N562AS
Service difficulty reports · 600
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 = 'N562AS' 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 = 'N562AS' 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 ASAA2023013081705Fmc · faultedAT CRUISE FL370, APPOX 3HRS 20 MINUTES INTO FLIGHT, LEFT FMC FAILED. LOST COURSE INTO LEFT NAV DISPLAY. SAW CWS ON PFD, VTK ON LEFT NAV DISPLAYS, LOST FMC PROMPT ON BOTH MCDU'S. FMC RECOVERED BEFORE WE INITIATED QRH PROCEDURE (ABOUT 30 SECONDS). HIGHEST ANP WESDR ASAA2023012641716Valve · faultyDURING TAXI (AFTER #1 ENGINE START) CONT CAB ZONE TEMP LIGHT ILLUMINATES ON RECALL.EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. REMOVED AND REPLACED CONTROL CABIN TRIM MODULATING VALVE (V143) REF B737-800 AMM 21-61-21/401.SDR ASAA2023012641652Unknown · unknownFWD LAV AND ACFT RH AFT LAV UNABLE TO FLUSH IN FLT NOTED WASTE LEVEL INDICATOR INDICATING FULL.UPON LANDING INDICATOR INDICATED 1/2 FULL SERVICED REPEATED THEY REMOVED 1/4 WASTE. GROUNDED - YES. DIVERSION -- SERVICED WASTE TANK MULTIPLE TIMES REF B737-800 AMM SDR ASAA2023011741528Indicator · faulted#2 REFUEL QTY INDICATOR DOES NOT TEST, READS CORRECTLY. GROUNDED - YES. REMOVED AND REPLACED # 2 REFUEL QTY INDICATOR IAW B737-800 AMM 28-41-61.SDR ASAA2023011741529Indicator · inoperativeFUELER REPORTS #1 TANK INDICATOR GUAGE INOP ON PRESSURE FUELING PANEL. GROUNDED - YES. REPLACED #1 TANK REFUEL QUANTITY INDICATOR WITH SERVICEABLE UNIT, OPS CHECKS OK. REF B737-800 AMM 28-41-61.SDR ASAA2023011241526Motor · faultedNUMBER ONE ENGINE FWD FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED AT FL 410. LIGHT EXTINGUISHED AFTER 10 SECONDS THEN ON AGAIN 10 MINUTES LATER. GROUNDED - YES. REMOVED & REPLACED #1 FWD FUEL PUMP PER B737-800 AMM 28-22-41.SDR ASAA2022122761250Door · out of adjustFA REPORTS L1 DOOR ISN'T SHUTTING RIGHT. HAVE TO USE MORE THAN NORMAL FORCE. DOOR WAS NOT CLOSING RIGHT OR FLUSH W A/C ON FIRST FEW ATTEMPTS. GROUNDED - YES. CHECKED DOOR STOP GAPS & DOOR CLOSE TORQUE, TORQUE EXCEEDS ALLOWABLE VALUE FOR CLOSING DOOR REF B737-8SDR ASAA2022122541264Igniter · failedUNABLE TO START #2 ENGINE, NO EGT RISE WITHIN 15 SEC SLOW N2 RISE AND HANGS AT 30. GROUNDED - YES. REMOVED AND REPLACED BOTH LH AND RH ENG IGNITERS ON #2 ENG PER B737-800 AMM 74-21-02.SDR ASAA2022122541257Warning Light · false activationON RECALL ZONE TEMP ILLUMINATED RESETS WITH PUSH OF MASTER CAUTION. GROUNDED - YES. PERFORMED PACK TEMP CONTROL BITE PROCEDURE PER B737-800 FIM 21-62 TASK 801. FOUND TRIM VALVE RED LIGHT UNDER PREV FLT ON TEMP CONTROLLER. PRESSED VERIFY SWITCH ON CONTROLLER GRSDR ASAA2022122741248Fmc · faultedFMC SINGLE FMC MESSAGE FOLLOWED BY "MAP" ON ND AND "NO VSD" ON PFD. SAME MESSAGES AS REPORTED PG 60425582. GROUNDED - YES. PERFORMED FMC BITE FOUND "DISCR OUT LOOP" ON ACTIVE. REPLACED R/H FMC WITH SERVICEABLE ONE. ACCOMP FMC SOFTWARE CROSS LOAD & VERIFIED. ACSDR ASAA2022122741246Fmc · faultedFO SAW SINGLE FMC FOLLOWED BY MAP ON ND & NO VSPD ON PFD. GROUNDED - YES. PERFORMED B737-800 FIM 34-61 TASK 801 FOUND NO ACTIVE FAULTS PERFORMED FIM 34-61 TASK 836 OPENED AND CLOSED 4 EA C/B. ALL FAULTS NO LONGER ACTIVE.SDR ASAA2022122141212Control Panel · inoperativeMODE CONTROL PANEL WINDOW LIGHTING INOP. GROUNDED - YES. CONFIRMED MCP INOP, PERFORMED MCP BITE AUTOTEST. TEST FAILED "NO MCP DATA" INTERFACE PINS FCC-B (J1A-K06) (J1A-J06) MSG 22-11063. REMOVED AND REPLACED MCP IAW B737-800 AMM 22-11-34/401. PERFORMED B737-80SDR ASAA2022121641157Lamp · inoperativeWHILE PERFORMING ASA T/C 78233008, FOUND L2 DOOR EMERGENCY LIGHT OUT. GROUNDED - YES. RELAMPED L2 DOOR EMERGENCY LIGHT WITH SERVICEABLE FROM STOCK BULB AND PERFORMED OPS CHECK REF B737-800 AMM 33-51-00-720-801. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.SDR ASAA2022121641155Display · faultedMCP DISPLAYS UNREADABLE AND WITH F/D'S ON VOR/LOC CYCLING ON. GROUNDED - YES. REPLACED MCP, INSTALLATION TEST GOOD REF B737-800 AMM 22-11-34.SDR ASAA2022121241111Fmc · faultedLNAV/VNAV WILL NOT ENGAGE ON GROUND. GROUNDED - YES. FMC BITE SHOWS FCC DATA SYNC ERR, DFCS SHOWS MCP MSG 22-11063. RESET MCP 9 C/B'S OPEN AND CLOSED, RESET FMC(S) 2 C/B'S OPEN AND CLOSED. RELOAD FLT PLAN, DFCS CURRENT STATUS PASS AND FMC OPS CKS NORMAL REF B7SDR ASAA2022120841098Valve · leakingFUEL DRIPPING AT APPROX 1 DROP PER SEC FROM BOTTOM OF NR 2 ENGINE. GROUNDED - YES. REPLACED NR 2 ENG HPTACC VALVE IAW AMM 75-21-01-000/400-801-F00.SDR ASAA2022120541021Circuit Breaker · faultedLNAV & VNAV WILL NOT ENGAGE. CO-PILOT COURSE WINDOW DISPLAYS ALL 8'S. GROUNDED - YES. RESET C/B IAW FIM 22-11 TASK 803. OPS CK NORMAL.SDR ASAA2022120441042Fmc · faultyFO PFD HAS NO VSPD AND MAP DISPLAYS MAP UNABLE TO ENGAGE LNAV/VNAV. OPS NORM ON FMC 1. GROUNDED - YES. PERFORMED FMCS BITE PER B737-800 FIM 34-61 TASK 801 AND ON R/H FMC HAD ARINC FAULT. FIM 34-61 TASK 837 STATES FMC WITH ARINC FAULT HAS HARDWARE FAULT. REMOVESDR ASAA2022112140875Control Panel · faultedINFLIGHT WITH CA FD AS MASTER AP KICKED OFF COULD NOT ENGAGE HEADING MODE , COULD NOT ENGAGE LNAV. RECOVERED BY PUTTING FD 2 ON AS MASTER AND LNAV/VNAV ON WITH B AUTOPILOT. CA HEADING BUG FROZEN ENTIRE TIME. NO LOC,NO GS DIAMONDS ON CA PFD. AT GS CAPTURED, CA SDR ASAA2022112040877Unknown · unknownDURING PREFLIGHT WITH CA FD AS MASTER, NO MODES WOULD ENGAGE. WITH F/O FD AS MASTER, NO LNAV/VNAV MODES WOULD ENGAGE, BUT OTHER MODES ENGAGE OKAY. AIRSPEED WINDOW WOULD NOT CHANGE, WHEN SPINNING SPEED KNOB, WITH FDS OFF AND WITH CA FD ON AS MASTER. SPEED KNOB SDR ASAA2022111940876Control Panel · faultyIN FLIGHT AT FL350 ABOUT 2 HRS INTO FLIGHT, AP KICKED OFF, COULD NOT ENGAGE HEADING MODE, COULD NOT ENGAGE LNAV. RECOVERED BY PUTTING FD 2 ON MASTER, AND LNAV/VNAV ON WITH B AUTOPILOT. CA HEADING BUY FROZEN ENTIRE TIME. NO LOC, GS DIAMONDS ON CAP FD. AT GS CAPSDR ASAA2022111940849Control Panel · unresponsiveAFTER TAKEOFF, MODE CONTROL PANEL DID NOT RESPOND TO INPUTS. PERFORMED MODE CONTROL PANEL LOCKUP QRH. MODE CONTROL PANEL OPERATES NORMALLY. GROUNDED - YES. REF B737-800 AMM TASK 22-11-00-740-806, DFCS BITE LIBARY MCP TEST PASSED W/O FAULTS. A/C RESTORED TO NORSDR ASAA2022110940696Unknown · multiple failPWS FAILED AND TCAS FAILURE ON N.D.'S. GROUNDED - YES. ON ARRIVAL @ AIRCRAFT, TCAS AND PWS NO FLAGS ON ND. 'CYCLED TCAS AND WX RADAR C/B'S P18-B6 AND P6-1 D13. NO PWS FAIL FLAG AFTER RESET WX RADAR BITE TEST GOOD REF B737-800 FIM 34-43 TASK 801 AND 34-43 TASK SDR ASAA2022110440660Start Valve · faultedENG 2 ON GRD START N2 IS VERY SLOW TO SPOOL UP WHILE ON STARTER PRESSURE. ON LIGHT OFF SPOOLS UP NORMALLY. GROUNDED - YES. REMOVED AND REPLACED #2 ENG START VALVE REF B737-800 AMM 80-11-03.SDR ASAA2022110240595Indicator · inoperativeRE FUELER REPORTS CENTER TANK INDICATOR INOP. GROUNDED - YES. REMOVED AND REPLACED CENTER REFUEL PNL INDICATOR REF B737-800 AMM 28-41-61.SDR ASAA2022110240560Warning Message · false indicationHF ONE FAILED (RTP). GROUNDED - YES. ACCOMPLISHED B737-800 FIM 23-11 TASK 802, GROUND VERIFICATION HF #1, OPS NML.SDR ASAA2022103140544Warning Light · false activationNOTICED ENROUTE ON THE FLIGHT CONTROL PANEL THE A/T AUTO THROTTLE AFAR LIGHT NOT ILLUMINATED, RE-ILLUMINATED - OPS APPEAR NORMAL. GROUNDED - YES. PERFORMED AUTO THROTTLE OPERATIONAL TEST PER B737-800 AMM 22-31-00-710-801 OP'S NORMAL, NO DEFECT'S NOTED.SDR ASAA2022102240486Control Panel · faultedFLT CREW REPORTS FD FLAG ON PILOT DISPLAY (CAPT SIDE). GROUNDED - YES. PERFORMED ILS SYSTEM TEST PER B737-800 AMM 34-31-00-730-801 SYSTEM TEST PASSED DFCS BITE GROUP 12 FLIGHT DIRECTOR BITE TEST PASSED. PERFORMED DFCS BITE PER B737-800 FIM 22-11 TASK 801 INSDR ASAA2022102240408Trim System · faulty"MACH TRIM FAIL" ILLUMINATED ON RECALL. GROUNDED - YES. A/C POWER RESET REF B737-800 AMM 20-60-99. OPS CHECK GOOD. NO DEFECTS NOTED ANY FURTHER.SDR ASAA2022100940230Anti-Ice Valve · warning lightTHE TAI ICON KEEPS GOING ON AND OFF, BOTH IN CRUISE AND ON DESCENT. GROUNDED - YES. REMOVED AND REPLACED #1 ENG TAI VALVE REF B737-800 AMM 30-21-11.SDR ASAA2022100840238Indicator · failedCENTER FUEL TANK REFUEL IND. FLASHED FAIL. GROUNDED - YES. ON DEFERRAL.SDR ASAA2022090539816Controller · unknownCONT CAB TEMP CABIN LIGHT ILLUMINATED ON RECALL AND EXTINGUISHED ON RESET. GROUNDED - YES. PERFORMED PZTC BITE IAW B737-800 FIM 21-62 TASK 801. #2 CONTROLLER HAD FLT DECK TRIM VALVE ON BITE, CLEARED GREEN ON VERIFY. PER FIM 21-53 TASK 821, NO FURTHER ACTION RESDR ASAA2022082939701Control Panel · faultyIN CRUISE AND AT TOP OF DESCENT, AUTO PILOT DISCONNECTED A/C IN TRIM, NO PILOT INPUTS. GROUNDED - YES. DEBRIEFED CREW BOTH A & B DISCONNECTED MULTIPLE TIMES, A FCC FLIGHT FAULTS 22-11607, 22-11627, B FCC FAULTS 22-11607, 22-11627, ALL RELATED TO MCP-HAS HISTORSDR ASAA2022082539668Unknown · unknownA AUTOPILOT DISCONNECTED MULTIPLE TIMES ON ARRIVAL. GROUNDED - YES. PERFORMED DFCS FAULTS REVIEW CHECK NO FAULTS FOUND B737-800 AMM 22-11-00.SDR ASAA2022082139592None · noneNUMBER 2 AUTOPILOT INOP. DISENGAGED MULTIPLE TIMES AT CRUISE. GROUNDED - YES. REMOVED/REPLACED MCP B737-800 AMM 22-11-34.SDR ASAA2022081639538Lamp · inoperativeEMERGENCY EXIT LIGHT INOP OVER ROW 16 ABC. GROUNDED - YES. RELAMPED EMERGENCY EXIT LIGHT AND OPS CHECK GOOD IAW ASA B737-800 AMM 33-51-03.SDR ASAA2022071739247Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL FROM STA. 722J - STA 767 CORRODED OUT OF LIMITS. GROUNDED - YES. REPAIRED AFT PIT L/H TRANSITION PANEL FROM STA 727H+12 TO 794 IAW B737-800 SRM 53-00-53-2R-5.SDR ASAA2022070839226Floor Panel · delaminatedCABIN FWD WET AREA FLOOR PANEL 235 PART # 141A5810-286 HAS SEVERAL DELAMATION AREAS ON THE BOTTOM AND CORRODED INSERTS AS MARKED. GROUNDED - YES. REPAIRED DAMAGE TO FLOOR PNL P/N 141A5810-286 WITH FIBERGLASS DOUBLER WET LAY UP IAW B737-800 SRM 53-00-50-2R-1, SDR ASAA2022070739246Transition Panel · corrodedLOWER AFT CARGO COMPARTMENT, STATION 727H TO 727J, RIGHT HAND TRANSITION AREA UPPER AND LOWER SURFACES HAVE MUTILPLE AREAS OF CORROSION AND BARE METAL.DOT: J254. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT RH TRANSITION PANEL STA 727H TO 727J. 100% MAT SDR ASAA2022070739245Strap · corrodedAFT CARGO COMPARTMENT DOOR LOWER SILL INTERCOSTAL IS CORRODED AT ALL VISIBLE NUT PLATES BETWEEN STA 807 AND 827 (MARKED). GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT LOWER SILL STRAP PER B737-800 SRM 53-60-5-1A-1. 2.A. ORIG. THICKNESS IS .100 PER B737-8SDR ASAA2022070739244Transition Panel · corrodedAFT CARGO COMPARTMENT R/H SIDE FLOOR TO WALL TRANSITION ANGLE IS CORRODED IN MULTIPLE SPOTS BEWTEEN STA 767 AND 787 (MARKED)DOT: Z802. GROUNDED - YES. REMOVED AND REPLACED THE AFT PIT SHIELD AT STA 767-787 IAW B737-800 SRM 51-40-05 AND SRM 51-40-02REMOVED DOT.SDR ASAA2022070739243Shield · corrodedFWD CARGO R/H TRANSITION PANEL AT VS 500-500A HAS MULTIPLE AREAS OF LIGHT CORROSION. GROUNDED - YES. REMOVED AND REPLACED THE FWD PIT SHIELD AT STA 500-500A PER B737-800 SRM 51-40-05 AND SRM 51-40-02. PO: 1036786.1.SDR ASAA2022070539338Skin · corrodedLOWER FUSELAGE, JSUT FWD OF APU COMPT LEFT SIDE, SKIN IS CORRODED AT LAP SPLICETIPR833K. GROUNDED - YES. REMOVED CORROSION FROM LOWER SKIN, FWD OF APU COMPT, ORIGINAL THICKNESS 0.080", WITH LOSS OF 0.004", AND 0.076" REMAINING. FOUND TO BE WITHIN LIMITS IAW B7SDR ASAA2022070539334Skin · corrodedLOWER FUSELAGE, SKIN AFT AFT TAIL JACKING POINT IS CORRODED, JUST FWD OF APUL COMPTTIPR833K. GROUNDED - YES. REMOVED CORROSION FROM LOWER SKIN AT AFT TAIL JACKING POINT. ORIGINAL THICKNESS OF 0.080", LOSS OF 0.004", AND 0.076" REMAINING FOUND TO BE WITHIN LIMISDR ASAA2022070439331Skin · corrodedLOWER EXTERIOR FUSELAGE, STA 500A-500G, BL-0, SKINIS CORRODED AT 5EA DRAIN PLUGS. DOTS N074 AND N073DOT: N074TIPR833K. GROUNDED - YES. REMOVED CORROSION FROM LOWER SKIN AT STA 500A-500G BL-0 AT 5EA DRAIN PLUGS ORIGINAL THICKNESS OF 0.080", LOSS OF 0.003", WITHSDR ASAA2022070439330Skin · corrodedLOWER EXTERIOR FUSELAGE, STA 887, LBL40-RBL40, LOWER SKIN IS CORRODED ON FWD SIDE OF BUTT SPLICEDOT: N076TIPR833K. GROUNDED - YES. REMOVED CORROSION AT LOWER SKIN STA 877 BUTT SPLICE, ORIG THICKNESS 0.080", WITH 0.003" REMOVED, 0.077" REMAINING THICKNESS. FOUNSDR ASAA2022070439329Skin · corrodedLOWER EXTERIOR FUSELAGE, STA 887, LBL40-RBL40, LOWER SKIN IS CORRODED ON AFT SIDE OF BUTT SPLICE.DOT: N077TIPR833K. GROUNDED - YES. REMOVED CORROSION AT LOWER SKIN ATA STA 887 BUTT SPLICE, ORIG THICKNESS 0.080" WITH 0.003" REMOVED, 0.077" REMAINING THICKNESS FSDR ASAA2022070439317Skin · corrodedLOWER EXTERIOR FUSELAGE, AT LAV VENT, SKIN IS CORRODED BETWEEN VENT TUBE AND INTERIOR SKIN. GROUNDED - YES. REMOVED CORROSION FROM LOWER SKIN AT LAV VENT, ORIGINAL THICKNESS 0.125", WITH 0.005" REMOVED, AND 0.120" REMAINING, FOUND TO BE WITHIN LIMITS IAW B737-SDR ASAA2022070439316Skin · corrodedLOWER EXTERIOR FUSELAGE, STA 967, LBL6, LOWER SKIN IS CORRODED AROUND AFT DOOR SILL WATER DRAIN.DOT: N081TIPR833K. GROUNDED - YES. REMOVED CORROSION FROM LOWER SKIN AT STA967, LBL6, ORIGINAL THICKNESS 0.063", WITH 0.005" REMOVED, AND 0.058" REMAINING FOUND TO SDR ASAA2022070439315Skin · corrodedLOWER EXTERIOR FUSELAGE, STA 1016, LBL30-RBL40, SKIN IS CORRODED ON AFT SIDE OF BUTT SPLICE GROUNDED - YES. REMOVED CORROSION AT LOWER SKIN STA 1016 BUTT SPLICE, ORIG THICKNESS, 0.080, WITH 0.003 REMOVED, 0.077" REMAINING. FOUND TO BE WITHIN LIMITS IAW B737-80
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