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 ASAA2015113014047Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH, SATCOM RESTORED NORMAL.Nov 30, 2015 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2015112614015Bowl · missingIAW T/C N2479000, DURING INSPECTION FOUND GLASS INSPECTION BOWL MISSING AT LT ENGINE OIL FILTER POP OUT INDICATOR. ACFT GROUNDED. REPLACED GLASS INSPECTION BOWL IAW AMM 79-21-03.Nov 26, 2015 · N581AS · Boeing 737890 · Engine Oil Distribution (Airframe Furnished)SDR ASAA2015112413967Circuit Breaker · trippedF/O REPORTS CIRCUIT BREAKER OPEN ON SPCU, " BATTERY BUSS SWITCH POSITION INDICATOR" CIRCUIT BREAKER. ACFT GROUNDED. RESET CIRCUIT BREAKER. TESTED SPCU IAW AMM 24-34-11. GROUND TEST OK. NO FURTHER TRIPPING NOTED.Nov 24, 2015 · N581AS · Boeing 737890 · DC Generating SystemSDR ASAA2015112213925Heater · failedNR 1 ENGINE FUEL HEATER SERVO LEAKING. ACFT GROUNDED. REMOVED NR 1 ENGINE SERVO FUEL HEATER REF AMM 73-11-07-000-801-F00. INSTALLED AND TORQUED FUEL FILTER COVER DRAIN PLUG REF AMM 73-11-07-00-801 H. 1,H AND I. INSTALLED NR 1 ENGINE SERVO FUEL HEATER IAW ANov 22, 2015 · N581AS · Boeing 737890 · Engine Fuel DistributionSDR ASAA2015112013902Idg · leakingNR 1 IDG DIFFERENTIAL PRESSURE INDICATOR EXTENDED. ACFT GROUNDED. R & R NR 1 IDG UP TO STEP H OF AMM 24-11-11-400-801 OF THE INSTALLATION. NO LEAKS FOUND AT IDG. INSTALLATION TEST PASSED. TASK COMPLETED IAW MM 24-11-11-400-801.Nov 20, 2015 · N581AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2015102813545Satcom · lockedSATCOM LOCKUP ACFT GROUNDED. QRH PERFORMED OPS RESTORED.Oct 28, 2015 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2015100113298Satcom · malfunctionedNO SATCOM PROMPT, ACFT GROUNDED. SATCOM LOCKUP QRH PROCEDURE ACCOMPLISHED, SATCOM RESTORED.Oct 1, 2015 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2015090712963Satcom · lockedSATCOM LOCKUP DURING POWER TRANSFER. ACFT GROUNDED. RESOLVED IAW QRH PROCEDURE.Sep 7, 2015 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2015082612925Generator · false indicationWITH APU RUNNING, APU GEN DISPLAYS ZERO VOLTS & FREQUENCY. ACFT GROUNDED. RAN BITE ON APU GCU, GREEN PASS LIGHT IAW MM 24-21-81. APU GENERATOR OPS TEST NORMAL IAW MM 24-21-00, ALL INDICATIONS NORMAL. GROUND VERIFICATION SUCCESSFUL.Aug 26, 2015 · N581AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2015080512873Floorbeam · corrodedFWD CARGO BAY FLOORBEAM CORRODED BS 500I, LBL 24-RBL 24. ACFT GROUNDED. R & R THE FLOORBEAM IAW SRM 51-40-02.Aug 5, 2015 · N581AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2015080512872Channel · corrodedFWD CARGO BAY TRANSITION PANEL CORRODED BS 500G - 500I, RBL 24. ACFT GROUNDED. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS WAS .040, LOST .011, REMAINING MATERIAL THICKNESS IS .029, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED CORRODED TRANSIAug 5, 2015 · N581AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015080412908Skin · crackedCRACK FOUND INBD OF STABILIZER BS 138.70, RT SIDE APPROXIMATELY 23" FORWARD OF REAR SPAR, MARKED. ACFT GROUNDED. REMOVED DAMAGE AND ACCOMPLISHED DOUBLER REPAIR IAW SRM 55-10-012R-11, FIG 204. REPAIR 11 IS A CATEGORY B.Aug 4, 2015 · N581AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015080412899Skin · crackedCRACK FOUND INBD OF STABILIZER STA 129.50 LT SIDE APPROXIMATELY 8 INCHES FWD OF REAR SPAR. ACFT GROUNDED. REMOVED DAMAGE AND ACCOMPLISHED DOUBLER REPAIR IAW SRM 55-10-01-2R-11, REPAIR 11. THIS IS A CATEGORY B REPAIR, INSPECTION THRESHOLD IS DUE AT 56,000 CAug 4, 2015 · N581AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015062512240Warning Light · false activationENGINE VALVE CLOSED LIGHT ILLUMINATED, APPEARS TO BE BRIGHT BLUE. ACFT GROUNDED. ACCOMPLISHED NR 1 ENGINE START PROCESS, ENGINE VALVE CLOSED, LIGHT OPS CHECKED NORMAL, IAW MM 73-06, TASK 804, NO HISTORY LAST 30 DAYS.Jun 25, 2015 · N581AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2015052311833Button · wornF/O FMC BUTTONS TOO WORN TO READ. ACFT GROUNDED. REPLACED F/O FMC KEYBOARD IAW AMM 34-61-01. OPS CHECKED IAW AMM 34-61-01. OPS CHECKED GOOD.May 23, 2015 · N581AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015052011803Blade · vibrationENGINE NR 2 VIB VARIES BETWEEN .7 AND 2.7 IN DIFFERENT PHASES OF OPERATION. ACFT GROUNDED. ACCOMPLISHED FAN LUBE IAW T/C 78472002, ACCOMPLISHED. VIBRATION SURVEY IAW AMM 71-00-00. ALL PARAMETERS PASSED.May 20, 2015 · N581AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2015052011802Blade · wornNR 2 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES FAN LUBE REQUIRED. ACFT GROUNDED. PERFORMED NR 2 ENGINE FAN LUBE REF TASKCARD 78472002 AND ALSO TAST 7 VIB SURVEY REF AMM 71-00-00. OPS CHECK GOOD OMay 20, 2015 · N581AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2015051811769Lamp · failedWHILE ACCOMPLISHING TC 78233008, FOUND LT AFT OVERWING EXIT LIGHT INOPERATIVE. ACFT GROUNDED. RELAMPED LT AFT OVERWING EXIT LIGHT IAW AMM TASK 33-51-04-960-801. OPS NORMAL.May 18, 2015 · N581AS · Boeing 737890 · Emergency LightingSDR ASAA2015051611749Valve · failedFOLLOW-UP TO RECENT HISTORY OF DUCT PRESSURE SPLIT WITH RT PRESSURE LOW. ACFT GROUNDED. WHILE ACCOMPLISHING NR 2 ENGINE BLEED AIR SYS HEALTH CHECK, TASK CARD NG-36WC-00001, FOUND PRE-COOLER CONTROL VALVE FAILED STEP F AND HIGH STAGE VALVE FAILED IAW STEPS J AMay 16, 2015 · N581AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2015042311501Starter · inoperativeNO ROTATION ON #1 ENGINE AT ENGINE START. GROUNDED - YES. REPLACED ENGINE #1 STARTER ALL OPS AND LEAK CHECKS GOOD. VERIFIED NO CONTAMINATION OF MAG PLUG ON OLD STARTER REF AMM 80-11-01.Apr 23, 2015 · N581AS · Boeing 737890 · Engine StarterSDR ASAA2015042111451Satcom · lockedSATCOM LOCK UP. ACFT GROUNDED. FOLLOWED QRH PROCEDURE 5.3 AND SATCOM WAS RESTORED. SATCOM PROMT CKS NORMAL 23-15, TASK 801.Apr 21, 2015 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2015041911415Fmc · malfunctionedAT CRUISE WITH VNAV SELECTED THE F/O'S PFD AIRSPEED WOULD NOT INDICATE A MACH NR, TARGET MACH NUMBER, GREATER THAN .79 EVEN THOUGH THE FMC WAS COMMANDING AT A TARGET MACH OF .80. CAPT'S PFD AIRSPEED INDICATED CORRECTLY. F/O'S COMMANDED MACH AND MAGENTA SPEED CApr 19, 2015 · N581AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015040711261Satcom · lockedSATCOM LOCK UP: ACFT GROUNDED. QRH CHECKLIST PROCEDURES COMPLETED. OPS NORMAL.Apr 7, 2015 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2015040611255Satcom · lockedSATCOM LOCK-UP, ACFT GROUNDED. SATCOM LOCK-UP PROCEDURE PERFORMED SUCCESSFULLY.Apr 6, 2015 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2015032811158Wire Harness · faultedNR 1 ENGEIN, ECONOMIC FAULT 77-10841 "THE TOP RT EGT SIGNAL, T495S1, IS OUT OF RANGE" FOUND. LEG 0-6. ACFT GROUNDED. ACCOMPLISHED T/C NR 78273000 AND VERIFIED FAULT CODE 77-10841 STILL PRESENT ON ENGINE NR 1. CLEANED ALL CONNECTIONS FOR T49.5. CHECKED REAMar 28, 2015 · N581AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA2015032611105Probe · failedDIAGNOSTICS REPORTS NR 1 ENGINE EGT HDM AND EGT CONTINUES TO SHOW GREATER THAN EXPECTED DATA SCATTER RESULTING IN A TREND SHIFT. INDICATION ERRORS STILL SUSPECT. ACFT GROUNDED. ACCOMPLISHED TROUBLESHOOTING IAW FIM 77-21-TASK 801. INITIAL CHECK OF INPUTS ON Mar 26, 2015 · N581AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015032411099Satcom · lockedSATCOM LOCKUP DURING POWER TRANSFER. ACFT GROUNDED. RESOLVED IAW QRH, OPS NORMAL.Mar 24, 2015 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2015032111041Satcom · lockedSATCOM LOCK-UP, ACFT GROUNDED. QRH PERFORMED- NORMAL OPS CONTINUED.Mar 21, 2015 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2015031911047Probe · faultedWHILE ACCOMPLISHING T/C 7827300, FOUND NR 1 ENGINE FAULT 77-10841, THE TOP RT SIGNAL IS OUT OF RANGE FLIGHT LEGS 1, 2, 3, 4. ECONOMIC FAULT, ESN894613. ACFT GROUNDED. ACCOMPLISHED TROUBLESHOOTING IAW FIM 77-21-TASK 801. INITIAL CHECK OF INPUTS ON CDU SHOWSMar 19, 2015 · N581AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015031711002Probe · faultedREF T/C 78273000, FOUND ECONOMIC FAULT NR 2 ENGINE MSG NR: 77-10852. THE BOTTOM RT EGT SIGNAL IS OUT OF RANGE. ESN895616. ACFT GROUNDED. ACCOMPLISHED T/C 78273000 FOUND NO RECENT FAULTS AND NO FAULT HISTORY FOR ENGINE NR 2. READINGS ALL ARE WITHIN LIMITS. Mar 17, 2015 · N581AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015022810812Fuel Nozzle · faultedNR 2 ENGINE HAS HISTORY OF FAULT CODE 77-10842 AND 73-31372 BEING REPORTED. ACFT GROUNDED. REPLACED NR 2 ENGINE FUEL NOZZLES IAW PWR PL-73 CMPT-07267-2, NOZZLES 1-6 AND 16-20.Feb 28, 2015 · N581AS · Boeing 737890 · Fuel Injector NozzleSDR ASAA2015021410647Wire Harness · damagedFOUND FAULT NR 77-10842-THE TOP RT EGT SIGNAL, T495S1, IS OUT OF RANGE ON NR 2 ENG REF T/C 78273000. ACFT GROUNDED. PERFORMED BITE OF NR 2 ENGINE AND FAULT 77-10842 IS STILL ACTIVE. INSPECTION OF T49.5 CONNECTORS AT PROBES WERE FOUND TO BE VERY DIRTY. WHIFeb 14, 2015 · N581AS · Boeing 737890 · Turbine Engine System WiringSDR ASAA2015013110486Satcom · failedDIFFICULTY COMMUNICATING WITH DISPATCH VIA SATCOM. SATCOM FAILED, OR DROPPED THREE DIFFERENT CALLS WITH DISPATCH AND FAILED TO CONNECT FOR ONE ATTEMPTED INCOMING CALL FROM DISPATCH. ACFT GROUNDED. OPEN.Jan 31, 2015 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2015013110485Warning Light · illuminated"SAT NR 1" BLUE LIGHT ILLUMINATED & NO SATCOM PROMPTS FOUND ON MCDU PAGE. ACFT GROUNDED. SATCOM LOCKED UP. CYCLED POWER TO SATCOM IAW FIM TASK 23-15, TSK 801. NORMAL OPS RESTORED- PROMPT RETURNED & LIGHT OUT. ETOPS GROUND VERIFICATION ACCOMPLISHED.Jan 31, 2015 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2015012510419Fuel Nozzle · malfunctionedFOUND "ECONOMIC" FAULT-UPPER EGT SECTORS READING HIGH NR 73-31372, NR 2 ENGINE. FOUND ON T/C 78273000. ACFT GROUNDED. REPLACED NR 2 ENGINE FUEL NOZZLES IAW POWER PL-73 CMPT-07267-2, NOZZLES 1-6 AND 16-20.Jan 25, 2015 · N581AS · Boeing 737890 · Fuel Injector NozzleSDR ASAA2015011610276Actuator · malfunctionedRT RAM AIR LINLET AREA EMITTING A HUMMING SOUND. ACFT GROUNDED. REPLACED RT RAM AIR ACTUATOR IAW AMM 21-51-21.Jan 16, 2015 · N581AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014121409950Sensor · reads highNR 2 ENGINE HAD FAULT 73-31372, ECONOMIC FAULT, UPPER EGT SECTORS READING HIGH. 500 FLIGHT HOURS TO CORRECT. ACFT GROUNDED. PERFORMED T/C 78273000, THERE WERE NO FAULTS FOR NR 2 OR NR 1 ENGINE. FAULT NO LONGER ACTIVE.Dec 14, 2014 · N581AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2014121109940Insulation · wornJ9 & J10 WIRE HARNESSES WORN THROUGH, OUTER SHEATHING WEAR CONNECTORS DP 0905 AND DP 1005. REF T/C N8420000. ACFT GROUNDED. R & R J9 AND J10 HARNESS IAW MM 73-21-06-000-802-F00. COMPLETED EEC TEST IAW MM 73-21-00-700-804-F00, IDENT/CONF TEST IAW MM 73-21-00-Dec 11, 2014 · N581AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2014121109939Insulation · wornLEFT ENGINE MW0311 HARNESS WORN THROUGH OUTER SHEATHING AND INTO INNER METAL BRAIDING WEAR, CONNECTOR DP1103, REF TC N8420000. ACFT GROUNDED. REPLACED LT ENGINE MW0311 HARNESS. REF AMM 73-21-06/401. ALL OPS CHECKS NORMAL, REF MM 73-21-06-400-802-F00.Dec 11, 2014 · N581AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2014121109928Solenoid · failedDURING GROUND WING TAI SOLENOID VALUE TEST, FOUND VALVE INOPERATIVE. ACFT GROUNDED. REPLACED NR 1 ENGINE GROUND WING TAI SOLENOID VALVE. OPS CHECKED GOOD IAW MM TASK 30-11-12-000-801 AND 30-11-12-400-801.Dec 11, 2014 · N581AS · Boeing 737890 · Airfoil Anti/De-ice SystemSDR ASAA2014112209728Warning Message · false activationFOUND MAINTENANCE MESSAGE 73-31372, UPPER EGT SECTORS READING HIGH, FOR NR 2 ENGINE. ACFT GROUNDED. ACCOMPLISHED T/C 78273000. FAULT NO LONGER EXISTS.Nov 22, 2014 · N581AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2014111809699Connector · dirtyNR 2 ENGINE, WHILE PERFORMING TC 78273000 HAD ECONOMIC FAULTS: 73-31372. UPPER EGT SECTORS READING HIGH, 77-10842, ECONOMIC FAULT, THE TOP RT EGT SIGNAL IS OUT OF RANGE. ACFT GROUNDED. ACCOMPLISHED FIM TASK 73-11, TASK 801 AND TASK 77-21, TASK 801. INSPECTENov 18, 2014 · N581AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA2014111309666Satcom · lockedSATCOM LOCKUP ON GROUND, ACFT GROUNDED. ACCOMPLISHED QRH CHECKLIST. RESET SUCCESSFUL.Nov 13, 2014 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2014110509904Housing · gougedFWD CARGO DOOR HANDLE STOW BUMPER MISSING WITH GOUGING ON CASTING. ACFT GROUNDED. REMOVED FWD CARGO DOOR HANDLE HOUSING & INSTALLED NEW HOUSING REF SRM 51-40-02.Nov 5, 2014 · N581AS · Boeing 737890 · Cargo/Baggage DoorsSDR ASAA2014100609357Valve · unknownNR 2 IDG REQUIRES FREQUENT SERVICING. ACFT GROUNDED. ACCOMPLISHED LEAK CHECK OF NR 2 ENGINE IDG IAW MM 24-11-00-700-801. NO LEAKS NOTED. R & R NR 2 ENGINE IDG VENT VALVE AND SERVICING COUPLING IAW MM 24-11-00-700-804. OPS AND LEAK CHECKED NORMAL.Oct 6, 2014 · N581AS · Boeing 737890 · Electrical Power SystemSDR ASAA2014092509231Satcom · malfunctionedON POWER TRANSFER ON GROUND SATCOM PROMPT ON FMC MENU PAGE DISAPPEARED. ACFT GROUNDED. QRH PROCEDURE 5.3, SATCOM LOCKED UP ON GROUND. PERFORMED, NORMAL SATCOM PROMPT RESTORED.Sep 25, 2014 · N581AS · Boeing 737890 · Communications SystemSDR ASAA2014091609142Servo · leakingNR 2 ENGINE FUEL HEATER SERVO LEAKING. ACFT GROUNDED. REMOVED AND REPLACED THE SERVO IAW 73-11-07-000-801-F00, 50340 09-16-2014, AND 73-11-07-400-801-F00, STEP E (1) THRU G(1). LEAK CHECKED GOOD.Sep 16, 2014 · N581AS · Boeing 737890 · Fuel HeaterSDR ASAA2014091509135Start Valve · failedSTART VALVE DID NOT OPEN ON THE NR 2 ENGINE. ACFT GROUNDED. PERFORMED FIM 80-07, TASK 803- LIGHT FOR NR 2 ENG START VALVE, OPS NORMAL. FOUND POSITION SWITCH FOR NR 2 ENG START VALVE INOPERATIVE. REPLACED START VALVE IAW MM 80-11-03-000-801-F00 AND 400-801-Sep 15, 2014 · N581AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2014090809078A/C Pack · unknownUNABLE TO MAINTAIN ACCEPTABLE CLIMATE IN CABIN WITH TEMP SELECTOR DIALS IN AUTO MODE. TOO HOT IN FORWARD CABIN, TOO COLD IN AFT. REVERTED TO MANUAL CONTROL IN OFF POSITION TO MAINTAIN ACCEPTABLE CABIN TEMPS. ACFT GROUNDED. ACCOMPLISHED FIM 21-61, TASK 863, NSep 8, 2014 · N581AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014081808879Control Panel · failedAUTOPILOT B DISENGAGED TWICE DURING LEVEL FLIGHT AT FL380, .80M. NO TURBULENCE. ACFT GROUNDED, DFCS LOGGED MESSAGE 22-111607 MCP DATA INV. R & R MCP IAW MM 22-11-34. OPS CHECK NORMAL.Aug 18, 2014 · N581AS · Boeing 737890 · Autopilot System
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