N560AS
Service difficulty reports · 562
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 = 'N560AS' 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 = 'N560AS' 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 ASAA2013013193794Autopilot Sys · malfunctionedWHILE AT 37,000 FT IN SMOOTH AIR, AUTOPILOT DISCONNECTED. RECONNECTED IMMEDIATELY (COMMAND A SIDE). ACCOMPLISHED FLT FAULTS REVIEW AND CURRENT STATUS TEST, NO FAULTS AND ALL TEST PASSED. ACCOMPLISHED LAND VERIFY TEST, GRP BITE 49, ALL TEST PASSED, REF MM 2SDR ASAA2013012093703Filter · dirtyCONT CAB LIGHT ON RECALL ZONE TEMP. BITE TEST OF PACK/ZONE TEMP CONTROLLERS SHOWED NO FAULTS AND VERIFY TEST PASSED FOR BOTH WITH NO TRIM VALVE FAULTS. FOUND CONTROL CABIN ZONE TEMP SENSOR AND FILTER VERY DIRTY. CLEANED TEMP SENSOR IAW MM 21-61-10-100-801 ANSDR ASAA2013011993704Warning Light · false activationAFTER LANDING, DURING TRANSFER FROM ENGINE GENERATOR TO APU POWER, PRESSURIZATION AUTOFAIL AND ALTN LIGHTS CAME ON. FOUND LRU FAIL OFV OII ON NR 2 DCPC. RESET IAW FIM TASK 21-31, TASK 802. ALL FAULTS CLEARED AND DID NOT RETURN. BOTH NR 1 AND NR 2 DCPCS CHECSDR ASAA2013011793707Circuit Breaker · trippedON PREFLIGHT, FOUND HF 2 CIRCUIT BREAKER TRIPPED. RESET HF 2 CIRCUIT BREAKER IAW AMM 20-60-01. CIRCUIT BREAKER REMAINS RESET. NO DEFECTS NOTED. PERFORMED HF 2 COMMUNICATION SYS TEST IAW AMM 23-11-00. SUCCESSFUL GROUND OPS CHECK. NO DEFECTS NOTED.SDR ASAA2013010193591Warning Light · false activationFMC DISAGREE ON TAXI OUT. RESET IAW QRH, OPS NORMAL.SDR ASAA2012123193592Sensor · malfunctionedAPU CTS ATP TREND DATA SHOWS MES EGT IS AT OR NEAR THE ESTABLISHED THRESHOLD. INDICATION ERRORS ARE SUSPECT. ACFT GROUNDED. R & R APU INLET TEMP SENSOR (T2). REMOVED THE INLET PRESSURE SENSOR (P2). EXAMINED THE ORFICE IN THE SENSOR TO MAKE SURE IT IS NOT BLSDR ASAA2012122093511Fmc · malfunctionedIAW TC 78273000 INTERROGATE THE FMC/CDU FOR NR 1 ENGINE, FOUND FAULT NR 73-30791 PS3 SIGNAL DISAGREE. ACCOMPLISHED FIM TASK 73-26 TASK 806. NO RECENT FAULTS FOUND. NO FAULT HISTORY FAULTS FOUND.SDR ASAA2012121093435Indicator · failedBACK LIGHTING FOR CABIN AIR TEMP INOPERATIVE. REPLACED CABIN TEMP INDICATOR, REF MM 21-61-32. OPS CHECK OF INDICATOR NORMAL IAW SAME.SDR ASAA2012112093336Autopilot Sys · malfunctionedDURING CRUISE, FL 380, AUTOPILOT A DISENGAGED. QRH ACCOMPLISHED AND AUTOPILOT A DID ENGAGE. LRU TESTS PASSED REF AMM 22-00-01-730-801. ACFT REMAINS CAT IIIA A/L & HGS QUALIFIED. STATUS IND REFLECTS SAME.SDR ASAA2012111993324Fmc · malfunctionedRT FMC INOPERATIVE. BOOTED RT FMC, NORMAL OPS RESTORED. FMC OPS CHECKED OK IAW FIM 34-61 TSK 832. VERIFIED MAP & VTK FLAGS PULLED, GROUND VERIFICATION OK.SDR ASAA2012111093280Shutoff Valve · failedDUCT PRESSURE SPLIT DURING CLIMB, EXCEEDS 20 PSI, FL 360L 43.0, R22.0, FL 400L 42.0 R 20.0. REPLACED NR 2 ENGINE PRSOV IAW AMM 36-11-04 LEAK AND OPS CHECK GOOD.SDR ASAA2012111093270Control Valve · failedECS DISCRETE FOR RT PACK DOES NOT SHOW OFF WHEN SELECTED OFF. REPLACED RT FLOW CONTROL VALVE REF MM 21-51-01. OPS CHECK GOOD, LK CHECK GOOD.SDR ASAA2012110993277Keyboard · malfunctionedNR 2 MCDU HAS LIGHT BLEED THRU ON SEVERAL BUTTONS. R & R NR 2 MCDU KEYBOARD & TEST GOOD IAW AMM 34-61-01-400-801.SDR ASAA2012110893255Probe · out of limitsNR 2 ENGINE TREND DATA SHOWS A SUDDEN SHIFT IN EGT HOT DAY MARGIN AND DELTA EGT ALL OTHER PARAMETERS NORMAL. EGT INDICATION ERRORS ARE SUSPECT. TROUBLESHOT & FOUND EGT PROBE T49.552 TO BE OUT OF LIMITS FOR ELECTRICAL. RESISTANCE REMOVED 749.552 IAW AMM 77-2SDR ASAA2012110693254Heater · leakingNR 1 ENGINE FUEL SERVO HEATER LEAKING. R & R NR 1 ENGINE SERVO FUEL HEATER IAW AMM 73-11-07, LEAK AND OPS CHECKED GOOD.SDR ASAA2012103093319Housing · gougedAFT CARGO DOOR EXTERNAL HANDLE HOUSING OTBD INTERNAL SURFACE CHAFED. 2 PLACES. ACFT GROUNDED. R & R AFT CARGO EXTERNAL HATCH ASSY, PN H414-69 IAW BAC DWG 149A6134 AND SRM 51-40-02.SDR ASAA2012103093241Structure · gougedAFT CARGO DOOR HANDLE BOX / LATCH ASSY FOUND TO BE CORRODED. ACFT GOUGED. R & R AFT CARGO EXTERNAL HATCH ASSY, PN H414-69 IAW BAC DWG 149A6134 AND SRM 51-40-02.SDR ASAA2012102593266Floor Support · crackedFLOOR SUPPORT CRACKED. REMOVED AND REPLACED.SDR ASAA2012102593238Floor Support · crackedINTERCOSTAL FLOOR SUPPORT STRUCTURE CRACKED. R & R FLOOR SUPPORT STRUCTURE ANGLE IAW SRM 51-40-02.SDR ASAA2012100893082Inverter · failedOVERHEAD ELEC LIGHT WAS FOUND ILLUMINATED DURING PREFLIGHT. REPLACED STATIC INVERTER IAW AMM 24-34-21, OPS CHECKED GOOD. GROUND TEST VERIFICATION GOOD IAW AMM 24-34-21-400-801, PARAGRAPH G.SDR ASAA2012090992856Valve · failedNR 2 ENGINE ANTI ICE VALVE APPEARS TO BE STUCK IN THE OPEN POSITION. VERIFIED ENGINE NR 2 COWL VALVE LIGHT ILLUMINATED. SUSPECT OUT OF SEQUENCE SHUTDOWN. ACCOMPLISHED ENGINE ANTI ICE OPS TEST FOR NR 2 ENIGINE. IAW AMM 30-21-00 COWL VALVE LIGHT EXTINGUISHED.SDR ASAA2012081792730Terminal · brokenFOUND MW0316 HARNESS TERMINAL LUG BROKEN. ACFT GROUNDED. REPLACED HARNESS TERMINAL LUG REF MM 26-11-02-960-801, OPS NORMAL REF MM 26-11-00-710-801.SDR ASAA2012071992574Panel · looseNR 2 ENGINE, FAN DUCT PANEL AT 400 O`CLOCK POSITION, UPPER ROW FWD BOLT LOOSE. ACFT GROUNDED. SECURED NR 2 ENGINE FAN DUCT PANEL BOLT AT THE 400 O`CLOCK POSITION IAW AMM 72-23-02-400-801-F00.SDR ASAA12511669Warning Light · illuminatedAT CRUISE, R2 WINDOW (SIDE) OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED AFTER WINDOW HEAT TURNED BACK ON (PERQRH) AFTER 2 MINUTES LIGHT NEVER CAME BACK ON REMAINDER OF FLIGHT. PERFORMED BITE CHECK WHCU NO CURRENT FAULTS. INTERMITTENT FAULT. FIM TASK 30-SDR ASAA12511587Cdu · malfunctionedAPPROACHING THE CRITICAL POINT, NR 1 CDU WENT COMPLETELY BLANK FOR 20 SECONDS. IT CAME BACK IN A BITE TEST MODE AND THEN RETURNED TO NORMAL FUNCTION. NO PILOT ACTIONS WERE TAKEN DURING THIS EVENT. ACFT GROUNDED. REMOVED LT FMC CDU REF 34-61-01. CLEANED COOSDR ASAA12511504Control Valve · failedRIGHT PACK LIGHT ILLUMINATES WITH MASTER CAUTION RECALL. EXTINGUISHES WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED PACK/ZONE TEMP CONTL BITE REF AMM 21-61-00, RT (NR 2) CONTROLLER HAS "TCV THIS PACK" FAULT ILLUM. RESET BUT SAME FAULT REAPPEARS ON 3 SUSDR ASAA12511469Sensor · malfunctionedAPU EGT HAS HISTORY OF INDICATING LOW AND ERRONEOUS. INDICATION ERRORS ARE SUSPECT. ACFT GROUNDED. R & R INLET TEMP SENOR REF AMM 49-61-31. OPS/BITE CHECKED GOOD REF AMM 49-61-00-700-801.SDR ASAA12511452Unknown · unknownSTARTED APU BUT NO VOLTS OR FREQ. ELECTRICAL METERS BATTERY AND GALLEY POWER MODULE TESTS GOOD IW MM 24-21-53. GROUND VERIFICATION SUCCESSFUL.SDR ASAA12511293Spinner · out of limitsNR 1 ENG INLET SPINNER CONE OUT OF LIMITS PER T/C 78472002 (FAN BLADE LUBE). REMOVED AND REPLACED SPINNER CONE PER AMM 72 21 01. T/C 78472002.SDR ASAA12511265Control Panel · malfunctionedVNAV SWITCH LIGHT OUT WHEN SELECTED AND ON LIGHTS TEST. VNAV WORKS NORMAL. REPLACED MCP PANEL REF MM 22 11 34. ACCOMPLISHED LWMP TEST BITE NR 32 AND BITE NR 49 AND HGS SENSOR TEST FCC/AT REF LWMP CHECKLIST MM 22 00 01 AND SMM 34 36 00. ALL TEST GOOD.SDR ASAA12511244Light · malfunctionedVNAV LIGHT ON MODE CONTROL PANEL INOP. V NAV LIGHT OPERATES NORMAL ON GRND. NO HISTORY FOR 30 DAYS.SDR ASAA12511209Light · inoperativeREF T/C 78233008 EMERGENCY LIGHTS OPS CHECK. EMERGENCY LIGHT AFT OF R2 DOOR INOP. RELAMPED EMERGENCY LIGHT AFT OF R2 DOOR. REF MM 33 51 04 960 801.SDR ASAA1251194Indicator · inoperativeREFUEL STATION CENTER TANK GAUGE WILL NOT TEST. VERIFIED FAULT. REMOVED REFUEL PANEL ACCOMP. GVI OF WIRE BUNDLE NO DEFECTS NOTED. REPLACED CENTER REFUEL IND WITH SERVICABLE ONE. RE-INSTALLED REFUEL PANEL. ACCOMP INSTALLED TEST OF REFUEL PNL TEST PASS REFSDR ASAA12510918Actuator · failedON APPROACH MASTER CAUTION RECALL CHECK SHOWED AIR COND ON ANNUNCIATOR PANEL & R PACK LIGHT ON OVERHEAD. REPLACED RT RAM AIR INLET ACTUATOR REF M/M 21 51 21. ACTUATOR TEST OPS NORMAL REF M/M 21 61 00.SDR ASAA12510894Warning System · false activationRIGHT PACK LIGHT ILLUMINATES WITH MASTER CAUTION RECALL. LIGHT EXTINGUISHES WITH RESET. PERFORMED BITE CK OF NR 2 ZONE TEMP CNTL PER AMM REF 21 61 00. FAULTS 32 PACK RAM AIR ACTUATOR. PERFORMED FAULT RESET PROCEDURE PER SAME REF FAULT CLEARED PACK LIGHT EXSDR ASAA11510851Unknown · malfunctionedON PREFLIGHT FO NOTED WING ANTI ICE VALVE C/B POPPED OUT. INSPECTED C/B PANEL & VALVE. NO DEFECT NOTED. RESET C/B REF AMM 20 60 01 PROCEDURE. OPS CHECK NORMAL REF AMM. 30 11 00. GROUND VERIFICATION GOOD.SDR ASAA11510730Unknown · malfunctionedRIGHT PACK ILLUMINATED ON RECALL RESET WITH MASTER CAUTION RESET. GROUNDED YES. PERFORMED FIM TASK 21 53 00 810 804 RIGHT PACK LIGHT ON DURING GROUND OPERATION AND STAYS OFF AFTER RESET. NO FAULTS FOUND GROUND VERIFICATION TESTS NORMAL.SDR ASAA11510718Indicator · defectiveREF TASK CARD NUMBER 78349013 APU OIL FILTER DELTA P INDICATOR EXTENDED. ACCOMPLISHED OIL FILTER DELTA P INDICATOR SERVICING REF TASK 49 91 13 NO CONTAMINATION NOTED ON EITHER MAGNETIC DRAIN PLUG OR OIL FILTER ELEMENT. REPLACED DELTA P INDICATOR. WOULD NOT SDR ASAA11510680Warning System · false activationPRESSURIZATION AUTO FAIL & ALTN LIGHTS ON. ACCOMPLISHED FIM TASK 21 31 00 (DCPC) BITE OPS CHECK NORMAL. GRD VERIFICATION TEST NORMAL.SDR ASAA11510678Unknown · malfunctionedON TAXI OUT FMC DISAGREE LIGHT ILLUM. PERFORMED QRH PROCEDURE. OPS NORMAL.SDR ASAA11510685Anti-Ice Valve · faultyDURING DESCENT FROM ABOUT 27,000' WHEN THE ENG ANTI ICE WAS TURNED ON THE NR 1 ENG ANTI ICE VALVE STAYED BRIGHT BLUE. SWITCH WAS CYCLED VALVE DID NOT CLOSE CORRECTLY BUT NOT OPEN. AFTER LANDING PILOT NOTED ON POST WALK AROUND THAT BOTH ENG COWLS WERE WARM ABSDR ASAA11510674Warning System · false activationRT PACK LIGHT ILLUMINATED UPON RECALL AFTER ENGINE START. NR 2 CTC LOGGED TCV FAULT PERFORMED BITE TESTS GOOD FAULT CLEARED.SDR ASAA11510647Unknown · malfunctionedENGINE NR 1 "A" FIRE LOOP WILL NOT TEST. COULD NOT DUPLICATE DEFECT. ENG/APU FIRE OVERHEAT WARNING OPS NORMAL FROM CONTROL STAND P8 OPS NORMAL AND MODULE M279 OPS NORMAL REF FIM 26 10 00 810 801.SDR ASAA11510459Unknown · malfunctionedFMC DISAGREE ON GROUND. PERFORMED QRH PROCEDURE. LIGHT RESET, OPS NORMAL.SDR ASAA11510399Control Module · faultyFOUND NR 1 ENG CONTROL LIGHT WILL NOT TEST. DUPLICATED DEFECT NR 1 ENG CONT LT WONT TEST WITH LIGHTS TEST. REPLACED ENG CONTROL MODULE REF MM:73 21 12 OPS TEST ALL CHECK NORMAL.SDR ASAA11510394Unknown · malfunctionedCONT CAB ZONE TEMP ILLUMINATED ON RECALL. EXTINGUISHES WITH RESET. ACCOMPLISHED PACK/ZONE TEMP CONT BITE TEST PER AMM 21 51 00. NO FAULTS NOTED. A/C GOOD FOR CONTINUED SERVICE.SDR ASAA11510384Idg · malfunctionedLEFT (GEN 1) "SOURCE OFF" LIGHT ILLUMINATED ON DESCENT AT 20 000 FT. REF FIM TASK 24 21 00 GCU BITE TST SHOWS NR 1 IDG FAULT. NR 1 GCU LRU BITE TEST OK. NR 1 IDG REQUIRES REPLACEMENT REF. FIM TASK 24 21 TSK 806. REPLACED NR 1 IDG PER MM 24 11 11. COMPLETESDR ASAA11510368Transceiver · failedHF 1 FAILED EN ROUTE. PERFORMED HF 1 COMMUNICATION SYS BITE REF TASK 23 11 00 810 801. FOUND NR 1 HF TRANSCEIVER INOP. FAULT WAS DUPLICATED. REPLACED NR 1 HF TRANSCEIVER REF AMM TASK 23 11 21 000 REMOVAL & AMM TASK 23 11 21 400 801 INSTALLATION. NR 1 HF RSDR ASAA11510215Control Valve · malfunctionedLEFT PACK OVHD AND AIR CONDITIONING MC LIGHTS ILLUMINATED ON RECALL. REPLACED RT TEMP CONTROL VALVE PER AMM 21 51 10 BITE TEST GOOD OPS CHECK GOOD, LEAK CHECK GOOD.SDR ASAA11510097Transceiver · malfunctionedNR 1 HF CB POPPED EN ROUTE (E 11). FOUND NR 1 HF T/R INOP WOULD NOT TEST. REPLACED NR 1 HF T/R PER AMM 23 11 21. OPS CHECKED NORMAL PER SAME AMM. RESET C/B PROCEDURE AMM 20 60 01, NO FAULTS NOTED ALL GROUND TESTS PASS.
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