N124SY
Service difficulty reports · 29
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 = 'N124SY' 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 = 'N124SY' 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 SWIA2025102400002Shear Tie · corrodedAFT WET AREA SHEAR CLIP IS CORRODED AT FRAME 88-89 BETWEEN STRINGERS 20L-21L. (C-CHECK RO 10/23/2025)REMOVED AND REPLACED AFT WET AREA SHEAR CLIP AT FRAME 88-89 BETWEEN STRINGERS 20L-21L REF EMB SRM 51-40-08. REPLACED WITH OEM PART AND DOES NOT EFFECT WEIGHT SDR SWI2025F01458Flap Track · out of limitsRH AFT FLAP TRACK 2A OB HAS A WIDTH REDUCTION OF 1.4 MM THAT IS OUT OF LIMITS (C-CHECK RO 10/23/2025)REMOVED AND REPLACED RH AFT FLAP TRACK 2A OB. REF AMB 175 AMM 57-54-25. ASSET# TC1-604, CDD 3-6-26. TC2-10241, CDD 3-20-26.SDR SWIA202510240001Flap Track · out of limitsRH FLAP TRACK 2 IB MAIN HAS A WIDTH REDUCTION OF 1.06MM THAT IS OUT OF LIMITS (C-CHECK RO 10/23/2025)REMOVED AND REPLACED RH FLAP TRACK 2 IB MAIN. REF AMB 175 AMM 57-54-23. ASSET# TC1-604, CDD 3-6-26. TC2-10241, CDD 3-20-26.SDR SWIA2025102400930Seat Track · gougedR/H LATERAL SEAT TRACK SEGMENT FR 59/73 IS GOUGED 59/60 AND 60/73. )REMOVED AND REPLACED R/H LATERAL SEAT TRACK SEGMENT BETWEEN FR 59/73. REF: SRM 51-40-08. FACTORY REOLACEMENT PART INSTALLED NO CHANGE TO AIRCRAFT WEIGHT AND BALANCE. SEE CONTINUATION CARD FORSDR SWI2025F01457Seat Track · corrodedFORWARD FUSELAGE FLOOR STRUCTURE SEAT TRACK, RIGHT UPPER SURFACE HAS CORROSION ON UPPER SURFACE AT FR 16. REPAIRED FORWARD FUSELAGE FLOOR STRUCTURE SEAT TRACK, RIGHT UPPER SURFACE AT FR 16. BY REMOVING DAMAGE AND INSTALLING A FABRICATED FILLER PLUG/DOUBLER RESDR SWIA2025102400929Floorbeam · corrodedFORWARD FUSELAGE FLOOR STRUCTURE CROSSBEAM FR 17 CENTER HAS TWO AREAS OF CORROSION ON THE UPPER SURFACE. (C-CHECK RO 10/23/2025)REPAIRED FR17 RH CROSSBEAM REF EMB SRM 53-00-10 REPAIR 03PSDR SWIA2025102400927Rib · crackedCRACK LH HORIZONTAL RIB 12 UPPER FWD FLANGE AFT RIVET AND AFT FLANGE FWD RIVET. (C-CHECK RO 10/23/2025)REMOVED AND REPLACED LH HORIZONTAL RIB 12A REF ETD2025-170-929972. REPLACED WITH OEM PART AND THERE IS NO CHANGE TO WEIGHT AND BALANCE,SDR SWIA2025F01339Skin · scratchedUPON INSPECTION, FOUND THE DAMAGED AREA BETWEEN THE AFT CARGO DOOR AND AFT LAV SERVICE PANEL TO BE 15.5"L X 2.5" W WITH A SCRATCH 1/16" DEEP. DAMAGE IS OUT OF LIMITS PER SRM 53-23-01 (FLIGHT 4653 - FILED CLOSED)TRANSFERED FROM EAML 1702353 : REF AML# 1702303SDR SWIA2022120266959Floorbeam · mechanic errorFWD FUSELAGE R/H CENTER FLOOR BEAM HAS A MISS DRILLED HOLE AT FR 14. WHERE THE LOWER STRAP ATTACHES TO THE BOTTOM OF THE FLOOR BEAM. PERFORMED PERMANENT REPAIR TO FWD FUSELAGE R/H CENTER FLOOR BEAM HAS A MISS DRILLED HOLE AT FR 14 WHERE THE LOWER STRAP ATTACHSDR SWIA2022120266958Beam · corrodedAFT CARGO COMPARTMENT LOWER BEAM HAS CORROSION AT FR77 - FR78. REMOVED AND REPLACED AFT CARGO COMPARTMENT LOWER BEAM IAW SRM 51-40-08.SDR SWIA202266957Seat Track · gougedLEFTOTBD SEAT TRACK HAD GOUGES AND EXPOSED METAL FROM FR74 TO FR84. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08,. SRM 51-23-04, 51-23-05, 51-23-06 AND CPM 51-25-00-910-001A.SDR SWIA202266956Seat Track · gougedRIGHT OTBD SEAT TRACK HAS GOUGES AND EXPOSED METAL FROM FR74 TO FR84. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08.SDR SWIA202266955Seat Track · corrodedRT INBD SEAT TRACK HAS CORROSION AT SEAT MOUNT LUGS AND ON FLOOR OF TRACK, GOUGES, AND EXPOSED METAL FROM FR74 TO FR84. REMOVED AND REPLACED RT INBD SEAT TRACK FROM FR74 TO FR84 REF EMB 175 SRM 51-40-08.SDR SWIA202266954Seat Track · gougedGOUGES ON RT INBOARD SEAT TRACK, BETWEEN FRMS 20-21. REMOVED AND REPLACED RT INBD SEAT TRACK FRMS 12-21 IAW SRM 51-40-08.SDR SWIA202266953Beam · corrodedAFT SERVICE DOOR BEAM HAS CORROSION. BETWEEN FR.85-86 AT STR. 17R. REMOVED AND REPLACED AFT SERVICE DOOR BEAM BETWEEN FR 85-86 AT STGR 17R. REF SRM 51-40-08.SDR SWIA202266952Floor Support · corrodedCORROSION IN AFT WET AREA, ON CENTER LT FLOOR SUPPORT AT FR 87. REMOVED AND REPLACED CENTER LT FLOOR SUPPORT FRAMES 86-89, IAW SRM 51-40-08. PART REPLACED WITH NEW.SDR SWIA2022120266951Seat Track · gougedGOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 23-34 IN 11 LOCATIONS. (C-CHECK) REMOVED AND REPLACED RT FLOOR SEAT TRACK BETWEEN FR 23-34 IAW SRM 51-40-08 AND REWORKED SEAT TRACK BEAN BACK TO ORIGINAL CONTOUR IAW ETD2022-170-034585.SDR SWIA2022120266950Seat Track · gougedGOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 21-23 IN 2 LOCATIONS. (C-CHECK) PERFORMED PERMENANT REPAIR TO RT FLOOR SEAT TRACK BETWEEN FR 21-23 IN 2 LOCATIONS IAW ETD2022-170-035282.SDR SWIA2022120266949Seat Track · gougedGOUGES ON L/H O/B FLOOR SEAT TRACK BETWEEN FR 23-34 IN 8 LOCATIONS AS MARKED. (C-CHECK RO) REMOVED AND REPLACED L/H O/B FLOOR SEAT TRACK BETWEEN FR 23-34 REF EMB 175 SRM 51-40-08.SDR SWIA202266948Waste Box · corrodedWASTE BOX FWD INNER CORNER HAS CORROSION. (C-CHECK RO 12/1/2022) REMOVED AND REPLACED WASTE BOX INNER DOUBLER BETWEEN FRAMES 89-88. / SEE CONTINUATION CARD FOR WORK PERFORMED. REF SRM 51-40-08 / THIS ACTION DOES NOT EFFECT THE AIRCRAFT WEIGHT AND BALLASDR SWIA202156723Skin · damagedREPORT OF AIRCRAFT MAJOR REPAIR" FOR DAMAGE TO FUSELAGE LOCATED UNDER 3RD PASSANGER WINDOW ON LH STGR 21 & STGR 23 AND FR25 & FR27 FILED CLOSED REVIEWED AND SIGNED FORM M-337SDR SWIA202052765Latch · brokenEMERGENCY GEAR EXTENSION DOOR COVER LATCH BROKEN. FILED CLOSED (9/24/2020). REMOVED AND REPLACED THE EMERGENCY GEAR EXTENSION DOOR, PER AMM. OPS CHECK GOOD AT THIS TIME.SDR SWIA2019120646827Floor Support · corrodedAFT WET AREA- FR88/FR90 R/H PANEL SUPPORT CORRODED. (C-CHECK) RO 9/11/2019 REMOVED CORROSION ON R/H PANEL SUPPORT IN AFT WET AREA- FR88/FR90. R/H PANEL SUPPORT NOMINAL: 0.050". MAX. MATERIAL REMOVED: 0.018". REMAINING MATERIAL: .032". NON SIGNIFICANT ALLOWABLSDR SWIA2019120646826Shear Panel · corrodedAFT WET AREA- FR87/FR88 CENTER SHEAR PANEL CORRODED. (C-CHECK) RO 9/11/2019 REMOVED CORROSION ON CENTER SHEAR PANEL IN AFT WET AREA- FR87/FR88. CENTER SHEAR PANEL NOMINAL: 0.050". MAX. MATERIAL REMOVED: 0.018". REMAINING MATERIAL: 0.032". ALLOWABLE DAMAGE: 0.SDR SWIA2019120646824Floor Support · corrodedCORROSION ON RH FLOOR SILL @ FR.12-14 (C-CHECK) RO 9/11/2019 REMOVED AND REPLACED OUT OF LIMITS RH FLOOR SILL @ FR.12-14. REF SRM. THIS SDR IS BEING REPORTED AS PART OF THE CORRECTIVE ACTION PLAN FOR VDR REGARDING SDRS OVER DUE.SDR SWIA2019120646823Floorbeam · corrodedAFT WET AREA- FR88 Y=+273 BEAM CORRODED. (C-CHECK) RO 9/11/2019 REMOVED CORROSION ON FR88 Y=+273 BEAM IN AFT WET AREA. FR88 Y=+273 BEAM CAP NOMINAL: 0.070". MAX. MATERIAL REMOVED: 0.022". REMAINING MATERIAL: 0.048" ALLOWABLE DAMAGE: 0.017". FR88 Y=+273 BEASDR SWIA2019120646825Beam · corrodedFORWARD CARGO BAY LOWER HORIZONTAL BEAM CLOSEOUT PANEL CORRODED AS MARKED. (C-CHECK) RO 9/11/2019 REMOVED DAMAGE TO LOWER HORIZONTAL BEAM CLOSEOUT PANEL BY BLENDING. NOMINAL THICKNESS IS .047" .MAX MATERIAL LOSS IS .008" WITH .039" REMANING AND IS OUT OF LIMSDR SWIA201540600Potable Water · leakingDURING APPROACH, LEFT AILERONS JAMMED. DISCONNECTED THE AILERON CONTROLS AND LANDED WITHOUT INCIDENT, NO EMERGENCY DECLARED. FORWARD POTABLE WATER SYSTEM HAD LEAKED, FLOODING THE BELLY UNDER THE FWD CARGO BAY. THE WATER HAD ENCAPSULATED THE CAPTAIN`S AILERONSDR SWIA201541377Control Column · failedAUTOPILOT KICKED OFFLINE. FOUND THE AILERONS TO BE UNMOVABLE. NO OTHER MESSAGES POSTED. FOLLOWED QRH AND LT AILERON REMAINED UNMOVABLE WHILE RT AILERON MOVED FREELY. CONTINUED TO DESTINATION. CONNECTED THE CONTROL YOKE. R & R THE AILERON FEEL UNIT. ALL
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