N586AS

Service difficulty reports · 485

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 = 'N586AS' 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 ASAA1159173Unknown · malfunctionedON TAXI GOT FMC DISAGREE. PERFORMED QRH PROCEDURE, OPS NORMAL.Mar 3, 2011 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159078Unknown · malfunctionedRT PACK LIGHT ON RECALL OUT ON RESET. PERFORMED RT PACK CONTROLLER BITE TEST PER AMM FIM TASK 21 62 00 810 811. NO FAULTS FOUND, OK FOR CONTINUED SERVICE. SEAMC NOTIFIED NO HISTORY FOR 30 DAYS.Feb 24, 2011 · N586AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1159077Valve · faultyRT PACK LIGHTS ON WHEN RECALL IS PRESSED GOES OUT WHEN RESET. RT PACK/ZONE TEMP CONTROLLER FAULTS "TCV THIS PACK". REPLACED RT TCV V141 REF MM 21 51 10. INSTALLATION TEST AND LEAK CHECK GOOD PER SAME.Feb 24, 2011 · N586AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1158929Unknown · malfunctionedAT COMPLETION OF START CHECKLIST FMC DISAGREE DISPLAYED. QRH CHECKLIST COMPLETED. NO FURTHER ABNORMALITIES.Jan 30, 2011 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1158740Unknown · malfunctionedFUEL TOTALIZER INOP. PERFORMED FQIS BITE FOUND FAULT 28 41315 ACCOMPLISHED FIM TASK 28 41 00 810 810. NO CURRENT FAULTS GROUND TESTS PASS. FQTY IND NORMAL. NO HISTORY 60 DAYS, OK FOR SVC.Jan 8, 2011 · N586AS · Boeing 737890 · Fuel Quantity SensorSDR ASAA1058589Unknown · malfunctionedFMC DISAGREE LIGHT ILLUMINATED ON GROUND. FOLLOWED QRH PROCEDURE RESET FMCS CMPRT 1 AND FMCS CMPTR 2 CB'S. OPERATION NORMAL.Dec 2, 2010 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1058537Unknown · malfunctionedAFTER PUSHBACK UPON RECALL RIGHT PACK LIGHT ILLUMINATED. PUSHING MASTER CAUTION EXTINGUISHED PACK LIGHT BIT & PREV FLT TESTS SHOW "TCV THIS PACK" FOR NR 2 CTRLR. VERIFY TEST IS GOOD. RESET FAULT BITE TEST NR 2 CTRLR GOOD. NO HISTORY 60 DAYS. GND VERIFICATNov 23, 2010 · N586AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1058483Start Valve · faultyNR 1 ENG STARTER DID NOT CUTOUT AUTOMATICALLY. REPLACED NR 1 ENG START VALVE REF MM 80 11 03 400 801 F00 80 11 03 000 801 F00 AND TEST 71 00 00 809 F00 LEAK CHECK GOOD. REPLACED NR 1 ENG START SWITCH (S266) IAW AMM 80 11 00 PAGE BLOCK 201. START SWITCH TESTNov 6, 2010 · N586AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA1058359Filter · faultyAPU FAULT LIGHT ILLUMINATED ON START CONTINUED TO BE ILLUMINATED AFTER SWITCH PLACED OFF. REPLACED STARTER/GENERATOR OIL FILTER AND LUBE FILTER ELEMENT AS PER AMM 49 91 12. INSPECTED MAGNETIC DRAIN PLUG AS PER 49 91 81 NO METAL PARTICLES NOTED. OPERATE APU Oct 12, 2010 · N586AS · Boeing 737890 · APU Oil SystemSDR ASAA1058331Regulator · failedNR 1 ENG BLEED AIR REGULATOR FAILED HEALTH CHECK. REMOVED AND REPLACED AND PERFORMED INSTALLATION TEST GOOD OF NR 1 ENG BLEED AIR REGULATOR REF B737 800 AMM 36 11 03 400 801.Oct 6, 2010 · N586AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1058330Regulator · failedNR 1 ENG HIGH STAGE REGULATOR FAILED HEALTH CHECK. REMOVED AND REPLACED NR 1 ENGINE HIGH STAGE REGULATOR. PERFORMED LEAK CHECK, GOOD NO LEAK NOTED REF B737 800 AMM 36 11 07.Oct 6, 2010 · N586AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1058329Control Valve · faultyNR 2 ENG PRECOOLER CONTROL VALVE MANUAL OVERRIDE NUT MISSING RETAINING SCREW. REMOVED AND REPLACED NR 2 ENG PRECOOLER CONTROL VALVE IAW B737NG AMM 36 12 02. PERFORMED INSTALLATION TEST GOOD REF B737 800 AMM 36 12 02 400 801 ITEM G.Oct 6, 2010 · N586AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1058246Filter · dirtyAFT CAB TEMP CONTROLLER IS EXTREMELY ERRATIC IN AUTO MODE AFT SUPPLY DUCT TEMP REMAINS BELOW 10 C WITH TEMP SELECT FULL HOT MANUAL MODE IS NORMAL. ACCOMPLISHED BITE TEST OF PACK/ZONE TEMP CONTROLLERS NO FAULTS NOTED REF MM 21 61 00 700 806 002. INSP CABIN TESep 2, 2010 · N586AS · Boeing 737890 · Cabin Temperature SensorSDR ASAA1058244Shim · wornFAN BLADE LUBE. FOUND FAN BLADE SHIMS WORN AND RETAINING RING ELASTOMERS WORN FULL SET OF BOTH NR 2 ENG. REPLACED FAN BLADE SHIMS AND RETAINING RING ELASTOMERS REF T/C 78472002.Sep 1, 2010 · N586AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA1058239Relay · failedWHILE PERFORMING T/C 78128006 CENTER TANK BOOST PUMP AUTO SHUTOFF FUNCTIONAL TEST STEP (C) FAILED. REMOVED AND REPLACED R936 LT AUTO SHUTOFF 115V AC RELAY, OPS CHECK NORMAL.Aug 30, 2010 · N586AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA1058126Circuit Breaker · trippedWINDOW HEAT L FWD OVERHEAT LIGHT ON. ON LIGHT OFF. CONFIRMED FAULT. FOUND LEFT FRONT WINDOW HEAT POWER C/B (C228) ON P6 12 PANEL OUT. NO HISTORY LAST 30 DAYS. RESET REF MM 20 60 01 & WDM 30 41 11 PG 3. GROUND FUNCTION CHECK GOOD REF FIM 30 41 TASK 801 & Aug 4, 2010 · N586AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA1058097Unknown · malfunctionedRECEIVED "APPROACH WARNING" AT 150 FEET AGL WITH AUTO PILOT DISCONNECT AIRBORNE WINDS INDICATED APX, 10 KT X WIND IN CONJUNCTION WITH LIGHT TURB WAS NOT IDEAL CONDITIONS FOR APPROACH HOWEVER WITHIN TOLERANCE. DFCS FFR SHOW CH A AND CH B + FGN FCC DROPPED IN AJul 22, 2010 · N586AS · Boeing 737890 · Autopilot SystemSDR ASAA1058061Sensor · faultyAFTER ENGINE START NUMBER 1 ENG VIB MONITOR INDICATION WAS OBSERVED WITH READING (BLANK) NO INDICATION. NUMBER 2 INDICATION 0.2. THE ENG VIB MONITOR CB ON P6 2 A 2 WAS VERIFIED IN. THE NUMBER 1 INDICATION RETURNED TO NORMAL DURING TAXI. ACCOMPLISHED FIM TAJul 14, 2010 · N586AS · Boeing 737890 · Engine RPM Indicating SystemSDR ASAA1058022Switch · malfunctionedCREW REPORTED NR 1 ENG "ENG FAIL" LIGHT ON NORMAL SHUTDOWN. PERFORMED FIM TASK 73 05 00 810 805. RESET SYSTEM OPS CHECKS OK. OK FOR SERVICE. CONFIRMED AND FOUND CUTOFF SWITCH NOT FULLY ENGAGED.Jul 4, 2010 · N586AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA1057924Engine · vibratesAT TOP OF CLIMB AND AT CRUISE LEFT ENG VIB HIGHER THAN RT. L 1.1 / R .5 ENG INDICATIONS NORMAL AT 360 88.5/88.4 648/ 640 92.3/ 92.3 272/ 272 47/ 47 106/ 107 16/17 1.1/.5 WITH TURB LEFT VIB WILL SPIKE. NO DEFECTS NOTED UPON GROUND ENG RUN TEST FROM IDLE TO TAKJun 12, 2010 · N586AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA1057923Balance Weight · out of toleranceAT CRUISE FL360 & FL380 NOTICEABLE OUT OF SYNC VIBRATION APPARENTLY FROM RIGHT ENGINE. VIBRATION NOT NOTICEABLE AT CLIMB POWER SETTINGS. LEFT VIB READS 1.0 RIGHT VIB VARIES BETWEEN 1.4 & 1.6. ALL OTHER ENG INDICATIONS NORMAL. RAN ENG CONFIRMED ENG NR 2 VIBJun 11, 2010 · N586AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA1057868Transceiver · unsecureWX RADAR HAS FREQUENT SPOKING. EXTENDS FROM AC NOSE TO EDGE OF DISPLAY OCCURS BOTH CAPT & F/O DISPLAY. DUPLICATED FAULT FOUND WX RADAR TRANSCEIVER NOT SECURED ON MOUNT. RE-SECURED TRANSCEIVER ACCOMPLISHED GROUND VERIFICATION CHECK REF 34 43 41, OPS CHECK NOMay 25, 2010 · N586AS · Boeing 737890 · Weather Radar SystemSDR ASAA1057831Unknown · malfunctionedHGS AIII/AUTOLAND UNSUCCESSFUL ON SEA RWY 16C. HAD HUD APPROACH WARNING AT 100FT. AIRCRAFT WENT SLIGHTLY BELOW GLIDESLOPE AND IN VFR CONDITIONS DID A NICE DID A NICE TOUCHDOWN AT 900' ON CENTERLINE. GROUNDED YES. NO FAULTS LOGGED IN DFCS ACCOMPLISHED LAND May 18, 2010 · N586AS · Boeing 737890 · Autopilot SystemSDR ASAA1057713Radio · malfunctionedHF1 RADIO FAIL. VERIFIED DISCREPANCY. PERFORMED FIM 23 11 806 AND HF1 TESTS OK. NO HISTORY.Apr 18, 2010 · N586AS · Boeing 737890 · HF Communications SystemSDR ASAA1057675Display · malfunctionedAFTER VARIOUS INPUTS NR 2 FMC BLANKS THEN AFTER 4 SECONDS ALL LIGHTS ILLUMINATE THEN BITE TEST FOR 2 OR 3 SECONDS. THEN FMC RETURNS TO NORMAL OPS. HAPPENED ABOUT 5 TIMES IN FLIGHT. REMOVED AND REPLACED F/O MCDU PER AMM REF 34 61 01 400 802/34 61 01 000 802,Apr 11, 2010 · N586AS · Boeing 737890 · Central DisplaySDR ASAA1057619Unknown · malfunctionedEN ROUTE RIGHT FMC BRIEFLY WENT COMPLETELY BLANK AND THEN RETURNED TO NORMAL. FMC OPS CHECK NORMAL AT THIS TIME NO LOG HISTORY 30 + DAYS NO FAULTS RECORDED IN FLIGHT FAULTS HISTORY OBSERVE FURTHER.Mar 29, 2010 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1057614Valve · sticksEXCESSIVE DUCT PRESSURE SPLIT DURING CLIMB LEFT 44 RIGHT 18, STABILIZED AT CRUISE TO L42 R24. FOUND HIGH STAGE VALVE NOT OPERATING NORMALLY STUCK IN BETWEEN OPEN AND CLOSED. REPLACED HIGH STAGE BLEED VALVE REF AMM 36 11 06 00 801, LEAK CHECK NORMAL, OPS CHECMar 28, 2010 · N586AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1057472Idg · defectiveNR 1 IDG HAS HISTORY OF FREQUENT SERVICING. REMOVED AND REPLACED IDG REF AMM 24 11 11 000 801, OPERATIONAL TEST GOOD AND NO LEAKS NOTED REF AMM 24 11 00 700 802.Feb 26, 2010 · N586AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1057417Shroud · damagedTWO (2) EA CRATERS FOUND IN ABRADABLE SHROUD NR 2 ENGINE AT 10 O’CLOCK AND 11 O’CLOCK POSITION. CRATER AT 10 O’CLOCK MEASURES 1.75 X 1.5 CRATER AT 11 O’CLOCK MEASURES 1.0 X .75 REPAIR OF BOTH CRATERS MUST BE ACCOMPLISHED IN 50 CYCLES OR 75 HOURS WHICHEVER COMFeb 19, 2010 · N586AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA1057412Autothrottle Sys · malfunctionedAUTO THROTTLE INOP WILL NOT ENGAGE. FOUND FAULT CODE 22 31501, PERFORMED FIM 22 31TASK 805. ALL GROUND VERIFICATION TEST PASS. NO HISTORY PASS 30 DAYS. BITE TEST GROUP NR 35 HGS SENSOR TEST FCC/AT TEST PASS. REF MM 22 11 33. SMM 34 36 00.Feb 17, 2010 · N586AS · Boeing 737890 · Auto Throttle SystemSDR ASAA1057411Accessory Unit · failedWHEN PRESSING RECALL ON MASTER CAUTION ZONE TEMP LIGHT FOR CONTROL CABIN COMES ON. PER QRH WHEN MASTER CAUTION IS RESET LIGHT GOES OUT. REPLACED M324 AIR CONDITIONING ACCESSORY UNIT TESTED ACAU NORMAL REF MM 21 51 02 400 801. RAN BOTH PACKS FOR 20 MIN PERFOFeb 15, 2010 · N586AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1057359Engine · oil consumptionDUE TO NR 2 ENGINE OIL SPIKE AT 0.71 AIRCRAFT REQUIRES TOP DEFERRAL. PER SEAMC THE NR 2 ENGINE OIL CONSUMPTION RATE HAS RETURNED TO NORMAL RANGE OF .09 QPH.Feb 8, 2010 · N586AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA1057353Hf Comm · malfunctionedPER REQUEST FROM SEAMC (ETOPS) FUNCTIONAL TEST OF HF1 AND HF2 RADIOS UNSUCCESSFUL ON GROUND (SEA) AND IN FLIGHT. TRIED BOTH FREQ'S PROVIDED BY SFO RADIO. ACCOMPLISHED SYSTEM TEST OF NR 1 AND NR 2 HF COMMUNICATION SYSTEM REF 23 11 00 CONTACTED SFO RADIO GROUNFeb 7, 2010 · N586AS · Boeing 737890 · HF Communications SystemSDR ASAA1057329Modulating Valve · faultedON RECALL AIR COND ZONE TEMP FOR CONT CAB REMAINS ILLUMINATED. ALL LIGHTS EXTINGUISH AFTER RESETTING THE MASTER CAUTION SYSTEM. RELEASED PER MEL 21-21F. AUTH BY SEAMC. NR 2 TEMP CONT FAULTED TCU FLT DK V143, WAS ABLE TO RESET VALVE REF MM 21-61-00-700-806-Feb 5, 2010 · N586AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0853708Probe · malfunctionedNR 2 ENG N1 FLUCTUATION RAPIDLY FORM 91.2 TO 100.1 BETWEEN ABOUT 2500FT TO 6000FT ON CLIMBOUT, AUTOTHROTTLE WAS FOLLOWING. ALL OTHER ENGINE PARAMETERS APPEAR NORMAL. ABOVE 6KFT ALL NORMAL. NR 2 ENG EEC LOGGED FAULTS 73-30902-T12 SIGNALS DISAGREE 73-21702 ADINov 7, 2008 · N586AS · Boeing 737890 · Fuel Controlling System
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