N8614M
Service difficulty reports · 215
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 = 'N8614M' 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 = 'N8614M' 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 SWAA2025040702529Angle · crackedCRACK ANGLE - CLIP LOCATED BS 500H AT LEVEL STR26R AFT POSITION AT FWD CARGO COMPARTMENT 2025-172034<[01] REPLACED ANGLE CLIP LOCATED BS 500H AT LEVEL STR26R AFT POSITION AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A75SDR SWAA2025040815098Angle · crackedCRACK ANGLE OUTBOARD AUXILIARY TRACK OF SLAT 7 AT TR WING 2025-171985<[01] REPLACED ANGLE LOCATED OUTBOARD AUXILIARY TRACK OF SLAT 7 AT RT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFFSDR SWAA2025040715100Nut Plate · crackedCRACK RAIL NUT PLATE OUTBOARD FIXED LEADING EDGE OFSS 604 AT RT WING 2025-171990<[01] REPLACED RAIL NUT PLATE OUTBOARD FIXED LEADING EDGE OFSS 604 AT RT WING BETWEEN OSS 362.51 TO 384.24 IAW. B737-800 SRM 51-10-02-0G-0 ITEM 9 ; SRM 51-40-02-0G-0 AND DWG 112A44SDR SWAA2025040702220Nut Plate · crackedCRACK RAIL NUT PLATE OUTBOARD FIXED LEADING EDGE OFSS 604 AT RT WING 2025-171990<[01] REPLACED RAIL NUT PLATE OUTBOARD FIXED LEADING EDGE OFSS 604 AT RT WING BETWEEN OSS 362.51 TO 384.24 IAW. B737-800 SRM 51-10-02-0G-0 ITEM 9 ; SRM 51-40-02-0G-0 AND DWG 112A44SDR SWAA2025040702222Nut Plate · crackedCRACK RAIL NUT PLATE OUTBOARD FIXED LEADING EDGE OFSS 632 AT RT WING 2025-171993<[01] REPLACED RAIL NUT PLATE OUTBOARD FIXED LEADING EDGE OFSS 632 BETWEEN OSS 384.24 TO 409.09 AT RT WING IAW. B737-800 SRM 51-10-02-0G-0 ITEM 9 ; SRM 51-40-02-0G-0 AND DWG 112A44SDR SWAA2025040715101Nut Plate · crackedCRACK RAIL NUT PLATE OUTBOARD FIXED LEADING EDGE OFSS 632 AT RT WING 2025-171993<[01] REPLACED RAIL NUT PLATE OUTBOARD FIXED LEADING EDGE OFSS 632 BETWEEN OSS 384.24 TO 409.09 AT RT WING IAW. B737-800 SRM 51-10-02-0G-0 ITEM 9 ; SRM 51-40-02-0G-0 AND DWG 112A44SDR SWAA2025040702221Nut Plate · crackedCRACK RAIL NUT PLATE OUTBOARD FIXED LEADING EDGE OFSS 567 AT RT WING 2025-171991<[01] REPLACED RAIL NUT PLATE OUTBOARD FIXED LEADING EDGE OFSS 567 AT RT WING IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG:112A4402 SHEET:41 REV.A; TOOL USED DIGITAL CSDR SWAA2025040702216Angle · crackedCRACK ANGLE OUTBOARD AUXILIARY TRACK OF SLAT 7 AT TR WING 2025-171985<[01] REPLACED ANGLE LOCATED OUTBOARD AUXILIARY TRACK OF SLAT 7 AT RT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFFSDR SWAA2025040402217Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2025-171980 <[01]. TOOLS USED: POWER PACK: P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 17-JUN-25; THERMOMETER P/N: FLUKE 566; S/N: 587770091WS; DUE DATE: 30-JAN-26; MULTIMETER PSDR SWAA2025040701856Floor Support · corrodedCORROSION ON INTERCOSTAL LOCATED BTW BS 947 TO BS 967 RBL 48 WL 208.1 AT AFT GALLEY AREA 2025-171971<[01] TOOL USED ON STEP 4:ULTRASONIC EQUIPMENT P/N 45MG; S/N:232017609; DUE DATE: 08-OCT-25.;[02] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 947 TO BS 96SDR SWAA2025040715091Floor Support · corrodedCORROSION ON INTERCOSTAL LOCATED BTW BS 947 TO BS 967 RBL 48 WL 208.1 AT AFT GALLEY AREA 2025-171971<[01] TOOL USED ON STEP 4:ULTRASONIC EQUIPMENT P/N 45MG; S/N:232017609; DUE DATE: 08-OCT-25.;[02] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 947 TO BS 96SDR SWAA2025040701623Floorbeam · corrodedCORROSION ON FLOOR BEAM LOCATED BS 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2025-171968<[01] TOOL USED ON STEP 9 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 210138103 DUE DATE: 10-JUN-25;[02] PERFORMED PERMANENT REPAIR LOCATED ON FLOOR BEAM BS 986.5 AND RBL 43SDR SWAA2025040815081Angle · crackedCRACK ANGLE ON AUXILIARY TRACK ON SLAT 1 AT LT WING 2025-171909<[01] REPLACED ANGLE LOCATED ON AUXILIARY TRACK ON SLAT 1 AT LT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02]SDR SWAA2025040815082Angle · crackedCRACK ANGLE ON AUXILIARY TRACK SLAT 8 AT RT WING 2025-171911<[01] REPLACED ANGLE LOCATED ON AUXILIARY TRACK SLAT 8 AT RT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] JOB CSDR SWAA2025040715088Skin · corrodedCORROSION INTERNAL SKIN TOILET SERVICE DOOR 145AL AT FUSELAGE EXTERIOR 2025-171919<[01] ON STEP 1. TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 45MG. S/N: 242232211. DUE DATE: 14-NOV-25.;[02] PERFORMED PERMANENT REPAIR LOCATED ON SKIN TOILET SERVICE DOOR 145AL ASDR SWAA2025040701490Skin · corrodedCORROSION INTERNAL SKIN TOILET SERVICE DOOR 145AL AT FUSELAGE EXTERIOR 2025-171919<[01] ON STEP 1. TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 45MG. S/N: 242232211. DUE DATE: 14-NOV-25.;[02] PERFORMED PERMANENT REPAIR LOCATED ON SKIN TOILET SERVICE DOOR 145AL ASDR SWAA2025040715085Support · crackedCRACK ANGLE - SUPPORT LOCATED BS 727B LBL53 UPPER AREA AT AFT CARGO COMPARTMENT 2025-171910<[01] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25;[02] PERFORMED PERMANENT REPAIRED ON ANGLE SUPPORT LOCATED FROM 727A TOSDR SWAA2025040715087Stringer Clip · crackedCRACK ON GUSSET LOCATED BS500I AT LEVEL STR19R AT FWD CARGO COMPARTMENT 2025-171915<[01] REPLACED GUSSET LOCATED BS500I AT LEVEL STR19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G AND SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 256 AND 257 REV B. SEE SDR SWAA2025040715086Stringer Clip · crackedCRACK ON GUSSET LOCATED BS500I AT LEVEL STR21L AT FWD CARGO COMPARTMENT 2025-171917<[01] REPLACED GUSSET LOCATED BS500I AT LEVEL STR21L AT FWD CARGO COMPARTMENT AND FASTENERS IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 143A7902 SHEET: 256 REV: BSDR SWAA2025040701386Frame · crackedCRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2025-171916<[01] PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW B737-800 EA M-22-153-01244. SEE INDIVIDUAL SIGN OFF BELOW.;[02] PERFORMED PERMSDR SWAA2025040701384Stringer Clip · crackedCRACK ON GUSSET LOCATED BS500I AT LEVEL STR21L AT FWD CARGO COMPARTMENT 2025-171917<[01] REPLACED GUSSET LOCATED BS500I AT LEVEL STR21L AT FWD CARGO COMPARTMENT AND FASTENERS IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 143A7902 SHEET: 256 REV: BSDR SWAA2025040701385Stringer Clip · crackedCRACK ON GUSSET LOCATED BS500I AT LEVEL STR19R AT FWD CARGO COMPARTMENT 2025-171915<[01] REPLACED GUSSET LOCATED BS500I AT LEVEL STR19R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G AND SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 256 AND 257 REV B. SEE SDR SWAA2025040701379Angle · crackedCRACK ANGLE ON AUXILIARY TRACK ON SLAT 1 AT LT WING 2025-171909<[01] REPLACED ANGLE LOCATED ON AUXILIARY TRACK ON SLAT 1 AT LT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02]SDR SWAA2025040701380Angle · crackedCRACK ANGLE ON AUXILIARY TRACK SLAT 8 AT RT WING 2025-171911<[01] REPLACED ANGLE LOCATED ON AUXILIARY TRACK SLAT 8 AT RT WING IAW B737-800 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG 114A5020; SHEET 40; REV A.<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] JOB CSDR SWAA2025040701383Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 727B LBL53 UPPER AREA AT AFT CARGO COMPARTMENT 2025-171910<[01] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25;[02] PERFORMED PERMANENT REPAIRED ON ANGLE SUPPORT LOCATED FROM 727A TOSDR SWAA2025040801239Web · crackedCRACK ON WEB LOCATED BTW BS 312 TO BS 328 LBL 47.5 WL 208.1 AT FWD GALLEY AREA 2025-171883<[01] REPLACED WEB LOCATED BTW BS 312 TO BS 328 LBL 47.5 WL 208.1 AT FWD GALLEY AREA IAW B737-800 SRM 51-10-02 ITEM 9. AND DRAWING # 141A5400 SHEET 26 REV:-. SEE INDIVIDUSDR SWAA2025040801235Floor Support · crackedCRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 BL 0 WL 208.1 AT FWD GALLEY AREA 2025-171879<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 344 TO BS 360 BL 0 WL 208.1 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DWG 141A5400;SHEET 32 ANDSDR SWAA2025040815075Floor Support · crackedCRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 RBL 12 WL 208.1 AT FWD GALLEY AREA 2025-171882<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 344 TO BS 360 RBL 12 WL 208.1 AT FWD GALLEY AREA I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 141A5400;SDR SWAA2025040801237Floor Support · crackedCRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 RBL 12 WL 208.1 AT FWD GALLEY AREA 2025-171882<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 344 TO BS 360 RBL 12 WL 208.1 AT FWD GALLEY AREA I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG# 141A5400;SDR SWAA2025040701138Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 52 WL 208.1 AT PASSENGER CABIN 2025-171878<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 52 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG SDR SWAA2025040715077Web · crackedCRACK ON WEB LOCATED BTW BS 312 TO BS 328 LBL 47.5 WL 208.1 AT FWD GALLEY AREA 2025-171883<[01] REPLACED WEB LOCATED BTW BS 312 TO BS 328 LBL 47.5 WL 208.1 AT FWD GALLEY AREA IAW B737-800 SRM 51-10-02 ITEM 9. AND DRAWING # 141A5400 SHEET 26 REV:-. SEE INDIVIDUSDR SWAA2025040715074Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 52 WL 208.1 AT PASSENGER CABIN 2025-171878<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 52 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG SDR SWAA2025040701236Floor Support · crackedCRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA 2025-171880<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA IAW B737-800 SRM 51-10-02 ITEM 9. AND DRAWING #141A5400 SHEET 46.SDR SWAA2025040815063Floorbeam · corrodedCORROSION ON EXISTING REPAIR LOCATED FLOOR BEAM BS 344 BL 0 WL 208.1 AT FWD GALLEY AREA 2025-171798<[01] TOOL USED ON STEP 7 AND 8 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] REPLACED FILLER 1(E/A) AND FASTENERS COMMON TO EXISDR SWAA2025040800777Floorbeam · corrodedCORROSION ON EXISTING REPAIR LOCATED FLOOR BEAM BS 344 BL 0 WL 208.1 AT FWD GALLEY AREA 2025-171798<[01] TOOL USED ON STEP 7 AND 8 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] REPLACED FILLER 1(E/A) AND FASTENERS COMMON TO EXISDR SWAA2025040700779Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 WL 208.1 AT PASSENGER CABIN 2025-171807<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 WL 208.1 AT PASSENGER CABIN AND FASTENERS IAW B737-800 SRM 51-40-02 AND DWG 143A5400; SHEET 142 ASDR SWAA2025040715066Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 BL 0 WL 208.1 AT PASSENGER CABIN 2025-171812<[01] REPLACED ANGLE AND FASTENERS LOCATED BTW BS 500I TO BS 520 BL 0 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A5400 SSDR SWAA2025040700789Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 500I TO BS 520 BL 0 WL 208.1 AT PASSENGER CABIN 2025-171812<[01] REPLACED ANGLE AND FASTENERS LOCATED BTW BS 500I TO BS 520 BL 0 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A5400 SSDR SWAA2025040400787Support Bracket · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN 2025-171811<[01]. REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN AND FASTENERS IAW B737-800 SRM 51-40-02 AND DWG 143A5400; SHEET 138SDR SWAA2025040400781Support Bracket · crackedCRACK SUPPORT BRACKET LOCATED BODY STATION 540 AND LBL 6 KEEL BEAM 2025-171809 <[01]. REPLACED SUPPORT BRACKET LOCATED BODY STATION 540 AND LBL 6 KEEL BEAM I.A.W B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; [02] CORRECTED STEP 1. REPLACED SUPPORT BRACKET LSDR SWAA2025040400780Support Bracket · crackedCRACK SUPPORT BRACKET BODY STATION 540 LOCATED RBL 6 KEEL BEAM 2025-171810 <[01]. REPLACED SUPPORT BRACKET BODY STATION 540 LOCATED RBL 6 KEEL BEAM IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. LENGHT OF CRACK IS: 1.028 INCHES. TOOL USED IS: ELECTRONIC SDR SWAA2025040400778Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN 2025-171805 <[01]. REPLACED ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 50-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A5SDR SWAA2025040815049Vapor Barrier · crackedCRACK LH VAPOR BARRIER LOCATED BS 663.75 ON LBL 31.83 AT MAIN WHEEL WELL COMPARTMENT 2025-171717<[01] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 18185847; DUE DATE: 01-OCT-25.;[02] TOOL USED: SCALE PN: 1863T62; SN: AE-40571; DUE DATE: 27-AUG-25;[03] TOOL USED: SDR SWAA2025040700260Vapor Barrier · crackedCRACK LH VAPOR BARRIER LOCATED BS 663.75 ON LBL 31.83 AT MAIN WHEEL WELL COMPARTMENT 2025-171717<[01] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 18185847; DUE DATE: 01-OCT-25.;[02] TOOL USED: SCALE PN: 1863T62; SN: AE-40571; DUE DATE: 27-AUG-25;[03] TOOL USED: SDR SWAA2025040700641Lens · brokenBROKEN LENS EMERGENCY LIGHT ON COVE BULLNOSE ROW 2 RH SID 2025-171756<[01] REPLACED LENS EMERGENCY LIGHT ON COVE BULLNOSE ROW 2 RH SID I.A.W B737-800 AMM 33-51-03-960-803.TEST IS OK;[02] JOB COMPLETEDSDR SWAA2025040715060Light · brokenBROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE AT PASSENGER CABIN (9 EA) 2025-171690<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE AT PASSENGER CABIN (9 EA) I.A.W. B737-800 AMM-33-51-15-400-802 AND DWG 33510501 REV. IR;[SDR SWAA2025040715061Light · brokenBROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE AT PASSENGER CABIN (9 EA) 2025-171691<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE AT PASSENGER CABIN (9 EA) I.A.W. B737-800 AMM-33-51-15-400-802 AND DWG 33510503 REV. IR;[SDR SWAA2025040700643Light · brokenBROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE AT PASSENGER CABIN (9 EA) 2025-171691<SDR SWAA2025040700642Light · brokenBROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE AT PASSENGER CABIN (9 EA) 2025-171690<SDR SWAA2025022097797Skin · debondedL/H WING OUTBOARD AFT FLAP INBD EDGE AND TRAILING EDGE SKIN DISBONDED. R&R L/H WING OUTBOARD FLAP. IAW AMM 27-51-22. R&R L/H WING OUTBOARD AFT FLAP. IAW AMM 27-51-22.
Back to N8614M