLOORBOARD SUPPORT HAS LEVEL 2 CORROSION ON UPPER SURFACE. REPLACED WITH OEM PART.SDR COEA2020060902917Stringer · crackedSTRINGER 1L IS CRACKED AT FRAME 17 DRAIN HOLE. REPAIRED PER SRM 53000-300-826-A01.SDR COEA2020062409917Stiffener · corrodedHEAVY CHECK COE/MAJOR REPAIR: FWD PRESSURE BULKHEAD LT MOST OUTBOARD STIFFENER HAS LEVEL 2 CORROSION NEAR THE TOP END. CORRECTIVE ACTION: REPAIRED PER SRM 531110-300-807-A01.SDR COEA2020061806917Skin · corrodedHORIZONTAL STABILIZER L/H LEADING EDGE LOWER ATTACH FLANGE INNER SURFACE HAD CORROSION. REPAIRED PER SRAS CETS-1484/16...10549 ISSUE B, DATED 6/8/2020.SDR COEA2020061805917Fitting · corrodedL/H ELEVATOR TIP FITTING HAD CORROSION. REPLACED FITTING WITH OEM PART.SDR COEA2020061603917Skin Panel · corrodedHEAVY CHECK COE/MAJOR REPAIR: FORWARD FUSELAGE RT UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 16-17 AND STRINGERS 10AR-11R. REPAIRED PER SRM 530000-300-803-A01.SDR COEA2020060301917Skin Panel · nickedHEAVY CHECK COE, MAJOR REPAIR. FORWARD FUSELAGE RT LOWER SKIN PANEL HAS MULTIPLE NICKS BETWEEN FRAMES 13-14 AND STRINGERS 14R-15R. CORRECTIVE ACTION REPAIRED PER SRM 530000-300-805-A01.SDR COEA2020062307917Floorbeam · corrodedHEAVY CHECK COE/MAJOR REPAIR: FLOORBEAM 17 HAS LEVEL 2 CORROSION AT THE LT OUTBOARD END. REPAIRED PER SRM 530000-300-852-A01.SDR COEA2020061804917Stringer · crackedWO 213629 NR 200018 HEAVY CHECK COE/MAJOR REPAIR: STRINGER 1AR IS CRACKED BETWEEN FRAMES 20-21. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-826-A01.SDR COEA2018071308917Stringer · corrodedHEAVY CHECK COE/MAJOR REPAIR: LEVEL 2 CORROSION ON STRINGER 18R BETWEEN FRAMES 14-20. REPAIRED PER SRM 530000-300-826-A01.SDR COEA2018070603917Floor Support · crackedHEAVY CHECK COE/MAJOR REPAIR: LT LONGITUDINAL FLOORBEAM CRACKED AFT OF FRAME 23. REPAIRED PER EO 5315-01.SDR COEA2018070602917Floor Support · crackedHEAVY CHECK COE/MAJOR REPAIR: LT LONGITUDINAL FLOORBEAM IS CRACKED FWD OF FRAME 19. REPAIRED PER EO 5315-01.SDR COEA2018070601917Stringer · corrodedHEAVY CHECK COE/MAJOR REPAIR: LEVEL 2 CORROSION ON STRINGER 16R BETWEEN FRAMES 34-35. REPAIRED PER SRM 530000-300-828-A01.SDR COEA2018071307917Panel · corrodedHEAVY CHECK COE/MAJOR REPAIR: RT WING UPPER REMOVABLE PANEL HAS FRETTING DAMAGE AT LANDING FOR ACCESS PANEL 622CT. LEVEL 2 REPAIRED PER DO/TS-4504/08...4888 ISSUE D, DATED 7/2/2018.SDR COEA2018071306917Panel · corrodedHEAVY CHECK COE/MAJOR REPAIR, LT WING UPPER REMOVABLE PANEL HAS FRETTING DAMAGE AT LANDING FOR ACCESS PANEL 521DT. LEVEL 2 REPAIRED PER SRAS DO/TS-4504/08.4888 ISSUE D, DATED 7/2/2018.SDR COEA2018071305917Panel · corrodedHEAVY CHECK COE/MAJOR REPAIR, LT WING UPPER REMOVABLE PANEL HAS FRETTING DAMAGE AT LANDING FOR ACCESS PANEL 522CT. LEVEL 2 REPAIRED PER SRAS DO/TS-4504/08...4888 ISSUE D, DATED 7/2/2018.SDR COEA2018060504917Seat Track · gougedHEAVY CHECK COE/MAJOR REPAIR, RT OUTBOARD SEAT TRACK GOUGED BETWEEN FRAMES 32-33. REPAIRED PER SRM 530000-300-856-A01.SDR COEA2018060309917Fitting · nickedHEAVY CHECK COE/MAJOR REPAIR, LT MLG ACTUATOR FITTING HAS NICKS AND ALL 4 HOLES HAVE SLIGHT WEAR. REPAIRED PER SRAS ES-3162/18...13189 DATED 7/13/2018.SDR COEA2017051602917Unknown · odorCREW REPORTED A SLIGHT ELECTRICAL BURNING ODOR IN THE COCKPIT. COMING THROUGH AT 11,000FT. SEEMED TO GO AWAY BELOW 7000FT. AFTER EXTENSIVE TROUBLESHOOTING, MAINTENANCE WAS UNABLE TO REPRODUCE THE ISSUE ON THE GROUND AND COULD NOT FIND ANY SIGNS OF ELECTRICASDR COEA2017020701917Adc · faultedNR 1 AIR DATA COMPUTER FAULTED. THE CREW ELECTED TO RETURN TO DEPARTURE, NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AIR DATA COMPUTER. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
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