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.

SDR ASAA1159340Sensor · failedWHEN R FWD WINDOW HEAT SWITCH IS SELECTED ON OVERHEAT ILLUMINATES. REMOVED AND REPLACED WHCU DUE TO LRU FAIL LIGHT ILLUMINATED AND TESTED FOR FAILED SENSOR. TRANSFERRED TO SPARE SENSOR AND OPS CHECK GOOD REF AMM 30 41 11. SYSTEM GROUND VERIFIED GOOD.Mar 26, 2011 · N581AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA1159193Unknown · malfunctionedAT CRUISE: RIGHT SIDE WINDOW OVERHEAT LT CAME ON TURNED OFF FOR 5 MIN THEN TURNED BACK ON OPS NORMAL. PERFORMED BITE CHECK ON RIGHT SIDE WINDOW HEAT CONTROL UNIT NO FAULTS NOTED REF FIM 30 41 00 810 AND WINDOW HEAT OPS NORMAL. OK FOR SVC.Mar 8, 2011 · N581AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA1159031Valve · malfunctionedDURING CRUISE CLIMB APPROACHING FL360 NR 2 ENGINE "BLEED TRIP OFF" ILLUMINATED. IAW THE QRH PROCEDURE SUCCESSFULLY RESET THE BLEED VALVE. LATER APPROACHING FL370 NR 2 ENG. "BLEED TRIP OFF" OCCURRED AGAIN. ATTEMPTED TWO MORE RESETS. THESE RESETS FAILED AFTFeb 13, 2011 · N581AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1159022Transceiver · faultyUNABLE TO TRANSMIT ON NR 1 HF RADIO. REPLACED NR 1 HF TRANSCEIVER PER 23 11 21 SYS OPS CHECKS NML PER SAME GROUND VERIFICATION PASS.Feb 11, 2011 · N581AS · Boeing 737890 · HF Communications SystemSDR ASAA1158969Unknown · malfunctionedFMC DISAGREE LIGHT ILLUMINATED ON GROUND. ACCOMPLISHED QRH PROCEDURE. LIGHT EXTINGUISHED. OPS NORMAL.Feb 5, 2011 · N581AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1158965Unknown · malfunctionedAFTER PUSHBACK IN SJC "FMC DISAGREE" MESSAGE ILLUMINATED. COMPLETED THE "FMC DISAGREE" CHECKLIST IN THE QRH. PROCEDURE SUCCESSFUL. "FMC DISAGREE" MESSAGE NO LONGER DISPLAYED.Feb 2, 2011 · N581AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1158861Fmc · warning lightFMC DISAGREE MESSAGE ON GROUND IN KSAN. RAN QRH CHECKLIST. CLEARED FMC DISAGREE MESSAGE. OPS NORMAL.Jan 22, 2011 · N581AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1058666Unknown · malfunctionedPERFORMED TASK CARD 78273000 "INTERROGATE THE FMC CDU FOR ENGINE FAULTS" NR 1 ENGINE HAD CODE 73 31711 / NR 2 ENGINE HAD CODE 73 31712 BOTH ARE "ADIRU 1 TAT DATA AND ADIRU 2 TAT DATA DISAGREE" SHORT TERM FAULT. PERFORMED FIM 73 28 TASK 808 EEC TEST PASSES FORDec 20, 2010 · N581AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA1058533Apu · oil consumptionAPU HAS A HISTORY OF OIL SERVICING CURRENT APU OIL CONSUMPTION .06 QPH GROUNDED YES. REPLACED APU IAW AMM 49 11 00 400 803 OPS CHECK AND LEAK CHECK OK.Nov 21, 2010 · N581AS · Boeing 737890 · APU Core EngineSDR ASAA1058527Valve · failedCONT CAB TEMP CONTROLLER RUNS FULL HOT UNTIL YOU TURN OFF THE LEFT PACK AND LET IT COOL DOWN. TURN PACK BACK ON IT WORKS FINE UNTIL THE NEXT START. INSPECTED CONTROL CABIN AND FWD AND AFT PASSENGER CABIN TEMP SENSOR FILTERS AND FOUND ALL THREE DIRTY AND REPLNov 20, 2010 · N581AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1058507Exciter · failedDURING APU REPLACEMENT FOUND IGNITION EXCITER INOP. REPLACED APU EXCITER REF MM 49 41 31, OPS CHECKS GOOD.Nov 14, 2010 · N581AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA1058496Apu · leakingAPU MAINT LIGHT ILLUMINATED AFTER PUSHBACK. PERFORMED FIM TASK 49 95 00 810 801, NO OIL LEAKS FOUND IN DRAINS OIL COOLER OR IN APU COMPT FOUND EVIDENCE OF OIL LEAKING IN EXHAUST PIPE. REMOVED AND REPLACED APU REF T/C 78349010.Nov 11, 2010 · N581AS · Boeing 737890 · APU Core EngineSDR ASAA1058493Fmc · malfunctionedFMC DISAGREE DISPLAYED ON SCRATCH PADS ON GRD HAD PREVIOUS PWR INTERRUPTION AT GATE. PERFORMED QRH CHECK LIST. RE-STORED BOTH FMC'S. NO OTHER ANOMALIES NOTED.Nov 9, 2010 · N581AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1058457Controller · malfunctionedAFTER TAKEOFF LEFT PACK TEMP 80C CONT CAB SUPPLY TEMP 78C UNABLE TO CONTROL CONT CAB TEMP ATTEMPTED TRIM AIR OFF MANUAL CONTROL AND AUTO CONTROL. AFTER 5 MIN SYSTEM RETURNED TO NORMAL OPERATION. FWD AFT TEMP CONTROL OPS NORMAL. UNABLE TO DUPLICATE FAILURE LOct 30, 2010 · N581AS · Boeing 737890 · Cabin Temperature ControllerSDR ASAA1058409Display · damagedCAPT'S FMS/CDU CLEAR KEY DAMAGED AND DIFFICUT TO USE. DUPLICATED DEFECT REPLACED LT CAPT FMC CDU REF MM 34 61 01. OPS CHECK NORMAL.Oct 18, 2010 · N581AS · Boeing 737890 · Central DisplaySDR ASAA1058399Apu · leakingON DESCENT WITH POWER BACK THERE WAS A VERY BAD SMELL LIKE DIRTY SOCKS IN THE CABIN & FLIGHT DECK. FOUND OIL IN LOAD COMPRESSOR DRAIN CAVITY. REPLACED APU REF T/C'S 78349010 78349000 78349001 78349008 78349015 & 78349016 AND MM 49 11 00.Oct 17, 2010 · N581AS · Boeing 737890 · APU Core EngineSDR ASAA1058380Unknown · malfunctionedON DEPARTURE A "ZONE TEMP" (CONTROL CABIN) LIGHT CAME ON. FOLLOWED QRH LIGHT WENT OFF. TEMP IN FLIGHT DECK WAS HOTTER THAN NORMAL ON TAXI OUT BUT COOLED AFTER LIGHT EXTINGUISHED. ACCOMPLISHED BITE TEST OF THE ZONE/TEMP. CONTROLLERS REF FIM TASK 21 62 TASK Oct 17, 2010 · N581AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1058338Indicator · damagedWHILE ACCOMPLISHING T/C 78349013 FOUND APU OIL FILTER DPI EXTENDED AND DAMAGED. REMOVED AND REPLACED OIL DPI AND FILTER REF MM 49 91 13. OLD FILTER SHOWED NO INDICATION OF CONTAMINATION OR CLOGGING. RAN APU LEAK CHECKS GOOD. APU OK FOR SERVICE.Oct 8, 2010 · N581AS · Boeing 737890 · APU Oil SystemSDR ASAA1058258Hf Comm · malfunctionedHF RADIO NR 1 WILL NOT TRANSMIT. UNABLE TO VERIFY DISCREPANCY. TRANSMIT WAS LOUD AND CLEAR PER SFO FREQ 6.640. TRANSMIT AND RECEIVE ACCOMPLISHED MULTIPLE TIMES GOOD. OPS TEST GOOD REF HF COMM TEST MM 23 11 00 730 801. WAITING FOR VERIFICATION FLIGHT.Sep 6, 2010 · N581AS · Boeing 737890 · HF Communications SystemSDR ASAA1058248Transceiver · malfunctionedHF NR 1 INOP. ACCOMPLISHED FIM 23 11 TASK 806 VERIFIED HF 1 INOP RESET CB ON P18 2 HF 1 OPS RESTORED TO NORMAL AS PRECAUTION. REMOVED AND REPLACED NR 1 TRANSCEIVER PER AMM 23 11 21. BITE AND VOICE COMMUNICATION, OPS NORMAL.Sep 2, 2010 · N581AS · Boeing 737890 · HF Communications SystemSDR ASAA1058232Regulator · defectiveCONTINUING HISTORY OF RIGHT ENGINE BLEED TRIP WITH NO ASSOCIATED SIGN OF DUCT SPLIT. UNABLE TO REPRODUCE BLEED TRIP INDICATION OR FOUND ANY DEFECTS ON HARNESS MW0311. REPLACED NR 2 ENG BLEED AIR REGULATOR IAW AMM 36 11 03 PAGE BLOCK 401. REPLACED NR 2 ENG MAug 27, 2010 · N581AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1058214Sensor · faultyA FEW MINUTES PRIOR TO TOP OF DESCENT GOT A RIGHT SIDE BLEED TRIP LIGHT. RESET PER QRH AND THE LIGHT WENT OUT FOR A FEW MINUTES THEN CAME BACK ON AGAIN. TURNED OFF RIGHT PACK PER QRH. PERFORMED SYSTEM HEALTH CHECK REF MM 36 11 00 07 801 NO DISCREPANCIES FOUAug 20, 2010 · N581AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1058073Control Valve · faultyLEFT PACK LIGHT ILLUMINATED ON RECALL. INITIATED BITE TEST, DETERMINED NR 1 TCV FAULTY. REPLACED NR 1 TCV REF AMM 21 51 10, BITE TEST OK, LEAK CHECK OK.Jul 13, 2010 · N581AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1058051Regulator · failedON DESCENT FROM FL410 BLEED TRIP OFF RIGHT SIDE (NR 2). RESET WITH TRIP RESET BUTTON AND DUCT PRESSURE INCREASE AND PRESSURIZATION CABIN CLIMB. PERFORMED FIM TASK 36 10 00 810 801 AND PNEUMATIC SYSTEM TROUBLESHOOTING TASK 36 10 00 810. PERFORMED HIGH STAGE Jul 11, 2010 · N581AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1057862Packing · leakingWHILE T/S FAULT CODE 73-30351 RAN NR 1 ENGINE FOR 5 MIN. AFTER RUN NOTED PUDDLE OF FUEL UNDER ENGINE. GROUNDED YES. PERFORMED IDLE RUN FOUND LEAK FROM NR 1 ENG FUEL FILTER COVER (30236) REFERENCE MM 71 71 00. REMOVED AND REPLACED NR 1 ENGINE FUEL FILTER COVER May 23, 2010 · N581AS · Boeing 737890 · Engine Fuel DistributionSDR ASAA1057854Hmu · faultyWHILE ACCOMPLISHING T/C 78273000 FOUND SHORT TERM FAULTS ON NR 1 ENG MAINT MSG 73 20351 73 10351 FMV POSITION SIGNAL DISAGREE. REPLACED NR 1 ENGINE HMU REF AMM 73 21 10 000 801 F00. ACCOMP TEST 3A IDLE LEAK CHECK, NO LEAKS NOTED. ACCOMP TEST 13 ENGINE RUN WMay 21, 2010 · N581AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA1057848Valve · failedRT BLEED TRIP LIGHT ILLUMINATED AT FL 400 AS THROTTLES RETARDED FOR DESCENT. CHECKLIST ACCOMPLISHED. LIGHT RESET. HIGH STAGE VLV FOUND DEFECTIVE REF FIM 36 10 00 810 801, REPLACED REF MM 36 11 06. NR 2 ENG BLEED AIR REG FAILED SYS HEALTH CHECK. REPLACED BMay 20, 2010 · N581AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1057782Support Angle · crackedLT WING TRAILING EDGE BULKHEAD AT RSS 289 SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED CRACKED ANGLE.May 9, 2010 · N581AS · Boeing 737890 · Wing Miscellaneous StructureSDR ASAA1057604Valve · defectiveNR 2 IDG HAS RECENT HISTORY OF FREQUENT SERVICING. ACCOMPLISHED STATIC LEAK CHECK REF AMM 24 11 00 700 801. NO LEAKS NOTED. BAGGED IDG DRAIN AND RAN ENGINE AT IDLE FOR 10 MINUTES. NO LEAKS NOTED. REPLACED IDG VENT VALVE. REPLACED IDG SERVICE PORT. BOTH Mar 24, 2010 · N581AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1057502Gcu · faultedNR 1 GENERATOR CONTROL UNIT SHOWS "GCU FAIL" FAULT LIGHT AND WILL NOT RESPOND TO BITE. REMOVED AND REPLACED GCU 1. ETOPS ROTABLE COMPONENT VERIFICATION. C/B P6 4 F10 CLOSED. PERFORMED GCU INSTALLATION TEST AND OPERATIONAL TEST OF AC GENERATION AND CONTROL Mar 8, 2010 · N581AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1057372Actuator · failedLEFT SPAR VALVE CLOSED LIGHT ILLUMINATED. SPAR LIGHT REMAINED ON UNTIL CYCLED ON THE GROUND WORKED NORMALLY ON THE GROUND. REPLACED SPAR VALVE ACTUATOR NR 1 ENG REF AMM 28 22 11 400 804. NR 1 ENG FUEL SPAR VALVE ELECTRICAL CONTROL AND INDICATOR TEST GOOD REFeb 13, 2010 · N581AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA1057314Valve · faultedAFT ZONE TEMP ANNUNC ILLUMINATED. EXTINGUISHES WHEN MASTER CAUTION IS RESET. CONFIRMED ZONE TRIM VALVE FAULT ON NR 1 PACK ZONE TEMP CTL REF MM 21-61-00. REPLACED NR 1 ACAU REF MM 21-51-02. OPS NORMAL REF SAME. RE-ACCOMPLISHED PACK/ZONE TEMP CTL BITE TEST Feb 1, 2010 · N581AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1057290Valve · stuckAFT ZONE TEMP ILLUMINATED ON RECALL EXTINGUISHES ON MASTER CAUTION RESET. AFT ZONE MODULATING VALVE STUCK OPEN DUE TO ZONE TEMP CONTROL VALVE FAULTY. VALVE ASSY ZONE TEMP CONT IPC 21 62 01 03 ITEM 10. 3214972 1. REMOVED & REPLACED TRIM AIR PRESSURE REGULATIJan 28, 2010 · N581AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0751826Light · odorELECTRICAL TYPE SMELL IN CABIN DURING FLIGHT. F/A'S REPORT MOST NOTICEABLE AT ROWS 9, 11 AND NEAR AFT GALLEY VENT. SLIGHTLY NOTICEABLE IN COCKPIT. TURNED OFF CABIN LIGHTING AND SMELL DISSIPATED. CHECKED AFT GALLEY OVENS COFFEEMAKERS HOT PLATES FOR DEBRIS NJun 28, 2007 · N581AS · Boeing 737800* · Passenger Compartment Lighting
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