N8575Z
Service difficulty reports · 37
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 = 'N8575Z' 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 = 'N8575Z' 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 SWAA2026092128212Battery Pack · inoperativeSEVERAL EXTERIOR AND INTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED & REPLACED THE BATTERY PACKS AT THE M2816, M1670, M1671, M1694, M2335, M1673, & M1672 IAW AMM 33-51-06-960-805. PERFORMED SATISFACTORY OPS CHECK IAW B737 AMM 33-51-06-960-805.SDR SWAA2026092128987Skin · damagedLH FUSELAGE SKIN DAMAGE DUE TO BIRD STRIKE AT BS 177.73 AND WL 237 - PERMANENT) REMOVED NOSE RADOME TO FOM IAW B737 AMM 53-52-00 P/N 1001002-78 S/N NRD-1075 REMOVED NOSE RADOME TO FOM IAW B737 AMM 53-52-00 P/N 1001002-78 S/N NRD-1075 REMOVED PILOTS SEAT IAW B7SDR SWAA2026082526970Fire Loop · inoperativeNR 1 ENGINE, FIRE DETECTOR LOOP B INOPERATIVE. OK TO CONTINUE IAW MEL 26-2-01 XB. NR 1 ENGINE 34B& 34 LOOPS, ENGINE OVERHEAT & FIRE DETECTION SYS . PERFORMED AN OPS TEST OF NR1 ENGINE FIRE DETECTOR LOOP B IAW AMM 26-11-00. OPS CHECKED GOOD.SDR SWAA2026080538967Bushing · missingFWD SERVICE DOOR GIRT BAR BUSHING FELL OFF. REINSTALLED BUSHING IAW AMM 25-66-01. A/C OK FOR SERVICE.SDR SWAA2026070718183Table · out of limitsTRAY TABLES ON SEAT BACKS OF PAX SEATS 14C; 14B; 14D; 14E DO NOT EXTEND ENOUGH FOR EXIT ROW. ADJUSTED TRAY TABLES AT SEAT BACKS OF PASSENGER SEATS 14C; 14B; 14D; AND 14E IAW CMM 25-23-67;[02] READJUSTED TRAY TABLE OF PASSENGER SEATS 14C; 14B; 14D; AND 14E TO SDR SWAA2026052004467Slide · low pressureCHECKED R1 SLIDE PRESSURE, SHOWING IN RED. REMOVED AND REPLACED IAW AMM 25-66-01-401-NG, MT 725-61-06SDR SWAA2026010557652Flashlight · inoperativeFLASHLIGHT BELOW AFT RIGHT SIDE JUMPSEAT INOPERATIVE. AFT EMERGENCY FLASHLIGHT OP CHECK GOOD PER AMM 25-64-00.SDR SWAA2025072494559Battery Pack · inoperativeAFT FLIGHT ATTENDANT FLASHLIGHT FO SIDE NOT CHARGING. REPLACED FLASHLIGHT BATTERY AND SEAL IAW AMM 25-64-00.SDR SWAA2024082830531Megaphone · inoperativeFWD MEGAPHONE INOP<[01] REMOVED AND REPLACED FWD MEGAPHONE AND PERFORMED OPERATIONAL CHECK REF AMM 25-64-00SDR SWAA2024062706222Battery Pack · inoperativeFWD FA FLASHLIGHT INOP<[01] REMOVED AND REPLACED OUTBD FWD FA FLASHLIGHT AND BATT PER AMM 25-64-00 OPS CHECK OK.SDR SWAA2024060686537Web · crackedCRACK WEB OUTBOARD FAN COWL ON ENGINE 2 2024-318208<[01] REPLACED WEB OUTBOARD FAN COWL ON ENGINE 2 IAW B737-800 SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] REPLACED WEB OUTBOARD FAN COWL ON ENGINE 2 IAW B737-800 SRM 51-40-02-0G-0 AND CMM 71-13-30 TOOL USED CALIPESDR SWAA2024060686536Support Bracket · damagedELONGATED HOLE SUPPORT BRACKET LOCATED IB LEADING EDGE AT LEVEL IFSS 151 AT LT WING 2024-318209<[01] REPLACED SUPPORT BRACKET LOCATED IB LEADING EDGE AT LEVEL IFSS 151 AT LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-40-04.;[02] REPLACED SUPPORT BRACKET LOCATEDSDR SWAA2024060686361Web · crackedCRACK WEB INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 2024-318200<[01] REPLACED WEB LOCATED ON INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 IAW B737-800 SRM 51-10-02 ITEM 9 AND GOODRICH AEROSTRUCTURES CMM 71-13-30. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEBSDR SWAA2024060685757Angle · crackedCRACK ANGLE - CLIP LOCATED BS500H STR26L FWD FACE FWD CARGO COMPARTMENT 2024-318189<[01] REPLACED ANGLE - CLIP LOCATED BS500H STR26L FWD FACE FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 175 REV -.;[02] CORRECTED STEP 1. REPLACEDSDR SWAA2024060685758Support Angle · corrodedCORROSION ON SUPPORT ANGLE LOCATED BS500I WL156 AND BTW STR26L TO STR26R AT FWD CARGO COMPARTMENT 2024-318190<[01] REPLACED SUPPORT ANGLE LOCATED BS500I WL156 AND BTW STR26L TO STR26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRAWING 143A9481 SHEESDR SWAA2024060685370Angle · crackedCRACK ANGLE LOCATED BS867 AND LBL11 AFT CARGO COMPARTMENT 2024-318172<[01] REPLACED ANGLE LOCATED BS867 AND LBL11 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-05-0G-0; DWG 149A8102 SHEET 19 REV A. AND DWG 149A8104 SHEET 1 REV B.;[02] CORRECTED STEP 1. REPLACEDSDR SWAA2024060684943Floorbeam · corrodedCORROSION FLOORBEAM LOCATED BS 947; RBL 50; WL 208.1 AT AFT GALLEY AREA. REPAIRED FLOOR STRUCTURE BEAM LOCATED BS 947; RBL 50; WL 208.1 AT AFT GALLEY AREA THE REPAIR WAS ACCOMPLISHED IAW SRM 53-70-51-2R-5 WITH MINOR DEVIATIONS DOCUMENTED IN EA 24-153-01398. SDR SWAA2024060684947Floorbeam · corrodedCORROSION FLOOR STRUCTURE BEAM LOCATED BS 947; LBL50; WL 208.1 AT AFT GALLEY AREA. REPAIRED FLOOR STRUCTURE BEAM LOCATED BS 947; LBL38 TO LBL 60; WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM-53-70-51-2R-5 REPAIR 5; THIS IS REPAIR CATEGORY A .SDR SWAA2024060684948Floor Support · corrodedCORROSION FLOOR STRUCTURE FITTING LOCATED BS 947; LBL 49; WL 208.1 AT AFT GALLEY AREA 2024-318126<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45 MG; S/N: 130066701; DUE DATE: 09-JUN-24.;[02] REPLACED INTERCOSTAL LOCATED BS 947 T0 967; LBL 49; WL 208.1 AT ASDR SWAA2024060684946Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 280 DEFLECTION CONTROL RIB AREA LT WING 2024-318124<[01] REPLACED ANGLE ON TRAILING EDGE ORSS 280 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02-0G AND DWG 115A6200 SHEET 24 REV A;[02] COMPLETED TASK CERTIFIEDSDR SWAA2024060684945Angle · crackedCRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2024-318123<[01] REPLACED ANGLE LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DWG 115A2930 SHEET 17 REV -. MEASURES OF THE CRACK ARE:SDR SWAA2024060684742Access Panel · crackedCRACK ACCESS PANEL 191D BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191D BODY FAIRING AT LOWER FUSELAGE IAW B737-800 SRM 51-70-04-2R-2 REPAIR 2.SDR SWAA2024060784567Fitting · corrodedCORROSION LOWER FITTING LOCATED G1 AT FWD GALLEY AREA (2 EA) 2024-318079<[01] REPLACED LOWER FITTING LOCATED G1 AT FWD GALLEY AREA (2 EA) IAW B737-800 SOPM 20-50-01 REV. 38;[02] CORRECTED STEP 2. REPLACED LOWER FITTING LOCATED G1 AT FWD GALLEY AREA (2 EA) IAW SDR SWAA2024060684570Floor Panel · crackedCRACK FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT 2024-318104<[01] REPLACED FLOOR PANEL 120CF FWD CARGO COMPARTMENT IAW B737-800 AMM 25-52-01-201-801 AND DWG 453A1610 SHEET 65 REV-<BR>MATERIAL USED ALUMINUM SHEET : P/N: 2024-T3 0.071. SEE INDIVIDUAL SIGN OFF BESDR SWAA2024060684261Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE OF AFT CARGO DOOR CUTOUT 2024-318054<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23399190; DUE DATE: 04-MAR-25.;[02] ON STEP 4 ; TOOL USED: RADIOMETER/PHOTOMETER KIT. P/N:XRP-3000. S/N:1859843. DUE DATE:24-JUL-24.;[03]SDR SWAA2024060684262Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE OF AFT CARGO DOOR CUT OUT 2024-318055<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23272782; DUE DATE: 06-MAR-25.;[02] TOOL USED IN STEP 4: RADIOMETER PHOTOMETER KIT P/N: XRP-3000 S/N: 1859843 DUE DATE: 24-JUL-24;[03] RESDR SWAA2024060682896Floor Panel · crackedCRACK FLOOR PANEL 140EF AT AFT CARGO COMPARTMENT 2024-317742<[01] REPLACED FLOOR PANEL 140EF AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-20-01-0G-0 AND DWG 453A2610 SHEET 38 REV C.;[02] CORRECTED STEP 1. REPLACED FLOOR PANEL 140EF AT AFT CARGO COMPARTMENT IAWSDR SWAA2023113025918Megaphone · failedFWD MEGAPHONE WILL NOT TEST<SDR SWAA2023091400076Flashlight · no testRIGHT SIDE OTBD AFT EMERGENCY FLASHLIGHT WONT TEST. OK TO CONT PER MEL 25-12-01 SP#1B. R & R FLASHLIGHT ASSY PER SIP.SDR SWAA2023032320042Support · crackedFLOOR BOARD SUPPORT R/H PANEL BRAKE ASSY. CRACKED - LOCATED AT STA 540<[01] REMOVED AND REPLACED BREAKER PANEL R/H AT STA. 540 PER SRM 51-40-02.SDR SWAA2023032320043Support · crackedFLOOR BOARD SUPPORT L/H PANEL BRAKE ASSY. CRACKED - LOCATED AT STA 540<[01] REMOVED AND REPLACED BREAKER PANEL L/H PER SRM 51-40-02 AT STA. 540.SDR SWAA2021121752562Slide · lowAFT ENTRY DOOR SLIDE PRESSURE GAUGE READING EXACTLY ON THE LINE BETWEEN RED AND GREEN ; / [01] AFT ENTRY DOOR SLIDE REPLACED PER MT 725-61-06SDR SWAA2021120149134Indicator · out of toleranceFLAPS WOULD NOT EXTEND BEYOND FLAPS 10 PREFORMED ALTERNATE FLAPS EXTENSION + FLAPS 15 FOR LANDING ; / [01] PREFORMED FSEU BITE IAW FIM 27-51 TASK 801 AND PSEU BITE IAW FIM 32-09 TASK 801 NO FAULTS OR FAULT HISTORY FOUND. PREFORMED TRAILING EDGE LOAD RELIEF TESSDR SWAA2020090914575Flashlight · inoperativeLEFT AFT INBOARD FLASHLIGHT WILL NOT TEST. R&R LEFT AFT INBOARD FLASHLIGHT, PER AMM 25-64-00. OPS CHECK GOOD.SDR SWAA2020083110987Flashlight · inoperativeAFT LEFT FLIGHT ATTENDANT FLASHLIGHT INOP. OK TO COTNINUE PER MEL 25-12-01 SP1B TRACKING # 97915( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) / REMOVED AND RECREDLED BOTH AFT FLASH LIGHTS; OPS CK NORMAL REF 25-64-00.SDR SWAA2020021741398Flashlight · inoperativeAFT JUMPSEAT AIRCRAFT RIGHT OUTBD FLASHLIGHT DEAD. ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ). / R/R AFT O/B EMERG FLASHLIGHT PER MM 25-64-00. CLEARING #74318SDR SWAA2018061822797Holder · out of adjustR1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED HOLDER IAW SIP.
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