N8663A
Service difficulty reports · 82
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 = 'N8663A' 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 = 'N8663A' 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 SWAA2026100598019Door · crackedRIGHT MLG INNER DOOR WAS CRACKED, FWD SIDE OF AFT HINGE. OK TO CONTINUE IAW CDL 32-10-4. 342594.SDR SWAA2026022071807Door Frame · corrodedCABIN AFT LEFT LAVATORY SHOWS EVIDENCE OF CORROSION AT INBD AFT LAV POST. REMOVED CORROED PORTION OF FRAME ASSY AT AFT LT LAV INBD AFT POST AND REPLACED WITH A SERVICIABLE PART IAW CMM 25-48-25 PAGE 607.03. OPERATED LAV DOOR; OP CHECKED GOOD.SDR SWAA2025123051936Wire · pulledWIRES PULLED OUT OF CONNECTORS ON FILLER PANEL 231LW EMERGENCY EXIT LIGHT. TERMINATED CONNECTOR D15242 PER SWPM 20-30-12 AND WDM 33-51-13. FUNCTIONAL TEST OF EMERGENCY EXIT SIGN L1070 TO BE PERFORMED ON CCN TTG8Q019B7Q1.SDR SWAA2025101624624Battery Pack · inoperativeMEGAPHONE INOPERATIVE. R & R BATTERIES PER AMM 25-64-00.SDR SWAA2025092316844Bracket · looseAFT MEGAPHONE MOUNTING BRACKET LOOSE. RESECURED BRACKET PER AMM 25-64-00.SDR SWAA2025091915885Power Supply · inoperativeAFT RT EMERGENCY EXIT LIGHTS WONT LIGHT ABOVE ROW 25; ABOVE AFT R/H SERVICE DOOR AND EXTERNAL R/H AFT OF SERVICE DOOR. REMOVED AND REPLACED PER AMM 33-51-06-960-806-NG.SDR SWAA2025082206039Wedge · debondedLH INBOARD MAIN FLAP (P/N: 113A2100-71; SN: 000489) TRAILING LOWER SKIN DISBOND - PERMANENT REPAIR)<[01] REMOVED L/H I/B DAMAGED FLAP WEDGE AND UPPER PANEL TO FOM PER SRM 51-40-02;[02] REMOVED L/H I/B MAIN FLAP DAMAGED TRAILING EDGE WEDGE ASSEMBLY FOR REPLACEMSDR SWAA2025060978941Battery Pack · inoperativeRH EMERGENCY LIGHTS INOP AT ROWS 6, 10, & 14. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT RT STA 500C+7 IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2025060978057Handle · looseFWD SERVICE DOOR HANDLE LOOSE. TIGHTENED FWD GALLEY SERVICE DOOR HANDLE IN REF TO AMM 52-41-11.SDR SWAA2025020392106Sign · looseOVERWING EXIT SIGN; CAPTAINS SIDE FELL OFF<[01] RESECURED PER SIP.SDR SWAA2024102953726Skin · delaminatedR/H OUTBOARD AFT FLAP LOWER SURFACE IS DELAMINATED AT THE INBOARD END. DELAMINATION MEASURES 8.75' X 7.5'.<[01] REMOVED AND REPLACED R/H O/B AFT FLAP IAW B737 AMM 27-51-22. UP TO ADJUSTMENTS.;[02] REMOVED AND REPLACED R/H O/B AFT FLAP IAW B737 AMM 27-51-22. UPSDR SWAA2024061802205Lens · missingCREW REPORTS: AFT GALLEY EXIT SIGN LENS/INDICATOR MISSING.<[01] INSTALLED INDICATOR LENS REF. AMM 33-51-01SDR SWAA2024040566507Shield · cracked#1 ENGINE INBOARD FAN COWL OIL TANK ACCESS DOOR SHIELD IS CRACKED<[01] #2 ENGINE INBOARD FAN COWL REMOVED AND REPLACED THE OIL TANK ACCESS DOOR SHIELD IAW SRM 51-40-02-0G-0 STEPS 4. AND 5.;[02] EDIT CORRECTIVE ACTION STEP 1: #1 ENGINE INBOARD FAN COWL REMOVED SDR SWAA2024040366342Attach Angle · crackedWING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE IS CRACKED BS 663; LBL 8<[01] REPAIRED WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE BS 663; LBL 8 PER SRM 57-10-10-2R-5 REPAIR 5.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASURESDR SWAA2024040366343Attach Angle · crackedWING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE IS CRACKED BS 663; RBL 8<[01] REPAIRED WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE BS 663; RBL 8 PER SRM 57-10-10-2R-5 REPAIR 5.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASURESDR SWAA2024030759750Engine · overspeedAPU OVERSPEED/SHUTDOWN IN FLIGHT<[01] ACCOMPLISHED FIM 49-30 TASK 802 ; APU NORMAL OPERATION REF AMM 49-11-00-710-801SDR SWAA2023121832420Cover · looseL/H OVERWING EXIT SIGN COVER IS UNATTACHED<[01] RE SECURED L/H OVERWING EXIT SIGN COVER PER SIP.SDR SWAA2023113025842Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS ARE INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT ROW 20 DEF AND ROW 13 DEF IN REFERENCE TO AMM 33-51-06.SDR SWAA2023101911071Handle · looseR2 DOOR HANDLE LOOSE<[01] FOUND R2 DOOR HANDLE CAM NUT LOOSE. TIGHTENED LOOSE HANDLE CAM NUT REF: AMM 52-41-11.SDR SWAA2023030210606Battery Pack · faultyENROUTE; DURING ENTIRE FLIGHT; THE EMERGENCY LIGHTING SYSTEM ON AIRCRAFT LEFT (CA SIDE) FROM ROW 26 AFT FORWARD; AND INCLUDING THE AFT GALLEY AREA ILLUMINATED FOR APPROXIMATELY 30 SECONDS 6 MIN INTERV ENROUTE DURING ENTIRE FLIGHT THE EMERGENCY LIGHTING SYSTEM SDR SWAA2023030110555Battery Pack · intermittentAFT GALLEY EMERGENCY EXIT LIGHTS INTERMITTENTLY ILLUMINATE<[01] REMOVED AND REPLACED AFT GALLEY EMERGENCY EXIT LIGHTS BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2023022004315Girt Bar · looseFORWARD ENTRY GIRT BAR CLIP LOOSE<[01] ADJUSTED FWD ENTRY GIRT BAR CLIPS. PER AMM 25-66-00.SDR SWAA2023021502077Slide · out of adjustR2 DOOR ESCAPE SLIDE SKIRT RUBS AGAINST SCUFF PLATE WHEN OPEN/CLOSE DOOR.<[01] FAULT WAS RESOLVED USING MT 725-61-06 ON BARCODE TTG8Q00HMPRH;[02] VERIFIED STEP 1SDR SWAA2023021501428Battery Pack · inoperativeSEVERAL EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M1694 AND M1670 AS PER REF. B737 AMM 33-51-06-610-802. OPERATIONAL TEST OF EMERGENCY LIGHTS RELATED TO THESE BATTERY PACKS FOUND OK.;[02] VERIFIED STEP 1.;[03] PERFORSDR SWAA2023021503419Battery Pack · inoperativeSEVERAL EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M1694 AND M1670 AS PER REF. B737 AMM 33-51-06-610-802. OPERATIONAL TEST OF EMERGENCY LIGHTS RELATED TO THESE BATTERY PACKS FOUND OK.;[02] VERIFIED STEP 1.;[03] PERFORSDR SWAA2023021596650Panel · crackedAFT CARGO DOOR CUTOUT PANEL 142KW IS CRACKED.<[01] RECEIVED NEW AFT CARGO DOOR CUTOUT PANEL 142KW AND INSTALLATION TO BE ACCOMPLISH ON TASKCARD TTG8Q00GQ4MH.;[02] VERIFIED STEP #1.SDR SWAA2023021595846Scuff Plate · crackedAFT CARGO FWD SCUFF PLATE HAS A CRACK ON LOWER CUTOUT SIDE.<[01] RECEIVED WELDED SCUFF PLATE AND WORK WAS ACCOMPLISHED BY J.L WELDING INC AS PER SRM 53-60-15-2R-1.;[02] VERIFIED STEP 1SDR SWAA2022050301433None · deformedFLOORBOARD SAGGING AFT OF ROW 22 CENTER AISLE / [01] REPLACED FLOOR BOARD PER AMM 53-21-00SDR SWAA2022041191798Panel · crackedR/H BREAK PANEL CRACKED IN THE AIR CONDITIONING DISTRIBUTION BAY IN FORWARD CARGO COMPARTMENT AT B.S. 540. / [01] REMOVED AND REPLACED R/H BREAK PANEL AT STATION 540 IN A/C DISTRIBUTION BAY FWD CARGO COMPT. PER SRM 51-40-02.(FASTENERS)SDR SWAA2022041191797Panel · crackedL/H BREAK PANEL CRACKED IN THE AIR CONDITIONING DISTRIBUTION BAY IN FORWARD CARGO COMPARTMENT AT B.S. 540. / [01] REMOVED AND REPLACED L/H BREAKER PANEL AT STATION 540 IN THE A/C DISTRIBUTION BAY FWD CARGO COMPT. PER SRM 51-40-02. (FASTENERS).SDR SWAA2022041191999Bulkhead · crackedAFT CARGO FWD BULKHEAD LINER 142NWB HAS CRACK APPROX. 8 INCHES FROM BOTTOM EDGE AND APPROX. 6 INCHES IN LENGTH / [01] PERFORMED PERMANENT REPAIR OF AFT CARGO FWD BULKHEAD LINER 142NWB PER AMM 25-52-01SDR SWAA2022031882986Motor · inoperativeELECTRIC STAB TRIM INOP. / [01] REMOVED AND REPLACED STAB TRIM MOTOR PER AMM 27-41-71SDR SWAA2021112446572Girt Bar · out of adjustAFT SLIDE FO SIDE FALLING OUT OF CASE ; / [01] READJUSTED GIRT BAR AND SLIDE IAW AMM 25-66-00SDR SWAA2021112447377Slide · out of adjustAFT SLIDE FO SIDE FALLING OUT OF CASE ; / [01] READJUSTED GIRT BAR AND SLIDE IAW AMM 25-66-00SDR SWAA2021110841348Indicator · faultyON APPROACH HAD A TRAILING EDGE FLAP DISAGREEMENT-WITH FLAP HANDLE AT 30* THE FLAPS APPEARED TO BE BETWEEN 15* AND 25*. ; / [01] PERFORMED FIM TASKS 27-51TASKS 810- 801;802;803. ALL TESTS PASSED. NO REPORTED FAULTS.; [02] REMOVED AND REPLACED FLAP POSITION INDSDR SWAA2021070689048Lens · damagedOVERWING OVERHEAD EMEGENCY LIGHT LENS DAMAGED / R&R OVERWING OVERHEAD EMG LIGHT ASSY; OPS GOOD PER 33-51-00SDR SWAA2021062486116Lens · missingOVERHEAD BIN 14DEF LENS COVER MISSING. ( INTERIOR EMER EXIT LT SYS (EMERGENCY AISLE LIGHTS) ) / INSTALLED NEW LENS COVER 14DEF IAW AMM 33-51-03 CL#90060SDR SWAA2021060778760Cover · missingOVER WNG EMERGENCY EXIT LIGHT SIGN FORWARD LENS COVER MISSING / RESECURED OVERWING (OVERHEAD) LENS COVER IAW AMM 33-51-01SDR SWAA2021051471205Sign · detachedCENTER OVERWING EXIT SIGN FELL OFF / RESECURE CTR O/W EXIT SIGN AS REQID PER AMM 20-00-00SDR SWAA2021042365110Lens · displacedCEILING EMERGENCY EXIT LENS FOR OVERWING EXIT WAS DISPLACED. / RESECURED CEILING EMER EXIT LENS COVER FOR OVERWING EXIT PER SIP. LIGHT CHECKED GOOD.SDR SWAA2021040761429Floor Panel · crackedFWD CARGO PANEL 120ZAC WORN/CRACKED. / REMOVED AND REPLACED FWD CARGO PANEL 120ZAC PER AMM 25-32-09SDR SWAA2021040659459Floor Panel · corrodedAFT CARGO FLOOR PNL 140DF HAS NUMEROUS AREAS OF CORROSION AT FASTENER HOLES / REMOVED + REPLACED AFT CARGO FLOOR PNL 140DF PER AMM 25-52-10. OK TO INSTALL IS ON SA-M 565S IN 453A2610-20SDR SWAA2021040757474Support Angle · crackedRIGHT WING ORSS 279 UPPER FIXED TRAILING EDGE PANEL SUPPORTANGLE CRACKED. / REMOVED AND REPLACED UPPER FIXED TRAILING EDGE PANEL SUPPORT ANGLE IAW SRM 51-40-02 (S/N A1184611)SDR SWAA2021082510271Angle · corrodedLH TRANS. ANGLE HAS CORR. STA 500 TO 500D / REPAIRED L/H TRANSITION ANGLE FROM STA. 480 T10 TO STA. 500D T10 PER SRM 53-00-53-2R-5 AND EA 21-153-00635; PART1. SEE SA-M FROM 326 S/N A1184588 FOR INDIVIDUAL WORK ACCOMPLISHED..SDR SWAA2021082510270Angle · corrodedRH TRANS. ANGLE HAS CORR. 500A TO 500D / REPLACED TRANSISITON ANGLE SECTION FROM STA 500A TO 500G +10 PER SRM 53-00-53-2R-5 + EA 21-153-00635 PT 1 + PT 2SEE SA-M 326: A1184585SDR SWAA2021082510269Angle · corrodedRH TRANS. ANGLE HAS CORR. 500E TO 500I / REPLACED TRANISTION ANGLE SECTION FROM STA 500A TO 500G +10 PER SRM 53-00-53-2R-5 + EA .21-153-00635 PT1 +PT 2SEE SA-M 326: A1184583SDR SWAA2021040655866Floor Panel · delaminatedCABIN FLOOR PANEL 241 AF HAS FIBERS UP AND APART / REMOVED AND REPLACED CABIN FLOOR PANEL 241AF PER AMM 53-21-00.SDR SWAA2021040655696Angle · corrodedAFT CARGO RT TRANSITION ANGLE HAS NUMEROUS AREAS OF CORROSION OUT OF LIMITS FROM 727F + 15.5 INCHES TO 767. / REMOVED AND REPLACED SECTION TRANSITION ANGLE R/H FROM STA 727E + 10 TO 767 PER SRM. 51-10-02 INSTALLED SPLICES TRANSITION ANGLE PER SRM. 53-00-53-2R-SDR SWAA2021040755277Angle · corrodedAFT CARGO FLOOR STRUCTURE HAS CORROSION ON R/H TRANS ANGLE FROM STA 767-787 / REMOVED ERROR. ON TRANSITION ANGLE MATERIAL REMOVED FOUND OUT OF LIMITS PER SRM. 51-10-02; 53-00-53-1A-2; REMOVED AMD REPLACED R/H TRANSITION ANGLE FROM STATION 767 TO 793PER SRM 51-SDR SWAA2021040754558Plate · brokenR WING REAR SPAR ; OUTBD WAFFLE PLATE FOR PANEL #65EB HAS BROKEN NUT PLATE / REMOVED AND REPLACED WAFFLE PLATE FOR PANEL 651EB PER SRM 51-40-02
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