N793SA, cancelled May 5, 2025
Service difficulty reports · 342
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 = 'N793SA' AND deregistration_id = 'N793SA-2025-05-05' 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 = 'N793SA' AND deregistration_id = 'N793SA-2025-05-05' 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 SWAA2024083031266Slide · out of positionFWD GALLEY SERVICE DOOR SLIDE OUT OF POSITION IN CASE.<[01] REPOSITIONED FWD GALLEY SERVICE DOOR SLIDE <BR>REF AMM 25-66-01SDR SWAA2024042579314Starter · dislodged#1 ENGINE OIL LOW QUANTITY AT FL410. INITIALLY 17% THEN TO 0% IN DIVERSION TO DAL AFTER 20 MINUTES BOX FLASHED RED. THEN SHUT DOWN ENGINE. DEPARTED DEN WITH 88%<[01] FOUND STARTER QUAD RING CLAMP BROKEN AND STARTER DISLODGED FROM ACCESSORY GEAR BOX. R&R STARTESDR SWAA2024042579321Starter · dislodged#1 ENGINE OIL LOW QUANTITY AT FL410. INITIALLY 17% THEN TO 0% IN DIVERSION TO DAL AFTER 20 MINUTES BOX FLASHED RED. THEN SHUT DOWN ENGINE. DEPARTED DEN WITH 88%<[01] FOUND STARTER QUAD RING CLAMP BROKEN AND STARTER DISLODGED FROM ACCESSORY GEAR BOX. R&R STARTESDR SWAA2023112423524Battery Pack · inoperativeEMERGENCY LIGHT AT L/H OVERWING DOOR INT / EXT INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTRY PACK PER REF. AMM 33-51-06-960-801.PERFORMED EMERGENCY LIGHT OPERATIONAL TEST PER REF. AMM 33-51-00-720-801 FOUND NORMAL.;[02] VERIFIED REMOVED AND REPLACED EMSDR SWAA2023112423523Light · inoperativeEMERGENCY LIGHT ON BULLNOSE AT BIN 6ABC INOP<[01] RELAMPED EMERGENCY LIGHT AT BIN 6 ABC AS PER REF. AMM 33-51-03-960-801.<BR>PERFORMED OPERACIONAL TEST FOUND NORMAL AS PER REF' AMM 33-51-03-960-801.;[02] VERIFIED RELAMPED EMERGENCY LIGHT AT BIN 6 ABC; AND PERFSDR SWAA2023112222955Pressure Blkhd · canningREJECT-RII APB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3R; JUST BELOW RIGHT FITTING REPAIR HAS TOP RIVET BUCKED AND CUT 50% AT SECOND ROW OUTBOARD TO INBOARD.<[01] REMOVE AND REPLACED FASTENER AT STA 1016 AFT PRESSURE BULKHEAD REPAIR JUST BELOW RH FITTING SESDR SWAA2023112221477Pressure Blkhd · canningREJECT RII RIVET BUCKED INCORRECTLY AT APB OIL CANNING REPAIR STA 1016; BETWEEN BL-0 AND S-3R; JUST BELOW RIGHT FITTING; NINE RIVETS FROM TOP TO BOTTOM HOLDING STIFFNER..<[01] REMOVED AND REPLACED ALL MARKED FASTENERS (9 RIVETS) THAT NEEDED REPLACEMENT REF SRMSDR SWAA2023112221476Pressure Blkhd · canningREJECT- AS PER S/M SME REPLACE MARKED FASTENERS AT APB OIL CANNING REPAIR STA 1016 BETWEEN BL-0 AND S-3R JUST BELOW RIGHT FITTING 90% OF RIVETS MARKED ARE HOLDING STIFFNER.<[01] REMOVED ALL MARKED FASTENERS NEEDING REPLACEMENT REF SRM 51-40-02-0G-0.;[02] REMOVSDR SWAA2023112717815Bulkhead · out of toleranceCUSTOMER REJECT- FOUND SEVERAL EXISTING HOLES OUT OF TOLERANCE AT STA 1016 BULKHEAD.<[01] OVERSIDE FASTENERS FOUND OUT OF TOLERANCE OF APB BETWEEN RBL-4 AND RBL-16 AS PER B737-700 SRM 51-40-05-0G-0 FIG 4 A TOTAL OF 10 FASTENERS WERE STEP UP TO 2ND OVERSIDE(.21SDR SWAA2023112715727Bulkhead · canningAPB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3R; JUST BELOW RIGHT FITTING SEE TTG8Q00P9H5Q<[01] ACCOMPLISHED REPAIR AND PERFORMED EA 23-153-03288; REFERENCE FAULT 'TTG8Q00PF2MN & TTG8Q00PAJPT;[02] ACCOMPLISHED REPAIR AND PERFORMED EA 23-153-03288; REFERENCE FSDR SWAA2023112715726Bulkhead · canningAPB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3L; JUST BELOW LEFT FITTING. SEE TTG8Q00P9JY8<[01] ACCOMPLISHED REPAIR ON NR FAULT TTG8Q00PAHQ2.;[02] ACCOMPLISHED REPAIR ON NR FAULT TTG8Q00PAHQ2.SDR SWAA2023112715892Bulkhead · canningTRANSFERRED FROM LP 2479095: APB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3R; JUST BELOW RIGHT FITTING SEE TTG8Q00P9H5Q<[01] ACCOMPLISHED APB OIL CANNING REPAIR AT STA 1016; BETWEEN BL-0 AND S-3R IN REF TO B737 SRM 53-80-08-2R-13; EA 23-153-03288-WIP1 (TTG8Q0SDR SWAA2023112215887Fitting · unknownTRANSFERRED FROM LP 2479096: APB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3L; JUST BELOW LEFT FITTING. SEE TTG8Q00P9JY8<[01] ACCOMPLISHED AFT PRESSURE BULKHEAD OIL CANNING REPAIR AT STA 1016 BETWEEN BL-0 AND S-3L IN REFERENCE TO B-737-700 SRM 53-80-08-2R-13.;SDR SWAA2023103015371Bulkhead · canningAPB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3R; JUST BELOW RIGHT FITTING<[01] FOUND MEASUREMENTS OUT OF LIMITS.;[02] NON ROUTINE TRANSFERED TO LOGBOOK SEE LP# 2479095;[03] FOUND MEASUREMENTS TO BE OUT OF LIMITS IAW SRM 53-80-08-1A-1; NON ROUTINE TRANSFERRED SDR SWAA2023103015372Bulkhead · canningAPB OIL CANNING; STA 1016; BETWEEN BL-0 AND S-3L; JUST BELOW LEFT FITTING<[01] FOUND MEASUREMENTS TO BE OUT OF LIMITS;[02] EDIT MEASUREMENTS;[03] FOUND MEASUREMENTS TO BE OUT OF LIMITS IAW SRM 53-80-08-1A-1;[04] NON ROUTINE TRANSFERRED TO LOGBOOK SEE LP # 2479SDR SWAA2023090595891Flap · peelingREF 23-157-02669-TLD LH OB AFT FLAP PREVIOUS REPAIR PEELING - PN 113A3700-7; SN 000054 - TIME LIMITED REQUIRES REPLACEMENT.<[01] REMOVED AND REPLACED L/H OUTBOARD AFT FLAP ASSEMBLY PER AMM. 27-51-22.SDR SWAA2023062060119Light · inoperativeEMERGENCY LIGHT BY FORWARD SERVICE DOOR INOP<[01] RELAMPED EMERGENCY LIGHT BY FORWARD SERVICE DOOR (ON FUSELAGE EXTERIOR) IAW AMM 33-51-04. OPS CHECK GOOD.SDR SWAA2023012493183Bulb · inoperativeCUSTOMER WALK: LT OVERWING EXIT INTERIOR EXIT MAKER HAS BULBS OUT.<[01] RE-LAMPED LT OVERWING INTERIOR EXIT SIGN AS PER REF AMM 33-51-01-960-801 LIGHT TEST OK;[02] VERIFIED STEP 1SDR SWAA2023012493190Handle · looseL1 DOOR LOWER ASSIST HANDLE LOOSE. SECURED FWD ENTRY DOOR LOWER ASSIST HANDLE PER B737 AMM 52-11-31-400-802-NGSDR SWAA2023012491721Battery Pack · inoperativeASSOCIATED EMERGENCY LIGHTS WITH FWD ENTRY BATTERY PACK M1674 ARE INOP.<[01] REMOVED AND REPLACED (M1674) EMERGENCY BATTERY PACK IN REF WITH B737 AMM 33-51-06-960-805.;[02] EMERGENCY BATTERY PACK TEST NORMAL IN REF WITH B737 AMM 33-51-06-960-805.;[03] VERIFIEDSDR SWAA2023012490005Skin · crackedCRACK FOUND AT EXTERNAL LOWER SURFACE OF RH I/B AFT FLAP 19.5' FROM I/B EDGE AND 3.375' FROM T/E. CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 0.393'. CUT OUT DAMAGED AERA AT R\H I\B AFT FLAP ON LOWER SURFACE SIZE 1.5'X0.5' NO CORESDR SWAA2023012588572Scuff Plate · crackedAAFT CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED<[01] RECEIVED AFT CARGO DOOR FWD CORNER SCUFF PLATE IN SERVICEABLE CONDITION (REPAIRED BY OUTSIDE VENDOR J.L. WELDING INC. REF. BOEING 737-700 SRM 53-60-15-2R-1 UNDER AAR PO# 413820);[02] VERIFIED STEP 1SDR SWAA2023012588091Door · brokenEXTERNAL POWER DOOR GROUND BROKEN<[01] REMOVED AND REPLACED EXTERNAL POWER DOOR GROUND AS PER SWPM 28-20-00 AND SWPM 20-20-10.<BR>BONDING METER B/C 168697.;[02] VERIFIED REMOVAL AND REPLACEMENT OF EXTERNAL POWER DOOR GROUND.SDR SWAA2022082243711Pump · leakingB LOW PRESSURE LIGHT ILLUMINATED; COMPLIED W/QRH; FOLLOW BY B ELEC LOW PRESSURE. B QTY SHOWED ZERO. LOSS OF SYS B @ 5 MINS AFTER THE LOW PRESSURE ENG 2 IS WHEN COMPLETE LOSS HAPPENED. / [01] REMOVED AND REPLACED SYS B EMDP PER AMM 29-11-21. PUMP LEAK CHECKED GSDR SWAA2022081541675Light · faultyLEFT SLIDE/OVER WING EMERGENCY LIGHT EXTINGUISHED. / [01] RELAMPED LEFT SLIDE/OVER WING EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.SDR SWAA2022061619248Battery Pack · failedEMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674; M1669; M1672; M1673; M1670 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674 M1669 M1672 M1673 M1670 / [01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1674; M1669; M1672; SDR SWAA2022061619250Battery Pack · failedEMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674; M1669; M1672; M1673; M1670 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674 M1669 M1672 M1673 M1670 / [01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1674; M1669; M1672; SDR SWAA2022061619249Battery Pack · failedEMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674; M1669; M1672; M1673; M1670 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674 M1669 M1672 M1673 M1670 / [01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1674; M1669; M1672; SDR SWAA2022061618412Battery Pack · failedEMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674; M1669; M1672; M1673; M1670 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1674 M1669 M1672 M1673 M1670 / [01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1674; M1669; M1672; SDR SWAA2021120850399Megaphone · brokenSUPPLEMENTAL INFORMATION: FA FWD MEGAPHONE; MEGAPHONE HANDLE IS BROKEN ; / [01] R&R'ED FWD FA MEGAPHONE IAW AMM 25-64-00. OK FOR SERVICE.SDR SWAA2021110333488Scuff Plate · crackedAFT CARGO SCUFF PATE HAS A CRACK .(AFT PLATE) ; / [01] SCUFF PLATE WAS SENT TO J.L WELDING FOR REPAIR AND RECEIVED SERVICEABLE. ITEM WILL BE INSTALLED ON CUSTOMER CARD #TTG8Q0032CYS.; [02] VERIFIED 1.SDR SWAA2021110327547None · crackedLT HORIZONTAL STAB RIB #5 STIFFENER #4 CRACKED ; / [01] 1.PERFORMED HFEC ON RIB #5 STIFFENER #4 IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK FOUND AT LOWER AREA . CRACK LENGTH : 0.472'. <BR><BR>2.PERFORMED HFEC ROTO ON OPEN FASTENER HOLES IAW NDTM PART 6;51-00SDR SWAA2021110325355Seat Track · corrodedF/O SEAT TRACK HAS CORROSION ON LWR SURFACE FWD I/B. 8-79 ; / [01] REFER TO CUSTOMER CARD #(753-330-00-01Y) BARCODE# TTG8Q0032DAH FOR INSTALLATION.; [02] VERIFIED 1.SDR SWAA2021110324817Strap · crackedAT ELECTRICAL AND ELECTRONICS COMPARTMENT(E/E) BS 312 TO BS 344;STABILIZER STRAP ON RBL 31.60 IS CRACKED. ; / [01] REMOVED DAMAGED STABILIZER STRAP AT E/E. COMPARTMENT BS. 312 TO BS. 344 RBL 31.60 IAW. B737-700 SRM. 51-40-02-0G-0; [02] MATCH DRILLED NEW STABILSDR SWAA2021110324333Floor Panel · delaminatedFLOOR PANEL 221CF HAS LAMINATE DAMAGE AT FASTENER INSERT ; / [01] PREPARED FOR REPAIR FLOOR PANEL #221CF AS PER BOEING 737 SRM 53-00-50-2R-0; [02] REPARED FLOOR PANEL #221CF SMALL AREA AND REPLACED DAMAGE INSERTS AS PER BOEING 737 SRM53-00-50-2R-0 .MATERIAL USSDR SWAA2021110323144Bulkhead · crackedAFT CARGO BUKLHEAD PNL 142NWB CRACKED. 8-78 ; / [01] RECEIVED A BRAND NEW AFT CARGO BULKHEAD PANEL 142NW. P/N: 453A2510-1. PANEL WILL BE INSTALLED ON TASK CARD# TTG8Q005ZBPS.; [02] VERIFIED 1SDR SWAA2021110322678None · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE PANEL #341B; INTERNAL RIB LE STA 105.26 (RIB #4) BOTTOM EDGE RIVET HOLE CRACK NOTED. ; / [01] REMOVED DAMAGE INTERNAL RIB #4 AT RIGHT HORIZONTAL STABILIZER L/E. PANEL #341B STA.105.26 IAW B-737-700 SRM 51-40-02-0G-0; [0SDR SWAA2021110322680None · crackedLEFT HORIZONTAL STABILIZER (LE STA 105.26); INTERNAL RIB #4 BOTTOM EDGE RIVET HOLE CRACK NOTED. ; LEFT HORIZONTAL STAILIZER LEADING EDGE PANEL #331B; INTERNAL RI LE STA 105.26 (RI #4) OTTOM EDGE RIVET HOLE CRACK NOTED. / [01] REMOVED CRACKED INTERNAL RIB #4 ATSDR SWAA2021110322681None · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE PANEL #341B; INTERNAL RIB LE STA 95.96 (RIB #3) BOTTOM EDGE RIVET HOLE CRACK NOTED. ; / [01] MATCH DRILLING NEW INTERNAL RIB L/E AT RIGHT HORIZONTAL STABILIZER L/E. PANEL #341B STA. 95.96 [RIB #3] IAW. B-737-700 SRM.51-SDR SWAA2021110322689Seat Track · corrodedCAPT SEAT TRACK HAS CORROSION ON LWR SURFACE FWD I/B. 8-56 ; / [01] RECEIVED NEW CAPT. SEAT TRACK POSITION FWD I/B REF B 737-700 IPC 25-11-01-55A<BR>INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q0032DAH; [02] VERIFIED 1.SDR SWAA2021110322688Seat Track · corrodedCAPT SEAT TRACK HAS CORROSION ON LWR SURFACE AFT I/B. 8-57 ; / [01] RECEIVED NEW CAPT. SEAT TRACK POSITION AFT I/B REF B 737-700 IPC 25-11-01-55A<BR>INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q0032DAH; [02] VERIFIED 1.SDR SWAA2021110322683Seat Track · corrodedCAPT SEAT TRACK HAS CORROSION ON LWR SURFACE FWD O/B. 8-55 ; / [01] RECEIVED NEW CAPT. SEAT TRACK POSITION FWD O/B REF B 737-700 IPC 25-11-51-09A<BR>INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q0032DAH; [02] VERIFIED 1.SDR SWAA2021110322682Seat Track · corrodedF/O SEAT TRACK HAS CORROSION ON LWR SURFACE AFT I/B. 8-52 ; / [01] RECEIVED NEW F/O. SEAT TRACK POSITION AFT I/B REF B 737-700 IPC 25-11-01-55A<BR>INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q0032DAH; [02] VERIFIED 1.SDR SWAA2021110322686Seat Track · corrodedF/O SEAT TRACK HAS CORROSION ON LWR SURFACE FWD O/B. 8-54 ; / [01] RECEIVED NEW F/O. SEAT TRACK POSITION FWD O/B REF B 737-700 IPC 25-11-51-09A<BR>INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q0032DAH; [02] VERIFIED 1.SDR SWAA2021110322009Stub Frame · crackedFOUND CRACK AT R1 DOOR CUT OUT FWD UPPER STUB FRAME. ; / [01] REMOVED R1 DOOR FWD CUTOUT UPPER STUB FRAME RE B737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW STUB FRAME AT R1 DOOR UPPER FWD CUTOUT REF B737-700 SRM 51-40-05-0G-0 AND DWG# 141A8370.; [03SDR SWAA2021110322019Intercostal · crackedAFT OF FWD CARGO INTERCOSTAL CRACKED BS 520 S-25R. 8-90 ; / [01] REMOVED INTERCOSTAL AT AFT OF FWD CARGO ;STA 520 STGR - 25R AS PER B737-700 SRM 51-40-02-0G-0; [02] FABRICATED INTERCOSTAL FOR AFT OF FWD. CARGO BS. 520 S-25R IAW. DWG#143A9803-58; HEAT TREATED FSDR SWAA2021110321653Bulkhead · crackedLEFT A/C COMPT BS 663 BULKHEAD HAS 1.5' CRACK FROM LWR EDGE LBL 13. 8-19 ; / [01] PERFORMED VISUAL INSPECTION AND TAP TEST INSPECTION AT LEFT HAND VAPOR BARRIER; FOUND CRACK 1.5''; WATER NOTE REF B737 NDT PART 1 51-05-01. MADE STOP-DRILLING OF CRACK REF B737-7SDR SWAA2021110320867None · crackedFWD CARGO COMPARTMENT BILGE R/H FLOOR SUPPORT Z CHANNEL CRACKED AT STA 5OO ; S-26R ; / [01] RECEIVED NEW Z CHANNEL (SHIELD); FOR FWD CARGO COMP LOWER BILGE STR 26R BETWEEN STA 500AND 500A; LOCATED AND DRILLED PER B737 SRM 51-40-05-0G-0 AND DWG 143A0080 INSTALLSDR SWAA2021110320865None · corrodedCORROSION AT FASTENERS HOLES FWD CARGO BILGE R/H FLOOR SUPPORT Z CHANNEL S-26R BETWEEN STA 480 AND 500A ; / [01] REMOVED CORRECTION ON AREAS AT S-26R BTW STA 480-500A AS PER B737-700 SRM 51-10-02-0G-0; [02] THIS FAULT WILL BE RESOLVE ON FAULT TTG8Q006LM5N.<BR>SDR SWAA2021110319966None · corrodedCORROSION AT FASTENERS HOLES FWD CARGO BILGE R/H FLOOR SUPPORT Z CHANNEL S-26R BETWEEN STA 480 AND 500A ; /
Back to N793SA, cancelled May 5, 2025