N786SW, cancelled Oct 1, 2025
Service difficulty reports · 257
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 = 'N786SW' AND deregistration_id = 'N786SW-2025-10-01' 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 = 'N786SW' AND deregistration_id = 'N786SW-2025-10-01' 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 SWAA2024080723039Megaphone · failedFWD MEGAPHONE DOES NOT TEST<[01] REMOVED AND REPLACED MEGAPHONE IAW AMM 25-64-00SDR SWAA2024070105857Indication Sys · false indicationIN CRUISE 'A' SYSTEM HYDRAULICS DROPPED TO 56% SUSPECTED LEAK NO 30 HIST<[01] OK TO CONTINUE PER MEL 29-11-01; C/W SP-1; AUTHORIZATION # 200538;[02] AFTER FURTHER INSPECTION & OPS CHECKS OF SYS A QUANTITY TRANSMITTER & FLIGHT CONTROLS; FOUND NO LEAKS & NO DEFESDR SWAA2024050983522Balance Weight · corrodedRUDDER WEIGHT MISSING MATERIAL AND CORRODED<[01] R&R RUDDER WEIGH PER CMM 55-40-09;[02] INSPECTION C/W R&R RUDDER WEIGH PER CMM 55-40-09SDR SWAA2024041173528Slide · looseEMERGENCY SLIDE, AFT FO SIDE, HAS EXCESS MATERIAL EXPOSED. ONLY VISIBLE WHEN DOOR IS ARMED. INSPECTED AFT SERVICE DOOR EMERGENCY SLIDE IAW AMM 25-66-01. FOUND SLIGHT LOOSE MATERIAL ON LEFT SIDE, ADJUSTED MATERIAL AS REQUIRED.SDR SWAA2024031362199Floor Panel · crackedFWD CARGO PIT AFT FLOOR HAS CRACKS.<[01] OK TO CONTINUE AS PER MEL 25-16-01 SP1B AUTH#183645;[02] REMOVED AND REPLACED FWD CARGO AFT FLOOR PANEL PER AMM 25-52-10.SDR SWAA2024012242897Fairing · delaminatedWING-TO-BODY FAIRING PANEL 194CL HAS PUNCTURE DAMAGE WITH DELAM IN OUTER SKIN. -MARKED-<[01] REMOVED AND REPLACED PANEL 194CL IN REF WITH AMM 20-50-11.SDR SWAA2024012242899Panel · delaminatedWING-TO-BODY FAIRING PANEL 194CR HAS TWO PUNCTURE DAMAGED AREAS WITH DELAM. -MARKED-<[01] REMOVED AND REPLACED 194CR PANEL IN REF WITH AMM 20-51-11 AND TASK CARD 5351-E-16723-NG.SDR SWAA2024012242898Fairing · pulledWING-TO-BODY FAIRING PANEL 193AR SEVERAL SCREWS PULLED THROUGH AT THE IB END OF PANEL.<[01] REMOVED AND REPLACED 193AR PANEL IN REF WITH AMM 20-51-11 AND TASK CARD 5351-E-16723-NG.SDR SWAA2024012242900Fairing · pulledWING-TO-BODY FAIRING PANEL 194CR HAS A SCREW PULLED THROUGH AT THE FWD IB MOST CORNER.<[01] REMOVED AND REPLACED 194CR PANEL IN REF WITH AMM 20-51-11 AND TASK CARD 5351-E-16723-NG.SDR SWAA2024012242901Fairing · bulgedWING-TO-BODY FAIRING PANEL 193AR HAS TWO BULGED AREAS IN EXTERIOR SKIN WITH TAP TEST SOUND OF DELAM. -MARKED-<[01] REMOVED AND REPLACED 193AR PANEL IN REF WITH AMM 20-51-11 AND TASK CARD 5351-E-16723-NG.SDR SWAA2023122735208Door · delaminatedRT AC BAY DOOR; RT FWD O/B CORNER DELAM; MEASURES 4.25' X 4.25'<[01] REFERENCE EA 23-153-03744SDR SWAA2023100908178Tail Cone · delaminatedLEFT WING #3 FLAP FAIRING TAIL CONE DELAMINATED.<[01] REMOVED AND REPLACED LH WING #3 FLAP FAIRING TAIL CONE PER SRM 51-40-02SDR SWAA2023091499492Slide · out of adjustAFT SVC DOOR SLIDE HAS EXCESS MATERIAL OUT OF SLIDE COVER<[01] REPOSITIONED SLIDE ASSY REF AMM 25-66-01 / MT 725-61-06SDR SWAA2023062972746Stud · missingAFT CARGO DOOR HANDLE TEFLON STUD MISSING<[01] INSTALLED AFT CARGO DOOR HANDLE TEFLON STUD PER AMM 52-31-14.SDR SWAA2023052552297Light · inoperativeR1 DOOR ESCAPE SLIDE EMERGENCY LIGHT INOP.<[01] RELAMPED R1 EXTERNAL SLIDE EMERGENCY LIGHT.<BR>IAW B737 MM 33-51-04SDR SWAA2023050131173Cover · brokenRH LOWER EMERGENCY EXIT LIGHT COVER BROKEN<[01] REPLACED RH LOWER EMERGENCY EXIT LIGHT COVER PER AMM 33-51-01SDR SWAA2022101860517Sign · inoperativeCUSTOMER WALK. L-1 DOOR EMERGENCY LIGHT TWO BULBS OUT NEED SIX WORKING. / [01] RELAMPED L-1 DOOR EMERGENCY EXIT SIGN 2EA AS PER REF B737 AMM 33-51-01-960-801. TEST OK.;[02] VERIFIED STEP 1.SDR SWAA2022101858000Sign · brokenR-1 DOOR LOWER EXIT SIGN LENS BROKEN / [01] REMOVED AND REPLACED R-1 DOOR LOWER EXIT SIGN. REF. BOEING 737-700 AMM 33-51-01-960-802.;[02] VERIFIED 1SDR SWAA2022101858004Sign · brokenR-2 DOOR LOWER EXIT SIGN BROKEN / [01] REMOVED AND REPLACED R2 LOWER EXIT SIGN AS PER AMM 33-51-01-960-802-NG.;[02] VERIFIED STEP 1SDR SWAA2022101852289Sign · brokenL-1 DOOR LOWER EXIT SIGN LENS BROKEN. / [01] REMOVED AND REPLACED L-1 DOOR LOWER EXIT SIGN. REF. BOEING 737-700 AMM 33-51-01-960-802.;[02] VERIFIED 1SDR SWAA2022101851666Panel · deterioratedPANEL 231XF (PANEL 231XF FLOOR PANEL) UPPER SURFACE RESIN DETERIORATED / [01] MEASUREMENTS;[02] PREPARED AND REPAIRED FLOOR PANEL #231XF AT DAMAGED AREA PER B737 SRM 53-00-50-2R-1 PARAGRAPH 3.M. MATERIALS USED RESIN P/O#1783720; CLOTH P/O#1690463;[03] VERIFIEDSDR SWAA2022101951668Skin Panel · crackedRT WING LOWER MID SPAN T/E PANEL 661BB - INNER SKIN HAS CRACKS AND BULGING AROUND NUMEROUS FASTENER HOLES AS MARKED. 124-023 / [01] CLEANED AND PREPARED DAMAGE FASTENER HOLES FOR REPAIR; PER FORMED DRY OUT FOUND NO WATER AS PER B737 SRM 51-70-04-2R-9;[02] REPASDR SWAA2022101851221Scuff Plate · crackedAFT CARGO AFT CORNER SCUFF PLATE CRACKED / [01] RECEIVED SCUFF PLATE PART # 146A8341-9 FROM JL WELDING TAG #011178 LOCATED AND DRILLED AS PER B 737-700 SRM 51-40-05-0G-0 SCUFF PLATE TO BE INSTALLED ON ITEM #TTG8Q00F4DRW;[02] [FINAL] VALIDATED STEP 1SDR SWAA2022101949319Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #3 RIB CRACK NOTED (DOT-223 LHLE3). / [01] REMOVED #3 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW #3 RIB AT L/H HORIZONTAL STAB AS PER REF SRM 51-40-05-0G-0.;[03] VSDR SWAA2022101949318Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #5 RIB CRACK NOTED AT RIVET EDGE HOLE (DOT-223 LHLE5). / [01] REMOVED L/H HORIZONTAL STAB #5 RIB AS PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW L/H HORIZONTAL STAB AS PER B737-700 SRM 51-40-05-0SDR SWAA2022101949317Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #4 RIB CRACK NOTED AT RIVET EDGE HOLE (DOT-223 LHLE4). / [01] REMOVED #4 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED #4 NEW RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRSDR SWAA2022101949316Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE; INTERNAL #2 RIB CRACK NOTED (DOT-223 LHLE2). / [01] REMOVED #2 RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED # 3 NEW RIB AT L/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-0.;[SDR SWAA2022101852288Floor Panel · delaminatedPANEL 241AF HAS SURFACE DELAMINATION / [01] MEASUREMENTS;[02] CLEANED AND PREPARED DAMAGE AREAS AS MARKED FOR REPAIR ON TOP SURFACE OF MAIN CABIN FLOOR PANEL 241AF AS PER B737 SRM 53-00-50-2R-1;[03] VERIFIED STEPS 1 AND 2;[04] OK TO APPLY REPAIR;[05] REPAIRED SDR SWAA2022092082832None · missingEXIT SALINA SIGN MISSING FROM RH OVERWING EXIT / [01] INSTALL EXIT SALIDA COVER ON RH OVER WING EXIT DOOR PER SIPSDR SWAA2022091252175Panel · smokeAFT #1 COFFEE POT SMELLS OF ELECTRICAL SMOKE WHEN ON / [01] REMOVED AND REPLACED #1 COFFEE MAKER IAW AMM 25-30-01 OPS CK GOODSDR SWAA2022071126631Flap · delaminatedLEFT WING OUTBOARD AFT FLAP HAS SEVERAL SPOTS OF DELAMINATION ON THE UNDER AND UPPER SIDE OF THE INBOARD 15 INCHES. (MARKED) / [01] REPAIRED AFT FLAP PER SRM 51-70-05.SDR SWAA2022071126003Lens · brokenCREW REPORTS FWD ENTRY EMERGENCY EXIT SIGN LENS IS BROKEN / [01] C/W EA M-21-133-00720SDR SWAA2022031181441Lens · missingRIGHT OVERWING EMERGENCY EXIT LIGHT LENS ( AFT SIDE) MISSING DIRECTIONAL ARROW / [01] R & R LENS IAW AMM 33-51-01;[02] INSPECTEDSDR SWAA2021120249457Light · inoperativeLH OUTER OVERWING EMERGENCY EXIT LIGHT INOP ; / [01] RELAMPED LH OUTER OVERWING EMER LIGHT IAW 33-51-04. OPS CHECKS GOOD.SDR SWAA2021112446451Fitting · corrodedSUPPLEMENTAL INFORMATION: LFT MLG FWD TRUNNION SUPPORT FITTING UPPER O/B (#1) BORE HAS EVIDENCE OF CORROSION ; LFT MLG FWD TRNNION SPPORT FITTING PPER O (#1) ORE HAS EVIDENCE OF CORROSION / [01] REPAIRED PER EA 1-A57-3246 REV 14SDR SWAA2021112446450Fitting · corrodedSUPPLEMENTAL INFORMATION: LFT MLG FWD TRUNNION SUPPORT FITTING; LOWER O/B LUG (#3) BORE HAS EVIDENCE OF CORROSION ; LFT MLG FWD TRNNION SPPORT FITTING; LOWER O LG (#3) ORE HAS EVIDENCE OF CORROSION / [01] REPAIRED PER EA 1-A57-3246 REV 14SDR SWAA2021111842925None · brokenRT WING I/B FIXED T/E DEFLECTOR RIB LOWER SIDE ROD ATTACH LUG BROKEN. ; / [01] TRIMMED OUT AND REMOVED DMG TURNBUCKLE LUG AS PER B737-700 SRM 57-51-02-2R-2 REPAIR 2 AND SRM 51-10-02-0G-0; [02] VERIFIED STEP 1; [03] PERFORMED HFEC INSP. ON REWORKED AREA IAW B73SDR SWAA2021111742225Battery Pack · inoperativeINTERNAL EMERGENCY EXIT SIGN INOP; AT LEFT OVERWING DOOR. DURING T/S FOUND BATTERY PACK INOPERATIVE. REMOVED AND REPLACED BATTERY AND PERFORMED TEST; TEST PASSED IAW AMM FIM 33-50 TASK 801 AND AMM 33-51-06-960-805.SDR SWAA2021111742223Battery Pack · out of positionINTERNAL EMERGENCY EXIT SIGN INOP AT R/H OVERWING DOOR. REPOSITIONED BATTERY PACK ; PERFORMED OPERATIONAL TEST; TEST PASS IAW AMM 33-51-06=960-805.SDR SWAA2021111838750Cap · corrodedAFT CARGO FLOOR L/H CAP STRIPS WITH CORROSION ; / [01] AFT CARGO FLOOR L/H CAP STRIPS WITH EXFOLIATION CORROSION PASSING THROUGH MATERIAL; [02] RECEIVED CAP STRIP P/N: 453A2611-8. REF. TASK CARD TTG8Q004G35M FOR CAP STRIP INSTALLATION.; [03] VERIFIED STEPS 1 ASDR SWAA2021111838751Cap · corrodedAFT CARGO FLOOR R/H CAP STRIPS WITH CORROSION ; / [01] AFT CARGO FLOOR R/H CAP STRIPS WITH EXFOLIATION CORROSION PASSING THROUGH MATERIAL; [02] RECEIVED CAP STRIP P/N: 453A2611-9 AND 453A2611Y3. REF. TASK CARD TTG8Q004G35M FOR CAP STRIP INSTALLATION.; [03] VERSDR SWAA2021111838752Cap · corrodedAFT CARGO COMPARTMENT CAP STRIPS FWD AND AFT SIDE OF CARDO DOOR CUTOUT WITH CORROSION ; / [01] AFT CARGO COMPARTMENT CAP STRIPS FWD AND AFT SIDE OF CARGO DOOR CUTOUT WITH EXFOLIATION CORROSION PASSING THROUGH MATERIAL; [02] RECEIVED NEW CAP STRIPS P/N: 453A241SDR SWAA2021111833916Intercostal · crackedFWD CARGO COMPARTMENT FLOOR STRUCTURE INTERCOSTAL S25L BETWEEN STA 500B-500C CRACKED ; / [01] REMOVED DAMAGE INTERCOSTAL FROM FWD CARGO PER 737-700 SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT; [02] LOCATED AND DSDR SWAA2021111833917Intercostal · crackedFWD CARGO COMPARTMENT FLOOR STRUCTURE INTERCOSTAL S25L BETWEEN STA 500-500A CRACKED ; / [01] REMOVED DAMAGE INTERCOSTAL FROM FWD CARGO PER 737-700 SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT; [02] REMOVED INTERCSDR SWAA2021111832175Rib · crackedRT HORIZONTAL STAB NR 4 INSPAR RIB HSS 120 FWD LOWER OTBD CORNER CRACKED. REMOVED CRACK IAW SRM 51-10-02-0G-0 & 55-10-09-2R-5 REPAIR 5. PERFORMED HFEC INSP OF CUT EDGES ON REPAIR AREA IAW NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS NOTED. PERFORMED HFEC ROTSDR SWAA2021111831843Retainer · crackedRT WING T/E AT FLEX CONTROL RIB; TOP PANEL SEAL RETAINER CRACKED. REMOVED AND REPLACED R/H WING AT FLEX CONTROL RIB TOP PANEL SEAL RETAINER AS PER B737-700 SOPM 20-50-18.SDR SWAA2021101830289Rub Strip · missingAT FRAME BS 235.8 MISSING SECTION WHERE INITIAL RUBBING STRIP ATTACH. TRIMMED DAMAGE AREA AT FRAME STA 235.8 PER SRM 51-10-02-0G-0 VERIFIED STEP 1. PERFORMED HFEC INSP ON CUTOUT AREA IAW B737 NDTP6 51-00-00 PROC.23 NO CRACKS. FABRICATED AND INSTALLED REPAIR SDR SWAA2021111829855Shield · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE SHIELD PANEL AT S-25R BETWEEN STA 847-867 WITH EXFOLIATION CORROSION ; / [01] REMOVED CORROSION FROM AFT CARGO SHIELF STA 847-867 RBL 25 AS PER B737-700 SRM 51-10-02-0G-0; [02] VERIFIED STEP 1; CORROSION WAS THRU METAL; [0SDR SWAA2021111829276Panel · crackedFLAP SUPPORT NO.8 PANEL 644EB LOWER SECTION CRACKED/DELAMINATED ; / [01] REMOVED DAMAGED PLIES AND PREPARED DAMAGED AREA FOR REPAIR AT PANEL 644EB AS PER B737-700 SRM 51-70-04-2R-0; [02] VERIFIED STEP 1; OK TO INSTALL REPAIR; [03] REPAIRED DAMAGED AREA AT PANESDR SWAA2021111828877None · crackedLOWER FUSELAGE CENTER WING L/H AIR CONDITIONING EXHAUST AIR EXIT SEAL RETAINER CRACKED @ INB. SIDE ;STA 663.75 MKD DOT ; / [01] REMOVED PREVIOUS REPAIR FOR ACCESS AT LOWER FUSELAGE CENTER WING L/H AIR CONDITIONING EXHAUST. PER SRM 51-40-02-0G-0; [02] REMOVED S
Back to N786SW, cancelled Oct 1, 2025