N8659D
Service difficulty reports · 81
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 = 'N8659D' 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 = 'N8659D' 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 SWAA2026100554194Slide · detachedAFT SERVICE DOOR SLIDE FELL OUT OF THE CONTAINER. REINSTALLED R2 DOOR SLIDE IAW MT 725-61-06.SDR SWAA2026021168830Bulb · inoperativeAFT GALLEY OVERHEAD EMERGENCY EXIT SIGN BULB INOPERATIVE. REPLACED THE BULB AND PERFORMED A GOOD TEST IAW AMM 33-51-01-960-801.SDR SWAA2026021168829Bulb · inoperativeAFT LEFT OVERWING DOOR EMERGENCY EXIT SIGN HAD TWO BULBS INOPERATIVE. REPLACED THE BULB AND PERFORMED A GOOD TEST IAW AMM 33-51-01-960-801.SDR SWAA2026012964546Lens · missingLENS MISSING FROM CEILING LIGHT AT ROW 2 EMERGENCY LIGHT. INSTALLED THE MISSING LENS COVER IAW SIP.SDR SWAA2025111033650Window · failedL1 WINDOW OUTER LAYER SHATTERED AT FL350 NO CABIN PRESSURE CHANGES. R & R L1 WINDOW PER AMM 56-11-11 AND WHCU PER AMM 30-41-11. LEAK AND OP CHECKED GOOD.SDR SWAA2025010880115Floorbeam · crackedWING CENTER SECTION FLOOR SUPPORT AT STA 540 LBL1 AND RBL1 HAS CRACK STREAMER ATTACHED. DOT#P862.<[01] REMOVED AND REPLACED FLOOR SUPPORTS PN 143A5240-63 PO#0 AND 143A5240-64 PO#1109294.1 AT STA 540 LBL1 AND RBL1 IAW B737NG-SRM 51-40-02 AND BAC DWG#143A0060 RESDR SWAA2025010680117Floor Panel · pulledMAIN CABIN FLOOR PANEL 231XF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 231XF PEELING FIBERS IAW B737-800 SRM 53-00-50.;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]SDR SWAA2025010680118Floor Panel · pulledMAIN CABIN FLOOR PANEL 231YF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 231YF PEELING FIBERS IAW B737-800 SRM 53-00-50;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]SDR SWAA2025010680119Floor Panel · pulledMAIN CABIN FLOOR PANEL 242AF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 242AF PEELING FIBERS IAW B737-800 SRM 53-00-50;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]SDR SWAA2025010680120Floor Panel · pulledMAIN CABIN FLOOR PANEL 241AF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 241AF PEELING FIBERS IAW B737-800 SRM 53-00-50;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]SDR SWAA2025010680121Floor Panel · pulledMAIN CABIN FLOOR PANEL 241DF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 241DF PEELING FIBERS IAW B737-800 SRM 53-00-50;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT).SDR SWAA2025010680122Floor Panel · pulledMAIN CABIN FLOOR PANEL 241BF HAS PULLED FIBERS<[01] PREFORMED PERMEANT REPAIR TO MAIN CABIN FLOOR PANEL 241BF PEELING FIBERS IAW B737-800 SRM 53-00-50;[02] 04 - REPAIRED PER [SRM 53-00-50-2R-0-B00275 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]SDR SWAA2025010879499Bracket · crackedCRACK FOUND ON R/H VAPOR BARRIER LOWER BRACKET @ STA 663.75<[01] REMOVED R/H VAPOR BARRIER ANGLE; LOCATED AND DRILLED NEW VAPOR BARRIER ANGLE; PERFORMED OPEN HOLE HFEC OF AL HOLES IN THE REPAIR AREA USING T8257F CAL DUE 13MAY25 IAW B737 NDTM PT. 6 51-00-00 PROSDR SWAA2025010879500Angle · crackedL/H VAPOR LOWER ANGLE BARRIER CRACKS (2) FOUND @ STA 663.75<[01] REMOVED L/H VAPOR BARRIER ANGLE; LOCATED AND DRILLED NEW VAPOR BARRIER ANGLE; PERFORMED OPEN HOLE HFEC OF AL HOLES IN THE REPAIR AREA USING T8257F CAL DUE 13MAY25 IAW B737 NDTM PT. 6 51-00-00 PROSDR SWAA2025010879484Skin · delaminatedR/H WING O/B AFT FLAP DELAMINATED AT THE I/B AFT CORNER.<[01] ACCOMPLISHED TASK CARD R/H WING O/B AFT FLAP DELAMINATED AT THE I/B AFT CORNER. [TTG8Q00XQKUQ].<BR>B737-800 AMM 27-51-22;[02] VERIFIED ACCOMPLISHED TASK CARD R/H WING O/B AFT FLAP DELAMINATED AT THESDR SWAA2025010879027Vapor Barrier · crackedCR --- ACCOMPLISH GVI OF L/H VAPOR BARRIER ANGLE FOR CRACKS<[01] PERFORMED GVI OF L/H VAPOR BARRIER IAW 51-10-04. CRACKS (2) FOUND AT STATION 663.75;[02] PERFORMED GVI OF L/H VAPOR BARRIER IAW 51-10-04. CRACKS (2) FOUND AT STATION 663.75SDR SWAA2025010879028Vapor Barrier · crackedCR --- ACCOMPLISH GVI OF R/H VAPOR BARRIER ANGLE FOR CRACKS<[01] PERFORMED GVI OF R/H VAPOR BARRIER IAW 51-10-04. CRACK FOUND AT STATION 663.75;[02] PERFORMED GVI OF R/H VAPOR BARRIER IAW 51-10-04. CRACK FOUND AT STATION 663.75SDR SWAA2024120272805Sensor · inoperativeFLAPS WOULDNT RETRACK TO ZERO 0. FLAPS STAYED AT TWO 2<[01] R&R RIGHT WING FLAP TORQUE TUBE SUPPORT ASSEMBLY PER AMM 27-51-59;[02] R&R #8 FLAP SKEW SENSOR PER AMM 27-59-01SDR SWAA2024102953871Cover · looseEMER EXIT SIGN COVER LOOSE; O'WING EXIT F/O SIDE<[01] INSTALLED COVER AS PER MM 33-51-001SDR SWAA2024091336665Rib · crackedUPPER TAB ON LEFT WING DEFLECTION CONTROL RIB CRACKED/SEPARATED<[01] REMOVED DAMAGE; FLAP PEENED AREA AND TREATED AND PRIMED REF 57-51-02-2R-3.;[02] ACCOMPLISHED REPAIR 3 - LEFT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB CRACK DAMAGE REPSDR SWAA2024091336664Rib · crackedLEFT WING DEFLECTION CONTROL RIB ATTACHMENT CLIP UNDER FIXED UPPER PANEL CRACKED<[01] REPLACED LEFT WING DEFLECTION CONTROL RIB ATTACHMENT CLIP UNDER FIXED UPPER PANEL PER SRM 51-40-02SDR SWAA2024091336666Bracket · crackedLEFT WING PANEL 551GB INBOARD AFT SUPPORT ROD BRACKET CRACKED<[01] 01 - REMOVED AND REPLACED BRACKET PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]SDR SWAA2024083031005Rivet · missingFWD RIGHT SERVICE DOOR GIRT BAR RETAINER CLIP MISSING RIVET<[01] INSTALLED MISSING RIVET REF SRM 51-40-02SDR SWAA2024081927611Girt Bar · looseRT FWD SERVICE DOOR. RT LOWER GRIT BAR SILVER CLIP THAT HOLDS THE GRIT BAR IS LOOSE<[01] PERFORMED REPAIR PER EA-M-23-125-01839 FOR FWD SVC GRIT BAR CLIPSSDR SWAA2024080519893Lens · missingOVERWING EXIT SIGN MISSING COVER ON CEILING<[01] REINSTALLED EXIT LENS REF. AMM 33-51-01. LIGHT FUNCTIONS NML.SDR SWAA2024061300041Light · looseCENTER ISLE PHOTOLUMINESCENT ESCAPE PATH MARKING LOOSE CAPT SIDE BETWEEN ROW 12-13<[01] RESECURED PER AMM 33-51-15SDR SWAA2024031965467Skin · delaminatedL/H O/B TRAILING EDGE FLAP REQUIRES REPLACEMENT. REMOVED LH OTBD AFT FLAP IAW AMM 27-51-22. REMOVED AND REPLACED LH OB AFT FLAP PER AMM 27-51-26.SDR SWAA2024031864684Skin · delaminatedLH WING OUTBD TRAILING EDGE FLAP IS DELAMINATED AT LOWER INBD END. 17IN X 9IN<[01] CW EA 24-127-00702;[02] CWSDR SWAA2023100403928Slide · low pressureAFT SERVICE DOOR SLIDE PRESSURE GAUGE OUT OF LIMITS<[01] R&R SLIDE PER AMM 25-66-01 AND TC 725-61-06-AS;[02] INSPECTED THAT SLIDE WAS R&R PER AMM 25-66-01 AND TC 725-61-06-ASSDR SWAA2022120776196Intercostal · out of adjustSUPPLEMENTAL INFORMATION: REMOVED INTERCOSTAL BETWEEN STA 947 AND 967 AT RBL 51 FOR EVALUATION OF FLOOR PANEL HOLE ALIGNMENT.<[01] INSTALLED NEW INTERCOSTAL BETWEEN STA 947 AND 967 AT RBL 51 PER SRM 51-40-02 AND EA 22-153-03489-WIP1 (TTG8Q00GCT30).;[02] INSPECSDR SWAA2022120976197Skin · damagedNR 3 SLAT LEADING EDGE SKIN IS WRINKLED AND BENT AROUND FASTENERS. APROX 6 IN. LONG AND COMMON TO THE INBD MAIN TRACK. REMOVED THE NR 3 LEADING EDGE SLAT AND REPLACED WITH NEW SLAT IAW AMM 27-81-21. INSPECTED THE RIG AND OPS CHECK OF THE NR 3 SLAT.SDR SWAA2022113075863Floorbeam · damagedFLOORBEAM HAS 5 EACH ELONGATED FASTENER HOLES ON UPPER SURFACE. BS 950, RBL 28-46. REMOVED AND REPLACED FLOORBEAM IAW EA 22-153-03502 AND SRM 51-40-02.SDR SWAA2022113071981Battery Pack · weakEMERGENCY LIGHT BATTERY PACKS WEAK. REPLACED THE BATTERY PACKS IAW MM 33-51-06.SDR SWAA2022113069985Angle · corrodedFWD CARGO BS 490-500A, RT TRANSITION ANGLE CORRODED AROUND NUT-PLATE HOLES. REMOVED SURFACE CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 51-40-02.SDR SWAA2022113069987Angle · corrodedFWD CARGO BS 500B-500D, RT TRANSITION ANGLE CORRODED AROUND NUT-PLATE HOLES. REMOVED SURFACE CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED THE ANGLE IAW SRM 53-00-53-1A-2.SDR SWAA2022113069997Angle · corrodedFWD CARGO BS 500D-500F, RT TRANSITION ANGLE CORRODED AROUND NUT-PLATE HOLES. REMOVED SURFACE CORROSION AND FOUND TO BE OUT OF LIMITS.SDR SWAA2022113069999Angle · corrodedFWD CARGO BS 500F-500I, RT TRANSITION ANGLE CORRODED AROUND NUT-PLATE HOLES. REMOVED SURFACE CORROSION AND FOUND TO BE OUT OF LIMITED. LOCATED AND DRILLED A NEW RH TRANSITION ANGLE IAW SRM 51-40-02. INSTALLED THE NEW TRANSITION ANGLE IAW SRM 51-40-02.SDR SWAA2022120769957Angle · corrodedAFT CARGO RT SIDE PLATE CHANNEL HAS CORROSION AROUND FASTENER HOLES RBL 21, BS 727G-727H. THE TRANSITION ANGLE TO BE REPLACED ON NR TTG8Q00G0A7F.SDR SWAA2022120769958Angle · corrodedAFT CARGO RT SIDE PLATE CHANNEL HAD CORROSION AROUND FASTENER HOLES RBL 21, BS 727H-727I. THE RT TRANSITION ANGLE TO BE REPLACED ON NR TTG8Q00G0A7F.SDR SWAA2022120769959Angle · corrodedAFT CARGO R/H SIDE PLATE CHANNEL HAS CORROSION AROUND FASTENER HOLES RBL 21; BS 727I-727J. RT TRANSITION ANGLE TO BE REPLACED ON NR TTG8Q00G0A7F.SDR SWAA2022113069956Channel · corrodedAFT CARGO RT CHANNEL CORRODED AROUND FASTENER HOLES, RBL 21, BS 727F-727G. CHANNEL REPAIRED IAW SRM 53-00-53-2R-5, REPAIR 5, AND EAM-22-153-01550.SDR SWAA2022113069960Channel · corrodedAFT CARGO RT CHANNEL CORRODED AROUND FASTENER HOLES, RBL 21, BS 747-767. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM.53-00-53-1A-1. LOCATED AND DRILLED A NEW CHANNEL IAW SRM. 53-00-53-2R-5. TREATED AND PRIMED IAW SRM. 51-20-02. INSTALLED THE NSDR SWAA2022113069966Channel · corrodedAFT CARGO RT CHANNEL CORRODED AROUND FASTENER HOLES, RBL 21, BS 767-787. REMOVED THE CHANNEL DUE TO OUT OF LIMITS IAW SRM 51-40-02. LOCATED AND DRILLED, AND INSTALLED THE NEW CHANNEL IAW SRM 51-10-02.SDR SWAA2022113069943Channel · corrodedAFT CARGO R/H SIDE PLATE CHANNEL HAS CORROSION AROUND FASTENER HOLES RBL 21; STA 727J-747. RT TRANSITION CHANNEL REPLACED ON NR TTG8Q00G0A7F.SDR SWAA2022113069562Floorbeam · damagedFLOORBEAM BS 967 HAS ELONGATED FASTENER HOLES AT THE THREE MOST O/B HOLES ON R/H SIDE ON UPPER SURFACE.SDR SWAA2022113069556Floorbeam · damagedFLOORBEAM HAS 5 EACH ELONGATED FASTENER HOLES ON UPPER SURFACE, BS 950, RBL 28 - 46. REMOVED FLOORBEAM IAW SRM 51-40-02. LOCATED AND DRILLED A NEW FLOORBEAM IAW SRM 51-40-05. INSTALLED THE NEW FLOORBEAM IAW SRM 51-40-02.SDR SWAA2022120769206Handle · looseAFT SERVICE DOOR HANDLE LOOSE AT CAM PLATE SHAFT. SECURED THE HANDLE IAW AMM 20-10-44, AND AMM 52-41-11.SDR SWAA2022113069208Seal · crackedLT. STAB FWD UPPER SLIDING SEAL WORN AND CRACKED. R & R THE SEAL IAW MM 53-31-31.SDR SWAA2022113069207Seal · crackedRT. STAB FWD UPPER SLIDING SEAL CRACKED. MATCH DRILLED AND RIVETED BRACKETS ON NEW SLIDER IAW SRM 51-40-02. REMOVED AND REPLACED R/H UPPER SLIDING SEAL PER AMM 53-31-31.SDR SWAA2022100552469None · inoperativeFWD LH EMERGENCY LIGHTS INOP. / [01] REPLACED FWD LH EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.
Back to N8659D