N8609A
Service difficulty reports · 197
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 = 'N8609A' 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 = 'N8609A' 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 SWAA2025011776387Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BS685 AND RBL24.82 LOWER POSITION AT PASSENGER CABIN 2024-762958<[01] REPLACED ANGLE LOCATED BS685 AND RBL24.82 LOWER POSITION AT PASSENGER CABIN I.A.W B737-800 SRM 51-40-02 AND DWG 273A9110 REV:A. SEE INDIVIDUAL SIGN OFF BELOW;[SDR SWAA2025011775956Floorbeam · corrodedCORROSION ON EXISTING REPAIR ON UPPER T-CHORD FLOOR BEAM LOCATED BS947.5 AT RBL 50 AT AFT GALLEY AREA 2024-762763<[01] TOOL USED ON STEP 5 ULTRASONIC THICKNESS GAUGE P/N 45MG; S/N 130066701 DUE DATE 12-JUL-25;[02] PERFORMED PERMANENT REPAIR ON FLOOR BEAM 947.5SDR SWAA2025011676380Floor Support · crackedCRACK ON ANGLE FLOOR STRUCTURE LOCATED BTW BS380 TO BS400 AND LBL11 AT PASSENGER CABIN 2024-762945<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 11 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 143A5400 SHEET 13SDR SWAA2025011775953Floorbeam · corrodedCORROSION ON UPPER CHORD FLOOR BEAM 328 RBL21.79 AND WL208.1 AT FWD GALLEY AREA 2024-762739<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 10-JUN-25.;[02] TOOL USED ON STEP 22 RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: SDR SWAA2025011775317Light · inoperativeINOP EMERGENCY EXIT LIGHT ON SIDEWALL ROW 13 LEFT AT PASSENGER CABIN 2024-762677<[01] REPLACED EMERGENCY EXIT LIGHT ON SIDEWALL ROW 13 LEFT AT PASSENGER CABIN I.A.W. B737-800 AMM 33-51-01-960-802 OPERATIONAL TEST IS OK.;[02] TASK COMPLETEDSDR SWAA2025011775314Light · inoperativeINOP EMERGENCY EXIT LIGHT ON SIDEWALL ROW 13 RIGHT AT PASSENGER CABIN 2024-762678<[01] REPLACED EMERGENCY EXIT LIGHT ON SIDEWALL ROW 13 RIGHT AT PASSENGER CABIN I.A.W. B737-800 AMM 33-51-01-960-802 OPERATIONAL TEST IS OK.;[02] TASK COMPLETEDSDR SWAA2025011775319Lens · crackedCRACK EMERGENCY LIGHT LENS ON CEILING PANEL ROW 3 AT PASSENGER CABIN 2024-762687<[01] REPLACED EMERGENCY LIGHT LENS ON CEILING PANEL ROW 3 AT PASSENGER CABIN IAW B737-800 AMM 33-51-03-960-803;[02] REPLACED EMERGENCY LIGHT LENS ON CEILING PANEL ROW 3 AT PASSENGSDR SWAA2025011775320Lens · crackedCRACK EMERGENCY LIGHT LENS ON STRONGBACK ROW 18RH AT PASSENGER CABIN 2024-762688<[01] REPLACED EMERGENCY LIGHT LENS ON STRONGBACK ROW 18RH AT PASSENGER CABIN IAW B737-800 AMM 33-51-03-960-803;[02] REPLACED EMERGENCY LIGHT LENS ON STRONGBACK ROW 18RH AT PASSENGSDR SWAA2025011775403Light · deterioratedDETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT SIDE AT PASSENGER CABIN (9 EA) 2024-762698<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT SIDE AT PASSENGER CABIN (9 EA) IAW B737-800 AMM-33-51-15-960-801;[02] CERTIFIED WORK PERFORMEDSDR SWAA2025011775409Light · deterioratedDETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT SIDE AT PASSENGER CABIN (9 EA) 2024-762699<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT SIDE AT PASSENGER CABIN (9 EA) IAW AMM-33-51-15-960-801;[02] CORRECTED STEP 1: REPLACED PHOTOLUMINESSDR SWAA2025011775121Vapor Barrier · crackedCRACK VAPOR VARRIER LOCATED BS 663.75 ON LBL 48 AT MAIN WHEEL WELL COMPARTMENT 2024-762654<[01] TOOL USED: UT FLAW DETECTOR; P/N: EPOCH 650; S/N: 190984811; CAL DUE DATE: 11-JAN-25;[02] REPAIRED VAPOR VARRIER LOCATED BS 663.75 ON LBL 48 AT MAIN WHEEL WELL COMPSDR SWAA2024120273020Lamp · inoperativeCALL LIGHT ON AFT OVERHEAD EXIT SIGN INOP<[01] REMOVED AND REPLACED O/H CALL LIGHT LAMP REF BOEING 737 AMM 33-51-01. OPS CHECKED GOOD.SDR SWAA2024091838492Light · brokenOVERWING EXIT ROW OVERHEAD EMERGENCY EXIT LIGHT BROKE<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-00-710-801-NG (EMERGENCY LIGHTS - OPERATIONAL TEST - PERMANENT)];[02] 01 - REMOVED AND REPLACED PER [AMM 33-51-00-710-801-NG (EMERGENCY LIGHTS - OPERATIONAL TESSDR SWAA2024042579212Slide · dislodgedR-1 DOOR SLIDE PARTIALLY OUT OF CONTAINER<[01] RE-INSTALLED SLIDE IN CONTAINER ON R-1 DOOR PER MT 725-61-06SDR SWAA2024030759722Battery Pack · inoperativeRIGHT FORWARD OVERWING EMERGENCY EXIT; EMERGENCY LIGHTS OUT<[01] 01 - REMOVED AND REPLACED RH OVERWING EXIT BATTERY PACK AND CHARGER ASSY M1695 PER AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2023111319122Engine · stalledRIGHT ENGINE COMPRESSOR STALL; HIGH AIRFRAME VIBRATION. SHUT DOWN ENGINE PER QRL; QRH. COMPRESSOR STALL OCCURRED AROUND 6;000 FT ON CLIMB OUT.<[01] R/R #2 ENGINE IAW 771-00-01 (REM/INST - POWER PLANT) REF. [TTG8Q008M2ZC]SDR SWAA2023110316746Sign · looseEMERGENCY EXIT SIGN OVERWING ABOVE NEEDS TO BE FIXED<[01] RE-SECURED PER SIPSDR SWAA2023072581446Battery Pack · inoperativeFIRST 3 LH INTERIOR EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT ROW 7 ABC REF AMM 33-51-06. OPS CHECKED GOODSDR SWAA2023061257671Light · inoperativeAFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] RELAMPED AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT REF AMM 33-51-04.SDR SWAA2023021501114Panel · elongatedPANEL 193B HAS MULTIPLE ELONGATED FASTENER HOLES<[01] REPAIRED PER SRM 51-70-04-2R-9.SDR SWAA2023021598707Fairing · cracked#6 SUPPORT FAIRING 642BB IS CRACKED AT LOWER I/B SURFACE APPROX. THE CENTER POINT OF THE FAIRING. (MARKED) #6 SUPPORT FAIRING 642BB IS DAMAGED AT LOWER I/B SURFACE APPROX. THE CENTER POINT OF THE FAIRING. (MARKED)<[01] REMOVED AND REPLACED #6 AFT FAIRING PER ASDR SWAA2023021595385Fairing · elongated542EB FAIRING TAILCONE HAS LOOSE FASTENERS & ELONGATED HOLES.<[01] REMOVED AND REPLACED AFT TAIL CONE IAW SRM 51-41-02.;[02] C/W INSPECTION.SDR SWAA2023021595373Floor Panel · pulledCABIN FLOOR BOARD 242BF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRX4.;[02] C/W INSPECTION.SDR SWAA2023021595372Floor Panel · pulledCABIN FLOOR BOARD 241FF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRX6.;[03] C/W INSPECTION.SDR SWAA2023021595365Floor Panel · pulledCABIN FLOOR BOARD 241EF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRX8.;[03] C/W INSPECTION.SDR SWAA2023021595364Floor Panel · pulledCABIN FLOOR BOARD 241DF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXA.;[03] C/W INSPECTION.SDR SWAA2023021595371Floor Panel · pulledCABIN FLOOR BOARD 241CF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXC.;[03] PART ADDED.;[04] C/W INSPECTION.SDR SWAA2023021595363Floor Panel · pulledCABIN FLOOR BOARD 241BF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXE.;[03] C/W INSPECTION.SDR SWAA2023021595370Floor Panel · pulledCABIN FLOOR BOARD 241AF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXG.;[03] C/W INSPECTION.SDR SWAA2023021595362Floor Panel · pulledCABIN FLOOR BOARD 232SF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXL.;[03] C/W INSPECTION.SDR SWAA2023021595369Floor Panel · pulledCABIN FLOOR BOARD 232RF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXN.;[03] C/W INSPECTION.SDR SWAA2023021595368Floor Panel · pulledCABIN FLOOR BOARD 231ZF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXQ.;[03] C/W INSPECTION.SDR SWAA2023021595361Floor Panel · pulledCABIN FLOOR BOARD 231YF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXS.;[03] C/W INSPECTION.SDR SWAA2023021595360Floor Panel · pulledCABIN FLOOR BOARD 231XF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXU.;[03] C/W INSPECTION.SDR SWAA2023021595367Floor Panel · pulledCABIN FLOOR BOARD 242AF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWS0B.;[03] C/W INSPECTION.SDR SWAA2023021595359Floor Panel · pulledCABIN FLOOR BOARD 242CF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRX2.;[03] C/W INSPECTION.SDR SWAA2023021595366Floor Panel · pulledCABIN FLOOR PANEL 242DF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRX0.;[03] C/W INSPECTION.SDR SWAA2023021595376Panel · deformedFLIGHT COMPARTMENT FLOOR PANEL 211AF DEFORMED<[01] LOCATED AND DRILLED NEW ACCESS PANEL PER SRM 51-40-05.;[02] C/W INSPECTIONSDR SWAA2023021594524Barrier · debondedLEFT MAIN WHEEL WELL. STA 663 VAPER BARRIER. PREVIOUS REPAIR IS BECOMING DISBONDED. LOCATED AT LBL 44; WL 165. MARKED LEFT MAIN WHEEL WELL. STA 663 VAPER BARRIER. PREVIOUS REPAIR IS BECOMING DISBONDED. LOCATED AT LBL 44 WL 165. MARKED<[01] INSTALLED REPAIR PERSDR SWAA2022062923028Slide · looseFWD ENTRY DOOR SLIDE FALLING OUT OF BUSTLE / [01] REF AMM 25-66-01. REPACKED SLIDE AS REQUIRED. OK FOR SERVICESDR SWAA2022071222429Light · inoperativeSUSPECT AFT OVERWING EXIT LIGHT / [01] SLAVED IN LIGHT ASSEMBLIES AT 16 AND 21; NO HELP. RAN OUT OF TIME; SUSPECT AFT OVERWING EXIT LIGHT.SDR SWAA2022041893774Handle · looseCABIN FWD ENTRY DOOR LOWER AFT ASSIST HANDLE IS LOOSE / [01] READJUSTED CABIN FWD ENTRY DOOR LOWER AFT ASSIST HANDLE PER AMM 20-50-11;[02] READJUSTED CABIN FWD ENTRY DOOR LOWER AFT ASSIST HANDLE PER AMM 52-11-31SDR SWAA2022041893542Vapor Barrier · crackedL/H W/W FWD VAPOR WEB CRACKED JUST INBD OF A SYSTEM PRESSURE MODULE. CRACK MEASURES APPROX 4 / [01] L/H W/W FWD VAPOR WEB CRACKED JUST INBD OF ?A? SYSTEM PRESSURE MODULE. CRACK MEASURES APPROX 4?SRM 57-10-10-1A-2-B00453 (CRACK - STOP DRILL AND SEAL - DVI EVERYSDR SWAA2021122053710Rod · brokenRIGHT I/B TE FLAP HANGING DOWN WITH FLAPS UP. REPLACED BROKEN AFT FLAP DRIVE ROD AND DRIVE ROD FITTING IAW AMM 27-51-14. OPS CHECK GOOD.; [02] VERIFIED CORRECT INSTALLATION OF FLAP DRIVE ROD PER AMM 27-51-14.SDR SWAA2021121350928Battery Pack · inoperativeRH MID CABIN 3 EMERGENCY LIGHTS FWD OF EMERGENCY EXIT ROW INOP. ; / [01] R&R R/H MID CABIN 3 EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06SDR SWAA2021072295798Bulkhead Web · crackedLEFT WHEEL WELL VAPOR BARRIER CRACKED APPROX 6.5' EXTENDING O/B & DOWN FROM LBL 45.64 AND 9' FROM THE BOTTOM.APPLIED INTERIM PATCH REPAIR IAW SRM 57-10-10-1A-2 AND AVIATION PARTNERS BOEING STRUCTURAL REPAIR MANUAL SUPPLEMENT 737-800 57-10-10. REFER TO ATTACHEDSDR SWAA2021070890939Bulkhead Web · crackedCENTER WING REAR SPAR; FUSEAGE STA 663 VAPOR BARRIER WEB CRACKED IN RH WHEEL WELL AT RBL 31.83 - CRACK MEASURES APROX 4.00' ACTION REQUIRED REPETATIVE ACTION REQUIRED DO A CISUAL INSPECTION OF THE REPAIR AREA; MAKE SURE THE CRACK AS NOT GROWN PAST THE INTERIM SDR SWAA2021041964884Cabin Air Sys · odorDURING FLIGHT; FLIGHT ATTENDANTS STATED HEAVY PROPANE LIKE SMELL IN CABIN. SMELL SUBSIDED IN CRUSIE. AT GATE RAMPERS STATED PROPANE SMELL IN FWD CARGO BIN. / PERFORMED SMOKE OR FUMES IN CABIN CORD INSP PER AMM 05-51-56 NO DEFECTS NOTED A/C OK FOR CONTINUED SERSDR SWAA2021031153510Battery Pack · inoperativeEMERGENCY AISLE LIGHTS AT ROW 18R AND 21R INOP / REMOVED AND REPLACED BATTERY PACK AT STA 727R PER MM 33-51-06. EMERGENCY LIGHTS OPS CK GOODPER MM 33-51-00SDR SWAA2021031150318Angle · corrodedFWD CARGO; R/H TRANSITION ANGLE STA 500A TO 500G +10 NEEDS TO BE REPLACED DUE TO CORROSION OUT OF LIMITS REF N/R'S D177478; D177483; D177484 / REPLACED RH TRANS. ANGLE STA 500A TO STA. 500G+10 IAW SRM 53-00-53-2R-5 AND EA 21-153-00430.
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