N569AS
Service difficulty reports · 514
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 = 'N569AS' 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 = 'N569AS' 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 ASAA2023082144719Unknown · unknownUPON MC RECALL, LEFT PACK LIGHT. RESETS. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023080944502Lens · missingFA REPORTS LIGHT COVER MISSING ON WALL BETWEEN LAV D AND GALLEY. GROUNDED - YES. INSTALLED EMERGENCY LIGHT LENS COVER ON LAV D. OPS NML REF MM 33-51-00.SDR ASAA2023072144179Unknown · unknownIN CRUISE, RIGHT FMC FAILED. NO VTK DISPLAYED. F/O'S NAV DISPLAY DISPLAYED MAP. RIGHT FMC FAIL IN CDU SCRATCH PAD. GROUNDED - YES. ACCOMPLISHED FMCS BITE FIM 34-61 TASK 801 NO FAULTS FOUND NO HISTORY 30 DAYS.SDR ASAA2023071744106Heat Exchanger · leakingPASSENGER CABIN WOULD NOT COOL. AT ONE HOUR AFTER TAKEOFF, 30 MINUTES PAST LEVEL-OFF AT FL380, WITH TRIM AIR OFF AND AUTO TEMP SELECTORS FULL COLD (PER QRH) CABIN STILL UNCOMFORTABLY WARM, PAX AND F/AS COMPLAINING - FLIGHT DECK WAS FULLY COOL. PREFLIGHT, CABINSDR ASAA2023062443702Motor · faultySTAB OUT OF TRIM LIGHT ILLUMINATED WHEN AUTOPILOT ENGAGED AFTER A WHILE NOT IMMEDIATELY AFTER ABOUT 30 MINUTES AT CRUISE ALTITUDE. LEFT LIGHT ILLUMINATED WITH LEFT A AUTOPILOT RIGHT LIGHT ILLUMINATED WITH RIGHT B AUTOPILOT. GROUNDED - YES. ACCOMPLISHED DFCS SPSDR ASAA2023061743605Module · faultySTAB OUT OF TRIM LIGHT ON CLIMBOUT. MAIN ELECTRIC TRIM WORKS FINE. AUTOPILOT TRIM DOES NOT WORK. GROUNDED - YES. REF MAINT MSG 22-11167, PERFORMED B737-800 FIM TASK 22-14 TASK 818 STAB TRIM CLUTCH WRAP PROBLEM, PERFORMED WIRING CHECK ON COLUM SWITCHING MODULE SDR ASAA2023061443627Unknown · unknownDURING TAXI OUT JUST PRIOR TO HOLDING SHORT OF THE RUNWAY #1 ENGINE CONTROL LIGHT ILLUMINATED. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 73-06-801 ENGINE CONTROL LIGHT IS ON ACCOMPLISHED FIM 73-00 TASK 801 EEC BITE CHECK FAULT CODES 75-10581 AND 75-10531 ACCOMSDR ASAA2023061443625Hmu · out of limitsDURING TAXI OUT AND IN THE LINE UP FOR DEPARTURE #1 ENGINE CONTROL LIGHT ILLUMINATED. WE WERE APPROXIMATELY #5 FOR DEPARTURE AND THE CABIN TEMPERATURE WAS UNCOMFORTABLY WARM AS REPORTED BY FA'S. I SET THE PACK SWITCHES TO HIGH TO INCREASE AIR FLOW AFTER RETURNSDR ASAA2023061243557Access Panel · leakingFUEL LEAKING FROM # 1 TANK ( LEFT WING ) FROM # 5 INBOARD FUEL TANK ACCESS ENTRY PANEL ( FUEL STICK # 3 PANEL ). GROUNDED - YES. REMOVED AND REPLACED L/H WING FUEL TANK PANEL 532CB REF B737-800 AMM 28-11-11. LEAK CHECK, NO LEAK NOTED.SDR ASAA2023061143547Unknown · unknown(TRIM RUNAWAY AFTER TAKEOFF) ELECTRIC STAB TRIM DIDN'T WORK EITHER DIRECTION AFTER TAKE OFF. A/C CONTINUED TO TRIM AUTOMATICALLY BUT DID NOT RUNAWAY. STAB TRIM CUT OUT SWITCHES WERE CUT OUT AND MANUAL TRIMMED REMAINDER OF FLIGHT. GROUNDED - YES. AIR TURNBACK -SDR ASAA2023060443467Charger · faultyELEC LIGHT ILLUMINATED AFTER START. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 24-31 TASK 801, BITE SHOW AUX BATT CHARGER FAULT. ACCOMPLISHED FIM 24-31 TASK 825 BATTERY CHARGER FAULT AND DISCHARGE CHECK, FAULT WILL NOT CLEAR AND REMAINS INOP. REMOVED AND REPLACSDR ASAA2023042943051Unknown · unknownEXIT SIGN COVER ABOVE R1 DOOR NOT ATTACHED. GROUNDED - YES. REATTACHED EXIT SIGN AT R1 DOOR PER B737-800 AMM 33-51-01.SDR ASAA2023042042971Unknown · unknownL1 DOOR WOULD NOT CLOSE. GROUNDED - YES. ADJUSTED GUIDE ARM REF B737-800 AMM 52-11-21 OP CHECK GOOD.SDR ASAA2023032842620Unknown · unknownAT FL 380 CAPTAINS MAP DISPLAYED VTK. LNAV AND VNAV DISCONNECTED. WE SWITCHED TO F/O'S SIDE OPS NORMAL LEFT FMC POSITION ERRATIC. GROUNDED - YES. LEFT FMC FAULT FOR PREVIOUS FLT FMC HAD RESTORED TO NML ON ARRIVAL. CYCLED FMC CMPTR-1 C/B, FMC OPS CKS PASS REF BSDR ASAA2023022842120Connector · shortedASA TECH SERVICES FOLLOW-UP TO TANK 1 AFT BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED WITH GFI RELAY R18 TRIPPED. GROUNDED - YES. WIRE SHORTED AT BOOST PUMP CONNECTOR. WIRE RUN REPLACED AND CONNECTOR REPLACED REF B737-800 WDM 28-23-11. (REF ASA LOG PAGE 60504054SDR ASAA2023021341932Unknown · unknownAMBER FUEL INBALANCE LIGHT INFLIGHT CROSS FEED LEFT OPEN LEFT TANK WAS HEAVY SIDE. GROUNDED - YES. PERFORMED FQIS BITE TEST IAW B737-800 FIM 28-41 TASK 801 AND 820 TEST OK.SDR ASAA2023011141490Cover · missingLEFT FWD OVERWING EMERGENCY EXIT LT COVER IS MISSING. GROUNDED - YES. INSTALLED LEFT FWD OVERWING EMERGENCY EXIT LT COVER.SDR ASAA2023010841470Spacer · wornWHILE DOING FAN BLADES LUBE, FOUND #2 ENG FAN BLADE SPACER # 1, 6, 16, & 23 ARE WORN. GROUNDED - YES. REPLACED # 2 ENG FAN BLADE SPACERS # 1, 6, 16, AND 23 REF ASA T/C 78472010.SDR ASAA2023010841456Blade · debondedWHILE DOING FAN BLADES LUBE, FOUND #2 ENG FAN BLADE PLATFORM ELASTOMER SEAL DISBONDED AT #7, 10, 12, & 16 POSITION. GROUNDED - YES. TRIMMED #2 ENG FAN BLADE PLATFORM ELASTOMER SEAL DISBONDED AREAS AT # 7, 10, 12, & 16 POSITION. TRIMMED AREAS WITHIN LIMITS PER SDR ASAA2022122741307Control Panel · inoperativeHF 1 AND HF 2 RADIO CHECK PER MAINTENANCE CONTROL DID NOT PASS. GROUNDED - YES. REMOVED & REPLACED RADIO TUNING PANEL REF B737-800 AMM 23-12-41 & PERFORMED RTP INOP DISPLAY TOGGLE FOR BOTH HF1 & 2 REF AMM 23-12-41-800-802.SDR ASAA2022122641233Transceiver · faultedHF1 AND HF2 SHOWING INOP. GROUNDED - YES. PER B737-800 FIM 23-11 TASK 806. BOTH RTP SHOW INOP FOR HF1 AND HF2. BITE OF TRANSCEIVERS HF1 GREEN AND HF2 NO LIGHTS. RESET VHF 1,2,3 AND HF 1,2 CIRCUIT BREAKERS. NO HELP. REMOVED AND REPLACED HF2 TRANSCEIVER PER B737SDR ASAA2022112440929Warning Light · illuminatedDURING CLIMBOUT WITH AUTOPILOT ENGAGED THE "STAB OUT OF TRIM" ILLUMINATED, WE RAN THE QRH AND DISCOVERED THE ELECTRICAL STAB TRIM WAS INOP ON BOTH YOKES. GROUNDED - YES. AIR TURNBACK - RESET INTERNAL STM LOGIC PER B737-800 FIM 27-41 TASK 802, OPS CHECK GOOD, SSDR ASAA2022111940852Transceiver · inoperativeHF #1 INOP. GROUNDED - YES. CONFIRMED. RMVD & RPLCD #1 HF TRANSCEIVER REF B737-800 AMM 23-11-21. OPS NML PER SAME. ETOPS GND VERIFICATION TEST SUCCESSFUL.SDR ASAA2022101740397Support Angle · corrodedMAIN CABIN AFT WET AREA SUPPORT ANGLE IS CORRODED AT BS994 RBL32- RBL40. GROUNDED - YES. SUPPORT ANGLE HAS 100% MATERIAL LOSS AND IS OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1.DRILLED TO FIT NEW SUPPORT ANGLE IAW BAC DWG 147A5700 REV- ANGLE INSTALLED ON N/R SDR ASAA2022100840470Support · corrodedFWD PIT, AFT LOWER BULKHEAD SUPPORT HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM THE FWD PIT AFT LOWER BULKHEAD SUPPORT IAW B737-800 SRM 53-30-08-1A-1 STEP 2.CORIGINAL THICKNESS IS .071 IAW B737-800 SRM 53-30-08-0I-1 TABLE 2REMOVED .016REMAINING THICKNESSDR ASAA2022100840469Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL FROM STA 500H TO 500I HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM FWD PIT R/H TRANSITION PANEL FROM STA 500H TO 500I IAW B737-800 SRM 53-00-53-1A-2 STEP 4.A ORIGINAL THICKNESS IS .040 IAW B737-800 SRM 53-30-53-0I-2 TABLE 2RESDR ASAA2022100540242Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL FROM STA 727 TO 727E+10 IS CORRODED. GROUNDED - YES. REPAIRED THE AFT PIT L/H TRANSITION PANEL FROM STA 727 TO 727E+10 USING MAT BAC 1496-377 PER B737-800 SRM 53-00-53-2R-5.SDR ASAA2022100440498Floor Support · corrodedMAIN CABIN AFT WET AREA FLOOR STRUCTURE BS907- BS927, LBL.51 INTERCOSTAL IS CORRODED AT MOUNT. GROUNDED - YES. EVALUATED CORROSION -ORIGINAL THICKNESS .150,REMAINING THICKNESS .100,MATERIAL REMOVED .050AND FOUND TO BE OUT OF LIMITS AIW B737-800 SRM 53-70-15-1ASDR ASAA2022100440497Floor Support · corrodedMAIN CABIN AFT WET AREA FLOOR STRUCTURE BS907-BS927, LBL24, INTERCOSTAL IS CORRODED AT MOUNT. GROUNDED - YES. EVALUATED CORROSION -ORIGINAL THICKNESS .150,REMAINING THICKNESS .115,MATERIAL REMOVED .035AND FOUND TO BE OUT OF LIMITS AIW B737-800 SRM 53-70-15-1A-SDR ASAA2022100440439Floorbeam · corrodedMAIN CABIN AFT WET AREA BS986 FLOORBEAM IS CORRODED AT RBL44 FASTENER HOLE. DOT: L086. GROUNDED - YES. BLENDED OUT CORROSION. ORIGINAL THICKNESS 0.150. REMAINING THICKNESS 0.090, REMOVED 0.060. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. CUT OUT DAMAGE STA 9SDR ASAA2022100440438Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL P/N 147A5810-267 HAS PEELING FIBERS, CORRODED INSERTS. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OF PEELING FIBERS AND CORRODED FASTENER INSERTS ON MAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-267 IAW ASA B737-800 SRM 53SDR ASAA2022100440437Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL P/N 147A5810-123 HAS PEELING FIBERS, CORRODED INSERTS. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OFPEELING FIBERS AND CORRODED INSERTS ON MAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-123 IAW ASA B737-800 SRM 53-00-50-2R-SDR ASAA2022100440436Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL P/N 147A5810-90 HAS PEELING FIBERS, CORRODED INSERTS. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OF PEELING FIBERS AND CORRODED INSERTS ON MAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-9 IAW ASA B737-800 SRM 53-00-50-2R.SDR ASAA2022100440435Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL P/N 147A5810-345 HAS PEELING FIBERS, CORRODED INSERTS. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OFPEELING FIBERS AND CORRODED INSERTS ON MAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-345 IAW ASA B737-800 SRM 53-00-50-2R-SDR ASAA2022100440434Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL P/N 147A5810-137 HAS PEELING FIBERS, CORRODED INSERTS. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OF PEELING FIBERS AND CORRODED INSERTS ON MAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-137 IAW ASA B737-800 SRM 53-00-50-2RSDR ASAA2022100440433Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL P/N 147A5810-23 HAS PEELING FIBERS, CORRODED INSERTS. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-23 IAW ASA B737-800 SRM 53-00-50-2R-0G.SDR ASAA2022100440432Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL P/N 147A5810-136 HAS PEELING FIBERS, CORRODED INSERTS. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OFPEELING FIBERS AND CORRODED INSERTS ON MAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-136 IAW ASA B737-800 SRM 53-00-50-2R-SDR ASAA2022100440431Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL P/N 147A5810-28 HAS PEELING FIBERS. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-28 PEELING FIBERS IAW ASA B737-800 SRM 53-00-50-2R-0G.SDR ASAA2022100440430Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL P/N 147A5810-27 HAS PEELING FIBERS. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-27 PEELING FIBERS IAW ASA B737-800 SRM 53-00-50-2R-0G.SDR ASAA2022100440269Floor Panel · peelingMAIN CABIN FLOOR PANEL AT OVERWING P/N 144A5810-124 (RH) HAS PEELING FIBERS. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR OF MAIN CABIN FLOOR PANEL P/N 144A5810-124 (R/H) PEELING FIBERS IAW B737-800 SRM 53-00-50-2R-0 & SRM 53-00-50-2R-1.SDR ASAA2022100440268Floor Panel · peelingREPAIRED MAIN CABIN FLOOR PANEL PN 144A5810-129 PEELING FIBERS IAW B737-800 SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0. GROUNDED - YES. REPAIRED MAIN CABIN FLOOR PANEL PN 144A5810-129 PEELING FIBERS IAW B737-800 SRM-53-00-50-2R-1 AND SRM 53-00-50-2R-0.SDR ASAA2022100440267Floor Panel · peelingMAIN CABIN FLOOR PANEL AT OVERWING P/N 144A5810-189 (L/H) HAS PEEKING FIBERS. GROUNDED - YES. REPAIRED MAIN CABIN FLOOR PANEL PN144A5810-189 PEELING FIBERS IAW B737-800 SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0.SDR ASAA2022100440266Floor Panel · damagedMAIN CABIN FWD WET AREA FLOOR PANEL P/N 141A5810-157 HAS PEELING FIBERS. GROUNDED - YES. REPAIRED MAIN CABIN FWD WET AREA FLOOR PANEL 141A5810-157 PEELING FIBERS IAW B737-800 SRM 53-00-50-1A-1 & SRM 53-00-50-2R-0.SDR ASAA2022100440265Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL P/N 141A5810-286 HAS PEELING FIBERS. GROUNDED - YES. EVALUATED DAMAGE PEELING FIBERS IAW B737-800 53-00-50-2R-1. REPAIRED IAW B737-800 SRM 53-00-50-2R-1 AND B737-800 SRM 53-00-50-2R-0.SDR ASAA2022100440257Floor Panel · peelingMAIN CABIN FWD WET AREA FLOOR PANEL P/N 141A5810-236 HAS CORRODED INSERTS AND PEELING FIBERS. GROUNDED - YES. REPAIRED MAIN CABIN FWD WET AREA FLOOR PANEL 141A5810-236 CORRODED INSERTS & PEELING PLYS. IAW B737-800 SRM 53-00-50-1A-1 & SRM 53-00-50-2R-0.SDR ASAA2022100440256Floor Panel · damagedMAIN CABIN FWD WET AREA FLOOR PANEL P/N 141A5810-53 CORRODED INSERTS AND PEELING FIBERS. GROUNDED - YES. REPAIRED MAIN CABIN FWD WET AREA FLOOR PANEL 141A5810-53 CORRODED INSERTS & PEELING FIBERS IAW B737-800 SRM 53-00-50-1A-1 & SRM 53-00-50-2R-0.SDR ASAA2022092340049Wire · damagedL2 WINDOW HEAT CORD DAMAGED. GROUNDED - YES. REMOVED AND REPLACED L2 WINDOW HEAT COILED CORD. REF B737-800 AMM 30-41-00. WINDOW HEAT OPS TEST GOOD.SDR ASAA2022090639924Starter Gen · faultyAPU FAULT LIGHT DURING TAXIN IN. GROUNDED - YES. REMOVED AND REPLACED APU STARTER GENERATOR PER B737-800 AMM 49-41-21. PERFORMED OPS AND LEACK CHECKS . OPS AND LEACK CHECKS GOOD REF AMM 49-41-21-400-801 STEPS 3I -3L.SDR ASAA2022082339644Panel · detachedF/A REPORT PIECE WALL TRIM FELL NEAR 16-A SEAT. GROUNDED - YES. REINSTALL TRIM COVER PIECE IAW B737-800 AMM 52-22-51.SDR ASAA2022081639550Eec · faultedREF ASA LP 60396852, #1 ENG HAS A FAULT CODE 73-31161"MECH OVSPD PROTECTION SIGNAL OUT OF RANGE". GROUNDED - YES. REMOVED AND REPLACED EEC REF. B737-800 AMM 73-21-60/401.
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