N117SY
Service difficulty reports · 28
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 = 'N117SY' 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 = 'N117SY' 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 SWIA2026080676958Seat Track · corrodedFRAMES 17-21, Y + 10 RT SEAT TRACK CORRODED AT MULTIPLE LOCATIONS. R & R THE SEAT TRACK IAW SRM 51-40-08. NO FURTHER ACTION REQUIRED.SDR SWIA2026080676957Seat Track · corrodedFWD WET AREA, LT SEAT TRACK AT FR 14-18, Y - 10" CORRODED AT MULTIPLE LOCATIONS. R & R THE FWD WET AREA SEAT TRACK IAW SRM 51-40-08.SDR SWI2025F01075Flap Track · out of limitsRH WING FLAP TRACK 2 OB HAS DEPTH REDUCTION THAT EXCEEDS 0.549INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED THE RH INBOARD FLAP TRACK #2 O/B REF. AMM 57-54-23. ASSET#: TC1-604 CAL: 03/06/26, ASSET#: TC2-10468 CAL: 10/07/25, SDR SWI2025F01074Flap Track · out of limitsLH WING FLAP TRACK 2 OB HAS DEPTH REDUCTION THAT EXCEEDS 0.549 INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED THE LH INBOARD FLAP MAIN TRACK #2 O/B REF. AMM 57-54-23. ASSET#: TC1-609 CAL: 03/06/26, ASSET#: TC2-10406 CAL: 06/19SDR SWI2025F01073Flap Track · out of limitsLH WING FLAP TRACK 3 OB HAS DEPTH REDUCTION THAT EXCEEDS 0.578 INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED THE LH OUTBOARD FLAP TRACK #3 O/B REF. AMM 57-57-33. ASSET#: TC1-604 CAL: 03/06/26, ASSET#: TC2-10468 CAL: 10/07/25,SDR SWI2025F01072Flap Track · out of limitsLH WING FLAP TRACK 3 IB HAS DEPTH REDUCTION THAT EXCEEDS 0.578 INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025) REMOVED AND REPLACED THE LH OUTBOARD FLAP TRACK #3 I/B REF. AMM 57-57-33. ASSET#: TC1-604 CAL: 03/06/26, ASSET#: TC2-10468 CAL: 10/07/25SDR SWI2025F01071Flap Track · out of limitsRH WING FLAP TRACK 3 OB HAS DEPTH REDUCTION THAT EXCEEDS 0.578 INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED THE RH OUTBOARD FLAP TRACK #3 O/B REF. AMM 57-57-33. ASSET#: TC1-604 CAL: 03/06/26, ASSET#: TC2-10468 CAL: 10/07/25SDR SWIA2025081200721Flap Track · out of limitsRH WING FLAP TRACK 3 IB HAS DEPTH REDUCTION THAT EXCEEDS 0.578 INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED THE RH OUTBOARD FLAP TRACK #3 I/B REF. AMM 57-57-33. ASSET#: TC1-604 CAL: 03/06/26, ASSET#: TC2-10468 CAL: 10/07/25SDR SWIA2025081100721Seat Track · gougedMAIN CABIN LEFT OUTBOARD SEAT TRACK SECTION 34/43 - 59 HAS GOUGING AT FRS 45, 48, 50, 55, 57 AND 59. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED MAIN CABIN LEFT OUTBOARD (LATERAL) SEAT TRACK SECTION FR43 - 59. REF. EMB SRM 51-40-08. RESTORED SURFACE PROTECTIOSDR SWIA2025081100717Seat Track · gougedRH LATERAL SEAT TRACK HAS MULTIPLE GOUGES AND CORROSION AS MARKED FR 16- FR 20SDR SWIA20240514Warning Message · multiple failLOSS OF FMS 1 AND 2 ON ARRIVAL. LOSS OF AUTOTHROTTLES. LOSS OF ALL NAVIGATION. LOSS OF ALL FLIGHT PLAN INFO. (FLIGHT 4653 FILED CLOSED)POWERED UP AIRCRAFT AND ALLOWED SYSTEMS TIME TO INITIALIZE. THERE WERE NO CURRENT MESSAGES PERTAINING TO FMS 1, FMS2, AT, IRSSDR SWIA202405150004Mau · trippedLOSS OF FMS 1 AND 2 ON ARRIVAL. LOSS OF AUTOTHROTTLES. LOSS OF ALL NAVIGATION. LOSS OF ALL FLIGHT PLAN INFO. (FLIGHT 4653 FILED OPEN)POWERED UP AIRCRAFT AND ALLOWED SYSTEMS TIME TO INITIALIZE. THERE WERE NO CURRENT MESSAGES PERTAINING TO FMS 1, FMS2, AT, IRS'SSDR SWIA2024012200019Receptacle · sparksRAMP TRIED TO PLUG IN AC POWER AND WE SAW A A FLASH OF LIGHT AND ELECTRICAL SMOKE FILLING THE AIR. WE ALSO HEARD A LOUD SOUND FROM THE PANEL. (FLIGHT 4655 FILED CLOSED)EXTERNAL AC POWER SYSTEM DEFERRAL PREVIOUSLY COMPLIED WITH, PLEASE SEE EAML 1281939 AND 1282SDR SWIA202304240001Unknown · warning messageBLEED 1 LEAK IN CRUISE AT FL340. RAN QRH. MESSAGE DID NOT EXTINGUISH; HOWEVER IT FLUCTUATED ON AND OFF THE REMAINDER OF FLIGHT. ASSOCIATED BLEED 2 FAIL CAUTION MESSAGE AFTER QRH ACCOMPLISHED. (FLT 5401 FILED CLOSED)TROUBLESHOOT THE BLEED 1 LEAK CAUTION MESSAGESDR SWIA202265937None · corrodedCORROSION, ON END OF RH INBOARD SEAT TRACK BETWEEN FRAME 84 AND 85. (C-CHECK RO 6/14/2022) PERFORMED SPICE ON END OF RH INBOARD SEAT TRACK BETWEEN FRAME 84 AND 85 REF ETD2022-170-018629. SEE CONTINUATION CARD FOR WORK PERFORMED. REPAIR PART WEIGHT: 222.SDR SWIA202265936None · corrodedCORROSION, AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE CENTER AND RH SHEAR PANELS. (C-CHECK RO 6/14/2022) REMOVED AND REPLACED AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 87 REF SRM 51-40-08. RESTOSDR SWIA202265935None · corrodedCORROSION AROUND SCREW HOLE L/H TRACK AT FR 19 (C-CHECK RO 6/14/2022) REMOVED CORROSION FROM AROUND SCREW HOLE L/H TRACK AT FR 19 BY CUTOUT, FILLER AND DOUBLER FABRICATION AND INSTALLATION REF SRM 53-10-10/REPAIR01P. REFERENCE CARD FOR WORK PERFORMED. RSDR SWIA202265934None · corrodedCROSS BEAM CORRODED FR 17 CENTER BETWEEN L/H AND R/H TRACK BEAMS (C-CHECK RO 6/14/2022) REMOVED CORROSION ON FR 17 CROSS BEAM BETWEEN L/H AND R/H TRACK BEAMS BY PERFORMING CUTOUT, FILLER AND DOUBLER INSTALLATION REF SRM 53-00-10/REPAIR03P. REPAIR DOUBLESDR SWIA202265933None · corrodedR/H TRACK BEAM CORRODED FWD END OF SEAT TRACK AT FRAME 17 (C-CHECK RO 6/14/2022) REMOVED AND REPLACED R/H SEAT TRACK BEAM FR12-FR20 REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.SDR SWIA202265932None · corrodedSHEAR CLIP AT FRAME 88 BETWEEN STRINGERS 26R-27R CORRODED (C-CHECK RO 6/14/2022) REMOVED AND REPLACED SHEAR CLIP FR 88 STRINGER 26R-27R REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, 51-23-06. APPLIED C.I.C. REF CPM 51-25-SDR SWIA202265931None · corrodedSHEAR CLIP AT FRAME 85 BETWEEN STRINGERS 26R-27R CORRODED (C-CHECK RO 6/14/2022) REMOVED AND REPLACED SHEAR CLIP FR 85 STRINGER 26R-27R REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, 51-23-06. APPLIED C.I.C. REF CPM 51-25-SDR SWIA2020070650921Skin · dentedTWO DENTS FOUND OUT-OF-LIMITS ON THE LEFT SIDE FORWARD FUSELAGE SKIN PANEL LOCATED AT FRAME 11 AND BETWEEN STRINGERS 17L AND 18L. DENT FORWARD OF FRAME 11 MEASURES 3.84"L X 3.18"W X .060"D WITH A CREASE. DENT AFT OF FRAME 11 MEASURES 2.16"L X 1.45"W X .033"D.SDR SWIA2020060550921Skin Panel · dentedTWO DENTS FOUND OUT-OF-LIMITS ON THE LEFT SIDE FORWARD FUSELAGE SKIN PANEL LOCATED AT FRAME 11 AND BETWEEN STRINGERS 17L AND 18L. DENT FORWARD OF FRAME 11 MEASURES 3.84"L X 3.18"W X .060"D WITH A CREASE. DENT AFT OF FRAME 11 MEASURES 2.16"L X 1.45"W X .033"D. SDR SWIA2019012145457Pressure Switch · failedWHILE IN CRUISE WE RECEIVED A PRKG BRK NOT RELEASED MESSAGE. PERFORMED QRH, MESSAGE DID NOT CLEAR. DECLARED EMERGENCY. (FLT 5996) CLOSED REMOVED AND REPLACED NR 2 PARKING BRAKE PRESSURE SWITCH. OPS CHECK GOOD. NO FURTHER DEFECTS IAW AMM.SDR SWIA201541403Retainer · damagedDAMAGE TO PAX DOOR SEAL RETAINERS. REPAIRED THE SEAL RETAINERS.SDR SWIA201541402Retainer · damagedDAMAGE TO PAX DOOR. REPAIRED THE DOOR SEAL RETAINERS.SDR SWIA201440011Battery Pack · failedCEILING EMERGENCY LIGHT NR 4 NOT WORKING. R & R NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM.SDR SWIA201439904Blade · vibrationDURING FLIGHT, THE NR 1 ENGINE LOW PRESSURE VIBRATION REACHED 4.0 CAUTION AND FLUCTUATED BETWEEN 3.7 AND 4.0 ENTIRE FLIGHT. DIVERTED, REMOVED NR 1, 25, 26 FAN BLADES PINS OF LT ENGINE AND CLEANED AND INSPECTED AND LUBRICATED IAW AMM. PERFORMED VIBRATION CHEC
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