N581AS
Service difficulty reports · 484
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 = 'N581AS' 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 = 'N581AS' 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 ASAA2014072608675Controller · malfunctionedON RECALL FWD CAB ZONE TEMP. ACFT GROUNDED. R & R, AND TESTED NR 1 PACK/ZONE TEMPERATURE CONTROLLER IAW MM 21-61-20-000-801 & MM 21-61-20-400-801. OPS NORMAL.SDR ASAA2014072208646Warning Message · false activationFMC DISAGREE. ACFT GROUNDED. RESET IAW QRH PROCEDURE.SDR ASAA2014072008614Satcom · malfunctionedSATCOM LOCKED UP ON GROUND. ACFT GROUNDED. SAT PROMPT IS DISPLAYED AFTER FOLLOWING QRH.SDR ASAA2014072008612Filter · dirtyFWD CAB ZONE TEMP LIGHT CAME ON DURING RECALL OF MASTER CAUTION DURING LANDING CHECK. ALSO, COMES ON DURING RECALL ON THE GROUND. ACFT GROUNDED. REPEAT WRITE-UP, THE STBY PACK FAULT LIGHT CAME UP ON THIS AND 2 PREVIOUS WRITE UPS BUT SUBSEQUENT TESTS ARE GOOSDR ASAA2014071908587Warning Light · false activationFLIGHT CREW REPORTED FWD CABIN ZONE TEMP LIGHT ILLUMINATED DURING RECALL, EXTINGUISHES WITH MASTER CAUTION. ACFT GROUNDED. NO FAILURES WHEN TROUBLESHOOTING. RESET SYSTEM AND CHECKED SYSTEM IAW AMM 21-51-00-700-803, GROUND FUNCTIONAL TESTED GOOD. RAN BOTH PACSDR ASAA2014071608570Transceiver · failedSATCOM LOCKED UP. NO SATCOM PROMPT ON MCDU MENU PAGE. ACFT GROUNDED. CYCLED SATCOM CIRCUIT BREAKER, NO HELP. SATCOM LRU SHOWS RED LED ON, ALL LED'S SHOULD BE GREEN. REMOVED AND INSTALLED NEW IRIDIUM TRANSCEIVER IAW 23-15-00-400-801. PERFORMED SYS OPS TESSDR ASAA2014071508565Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. RESOLVED VIA QRH PROCEDURES.SDR ASAA2014070808489Warning Message · false activationFMC DISAGREE LIGHT ON TAXI OUT GROUNDED. QRH FOLLOWED PROCEDURES RESET NORMALLY DUAL FMC OPS RESTORED.SDR ASAA2014070708472Controller · failedCOCKPIT TEMP LIGHT ON RECALL. RESETS NORMALLY. ACFT GROUNDED. PERFORMED PACK/ZONE TEMP CONT BITE TEST IAW AMM TASK 21-51-00-700-803. FOUND NR 1 PACK ZONE CONTROLLER FAULT ON BOTH BIT AND PREV FLT TEST. REPLACED NR 1 PACK ZONE TEMP CONTROLLER, OPS CKS GOODSDR ASAA2014061708254Module · failedDURING PREFLIGHT, THE R2 WINDOW OVERHEAT LIGHT ILLUMINATED AFTER SWITCHING WINDOW HEAT ON. ACFT GROUNDED. BITE OF WHCU SHOWS P5-9 MODULE FAULTS LAST 3 LEGS. DUPLICATED OVERHEAT LIGHT. REPLACED P5-9 WINDOW AND PITOT HEAT MODULE REF 30-41-41. OPS CHECK NORSDR ASAA2014061608234Warning Light · false activationF/O'S SIDE WINDOW HEAT "OVERHEAT" LIGHT ILLUMINATED WILL NOT RESET. ACFT GROUNDED. INDICATIONS ON OVERHEAD PANEL WERE NORMAL, GREEN ON LIGHT ILLUMINATED OVERHEAT LIGHT OFF WHEN CHECKED. C/W FIM TASK 30-41-00-810-801 BITE OF WINDOW HEAT CONTROL UNIT. FOUNDSDR ASAA2014061308181Hsi · faultedFORWARD FLAG ON CAPTAIN`S EHSI. ACFT GROUNDED. ACCOMPLISHED FIM 22-11, TASK 801, DFCS BITE, FFR SHOWS FOUR GROUND FAULTS ON 6-13-2014. MSG 22-11309, SPD TRIM WARN CH-A, MSG 22-11315 MTS WARN CH-A, MSG NR 22-11191, MT CMD MON CH-A, AND 4 MSG 22-11303, FCC-A SDR ASAA2014061308172Computer · malfunctionedSPEED TRIM FAILED AND MACH TRIM LIGHT ILLUMINATED AFTER PUSHBACK DURING RECALL. ACFT GROUNDED. AFTER POWER DROP OFF AT GATE FAULTS SHOWED ON RECALL, SPEED TRIM, MACH TRIM FAIL. PERFORMED DFCS BITE SHOWED FAULTS 11101, 11102, 11302, 11321. POWERED DOWN ACFTSDR ASAA2014060608088Lens · looseFOUND R2 DOOR SLIDE EMERGENCY LIGHT LENS LOOSE IN RETAINER. ACFT GROUNDED. REPLACED R2 DOOR SLIDE LIGHT RETAINER IAW MM 33-51-04-960-801.SDR ASAA2014060108002Warning Message · false activationFMC DISAGREE ILLUMINATED, ACFT GROUNDED. PERFORMED QRH PROCEDURE, OPS NORMAL.SDR ASAA2014052807964Control Panel · failedAPU GENERATOR NOT COMMING ON LINE. ACFT GROUNDED. REMOVED AND INSTALLED NEW P5-4 PANEL. PERFORMED OPS TEST REF 24-21-00. SYS CKS NORMAL.SDR ASAA2014052207917Controller · faultedAFTER ENGINE START, MASTER CAUTION REVEALED AIR CONDITION ANNUNCIATOR LIGHT WITH AUTO FAIL LIGHT AND GREEN ALTN LIGHT ON. ACFT GROUNDED. PERFORMED FIM 21-31, TASK 827. NR 2 AND NR 1 CONTROLLERS SHOW NO EXISTING FAULTS. NR 1 CONTROLLER FAULT HISTORY SHOWS LEGSDR ASAA2014052107897Warning Light · false activationAPU FAULT LIGHT CAME ON. NO APU ROTATION SHUTDOWN, ACFT GROUNDED. PERFORMED GROUND VERIFICATION IAW FIM TASK 49-40, TASK 803. NO DEFECT NOTED. APU STARTS NORMAL. NO HISTORY 30 DAYS. FIM TASK 49-40TASK 803. PASSED CSS NO APU CAUTION LIGHTS PERFORMED AT FSDR ASAA2014051707864Control Panel · failedBANK SELECTOR KNOB, MODE CONTROL PANEL 25 & 30 ONLY. ACFT GROUNDED. REPLACED MCP IAW MM 22-11-34, OPS CHECKED NORMAL. ACCOMPLISHED DFCS LRU MCP NR 32 TEST, LAND VERIFY NR 49, & HGS FCC/AT SENSOR TEST, ALL TEST NORMAL IAW MM 22-11-34, 22-11-00, & SMM:34-36-SDR ASAA2014051307795Satcom · malfunctionedSATCOM PROMPT MISSING AFTER POWER TRANSFER. ACFT GROUNDED. QRH PROCEDURE ACCOMPLISHED SATCOM OK.SDR ASAA2014041807512Igniter · failedAPU WILL NOT START AS REPORTED BY FLT CREW. ACFT GROUNDED. REPLACED APU IGNITOR PLUG & IGNITION UNIT IAW AMM 49-41-51-000-801, 49-41-51-400-801, 49-41-31-000-801 & 49-41-31-400-801. APU START NORMAL.SDR ASAA2014041707513Panel · looseNR 2 ENGINE FAN DUCT PANELS AT 12:30 AND 2:00 POSITIONS HAVE SEVERAL LOOSE BOLTS EACH. ACFT GROUNDED. TIGHTENED FASTENERS AS REQUIRED, REF: AMM 72-23-07.SDR ASAA2014032607324Warning Light · false activationRT SIDE WINDOW HEAT OVERTHEAT LIGHT ILLUMINATED ON GROUND. ACFT GROUNDED. FOUND SIDE WINDOW CONTROL BREAKER OPEN GVI WINDOW CIRCUIT BREAKER AND ACCESSIBLE WIRING. NO DEFECTS NOTED RESET CIRCUIT BREAKER WINDOW HEAT OPS CHECKED OK. IAW AMM 20-60-01-860-801 AND SDR ASAA2014020606798Warning Message · false activationFMC DISAGREE DURING TAXI. ACFT GROUNDED. FOLLOWED QRH FOR REBOOT & RELOAD. OPS NORMAL RESTORED.SDR ASAA2014012712505Warning Message · false activationFMC DISAGREE MESSAGE DISPLAYED. ACFT GROUNDED. PERFORMED QRH PROCEDURE, OPS NORMAL.SDR ASAA2014012712504Radar · failedWEATHER RADAR FAIL DURING CLIMB, WORKING CORRECTLY AFTER FIVE MINUTES AFTER FAIL. ACFT GROUNDED. WEATHER RADAR SYS OPS TEST PERFORMED IAW MM 34-43-00-710-802-001. OPS CHECKED GOOD. GROUND VERIFICATION TEST OK, NO HISTORY 30 DAYS.SDR ASAA2013112696548Warning Light · illuminatedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL AND WILL NOT RESET WITH TRIP RESET. AIRCRAFT GROUNDED. CONFIRMED CONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL. PERFORMED PACK/ZONE CONTROL BITE TEST IAW AMM 21-61-00. FOUND NR 2 PACK/ZONE TEMP CONTROSDR ASAA2013111396408Actuator · warning messageUPON LANDING CHECKLIST RECALL, THE LT PACK LIGHT ILLUMINATED. EXTINGUISHED ON MASTER CAUTION RESET. ACFT GROUNDED. BITE CHECK OF LT ZONE TEMP CONTROLLER LOGGED RAM AIR ACTUATOR FAULT. REPLACED LT RAM AIR INLET ACTUATOR. INSTALLATION TEST PASSES. ZONE TEMPSDR ASAA2013111296390Warning Message · false activationLEFT PACK ILLUMINATED ON RECALL, RESET WITH MASTER CAUTION. ACFT GROUNDED. PERFORMED PACK ZONE TEMP CONT BITE TEST REF MM 21-61-00-700-806-002. BITE TEST PASSED AND NO LT PACK LIGHT ON RECALL. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2013110896343Transceiver · failedUNABLE TO TRANSMIT ON SATCOM FROM CAPTAIN & F/O SIDES OR ON SATCOM 1 OR 2. ACFT GROUNDED. DISCOVERED THAT ACFT SATCOM PHONE NR WAS INOPERATIVE. REPLACED NR 1 IRIDIUM TRANSCEIVER (SATCOM) IAW AMM 23-15-00. OPS CHECKS GOOD.SDR ASAA2013110796340Power Unit · failedAFTER APU START 0 FREQUENCY AND 0 VOLTS DISPLAYED UNTIL SELECTING ON THE APU GENERATOR. ACFT GROUNDED. REPLACED THE P5-13 ELECTRIC METER AND GALLEY POWER PANEL, OPS CHECKED GOOD, REF AMM 24-21-53-400-801.SDR ASAA2013110596307Insulator · crackedNR 2 ENGINE LOWER EXCITER INSULATOR CRACKED. ACFT GROUNDED. REPLACED NR 2 ENGINE LOWER EXCITER BOX IAW AMM 74-11-01. ACCOMPLISHED IGNITION SYS AUDIBLE TEST IAW AMM 74-00-00-750-801-F00, TESTED GOOD.SDR ASAA2013103196266Seat Track · gougedSEAT TRACKS IN MAIN CABIN AT BS 520 RBL 45.50 GOUGED. ACFT GROUNDED. REPAIRED SEAT TRACK IAW SRM 53-00-52-2R-4, REPAIR 4.SDR ASAA2013103196265Seat Track · gougedSEAT TRACKS IN MAIN CABIN AT BS 520, RBL 24.75 GOUGED. GROUNDED. REPAIRED SEAT TRACK IAW SRM 53-00-52-2R-4, REPAIR 4.SDR ASAA2013103196264Seat Track · gougedSEAT TRACKS IN THE MAIN CABIN AT BS 520 LBL 24.75 GOUGED. ACFT GROUNDED. REPAIRED SEAT TRACK IAW SRM 53-00-52-2R-4, REPAIR 4.SDR ASAA2013103196263Seat Track · gougedSEAT TRACKS IN MAIN CABIN AT BS 520, LBL 45.50 GOUGED. ACFT GROUNDED. REPAIRED SEAT TRACK REF SRM 53-00-52-2R-4, REPAIR 4.SDR ASAA2013102496251Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED FS 312, RBL 35. ACFT GROUNDED. R & R MAIN CABIN FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5410, REV A.SDR ASAA2013092396041Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL NOT STAY ENGAGED. ACFT GROUNDED. ACCOMPLISHED AUTOTHROTTLE OPS TEST IAW MM 22-31-00, TEST PASSED. NO HISTORY 90 DAYS. FAULT REVIEW SHOWED 1 LEG WITH FAULTS, 22-31687 & 22-31675. ACCOMPLISHED AUTOTHROTTLE BITE TORQUE TEST, TEST PASSED.SDR ASAA2013090595935Warning Message · false activationFMC DISAGREE IN SCRATCHPAD ON TAXI. ACFT GROUNDED. PERFORMED QRH CHECKLIST MESSAGE NO LONGER DISPLAYED.SDR ASAA2013082795893Satcom · malfunctionedSAT DOES NOT APPEAR IN FMC. ACFT GROUNDED. DUPLICATED ACCOMP FIM23-15/801, SAT COM EXITED LOCKED-UP STATE. GROUND VERIFICATION CHECKED NORMAL.SDR ASAA2013082195863Display · failedDURING CRUISE, CAPTAIN`S MCDU WENT BLANK. ACFT GROUNDED. REPLACED C, OPS NORMAL IAW MM 34-61-01-400-802.SDR ASAA2013081595808Retainer · brokenASLE OVERWING EXIT SIGN MOUNT ACCESS COVER RETAINER ON FWD SIDE IS BROKEN. ACFT GROUNDED.SDR ASAA2013072995699Transceiver · failedNR 2 HF RADIO FREQUENCY WILL NOT SET AND WILL NOT TRANSMIT OR RECEIVE. ACFT GROUNDED. NR 2 HF TRANSCEIVER WILL NOT BITE TEST, NO LEDS COME ON, NR 1 HF BITE OK. REMOVED & REPLACED NR 2 HF TRANSCEIVER IAW AMM 23-11-21. BITE TEST & TUNE, TRANSMIT & RECEIVE WISDR ASAA2013072195654Filter Element · inoperativeRIGHT FUEL FILTER BYPASS LIGHT ILLUMINATED ON DEPARTURE. LIGHT WENT OUT AFTER WE LEVELED OFF AT 10000 FEET. ACFT GROUNDED. COMPLIED WITH ALL MX PROCEDURES. FUEL FILTER REPLACED. REVIEWED NR 2 ENGINE FAULTS. NO FAULTS FOUND. SPOKE TO INBOUND CREW. LIGHT SDR ASAA2013071195562A/C Pack · unknownLEFT PACK TRIP, ACFT GROUNDED. PERFORMED BITE ON LT & RT ZONE TEMP CONTROLLERS IAW FIM TASK 21-62, TASK 825, OPS CHECKED GOOD, LT PACK TRIP LIGHT RESET.SDR ASAA2013061195084Warning Message · illuminatedNR 1 ENGINE FOUND MAINTENANCE MESSAGE 73-31351. LONG TIME FAULT. THE APL INPUT VOLTAGE TO THE EEC IS OUT OF RANGE. ACFT GROUNDED. OPENSDR ASAA2013061195079Warning Message · illuminatedFOUND MAINT MESSAGE 74-30971. LONG TIME FAULT. THE APL INPUT VOLTAGE FOR THE LT EXCITER ( IGN 1) IS OUT OF RANGE ON NR 1 ENGINE. ACFT GROUNDED. ACCOMPLISHED FIM TASK 74-21, TASK 801. NO FAULTS FOUND. NO FAULTS LOGGED.SDR ASAA2013060594998Warning Light · false activationAUTO FAIL LIGHT ON, WENT TO ALT ON PRESSURE CONTROLLER. ACFT GROUNDED. RESET PRESSURE CONTROLLER. LIGHTS EXTINGUISHED, ACCOMPLISHED GROUND VERIFICATION OF PRESSURE CONTROL SYS BY ACCOMPLISHING BITE TEST OF NR 1 & NR 2 PRESSURE CONTROLLERS - SYS OPS NORMAL, SDR ASAA2013042894641Transceiver · failedWEATHER RADAR FAILED. ACFT GROUNDED. PERFORMED WEATHER RADAR OPS TEST REF MM 34-43-00-710-802-001, SYS WOULD NOT GO INTO TEST MODE AND WXR RANGE DISAGREE AND WEATHER RADAR ATT WAS DISPLAYED ON BOTH NAV DISPLAYS. R & R WEATHER RADAR TRANSCEIVER REF MM 34-43-SDR ASAA2013042294613Precooler · splitON CLIMBOUT, NOTED A DUCT PRESSURE DIFFERENTIAL THAT EXCEEDED 20PSI. THE RT SIDE WAS APPROX 23PSI AND THE LT SIDE WAS APPROX 46PSI. AT FL340 THE PRESSURE DIFF WAS 20 PSI AND ON CLIMB FROM 340 TO 360 THE DIFF EXCEEDED 20 PSI AGAIN. IN CRUISE AT FL360 THE DIFF
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