N114SY
Service difficulty reports · 32
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 = 'N114SY' 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 = 'N114SY' 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 SWIA202601080006Skin · damagedDURING LIGHTNING STRIKE INSPECTION FOUND 1 BURNED RIVET ON FR24 1ST RIVET BELOW STR22L. BURN DAMAGE IS 3/8 L X 3/8 W X 0.073 D AND OUT OF LIMITS PER SRM 53-00-00 REPAIR 03.DAMAGE IS OUT OF LIMITS AND THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR RSDR SWIA2026010700006Skin · damagedDURING LIGHTNING STRIKE INSPECTION FOUND 1 BURNED RIVET ON FR24 1ST RIVET BELOW STR22L. BURN DAMAGE IS 3/8 L X 3/8 W X 0.073 D AND OUT OF LIMITS PER SRM 53-00-00 REPAIR 03.DAMAGE IS OUT OF LIMITS AND THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR RSDR SWIA2025122307Stay · faultedLG LEVER DISAGREE MESSAGE AFTER TAKEOFF AND RETRACTION ATTEMPT.RIGHT MAIN DID NOT RETRACT, COULD HEAR AND FEEL RIGHT MAIN WAS STILL DOWN. QRH PROCEDURE FOLLOWED. GEAR CONFIRMED DOWN AND GREEN AS PER QRH PROCEDURE. (FLIGHT 5367) PERFORMED GEAR SWINGS IAW AMMSDR SWIA2025120800007Warning Message · illuminatedLG LEVER DISAGREE MESSAGE AFTER TAKEOFF AND RETRACTION ATTEMPT. RIGHT MAIN DID NOT RETRACT, COULD HEAR AND FEEL RIGHT MAIN WAS STILL DOWN. QRH PROCEDURE FOLLOWED. GEAR CONFIRMED DOWN AND GREEN AS PER QRH PROCEDURE. (FLIGHT 5367 - OPENSDR SWIA20250303206Seat Track · gougedRH I/B SEAT TRACK GOUGED AT FRAMES 46, 48, 50, 53, 55 AS MARKED (C-CHECK RO 3/1/2025) REMOVED AND REPLACED RH I/B SEAT TRACK FR43-59 REF. EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.O.E.M. PART INSTALLED NO CHANGE TO WEIGHT AND BALANCEAVISDR SWI2025F00277Shear Tie · corrodedCORROSION ON SHEAR CLIP AT FR88 BETWEEN STGR 28R-27R AS MARKED. (C-CHECK RO 3/1/2025) REMOVED AND REPLACED SHEAR CLIP AT FR88 BETWEEN STGR 28R-27R REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. REPLACED DAMAGED SHEAR CLIP WITH OEM REPLSDR SWIA20250303204Beam · corrodedAFT PASSENGER DOOR CUTOUT LOWER BEAM HAS CORROSION AT FWD AND AFT GIRT BAR FLOOR FITTING CUTOUTS AND IN THE CENTER OF THE LOWER BEAM IN THE UPPER SURFACE. (C-CHECK RO 3/1/2025) REMOVED AND REPLACED AFT PAX DOOR LOWER BEAM WITH NEW REF. ERJ175 SRM 51-40-SDR SWI2025F00279Seat Track · corrodedFWD WET AREA RIGHT INBOARD SEAT TRACK HAS CORROSION AT FR 17, 18, 18/19, 19. (C-CHECK RO 3/1/2025) REMOVED AND REPLACED RH INBOARD SEAT TRACK FR 12-20, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED. SEE CONTINUASDR SWI2025F00278Beam · corrodedFWD PAX DOOR LOWER BEAM HAS CORROSION AS MARKED BETWEEN FR 16/17 (C-CHECK RO 3/1/2025) REMOVED AND REPLACED THE FWD PAX DOOR LOWER BEAM. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. WEIGHT AND BALANCE WERE NOT EFFECTED BY THIS WORK O.SDR SWIA20250303203Beam · corrodedFWD SERVICE DOOR LOWER BEAM HAS CORROSION AT (3) LOCATIONS AS MARKED BETWEEN FR 16/17 (C-CHECK RO 3/1/2025) REMOVED AND REPALCED THE FWD SERVICE DOOR LOWER BEAM. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. WEIGHT AND BALANCE WAS NOT SDR SWI2025F00276Rib · crackedRH H-STAB RIBS 11A AND 12A HAVE SUSPECTED CRACKS AT UPPER ATTACH POINTS. (C-CHECK RO 3/1/2025) REMOVED AND REPLACED RH HSTAB RIB 11A AND 12A WITH NEW REF. ERJ175 SRM 51-40-08, ETD2025-170-902006. REPLACED WITH OEM PART NO CHANGE IN WEIGHT AND BALANCE. SSDR SWIA20250303202Rib · crackedLH H-STAB RIB 12A HAS A SUSPECTED CRACK AT UPPER ATTACH POINT. (C-CHECK RO 3/1/2025) REMOVED AND REPLACED CRACKED LH HSTAB RIB 12A WITH NEW REF. ETD2025-170-902006, ERJ175 SRM 51-40-08. REPLACED WITH OEM PART, NO CHANGE IN WEIGHT AND BALANCE. SEE CONTINSDR SWIA20250303201Doubler · corrodedWASTE SERVICE DOOR CUTOUT ON FUSELAGE INTERNAL DOUBLER CORRODED INBOARD OF HINGE POINT (C-CHECK RO 3/1/2025) REMOVED AND REPLACED WASTE SERVICE DOOR CUTOUT ON FUSELAGE INTERNAL DOUBLE REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART NO CHANGE TO WEIGHT SDR SWI202405200414Skin · puncturedHOLE IN FUSELAGE APPROXIMATELY 1 INCH BY 1 INCH APPROXIMATELY THREE FEET TO THE RIGHT OF MCD APPROXIMATELY ONE FOOT ABOVE FLOOR LEVEL. (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28236263 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH PEMSDR SWIA202266608None · noneD; LEFT PACK FAIL MESSAGE. BURNING SMELL FROM PACK WHEN MX TRIED TO TURN ON. / C; MEL 21-51-0A / CAT: "C" DUE 10/22 / AT GATE READY TO PUSH, STARTED TO SMELL SOMETHING BURNING THEN GOT A PACK 1 FAIL. (FLIGHT #5704 FILED CLOSED) OCT 12, 2022 STATION: ORDSDR SWIA202265953None · corrodedCORROSION ON SHEAR CLIP AT FRAME 86, STRINGER 18L. (C-CHECK RO 6/16/2022) REMOVED AND REPLACE SHEAR CLIP AT FRAME 86 STRINGER 18L IAW SRM 51-40-08.RESTORED SURFACE PROTECTION REF SRM 51-23-06. REPLACEMENT WITH OEM PART NO WEIGHT CHANGES. SEE CONTINUATISDR SWIA202265952None · corrodedRH TRACK HAS CORROSION AT FRAME 16 AS MARKED (C-CHECK RO 6/16/2022) REMOVED CORROSION BY CUTOUT AND APPLIED FILLER REPAIR REF EMB SRM 53-10-10/REPAIR01P. WEIGHT OF REPAIR PARTS: 37.5G. SEE CONTINUE CARD FOR WORK PERFORMED.SDR SWIA202265951None · gougedGOUGES ON L/H FLOOR SEAT TRACK BETWEEN FR60-74 IN 2 LOCATIONS AS MARKED. (C-CHECK RO 6/16/2022) REMOVED AND REPLACED L/H FLOOR SEAT TRACK BETWEEN FR60-74 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 / NO WEIGHT CHANGE- REMOVED AND REPLSDR SWIA202265950None · gougedGOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR60-74 IN 2 LOCATIONS AS MARKED. (C-CHECK RO 6/16/2022) REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN FR60-74 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 / NO WEIGHT CHANGE DUE TO REPLACEMESDR SWIA202265949None · gougedGOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR34-60 IN 15 LOCATIONS AS MARKED. (C-CHECK RO 6/16/2022) REMOVED DAMAGE PORTION OF RH INBD SEAT TRACK FROM FR 34-47. FABRICATED, LOCATED, DRILLED AND INSTALLED NEW PORTION OF RH INBD SEAT TRACK FR 34-47. REF EMB SSDR SWIA202265948None · corrodedCORRODED SHEAR CLIP FR88 STGR 28R-29R AS MARKED (C-CHECK RO 6/16/2022) REMOVED AND REPLACED SHEAR CLIP AT FR88 STGR28R-29R IAW SRM 51-40-08. REFERENCE CARD FOR WORK PERFORMED.SDR SWIA202265947None · corrodedCORRODED SHEAR CLIP FR88 STGR 28R-27R AS MARKED (C-CHECK RO 6/16/2022) REMOVED AND REPLACE CORRODED SHEAR CLIP AT FR88 STGR 28R-27R IAW SRM 51-40-08. RESTORED SURFACE PROTECTION IAW SRM 51-23-06. REFERENCE CARD FOR WORK PERFORMED. NO CHANGE TO MRB REQUISDR SWIA202265946None · corrodedCORRODED SHEAR CLIP FR87 STGR 28R-27R AS MARKED (C-CHECK RO 6/16/2022) REMOVED AND REPLACED CORRODED SHEAR CLIP AT FR 87 STGR 28R-27R IAW SRM 51-40-08. REFERENCE CARD FOR WORK PERFORMED.SDR SWIA202265945None · corrodedCORRODED SHEAR CLIP FR87 STGR 28R-29R AS MARKED (C-CHECK RO 6/16/2022) REMOVED AND REPLACED CORRODED SHEAR CLIP AT FR87 STGR 28R-29R IAW SRM 51-40-08. REFERENCE CARD FOR WORK PERFORMED.SDR SWIA202265944None · corrodedCORRODED SHEAR CLIP FR85 STGR 28R-27R AS MARKED (C-CHECK RO 6/16/2022) REMOVED AND REPLACED SHEAR CLIP FR 85 STGR 28R-27R REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06. RESTORED CIC IAW CPM 51-25-00-910-001-A. SEE CONTINUATION CARD FOR SDR SWIA202265943None · corrodedR/H I/B LONGITUDINAL TOP OF SEAT TRACK BETWEEN FR33-34 HAS CORROSION AS MARKED. (C-CHECK RO 6/16/2022) REMOVED AND REPLACED R/H I/B LONGITUDINAL SEAT TRACK BETWEEN FR 23-34 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06. NO WEIGHT CHANGSDR SWIA202265942None · corrodedRH I/B SEAT TRACK CORRODED BETWEEN FRAMES 81-82 (C-CHECK RO 6/16/2022) REMOVED AND REPLACED RH I/B SEAT TRACK BETWEEN FR74-84 REF EMB SRM 51-40-08. PART REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED. SEE CONTINUATION CARD FOR DETAILS OF WSDR SWIA202155903Skin · dentedTRANSFER FROM EAML 571985 : DENT LEFT SIDE FUSELAGE IN LINE WITH AFT OF CA DV WINDOW BELOW GOLD STRIP IS LOCATED ON THE LH SIDE OF THE FUSELAGE BETWEEN FR10 AND FR11. DAMAGE GOES UP TO STR17. THE LENGTH OF THE DENT IS 3.745". THE / WIDTH OF TSDR SWIA202155902Skin · dentedTRANSFER FROM EAML 571986 : DENT LEFT SIDE FUSELAGE IN LINE WITH STAR ALLIANCE LOGO BELOW GOLD STRIPE IS A COMBINATION OF 1 DENT, 1 CREASE, AND 2 RAISED AREAS. THE DAMAGE IS LOCATED AT FR12 AND STR18. THE CREASE MEASURES 7.0" IN LENGTH. THE WIDTH OF THE CREASSDR SWIA201946552Control Module · malfunctionedSTEER FAIL CAUTION MESSAGE CAME ON WHEN LOWERING LANDING GEAR. HAD NO NOSE WHEEL STEERING WHILE ON THE GROUND. FLT # 5481 CLOSEDREMOVED AND REPLACED STEERING CONTROL MODULE IAW AMM. OPS CHECK GOOD AT THIS TIME.SDR SWIA201844135Engine · shutdownLEFT ENGINE SHUTDOWN INFLIGHT. AT FL380, NO TURBULANCE, CREW THROTTLED THE LEFT ENGINE BACK, ITT SPIKED AND WENT RED. ENGINE ROLLED BACK AND SHUTDOWN. CREW DESCENDED TO FL270 AND THE ENGINE AUTO RELIT. WHILE AT FL100 THE CREW INCREASED POWER SLOWLY AND THESDR SWIA201439883Warning Light · false activationDURING GO AROUND WITH FLAP SELECTOR AT 2, RECEIVED FLAP OVERSPEED FOR 5 SECONDS, WHILE ENCOUNTERING INTERMITTENT TURBULANCE. NO FAULTS NOTED. ACFT OK FOR SERVICE IAW AMM.
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