N583AS
Service difficulty reports · 465
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 = 'N583AS' 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 = 'N583AS' 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 ASAA201808135737Filter · dirtyFWD AND AFT CABIN TEMP HYPER-SENSITIVE TO INPUTS IN AUTO MODE. ACFT GROUNDED. FOUND THE CABIN TEMP SENSOR FILTERS DIRTY. REMOVED AND REPLACED THE CABIN TEMP SENSOR FILTERS IAW AMM 21-61-06. PERFORMED CABIN TEMP CONTROL AND IND OPERATIONAL TEST. OPS CHECKED SDR ASAA20180815738Transceiver · failedCANNOT TRANSMIT OR RECEIVE ON THE NR 1 OR 2 HF COMMS, WILL GET SIDE TONE ON INITIAL HF FREQ CHANGE. ACFT GROUNDED. VERIFIED CONNECTORS D8517 AND D345B AT E8-1 SHELF SECURE. PERFORMED HF 1 TRANSCEIVER BITE IAW FIM 23-11, TASK 801. BITE FAILED WITH KEYLOGGERSDR ASAA2018081085731Autopilot Sys · malfunctionedON RNAV AT APPROXIMATELY 1500 MSL, VNAV PATH AND HUD GUIDANCE DEVIATE QUICKLY TO SHOW APPROXIMATELY 500' LOW ON PATH. AT THIS POINT THE AUTOPILOT FOLLOWS THIS GUIDANCE, PITCHES UP. AIRPORT WAS IN SIGHT, AUTOPILOT WAS DISCONNECTED AND GUIDANCE WAS IGNORED WITH SDR ASAA2018081375711Hf Comm · malfunctionedNR 1 HF DOES NOT TRANSMIT FROM EITHER PANEL. NO SIDE TONE, NO FREQUENCY CHANGE TONE. ACFT GROUNDED. AIR TURNBACK. RESET THE SYSTEM, NR 1 HF CHECKED GOOD IAW AMM 23-11-00-710-801.SDR ASAA2018073025572Computer · failedAUTOPILOT DISCONNECTED WOULD NOT RECONNECT. GROUNDED - YES. REPLACED FCC-A PER AMM 22-11-33/401. LRU TEST GOOD PER SUBTASK 22-11-33-74-001. NO FAULTS NOTED. LAND VERIFY TESTS ALL PASS PER AMM 22-11-00/20. CHECKED SPOILER POS SENSORS PER AMM 22-11-27/401. ALL WSDR ASAA2018073025550Computer · failedAUTO THROTTLE DISENGAGED AND WOULD NOT RENGAGE ON T/O. GROUNDED - YES. A/P DISCONNECT, THE FCC-A WAS REPLACED. ACCOMPLISHED A/T SYS TEST PER AMM TASK 22-31-00-710-802. NO FAULTS NOTED.SDR ASAA2018072425511Unknown · malfunctionedHF NR 2 WILL NOT CHANNELIZE. GROUNDED - YES. ACCOMPLISHED HF COMM SYS BITE, NO BITE. CYCLED HF1 AND HF2 C/B'S. HF TRANSCEIVERS BITE TEST GOOD. HF1 AND HF2 COMM OPS NORMAL. PILOTS ACCOMPLISHED GROUND VERIFICATION REF FIM 23-11 TASK 801.SDR ASAA2018071625372Autothrottle Sys · disengagedAUTOTHROTTLES DISENGAGED, WILL NOT RE- ENGAGE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2018070425276Iru · out of alignmentWXR FAIL. GROUNDED - YES. REALIGNED IRU'S, PERFORMED WEATHER RADAR SYS BITE TEST PER FIM 34-43 TASK 801. NO FAULTS FOUND. WXR FAIL LIGHT GONE. OK FOR SERVICE.SDR ASAA2018061845072Transceiver · malfunctionedNR 1 HF RADIO WILL NOT TRANSMIT, WILL RECEIVE. ACFT GROUNDED. CHECKED THE NR 1 HF RADIO, OPS CHECKED GOOD IAW AMM 23-11-00-730-801, NO DEFECTS NOTED. NO HISTORY IN THE LAST 30 DAYS.SDR ASAA2018061105000Transceiver · failedDURING CLIMBOUT, WEATHER RADAR MESSAGES DISPLAYED. PWS FAIL, WXR RANGE DISAGREE, AND WXR FAIL. ACFT GROUNDED. REMOVED AND REPLACED THE WEATHER RADAR RECEIVER/TRANSMITTER IAW AMM 34-43-41. OPS TESTED IAW AMM 34-43-00-710-802-001, ALL TESTS GOOD.SDR ASAA2018052754825Display · inoperativeCAPTAIN`S MCDU INOPERATIVE. DOES NOT RESPOND TO KEY INPUTS. ACFT GROUNDED. ACCOMPLISHED FIM 34-61 TASK 804. CAPTAIN'S CDU OPS TESTED NORMAL. NO INFLIGHT FAULTS LOGGED.SDR ASAA201805214708Elastomer · damagedIAW T/C 78472002, NR 2 ENG STEP 32, PLATFORM LOCATION 2, 8, 12, 13, 14, & 17 HAD MISSING, TORN OR UNBONDED ELASTOMERS. ACFT GROUNDED. REMOVED & REPLACED THE PLATFORMS IAW AMM 72-21-00 AND T/C 78472002.SDR ASAA201805214707Tie Rod · crackedNR 2 ENGINE FORWARD TIE ROD ON LOWER PNEUMATIC STARTER DUCT IS CRACKED THROUGH. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE FORWARD TIE ROD IAW 71-00-02 FIG 25-1.SDR ASAA201805214706Blades · damagedIAW T/C 78472002, NR 2 ENGINE STEP 29 BLADES NR 1, 8, 13, 14, 15, 17, 18, 19, AND 20, HAVE MISSING CU-NI-IN COATING BEYOND LIMITS ON THE CONVEX SIDE. BLADES 6, 15, & 16 HAVE MISSING CU-NI-IN COATING BEYOND LIMITS ON THE CONCAVE SIDE. NR 2 BLADE CU-NI-IN COATINSDR ASAA2018040224115Pad · debondedNR 1 ENGINE FOUND VBV DOOR PAD SEAL DISBONDED ALF AT AROUND 8 O'CLOCK POSITION. ACFT GROUNDED.SDR ASAA2018040224114Wire Harness · looseNR 1 ENGINE OTBD WIRE HARNESS FOR STATOR GENERATOR LOOSE. ACFT GROUNDED. ENGINE WIRE HARNESS J7. R & R THE NR 1 J7 WIRE HARNESS IAW AMM 73-21-06. OPS TESTED GOOD.SDR ASAA2018032123994Controller · faultedLEFT PACK LIGHT ILLUMINATED ON RECALL. EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. ON PREVIOUS FLT, FOUND PACK ZONE RIGHT CONTROLLER FAULT, STANDBY. PERFORMED IAW FIM 21-62 / 803. PASSED SUSPECT M1443 RT TEMP ZONE CONTROLLER. REMOVED NR 2 RT PSDR ASAA2018032023977Warning System · false activationLEFT PACK ILLUMINATED ON DESCENT WHEN RECALL WAS PRESSED. LIGHT CLEARED WHEN MASTER CAUTION PRESSED. GROUNDED - YES. PERFORMED PACK TEMPERATURE CONTROL-BITE PROCEDURE REF FIM 21-62 TASK 801. RESET AFTER VERIFIED. CHECKED GOOD ON SIX PACK. NO FAULT NOTED. OPS NSDR ASAA2018031523927Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON RECALL, RESET WHEN MASTER CAUTION PUSHED. ACFT GROUNDED. RESET SYSTEM AND RAN PACKS FOR FIVE MINUTES. TESTED SYSTEM IAW AMM 21-61-00, NO FAULTS.SDR ASAA2018031423882Controller · failedRIGHT PACK, ZONE TEMP CONTROLLER M1443, ZONE LIGHT DOES NOT ILLUMINATE WITH LAMP TEST PRESSED. ACFT GROUNDED. REMOVED AND REPLACED THE RIGHT PACK, ZONE TEMP CONTROLLER, INSTALLATION TEST, PASSED, IAW AMM 21-61-20.SDR ASAA2018031323881Warning Light · false activationCONTROL CABIN ZONE TEMP LIGHT ON TAXI OUT. LIGHT EXTINGUISHED WITH RESET. ACFT GROUNDED. ACCOMPLISHED THE LT AND RT PZTC BITE WITH NO FAULTS NOTED IAW AMM 21-61-00. ACCOMPLISHED AN EVALUATION IAW FIM 21-62 / 842, CONTROL CABIN ZONE TEMP LIGHT REMAINS EXTISDR ASAA2018030923804Transceiver · intermittentFAIL DISPLAY ON BOTH ACTIVE AND STBY WINDOWS OF THE NR 1 HF. ACFT GROUNDED. DISCREPANCY WAS INTERMITTENT. NR 2 HF WAS NORMAL. REPLACED THE NR 1 HF TRANSCEIVER. OPS NORMAL IAW AMM 23-11-21.SDR ASAA2018030623773Fmc · false indicationFMC SHUTDOWN AND RESTARTED DURING TAXI IN. ACFT GROUNDED. ACCOMPLISHED LEFT FMC SYSTEM OPS TESTED IAW AMM 34-61-00-710-801, TEST OK. ACCOMPLISHED RIGHT FMC SYSTEM OPS TESTED IAW AMM 34-61-00-710-801, TESTED OK.SDR ASAA2018022223665Unknown · unknownACARS/FMC WONT CLEAR FROM PREVIOUS FLIGHT. ACFT GROUNDED. TROUBLESHOT IAW FIM 34-61 TASK 837, ENSURED NR 1 & 2 FMC CIRCUIT BREAKERS WERE SET, THIS SUCCESSFULLY CLEARED PREVIOUS FLIGHT AND ALLOWED NEW FLIGHT PLAN ENTERED. CHECKED GOOD FOR SERVICE.SDR ASAA2018012123248Coupler · faultyAT CRUISE, UNABLE TO TRANSMIT ON HF. WHEN PUSH TO TALK SWITCH IN R/T POSITION, NO TRANSMISSION OCCURS WITH TRANSMITTER SELECTOR SWITCH ON HF. GROUNDED - YES. UNABLE TO DUPLICATE DEFECT. ACCOMPLISHED T/S PER B737-800 FIM 23-11 TASK 806 - INITIAL EVALUATION DID SDR ASAA2018012023231Coupler · faultyFOLLOW-UP TO RECENT HISTORY WITH NR 1 HF UNABLE TO TRANSMIT, TECHNICAL SERVICES REQUEST ADDITIONAL TROUBLESHOOTING. GROUNDED - YES. ENGINEERING REQUEST - ACCOMPLISHED STATIC DISCHARGER INSPECTION PER AMM 23-61-00-210-801 - NO DEFECTS NOTED. ACCOMPLISHED GVI OFSDR ASAA2018011523178Transceiver · malfunctionedINTERMITTENT NR 1 HF, FAILED PRIOR TO GATEWAY, FIXED WHILE STILL IN VHF CONTACT. REGAINED DUAL HF RADIO CAPABILITY PRIOR TO ENTERING OCEANIC AIRSPACE WITH NO FURTHER ISSUES. ACFT GROUNDED. OPS CHECKED THE NR 1 HF IAW AMM 23-11-00. OPS CHECKED NORMAL.SDR ASAA2018010923109Control Valve · faultedLEFT PACK LIGHT ILLUMINATED ON RECALL. EXTINGUISHED WHEN MASTER CAUTION RESET. OPS NORMAL. ACFT GROUNDED. REMOVED AND REPLACED THE LEFT PACK TEMP CONTROL VALVE. LEAK CHECKED GOOD. OPS CHECKED GOOD IAW AMM 21-51-10. PERFORMED A BITE CHECK, NO FAULTS NOTEDSDR ASAA2017120722812Attach Angle · crackedRIGHT WING REAR SPAR VERTICAL PRESSURE DECK WEB IS CRACKED AT DRAIN HOLE LOCATED AT APPROXIMATELY RBL35 AND MEASURES .300 IN LENGTH. GROUNDED - YES. REPAIRED ATTACH ANGLE SEE TASK CARD SB737-57-1330-NG-2 FOR ALL DOCUMENTATION.SDR ASAA2017111822773Transition Panel · crackedAFT PIT R/H TRANSITION PANEL IS CRACKED IN TWO PLACED STA 727J TO 747. GROUNDED - YES. REPAIRED TRANSITION PANEL IAW B737 800 SRM 53 00 53 2R 6 REPAIR 6.SDR ASAA2017111822759Cargo Track · crackedAFT PIT R/H CARGO TRACK IS CRACKED AT FRAME ATTACH POINT STA 727H. GROUNDED - YES. REPAIRED CARGO TRACK AT FRAME ATTACH POINT STATION 727H IAW B737 800 SRM 53 00 5 2R 3.SDR ASAA2017111722760Web · corrodedAFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB CORRODED IN NUMEROUS AREAS. GROUNDED - YES. REMOVED AND REPLACED AFT PIT LOWER SILL WEB IAW B737 800 SRM 51 40 02 0G 0 W 2 O .050 R .044 L 6 D .006.SDR ASAA2017111622892Skin · crackedL/H HORIZ STABILIZER LOWER SKIN CRACKED I/B OF RIB AT STAB STATION 147.90 MARKED WITH RED GREASE PENCIL. GROUNDED - YES. REPAIRED SKIN IAW B737 800 SRM 55-10-01-2R-11, THIS IS A CATEGORY B REPAIR ENTRY MADE IN FILEMAKER PRO FOR CAT B REQUIREMENTS 74711 RTOWELLSDR ASAA2017111522875Skin · dentedFOUND A DENT BELOW THE R1 DOOR BS 295, STRINGER 22R. ACFT GROUNDED. REPAIRED DAMAGE TO SKIN IAW B737 800 SRM 53 00 01 2R 1 THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 50,000 FLT. CYCLES, INTERVAL OF 3,440 FLT. CYCLES. REFER TO 737 800 APB SRM SDR ASAA2017110522461Fmc · malfunctionedFMC MESSAGE ILLUMINATED ON FINAL. GROUNDED. ACCOMPLISHED FIM 34-61 TASK 835. OPS CHECKED GOOD.SDR ASAA2017110422426Coupler · intermittentDURING OPERATIONAL TEST OF HF COUPLERS, THE NR 1 HF INTERMITTENTLY FAILED. ACFT GROUNDED. COULD NOT DUPLICATE FAILURE. CONTACTED ON 10.057, WAS RECEIVED 5 X 5 ON BOTH HF 1 & 2. TRANSCEIVER BITE SHOWED NO FAULTS.SDR ASAA2017103122370Transceiver · failedUNABLE TO TRANSMIT ON HF 1. HAD DIFFICULTIES INITIALLY CONTACTING SFO RADIO AND HF1 TUNER TOOK A LONG TIME TO TUNE. LONG AUDIO TONE. THE TRAMSMIT FUNCTION BECAME COMPLETELY INOPERABLE USING CAPT AND FO AUDIO PANELS. GROUNDED - YES. UNABLE TO VERIFY DEFECT ON SDR ASAA2017102222266Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON RECALL. LIGHT GOES OUT ON RESET. ACFT GROUNDED. PERFORMED A PACK TEMP BITE PROCEDURE IAW FIM 21-62, TASK 801. LEFT RAM ACTUATOR FAULT LIGHT ON. PERFORMED FIM 21-62, TASK 837, RAM ACTUATOR FAULT ISOLATION, NO FAULTS NOTED. SDR ASAA2017101822239Knob · unsecureFIRST OFFICER`S COURSE SELECTOR KNOB TURNS BUT DOES NOT CHANGE DIGITS, INTERMITTENT. ACFT GROUNDED. TIGHTENED THE COURSE SELECTOR KNOB. OPS CHECKED NORMAL AND KNOB REPONDS TO DIGITS DETENT NORMAL. PERFORMED BITE DFCS IAW AMM 22-11-00-700-740-806. NO HISTORY SDR ASAA2017092722067Transceiver · failedWHILE TRYING TO TUNE HF 1 TO NEW FREQUENCY, THERE WAS AN EXTENDED (APPROX 10-15 SECONDS) TONE AND WHEN IT STOPPED WERE UNABLE TO TRANSMIT ON HF 1. ATTEMPTED TO TRANSMIT ON VHF 1 OR 2 BUT WAS UNABLE. SELECTED ALTERNATE ON ACP NR 1 AND COULD COMMUNICATE ON VHFSDR ASAA2017091721943Warning Message · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL. RESET ON CAUTION RESET. ACFT GROUNDED. PERFORMED PACK/ZONE TEMP CONTROL BITE MULTIPLE TIMES, INITIAL FAULT SHOWN FLT DECK TRIM VALVE , TEMP CONTROLLER NR 2 . RESET FAULT, FAULT DID NOT RETURN. RAN RT PSDR ASAA2017091721938Warning Light · false activationAT THE GATE, AUTO FAIL AND ALTERNATE ILLUMINATED ON PRESSURIZATION PANEL. ACFT GROUNDED. PERFORMED FIM 21-31 TASK 801. NO FAULT NOTED.SDR ASAA2017090721892Connector · unsecureDIAGNOSTICS REPORTED A SPIKE IN EGT FOR THE NR 1 ENGINE. ACFT GROUNDED. ACCOMPLISHED TSR908608. PRIOR TO INSPECTION, ACCOMPLISHED T/C 78273000, NO CURRENT FAULTS OR FAULTS IN HISTORY. ON INITIAL GVI OF ENGINE HARNESSES, FOUND CJ10 CONNECTION LOOSE AND DIRTY. SDR ASAA2017082821740Fmc · malfunctionedDURING TAXI-IN, VTK WARNING ON THE FIRST OFFICER`S ND INTERMITTENTLY WITH SINGLE FMC OPERATION SCRATCH PAD. ALSO RECEIVED A RAAS WARNING WHILE ON TAXI WAY. ACFT GROUNDED. FLT 6 SHOWS LEFT & RIGHT FMC WITH OPPOSITE FMC FCC DATA SYNC ERR FAULT. KNOWN FMC WISDR ASAA2017081921666Display · malfunctionedON SHORT FINAL, 4 NM, FIRST OFFICER MCDU FAILED. MCDU APPEARED TO GO THROUGH A RESTART WENT TO FMC ON LEFT AND CONTINUED. ACFT GROUNDED. FIRST OFFICER`S MCDU TESTED IAW AMM 34-61-01 AND OPS CHECKED GOOD, NO HISTORY 30 DAYS.SDR ASAA2017081721676Ignition Sys · malfunctionedDURING THE NR 1 ENG START, NO EGT RISE ON LEFT IGNITION. ATTEMPTED TO SWITCH IGNITION TO RIGHT AND ENGINE STARTED NORMAL. ACFT GROUNDED. ACCOMPLISHED GROUND VERIFICATION IAW FIM 74-21 TASK 806. PERFORMED A BITE CHECK, NO FAULTS FOUND. PERFORMED IGNITION SYSDR ASAA2017081521638Hf Comm · malfunctionedACFT HF RADIO NR 1 INOPERATIVE. HF RADIO NR 2 STATIC BUILDS UP DURING TRANSMISSIONS AND CUTS OUT. ACFT GROUNDED. PERFORMED FIM 23-11, TASK 806, FOR BOTH NR 1 AND 2 HF RADIOS, NO FAULTS NOTED AT THIS TIME.SDR ASAA2017080721559Lens · brokenEMERGENCY LIGHT EXIT LOCATOR SIGN ADJACENT TO L2 DOOR HAS BROKEN LENS. ACFT GROUNDED. REMOVED AND REPLACED LENS AND TESTED LIGHT ASSEMBLY IAW AMM 33-51-01-960-801, OPS NORMAL.SDR ASAA2017080721558Lens · brokenEMERGENCY LIGHT EXIT LOCATOR SIGN ADJACENT TO R1 DOOR HAS BROKEN LENS. ACFT GROUNDED. REMOVED AND REPLACED THE LENS AND TESTED LIGHT ASSEMBLY IAW AMM 33-51-01-960-801 - OPS NORMAL.
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