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.

SDR ASAA2017042420525Warning Light · false activationCLIMB THROUGH 10,000 FEET, CABIN ALTITUDE WARNING LIGHT AND HORN SOUNDED. PRESSURE CONTROLLER HAD SHIFTED TO MANUAL. MAINTAINED 10,000 FEET AND RAN PRESSURIZATION IN MANUAL IAW QRH. ACFT GROUNDED. PERFORMED FIM TASK 21-31-00-810-801, PARA. A-E (9) (W). NO AApr 24, 2017 · N585AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2017040420360Autopilot Sys · failedAFTER TAKEOFF, FIRST OFFICER`S FLIGHT DIRECT FAIL LIGHT ON PFD ILLUMINATED. AUTOPILOT B WILL NOT ENGAGE. ACFT GROUNDED. VERIFIED DISCREPANCY. DOWN-POWERED AIRCRAFT. RESET ALL ASSOCIATED FCC B CIRCUIT BREAKERS. RACKED FCC B IAW AMM 22-11-33. APPLIED POWER-UPApr 4, 2017 · N585AS · Boeing 737890 · Autopilot SystemSDR ASAA2017040120314Probe · failedNR 1 FUEL TANK COMPENSATOR PROBE F15 AND TANK UNITS F1 AND F7 READING HIGH CAPACITANCE. ACFT GROUNDED. REMOVED AND REPLACED THE COMPENSATOR PROBE F15 AND TANK UNIT PROBES F1 AND F7 IAW AMM 28-41-21-400-801. LEAK CHECKED GOOD.Apr 1, 2017 · N585AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2017040120315Compensator · out of limitsPER T/C NG-28FCD-18090-1, REPLACE ANY TANK OR COMPENSATOR UNIT OF FUEL TANK NR 2 THAT ARE OUT OF LIMITS. GROUNDED - YES. TANK UNIT F9 IS OUT OF LIMITS, REF AMM 28-41-21-710-801. REMOVED AND REPLACED F9 UNIT IN NR 2 TANK, REF AMM 28-41-21. F9 IS NOW WITHIN LIMIApr 1, 2017 · N585AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2017032920295Fmc · malfunctionedAFTER LANDING, BOTH FMCS FAILED AND APPEARED TO BE CYCLING ON AND OFF, VTK ON CAPTS SIDE. ACFT GROUNDED. ACCOMPLISHED FIM 34-61 TASK 836, BOTH FMCS OPS NORMALMar 29, 2017 · N585AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2017030220000Warning Light · false activationDURING MASTER CAUTION RECALL, RIGHT PACK LIGHT ILLUMINATED, THE PACK LIGHT EXTINGUISHED ON RESET OF MASTER CAUTION. ACFT GROUNDED. PERFORMED PACK ZONE TEMP CONTROLLER BITE TEST IAW AMM 21-61-00-700-806-002. TEST PASSED. PACK LIGHT CLEARED.Mar 2, 2017 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017012819563Hf Comm · malfunctionedHF 1 FAILED, ACFT GROUNDED. ACCOMPLISHED BITE IAW FIM 23-11 TASK 801. HF LIGHT CHECK TEST PASSED NO FAULTS FOUND. GROUND VERIFICATION CHECKS GOOD IAW AMM 23-11-00.Jan 28, 2017 · N585AS · Boeing 737890 · HF Communications SystemSDR ASAA2017012319520Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED. GOES OUT WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED THE PACK/ZONE TEMP CONTROLLER BITE TEST IAW AMM 21-61-00-700-806-002. VERIFIED RIGHT PACK FAULT WAS INTERMITTENT AND DID NOT RETURN. ALSO, THERE IS NO MAINTENANCE HISTJan 23, 2017 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017012219511Warning Message · false activationNR 1 HF SHOWING FAIL ON BOTH DISPLAYS. ACFT GROUNDED. PERFORMED BITE IAW FIM 23-11 TASK 801. BITE CHECK PASSED, NO FAULTS FOUND. GROUND VERIFICATION TESTED GOOD IAW AMM 23-11-00-730-801.Jan 22, 2017 · N585AS · Boeing 737890 · HF Communications SystemSDR ASAA2017011319868Probe · faultyPER TASK CARD 78273000 ECONOMIC FAULT FOUND MSG 73-31372 ON NR 2 ENGINE. GROUNDED - YES. INSPECTED AND FOUND S1 OUT OF LIMITS BY PERFORMING LINE RESISTANCE CHECK. S4 PROBE IS WITHIN LIMITS. RMVD AND INSTALLED NEW S1 T49.5 PROBE REF AMM TASK 77-21-01-400-801-F0Jan 13, 2017 · N585AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA2016120218920Actuator · leakingDURING VSV ACTUATOR LEAK TEST OF NR 2 ENGINE LT ACTUATOR, FOUND THE NR 2 ENGINE RT VSV ACTUATOR LEAKING FUEL AT A STEADY STREAM OUT OF DRAIN. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 VSV ACTUATOR IAW AMM 75-31-01-400-802-F00. ACCOMPLISHED VSV ACTUATOR LDec 2, 2016 · N585AS · Boeing 737890 · Compressor Bleed ControlSDR ASAA2016120118919Actuator · leakingFOUND LARGE PUDDLE OF FUEL UNDER NR 2 ENG VERFIED STEADY DRIP. ACFT GROUNDED. FOUND LEFT VSV DRAIN LEAKING. REMOVED AND REPLACED THE NR 2 ENGINE INBD VSV ACTUATOR IAW AMM 75-31-01 STEP F.(1) THRU F. (6). ACCOMPLISHED VSV LEAK CHECK, OPS & LEAK CHECK GOOD IAWDec 1, 2016 · N585AS · Boeing 737890 · Compressor Bleed ControlSDR ASAA2016113018890Valve · faultedZONE TEMP LIGHT FOR CONT CAB ILLUMINATED DURING MASTER CAUTION RECALL. RAN QRH, LIGHT WENT OUT. ACFT GROUNDED. BITE CHECKED NR 2 ZONE TEMP CONT, SHOWS FLT DECK TRIM VALVE FAULT IAW FIM 21-61 TASK 861. REPLACED CONTROL CABIN TRIM AIR MODULATING VALVE IAW AMM Nov 30, 2016 · N585AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016112218831Heat Exchanger · leakingNR 2 ENGINE MAIN OIL/FUEL HEAT EXCHANGER DRAIN DRIPPING FUEL AT 35 DPM. STOPS WITH ENGINE AT IDLE POWER. ACFT GROUNDED. REMOVED AND REPLACED THE HEAT EXCHANGER IAW AMM 79-21-02-400-801-F00. OPS AND LEAK CHECKED GOOD.Nov 22, 2016 · N585AS · Boeing 737890 · Engine Oil CoolerSDR ASAA2016100118172Engine · faultedFOUND FMC CDU FAULT 73-31372 NR 2 ENGINE. UPPER EGT SECTORS READING HIGH. ECONOMIC FAULT. ACFT GROUNDED. ACCOMPLISHED EE TST RECENT FAULTS IAW AMM 73-21-00-740-803-F00 AND EEC TEST IAW AMM 73-21-00-700-804-F00. NO FAULTS.Oct 1, 2016 · N585AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2016092818142Control Valve · failedLEFT PACK LIGHT ILLUMINATES DURING RECALL, EXTINGUISHES WITH RESET. GROUNDED, YES. LEFT PACK LOGGED THIS PACK TCV. INITIAL EVALUATION REVEALED NO DEFECTS. REMOVED & REPLACED LEFT PACK TCV. OPS CHECK NORMAL, REF AMM 21-51-10.Sep 28, 2016 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016083117873Control Valve · fault messageON DECENT, THE LT PACK LIGHT ILLUMINATED ON RECALL. IT EXTINGUISHED WITH THE MASTER CAUTION PUSHED. QRH WAS FOLLOWED. ACFT GROUNDED. PERFORMED LT PACK ZONE TEMP CONTROL BITE, REF AMM 21-51-00. FAULT FOUND FOR LT TEMPERATURE CONTROL VALVE. R & R LT TEMPERAug 31, 2016 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016082617802Warning Light · false activationNR 1 PACK LIGHT ON RECALL AFTER ENGINE START. ACFT GROUNDED. PERFORMED NR 1 PACK/ZONE TEMP CONTROL BITE, FOUND TCV FAULT NR 1 PACK ON PREVIOUS FLIGHT. CLEARED FAULT PERFORMED 2 BITES NO DEFECTS NOTED IAW AMM 21-61-00.Aug 26, 2016 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016081717739Warning Message · false activationSATCOM SHOWS UNAVAILABLE VOICE COMMUNICATION. ACFT GROUNDED. PERFORMED OPERATIONAL TEST OF SATCOM, IAW AMM 23-15-00. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.Aug 17, 2016 · N585AS · Boeing 737890 · Communications SystemSDR ASAA2016080117607Actuator · leakingDURING NR 1 ENGINE SHUTDOWN, FOUND FUEL LEAK AT THE ENGINE DRAIN LINES. ACFT GROUNDED. ACCOMPLISHED NR 1 ENGINE FUEL LEAK, CHECK REF AMM 71-71-00-200-801-F00, STEP G1, B. FUEL LEAK WITHIN LIMITS. REF L/P 11536791, R & R NR 1 ENGINE RT VSV ACTUATOR IAW AMM Aug 1, 2016 · N585AS · Boeing 737890 · Compressor Bleed ControlSDR ASAA2016072017439Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. PERFORMED FIM 21-62 TASK 848 PACK LIGHT COMES ON DURING MASTER CAUTION RECALL FAULT ISOLATION, NO FAULTS LOGGED AND GROUND FUNCTIONAL TESTS NORMAL.Jul 20, 2016 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016071517381Audio Panel · failedWITH HF1 SELECTED ON AUDIO PANEL "FAIL" ILLUMINATED. ACFT GROUNDED. COMPLIED WITH HF OPS CHECK IAW AMM 23-11-00-710-801. CHECKED GOOD, GROUND VERIFICATION CHECKED GOOD, NO FURTHER FAULTS.Jul 15, 2016 · N585AS · Boeing 737890 · HF Communications SystemSDR ASAA2016070917317Fastener · wornNR 1 ENGINE FAN DUCT PANEL NR 12 HAS FASTENER WORN THROUGH. ACFT GROUNDED. REMOVED AND REPLACED NR 1 ENGINE FAN DUCT PANEL NR 12 IAW AMM 72-23-07. NO OTHER DEFECTS NOTED.Jul 9, 2016 · N585AS · Boeing 737890 · Nacelle/Pylon, Main FrameSDR ASAA2016070917316Seal · tornNR 1 ENGINE OUTLET GUIDE VANES INNER SEALS AT 2:30 AND 11:30 O'CLOCK POSITIONS BOTH HAVE MISSING MATERIAL. ACFT GROUNDED. REMOVED AND REPLACED THE SEALS IAW AMM 72-23-01.Jul 9, 2016 · N585AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016070617283Warning Light · illuminatedCONTROL CABIN ZONE TEMP ON, AT RECALL. CLEARS WITH MC RESET. ACFT GROUNDED. PERFORMED PACK/ZONE TEMP CONTROLLER BITE CHECK OF BOTH LEFT & RIGHT CONTROLLERS IAW AMM 21-60-00-700-806-002. FOUND "CABIN SENSOR " LIGHT RED ON BOTH CONTROLLERS FOR FLIGHT DECK. UPJul 6, 2016 · N585AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016062817195Unknown · unknownMISSING SAT SELECTION ON MCDU MENU PAGE AND NO SATCOM PAGES AVAILABLE. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE IAW QRH. SATCOM OPS RESTORED NORMAL.Jun 28, 2016 · N585AS · Boeing 737890 · Communications SystemSDR ASAA2016053116881Hmu · failedWHILE ACCOMPLISHING TASK CARD 78273000, NR 1 ENGINE HAS FAULT 73-31161, MECHANICAL OVERSPEED PROTECTION SIGNAL IS OUT OF RANGE, FAULT IS A LONG TIME FAULT. ACFT GROUNDED. ACCOMPLISHED HMU REMOVAL REF T/C N8473000, ACCOMPLISHED HMU INSTALL AT NR 1 ENGINE, RMay 31, 2016 · N585AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2016051416706Warning Light · false activationRIGHT PACK LIGHT ON RECALL RESET WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED BITE CHECK IAW FIM TASK 21-61-00-810-801. NR 2 "BIT" SHOWED "RAM AIR ACT", FAULT WENT AWAY WITH "VERIFY". RAN RT PACK 10 MINUTES AND REPEATED TEST; NO FAULTS FOUND. MASTEMay 14, 2016 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016042716550Converter · failedDURING APU START MAINTENANCE MESSAGE 49-41250, START CONVERTER UNIT SHOWS START SYSTEM INOPERATIVE. FOUND 18 LOGGED FAULTS OF THIS MESSAGE. ACFT GROUNDED. PERFORMED FIM TASK 49-40, TASK 811. R & R APU START CONVERTER UNIT, INSTALLATION TEST PASSED, REF AMM Apr 27, 2016 · N585AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2016042516532Control Unit · failedDURING APU START, FAULT LIGHT ILLUMINATED. ACFT GROUNDED. CHECKED AND FOUND EGT RISING DURING START UP AND SUBSEQUENT APU SHUTDOWN WITH FAULT LIGHT ILLUMINATING. CHECKED FAULT HISTORY IN CDU FOUND MSG 49-31016. RELEASED IAW MEL 49-1B. R & R APU FUEL CONTROLApr 25, 2016 · N585AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2016032716110Transceiver · failedON ILS APPROACH AUTO PILOT B UNCOMMANDED DISCONNECT. ACFT GROUNDED. DFCS FFR SHOWS FLIGHT 8, A/P DISCONNECT DUE TO RAD ALT-2 INV HGS SHOWS NUMEROUS RECENT AND AFTER FLIGHT 8 RAD ALT-2 INVALID. R & R NR 2 RAD ALT RECEIVER/TRANSMITTER REF AMM 34-33-21, OPS NORMar 27, 2016 · N585AS · Boeing 737890 · Autopilot SystemSDR ASAA2016032716105Fuel Sys · malfunctionedDURING DESCENT, RECEIVED AN UNCOMMANDED FUEL IMBALANCE OF 1300 POUNDS LOWER ON RT TANK THAN LT TANK. FUEL CROSSFEED WAS CLOSED. ALL FUEL PUMPS PRESSURIZED. THIS WAS NOT AN OPERATOR-INDUCED IMBALANCE. ACFT GROUNDED. REF FIM 28-41, TASK 801, PERFORMED FQIS Mar 27, 2016 · N585AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016030615764Servo · failedAUTO THROTTLE WILL NOT STAY ENGAGED. ACFT GROUNDED. ACCOMPLISHED A/T BITE REF FIM 22-31-TASK 801. FOUND FAULT MESSAGE 22-31687-ASM1. REMOVED AND INSTALLED NEW NR 1 ASM REF AMM 22-31-91. PERFORMED INSTALLATION TEST, SERVO MOTOR TEST REF AMM 22-31-00. ACCOMPMar 6, 2016 · N585AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016022615670Indication Sys · malfunctionedON A 1.5 HR FLIGHT, THE RT MAIN TANK SHOWED A 600 LBS LESS DIFFERENCE THAN THE LT MAIN TANK. THE FUEL USED SHOWED EVEN AND THE FUEL FLOW WAS THE SAME FOR EACH ENGINE. ACFT GROUNDED. PERFORMED FQIS BITE REF FIM 28-41, TASK 801, NO FAULTS FOUND, FQIS CHECKS GOFeb 26, 2016 · N585AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016022315642Switch · failedAPU WILL NOT SHUTOFF WITH APU SWITCH IN OFF. ACFT GROUNDED. INTERMITTENT APU SWITCH, VERIFIED ON APU BITE, INPUT MONITORING PAGE 2/4. APU ON SWITCH AND APU OFF SWITCH BOTH SHOWS, NO, FOR UP TO A MINUTE BEFORE YES SHOWED ON APU OFF SWITCH INPUT. R & R S248 AFeb 23, 2016 · N585AS · Boeing 737890 · APU ControlsSDR ASAA2016021515455Idg · failedNR 1 ENGINE DRIVE LIGHT INTERMITTENT. EXTINGUISHES WITH ASSOCIATED ELECTRONIC MASTER CAUTION LIGHT W/O ENGINE RUNNING. ACFT GROUNDED. NR 1 ENGINE TROUBLESHOOTING SHOWED CHARGE PRESSURE SWITCH FAULTY REF WDM 24-11-11. R & R THE NR 1 IDG REF AMM 24-11-11-000-Feb 15, 2016 · N585AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2016021415445Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL NOT STAY ENGAGED. ACFT GROUNDED. ACCOMPLISHED FIM 22-32/819. TORQUE VALUES WITHIN LIMITS. ASM TEST PASSES WITH NO FAULTS. CURRENT STATUS TEST PASSES WITH NO FAULTS, REF AMM 22-31-00/501.Feb 14, 2016 · N585AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016021115425Unknown · unknown600 LBS OVERBURN, LT FUEL REMAIN A.09 RT, 3.38. FUEL USED 4.7, 4.7, FUEL FLOW WITHIN 20LBS/HR. ACFT GROUNDED. USING ALTERNATE FUELING MANUAL CONFIRMED THAT GAUGES AND FUEL STICKS ARE IN SYNC WITH ONE ANOTHER. FUEL QTY IN TANK AT 5950 LBS, FUEL STICK NR 4 REFeb 11, 2016 · N585AS · Boeing 737890 · Aircraft Fuel SystemSDR ASAA2016020815340Compensator · failedAPPROXIMATELY 1 HR PRIOR TO LANDING, NR 2 FUEL TANK QTY BEGAN DECREASING AT SIGNIFICANT RATE. AT APPROXIMATELY 700 POUND DIFFERENCE BETWEEN NR 1 & NR 2 TANK QTY, 2 TANK WAS LOW TANK, FUEL WAS BALANCED. PRIOR TO LANDING, NR 2 TANK QTY INDICATED 500 POUNDS LOWFeb 8, 2016 · N585AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016011014721Warning Message · activatedWHILE ACCOMPLISHING TASK CARD NR 78273000, INTEROGATE THE FMC CDU FOR ENGINE FAULTS, FOUND MSG NR: 73-31161, THE MECHANICAL OVERSPEED PROTECTION SIGNAL IS OUT OF RANGE, NR 1 ENGINE. THIS IS A LONG TIME FAULT. ACFT GROUNDED. ACCOMPLISHED FIM 73-21, TASK 801, Jan 10, 2016 · N585AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2015121214210Check Valve · slowDURING CROSSFEED VALVE CHECK, VERY SLOW TO OPERATE. FIRST ATTEMPT ABOUT 45 SECS TO OPEN AND THEN CLOSE. AFTER THIRD ATTEMPT, OPEN, CLOSE IN 12 SECONDS. ACFT GROUNDED. REF FIM 28-22, TASK 807, CROSSFEED VALVE OPERATES NORMAL. REPLACED ENGINE FUEL FEED ACTUADec 12, 2015 · N585AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2015121214204Sensor · malfunctionedAILERON POSITION SENSOR FOUND OUT OF ADJUSTMENT ON DFCS EXTENDED MAINTENANCE UPGRADE T/C. ACFT GROUNDED. ACCOMPLISHED AILERON POSITION SENSOR ADJUSTMENT REF AMM 22-11-29-820-801. OPS NORMAL. DFCS LRU REPLACEMENT TEST FOR ROLL SENSOR 46, PASSED. ALL DFCS EDec 12, 2015 · N585AS · Boeing 737890 · Autopilot SystemSDR ASAA2015121114216Warning Message · false activationFMC DISAGREE ON THE GROUND. RAN QRH-PROBLEM RESOLVED. ACFT GROUNDED. ACCOMPLISHED FMC OPERATION TEST REF AMM 34-61-00, OPS NORMAL.Dec 11, 2015 · N585AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015120314136Floorbeam · corrodedAFT CARGO COMPARTMENT FLOOR PANEL TEE ASSY AT BS 772.6 IS CORRODED. ACFT GROUNDED. RECEIVED NEW FLOOR PANEL TEE ASSY, PN 146A9401-4. INSTALLED TEE ASSY ON CUSTOMER CARD NR G618016.Dec 3, 2015 · N585AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2015120114176Stop Fitting · chafedMAIN CABIN FORWARD ENTRY DOOR, AFT SIDE LOWER STOP FITTING CHAFED. ACFT GROUNDED. ACCOMPLISHED REPAIR TO FORWARD ENTRY, L1, DOOR, PN 141N6150-7, SN AC 00585, LOWER AFT STOP FITTING, 141A6104-10 IAW REO-G19414, REV A AND EA CMPT-52EA-16239. REMOVED DOT.Dec 1, 2015 · N585AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2015113014124Floorbeam · corrodedFWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT STA 500I IS CORRODED. ACFT GROUNDED. REMOVED CORROSION FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE BS 500I. ORIGINAL HICK WAS .071, LOST .016, REMAINING .055 FOUND TO BE OUT OF LIMITS IAW DWG 143A9485 AND SRM 53-00-5Nov 30, 2015 · N585AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2015112413926Fuel Nozzle · failedFOUND MESSAGE FAULT ON NR 1 ENGINE, ECONOMIC, MSG 73-31371, EGT SECTORS READING HIGH, WHILE PERFORMING TASK CARD 78273000. ACFT GROUNDED. R & R UPPER 11 FUEL NOZZLES IAW TASK CARD PWR PL-73 CMPT-07267-2.Nov 24, 2015 · N585AS · Boeing 737890 · Fuel Injector NozzleSDR ASAA2015111013718Shroud · crackedNR 1 ENGINE HAS 6" SECTION OF ABRAIDABLE SHROUD COMING LOOSE AT 5 O'CLOCK POSITION, LOOKING AFT; ABOVE NOTED SECTION HAS 1 CRACK STARTING AT AFT EDGE FORWARD 2" AND TURNING TOWARDS 6 O'CLOCK POSITION WITH L/E LIFTING UP. THE OTHER CRACK AT 6 O'CLOCK POSITIONNov 10, 2015 · N585AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2015110813689Warning Message · illuminatedWHILE PERFORMING AFTER START FLAPS, RECEIVED A MASTER CAUTION WITH WINDOW HEAT OVERHEAT ANNUNCIATED. ACFT GROUNDED. SWITCHED THE LT FRONT WINDOW SENSOR TO THE SPARE POSITION. LEFT WINDOW HEAT SYS, OPS CHECKS GOOD, REF MM TASK 30-41-00-71-801. GROUND VERIFICNov 8, 2015 · N585AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2015110113581Autothrottle Sys · disengagedAUTOTHROTTLES DISENGAGE IN FLIGHT, ACFT GROUNDED. A/T FLT FAULT REVIEW SHOWED ASM-1 FAULT. PERFORMED FIM TASKS 22-31 801, 805, AND 824. PERFORMED CURRENT STATUS AND INTERACTIVE SERVO MOTOR TEST 6 TIMES W/NO FAULTS. IAW FIMS, INTERMITTENT FAULT.Nov 1, 2015 · N585AS · Boeing 737890 · Auto Throttle System
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