N585AS
Service difficulty reports · 564
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 = 'N585AS' 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 = 'N585AS' 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 ASAA2012110593248Fmc · failedENROUTE, LEFT FMC FAILED - FAIL ANNUNCIATED. SCREEN WENT TO BLACK FOR APPROX 10 SECONDS, BIT TEST SCRIPT DISPLAYED WITH BLUE AND YELLOW FONT THEN OPS RETURNED TO NORMAL FOR DURATION OF FLIGHT. TESTED SYS IAW AMM 34-61-00, GROUND FUNCTIONAL CHECKED GOOD.SDR ASAA2012100693017Indicator · trippedNR 1 ENGINE IDG DPI RED BUTTON IS EXTENDED. ACFT GROUNDED. REMOVED AND INSPECTED THE NR 1 IDG SCAVENGE AND CHARGE FILTERS. DRAINED IDG OIL AND INSPECTED. FOUND NO EVIDENCE OF METAL OR SIGNS OF EXCESSIVE WEAR. RESET THE DPI BUTTON AND MARKED THE DECAL FOR SDR ASAA2012090592831Control Valve · faultedRIGHT PACK LIGHT COMES ON DURING RECALL, EXTINGUISHES WITH MASTER CAUTION RESET. PERFORMED RT PACK BITE 21-61-00-700-806-802. FOUND TEMP CONTROL VALVE FAULT. CLEARED FAULT . PERFORMED GROUND OPS CHECK OF RT PACK, BITE CHECKED AGAIN, NO FAULTS FOUND. SYS RESDR ASAA2012093092990Shutoff Valve · failedDURING PREFLIGHT NR 1 ENGINE VALVE CLOSED. LIGHT ILLLUMINATED BRIGHT. PERFORMED FIM TASK 73-06 TASK 804. FOUND HPSOV POSITION SWITCH AT THE HMU FAILED. R & R NR 1 ENGINE HMU IAW MM REF 73-21-10-000-801-F00 AND MM REF 73-21-10-400-801-F00.SDR ASAA2012093092980Modulating Valve · warning lightON DEPARTURE, RT PACK LIGHT CAME ON - FOLLOWED QRH - LIGHT EXTINGUISHED. ACFT GROUNDED. FOUND RT TCV BAD DURING PACK/ZONE TEMP CONTROLLER BITE TEST WOULD NOT RESET. REPLACED RT TEMP CONTROL VALVE REF AMM 21-51-10 LEAK CHECK WAS GOOD ACCOMPLISHED BITE TEST NSDR ASAA2012080692685Control Valve · malfunctionedRIGHT PACK ILLUMINATED DURING MASTER CAUTION RECALL. THE LIGHT EXTINGUISHED WHEN MASTER CAUTION SYS IS RESET. ACCOMPLISHED BITE TEST ON THE TEMP CONTROLLERS. FOUND NR 2 PACK THIS TEMP CONTROL VALVE LIGHT ON . RESET NR 2 CONTROLLER. SYS GROUND VERIFIED GOOSDR ASAA2012080592672Fmc · false indicationFMC DISAGREE MESSAGE APPEARED ON GROUND. ACFT GROUNDED. RAN CHECKLIST, SYS RESTORED TO NORMAL.SDR ASAA2012080392653Fmc · false indicationFMC DISAGREE ON GROUND. ACCOMPLISHED QRH PROCEDURE. OPS NORMAL.SDR ASAA2012081492720Light · intermittentAUTOTHROTTLE ARM LIGHT INOPERATIVE. ACFT GROUNDED. ACCOMPLISHED A/T SYS OPS TEST IAW AMM TASK 22-31-00-710-801, A/T SYSTEM TEST NORMAL. VERIFIED A/T ARM LIGHT OPERATES NORMAL. NO INFLIGHT FAULTS LOGGED.SDR ASAA2012081292706Filter · bypassingDURING PDC, FOUND THE NR 2 ENG IDG DPI INDICATOR EXTENDED. ACFT GROUNDED. PERFORMED TASK 12-13-21-200-802. REMOVED THE NR 1 ON THE DPI RESET DECAL, RAN ENGINE NO LEAKS NOTED DPI REMAINS SET. OK FOR SERVICE.SDR ASAA2012070992514Fmc · malfunctionedUNABLE TO LOAD FMCS. VERIFIED DEFECT, CYCLED NR 1 & 2 FMC CIRCUIT BREAKERS, BOTH OPS NORMAL REF MM 34-61-00. NO HISTORY PAST 30 DAYS. VERIFICATION FLIGHT SUCCESSFUL.SDR ASAA2012072192566Computer · malfunctionedFOUND FLAG CAPT. ACFT GROUNDED. PERFORMED FIM TASK 22-11-00-810-801. FOUND FCC NR 1 UNABLE TO TEST FAIL. RESET NR 1 FCC TESTS GOOD. NO FURTHER DEFECTS NOTED.SDR ASAA2012071592550Warning Light · false activationFMC DISAGREE LIGHT CAME ON DURING PREFLIGHT. ACCOMPLISHED QRH PROCEDURE, LIGHT REMAINED OUT, OPS NORMAL.SDR ASAA2012062792436Warning Light · false activationFMC DISAGREE AFTER ENGINE START. QRH PROCEDURE COMPLETED OPS NORMAL. PERFORMED FMC OPS TEST REF MM 34-61-00-710-801.SDR ASAA12511569Fmc · malfunctionedFMC DISAGREE ILLUMINATED ON GROUND. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE FMC DISAGREE EXTINGUISHED.SDR ASAA12511557Heater · inoperativeLEFT FORWARD WINDOW HEAT INOPERATIVE. ACFT GROUNDED. CONFIGURED WINDOWS NORMAL OPERATING TEMP WITH TEMP GUN GROUND VERIFICATION, CHECKED NORMAL. SYS CHECKED GOOD IAW 34-41-00.
SDR ASAA12511416Drive Assy · failedPWS FAIL LIGHT CAME ON AT THE GATE. GROUNDED, YES. REPLACED WEATHER RADAR PANEL WITH SERVICABLE ONE. ACCOMPLISHED OPS TEST. TEST FAILED. REINSTALLED ORIGINAL WEATHER RADAR PANEL. REPLACED WEATHER RADAR ANTENNA DRIVE UNIT WITH SERVICABLE ONE. ACCOMPLISHESDR ASAA12511400Transceiver · failed"PWS FAIL" ILLUMINATED ON BOTH ND'S AFTER TRANSFERRING POWER FROM GROUND POWER TO APU POWER. GROUNDED YES. REPLACED WEATHER RADAR TRANSCEIVER IAW 34-43-41. OPS CHECKED GOOD IAW 34-43-00-710-802-001.SDR ASAA12511402Transceiver · failedWHEN POWER WAS TRANSFERED TO APU POWER PWS FAIL ILLUMINATED. ACFT GROUNDED. VERIFIED ALL RADAR & TERRAIN BUSES ARE ACTIVE AND VALID. UNABLE TO CLEAR PWS FAIL. RADAR RT FAILS SELF TEST WITH WEATHER RADAR TRANSCEIVER & PWS FAIL ANNUNCIATED AT END OF TEST. R &SDR ASAA12511401Antenna · failedBOTH PWS FAIL AND WEATHER RADAR FAIL FLAGS ILLUMINATED ON GROUND DURING PREFLIGHT. ACFT GROUNDED. R & R ANTENNA DRIVE UNIT, REF MM 34-43-1. OPS CHECKED NORMAL.SDR ASAA12511398Autothrottle Sys · inoperativeAUTO THROTTLES DISENGAGED AND WILL NOT RE ENGAGE. ACFT GROUNDED. LAST FAULT LEG FAULTED ASM 1 SEVERAL TIMES. PERFORMED AUTOTHROTTLE SERVO TEST ASM 1 FAILS THROTTLE NR 1 DOES NOT MOVE. VERIFIED DISCREPANCY. REPLACED NR 1 ASM. OPS NORMAL. REF MM 22 31 91.SDR ASAA12511399Transceiver · failedWEATHER RADAR FAILED MESSAGE DISPLAYED ON PFD. ACFT GROUNDED. PERFORMED WEATHER RADAR BITE PROCEEDURE IAW FIM 34-43 TASK 801 AND WEATHER RADAR OPS TEST IAW AMM 34-43-00-710-802-001. UNABLE TO VERIFY. NO FAULTS. REPLACED WEATHER RADAR TRANSCEIVER IAW AMM 34-SDR ASAA12511380Transceiver · malfunctionedRADAR SPIKING FOR FIRST 45 MINUTES OF FLIGHT THEN APPEARED TO WORK NORMAL. REPLACED WEATHER RADAR TRANSCEIVER PER MM 34-43-41. OPS CHECKED GOOD PER MM 34-43-00.SDR ASAA12511253Idg · malfunctionedNR 2 DRIVE LIGHT OUT FOUND DURING PREFLIGHT. REMOVED NR 2 IDG PER TASK 24 11 11 000 801 PAGES 1 9. INSTALLED NR 2 IDG PER TASK 24 11 11 400 801 PAGES 1 10. PERFORMED LEAK CHECK NR 2 IDG PER TASK 71 00 00 700 801 F00 PAGES 1 3. NO LEAKS NOTED. OPS CHECK NRSDR ASAA12511094Panel · damagedNR 2 ENGINE FAN DUCT PANEL AT LT SIDE OF 6 O`CLOCK LLDLK STRUT AFT LOOKING FWD HAS TWO LOOSE FASTENERS ONE PULLED THRU PANEL. INSTALLED NEW PANEL PER AMM 72 23 07 000 801 F00 AND 400 801 F00.SDR ASAA12511069Valve · faultyIN CRUISE NOTICED A DUCT PRESSURE SPLIT LEFT 47 PSI RIGHT 21 PSI. LATER NOTICED THE SPLIT AT 43 PSI RIGHT 23 PSI. IN DESCENT POWER LEVELS IDLE SPLIT WENT AWAY L 20 PSI RIGHT 20 PSI. PERFORMED NR 2 ENG BLEED AIR HEALTH CHECK PRSOV BLEED AIR REG HIGH STAGE VASDR ASAA12511019Unknown · malfunctionedTHE "OFFSET" WARNING ON CAPT'S CDU BLINKS IN CONJUNCTION WITH THE CTR FUEL TANK LOW PRESS LIGHTS. WHEN PUMPS POSITIONED OFF BLINKING STOPS. F/O'S "OFFSET" WARNING ON F/O CDU DOES NOT BLINK IN CONJUCTION WITH FUEL TANK LOW PRESS LIGHTS. ALSO "OFFSET" WARNINGSDR ASAA12511016Control Panel · faultyTHE FIRST DIGIT ON THE GLARE SHIELD HEADING SELECTOR "FLUTTERS" (CONTINUALLY BLINKS VERY FAST) NO OTHER DIGITS ON GLARE SHIELD SELECTORS "FLUTTER". REPLACED MCP REF MM 22 11 34 OPS CHECK NORMAL. ACCOMPLISHED ALL MCP LWMP CHECKS REF LWMP CHECKLIST MM 22 00 01SDR ASAA12510945Idg · defectiveNR 1 ENG IDG DELTA P INDICATOR BUTTON EXTENDED. DUE TO HISTORY, REPLACED THE NR 1 ENGINE IDG PER MM 24 11 11. LEAK AND OPS CHECK GOOD.SDR ASAA12510928Unknown · malfunctionedMOMENTARY LOSS OF RIGHT FMC IN CRUISE FLIGHT. RIGHT FMC FAIL LIGHT ILLUMINATED AFTER TOUCHDOWN ALSO. PERFORMED TASK 34 61 TASK 807. FMC PROMPT SHOWS INDICATES INTERMITTANT FAULT.SDR ASAA12510874Unknown · malfunctionedCONT CABIN ZONE TEMP LIGHT ILLUMINATES ON RECALL. RAN BITE TEST NR 2 CONTROLLER FLT DECK TRIM VALVE ILLUMINATED. RAN GROUND VERIFY NO FAULTS RERAN BITE NO FAULTS NOTED.SDR ASAA11510846Duct · separatedON GROUND FLIGHT DECK TEMP CONTROLLER WILL NOT SUPPLY COLD AIR TO FLIGHT DECK. FULL COLD SELECTION ONLY SENDS 31 C AIR SUPPLY DUCK. FOUND DUCT CLAMP OFF AND DUCT SEPARATED AT RECIRCULATION FAN LEFT A/C BAY. CLAMP DAMAGED. DUCT ASSY GOUGE AT FLANGE NECK IS SDR ASAA11510798Shim · damagedREF T/C # 78472002 NR 2 ENGINE FAN LUBE. ALL 24 EA SHIMS MISSING MOLY DAG COATING. INSTALLED NEW SHIMS 24 EA PER TASK CARD 78472002 ON NR 2 ENG.SDR ASAA11510753A/C Pack · contaminatedSMELLED DIRTY SOCK / ENG OIL ON DESCENT BELOW 10000 DISSIPATED AFTER 5 MIN. REPLACED APU PER MM 49 11 00 000 803 & 49 11 00 400 803 STEPS THRU M(7). APU INSTALL AND TEST COMPLETED. REF MM 49 11 00 400 803 (N) & (O). OPS/LEAK CHECK GOOD. ACCOMPLISHED OIL CSDR ASAA11510729Warning System · false activationON PUSHBACK AFTER RECALL RIGHT "PACK" LIGHT ILLUMINATED. C/W ZONE TEMP CONTROL BITE REF FIM 21 62 00 810 801. NO FAULTS NOTED. VERIFIY TEST PASS.SDR ASAA11510727Acm · malfunctionedON DESCENT TO ARRIVAL "DIRTY SOCK" SMELL FROM AIR IN THE A/C. RAN LT & RT PACK 1 AT A TIME FOUND FAINT SMELL ON RT PACK. FOUND RT ACM HARD TO TURN. REPLACED RT PACK ACM OZONE CONVERTER AND LT AND RT RECIRCULATION FILTERS. RAN RT PACK LEAK CHECKED GOOD. NOSDR ASAA11510686Unknown · malfunctionedFMC POS SHIFT PG 3/3 SHOWS NO FMC GPS IRS DATA. SUSPECT POS SHIFT PG DISPLAYED IN AIR ONLY. POS REF PG 2 SHOW LAT AND LONG FOR ALL SENSOR. ACCOMPLISHED FMC BITE PER FIM 34 61 TASK 801 SENSORS AND IN FLIGHT FAULT SHOW NO FAULTS. A/C OK FOR SERVICE.SDR ASAA11510646Battery · faultyMAIN BATTERY SHOWS 27 VOLTS AND 1 AMP CHARGE THROUGHOUT THE FLIGHT. PERFORMED MAIN BATTERY CHARGER OPS TEST REF MM 24 31 21 710 801 OPS TEST GOOD. REPLACED MAIN BATTERY REF MM 24 31 11 000 802 002. BATTERY INSTALLATION TEST & GRD FUNCTIONAL TEST PASSED.SDR ASAA11510600Chip Detector · contaminatedENG 1 REF T/C #78472040 MAGNETIC CHIP DETECTORS INS. ON THE AFT SUMP MAGNETIC CHIP DETECTER FOUND MAGNETIC THREAD LIKE SILVER. CHECKED "IN SERVICE" OIL CONSUMPTION (PAST 165 HRS) AND FOUND TO BE WITHIN LIMITS NO OIL PRESS DISCREPANCIES FOUND. OKAY FOR CONTINSDR ASAA11510599Liner · delaminatedNR 1 ENGINE INLET ABRADABLE SHROUD AT 5 O'CLOCK LOOKING INTO FAN IS DELAMINATED APPX 12" LENGTH REF T/C 78472000. COMPLETED ABRADABLE SHROUD REPAIR THRU F 6 C REF 72 24 02 200 802 F00. COMPLETED ABRADABLE SHROUD REPAIR 6(D) 10(A) PER MM REF 72 24 02 200 802 SDR ASAA1150558Unknown · malfunctionedCAPT FMC OFST LIGHT WOULD NOT DIM WITH LIGHT SWITCH IN DIM POSTION. EVENTUALLY ALTERNATED BETWEEN BRIGHT AND DIM FO OFST LIGHT WORKED NORMALLY. TESTED CAPT FMC CDU FIXED OUTPUT DISCRET PAGE WITH THE LIGHTS SWITCH IN THE BRIGHT AND DIM MODES UNABLE TO DUPLICASDR ASAA1150409Filter · defectiveDURING ETOPS PDC CHECK FOUND: LT ENG DELTA P INDICATION PIN EXTENDED RED SHOWING. REFERENCE AMM 05 51 93 PG 2 STEP 6. REPLACED SCAVENGE FILTER AND CHANGED IDG OIL. CONDITION SATISFACTORY.SDR ASAA11510332Unknown · malfunctionedFD FLAG ON CAPT PRIMARY ATTITUDE GYRO. RECYCLED ACFT POWER ACCOMPLISHED FIM TASK 22 11 00 810 801. DFCS BITE (FD BITE) PASSED NORMAL.SDR ASAA11510255Filter Element · defectiveNR 1 ENG DPI POPPED ON IDG SCAVENGE FILTER AND CHARGE FILTER. DPI WAS RESET RUB NR 1 OFF DECAL. CHANGED SCAVENGE FILTER AND INSPECTED. NO METAL PARTICALS FOUND. REF AMM 24 11 41. SERVICED IDG REF AMM 12 13.21.SDR ASAA11510232Unknown · malfunctionedWX RADAR DOES NOT FUNCTION IN "WX" MODE WHEN "WX" IS SELECTED ON CAPT'S SIDE IT TRIPS OFF "TERRAIN" ON F/O'S SIDE AS WELL. UNABLE TO DUPLICATE WXR OPERATIONAL TEST NORMAL REF MM 34 43 00. BOTH DEU LOGGED 31 67550 ON PREVIOUS LEG. PERFORMED FIM 31 63 TASK 80SDR ASAA11510220Servo · malfunctionedAUTOTHROTTLES WILL NOT REMAIN ENGAGED. REPLACED ASM1 REF MM 22 31 91 OPS NORMAL. PERFORMED A/T OPERATIONAL TEST AND LAND VERIFY REF MM 22 11 00. A/C REMAINS CAT IIIA AUTOLAND & HGS QUALIFIED STATUS SCREW REFLECT SAME.SDR ASAA11510202Servo · failedAUTOTHROTTLES WILL NOT STAY ENGAGED. PERFORMED FIM TASK 22 31 00 810 805 AUTOTHROTTLE SERVO MOTOR FAILURE. CONFIRMED FAULT NR 1 AUTOTHROTTLE SERVO MOTOR FAILURE. REPLACED NR 1 AUTOTHROTTLE SERVO MOTOR PER M/M 22 31 91. OPS CHECK GOOD.SDR ASAA11510198Sensor · faultyDURING CLIMB HAD A DUCT PRESSURE SPLIT IN EXCESS OF 20 PSI. CLIMB AT FLIGHT LEVEL 350 N1 100.9 PERCENT WING & ENGINE ANTI ICE OFF ISOLATION VALVE AUTO PACK SWITCHES AUTO BLEED AIR SWITCHES ON LEFT BLEED AIR DUCT PRESSURE 42 PSI RIGHT BLEED AIR DUCT PRESSURE 2SDR ASAA11510173Circuit Breaker · openAFTER SELECTING "WX" ON RADAR CONTROL PANEL "WXR FAIL" APPEARED ON THE ND. WX RADAR APPEARED INOP. FOUND WX RADAR RT CB OUT. RESET CB PER AMM 20 60 01 860 801. NO DEFECTS NOTED DURING RESET ACP WX RADAR SYSTEM OPERATIONAL TEST PER AMM 34 43 00 710 802 001,SDR ASAA11510065Probe · out of toleranceGE DIAGNOSTICS REPORTS NR 2 ENGINE TREND DATA CONTINUES TO SHOW A SHIFT IN DELTA CRUISE AND TAKEOFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. ACCOMPLISHED T49.5 PROBE AND EGT SYSTEM INSPECTION REF MM 77 21 01. FOUND S2 PROBE OUT OF TOLERANCE. REPLACED S2
Back to N585AS