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 ASAA2014111809697Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. PERFORMED FMC DISAGREE ON GROUND PROCEDURE. RESUMED NORMAL OPS.Nov 18, 2014 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014111009631Lamp · malfunctionedF/A REPORTS EMERGENCY EXIT LIGHTING FLICKERING. ACFT GROUNDED. REPLACED THE LAMPS - OP`S NORMAL.Nov 10, 2014 · N586AS · Boeing 737890 · Emergency LightingSDR ASAA2014100809329Satcom · malfunctionedSATCOM LOCKED UP, ON GROUND, ACFT GROUNDED. RESET CIRCUIT BREAKER, OPS NORMAL.Oct 8, 2014 · N586AS · Boeing 737890 · Communications SystemSDR ASAA2014091609143Hmu · failedNR 2 ENGINE WAS VERY SLOW TO SPOOL UP TO 40 PERCENT N1. ACFT GROUNDED. PERFORMED ENGINE ACCEL TEST, 3 TIMES FAILED, EACH TIME WITH ACCEL TIMES OF 11.6,11.4 & 11.2 SECONDS IAW MM 71-00-00-700-824-F00. REPLACED NR 2 ENGINE HMU IAW N8473000 AND N8473001. PERFSep 16, 2014 · N586AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2014072908710Light · inoperativeONE LIGHT SEGMENT ON VNAV SELECT BUTTON ON MCP INOPERATIVE. ACFT GROUNDED. CONFIRMED FAULT. MCP VNAV SELECT PUSH-BUTTON LIGHT INOPERATIVE. R & R MCP IAW AMM 22-11-34. OPS CHECK NORMAL REF AMM 22-11-34 (GP32) DFCS LRU INTERFACE TEST, DFCS LAND VERIFY TEST (GJul 29, 2014 · N586AS · Boeing 737890 · Auto Flight SystemSDR ASAA2014071908593Lens · dislodgedMID CABIN OVERHEAD EXIT SIGN FELL OFF INFLIGHT. ACFT GROUNDED. SECURED EXIT SIGN.Jul 19, 2014 · N586AS · Boeing 737890 · Emergency LightingSDR ASAA2014071708588Control Panel · failedAUTOPILOT CLICKED OFF DURING CRUISE FLT, TWICE. ONCE WHILE CMP A ENGAGED AND ONCE WHILE CMP B ENGAGED, ACFT WAS IN TRIM AT DISCONNECT. ACFT GROUNDED. BITE TEST SHOWED MCP REPLACED MCP IAW MM 22-11-34 ETOPS PN 822-1567-102 AS VERIFIED SEAMC.Jul 17, 2014 · N586AS · Boeing 737890 · Autopilot SystemSDR ASAA2014071108531Lead · brokenFOUND CERAMIC SLEEVE BROKEN ON NR 1 ENGINE RT IGNITION LEAD. ACFT GROUNDED. R & R NR 1 ENGINE RT IGNITION LEAD IN REF AMM 74-21-01. OPS CHECK GOOD.Jul 11, 2014 · N586AS · Boeing 737890 · Ignition Harness (Distribution)SDR ASAA2014071008524Warning Message · false activationFMC DISAGREE GROUNDED. ACCOMPLISHED QRH. OPS NORMAL.Jul 10, 2014 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014062708379Warning Message · false activationAFTER ENGINE START FMC DISAGREE ANNUNCIATED. ACFT GROUNDED. FOLLOWED QRH PROCEDURE AND FMC NORMAL, OPS RESTORED.Jun 27, 2014 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014062308319Warning Light · false activationELECTRIC LIGHT ILLUMINATED ON OVERHEAD ELECTRICAL PANEL. ACFT GROUNDED. PERFORMED BITE FOUND FAULT AUX BATTERY CHARGER INOPERATIVE IAW FIM 24-31, TASK 801. CLEARED FAULT, CONFIRMED THAT NO MESSAGE AND TWO GREEN LIGHTS ON FRONT OF THE AUX BATTERY CHARGER IN Jun 23, 2014 · N586AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2014061708256Fuel Control · failedAPU WOULD NOT START AND INDICATED A "FAULT" LIGHT. ACFT GROUNDED. REPLACED APU FUEL CONTROL UNIT, OPS CHECKED NORMAL IAW AMM 49-31-11-400-801.Jun 17, 2014 · N586AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2014052407918Warning Message · false activationRECEIVED FMC DATALINK FULL ALERT MESSAGE. ACFT GROUNDED. PERFORMED PROCEDURE IAW FWB BULLETIN 14-3 AND MESSAGE CLEARED.May 24, 2014 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014032707339Warning Light · false activationLEFT PACK LIGHT ON RECALL ON LANDING CHECK. ACFT GROUNDED. TCV FAULT NR 1 ZONE TEMP CONTROLLER. RESET AND BITE TESTS NORMAL IAW FIM 21-61, TASK 801.Mar 27, 2014 · N586AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014032207265Warning Message · false activationFMC MESSAGE "DATALINK FULL" DISPLAYED. ACFT GROUNDED. CYCLED FMC C/B. OPS CK NORMAL REF FIM 34-61, TASK 801. OPS CK ACARS TEST PASS REF MM 23-27-00. NO HISTORY PAST 90 DAYS.Mar 22, 2014 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014022607182Seat Track · crackedMAIN CABIN SEAT TRACK BS 727B, RBL 45.50 INBD AND OTBD FLANGES ARE CRACKED AT FASTENER HOLE. ACFT GROUNDED. REPAIRED SEAT TRACK IAW EA 800-57EA-12253 AND REO-G17241, REV A.Feb 26, 2014 · N586AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2014022607181Seat Track · crackedMAIN CABIN SEAT TRACK BS 727B, LBL 24.75, OTBD FLANGE IS CRACKED AT FASTENER HOLE. ACFT GROUNDED. REPAIRED SEAT TRACK IAW EA 800-57EA-12253 AND REO G17241, REV A.Feb 26, 2014 · N586AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2014022607180Seat Track · crackedMAIN CABIN SEAT TRACK BS 727B, RBL 24.75 INBD FLANGE IS CRACKED. ACFT GROUNDED. REPAIRED SEAT TRACK IAW EA 800-57, EA-12253 AND REO G17241, REV A.Feb 26, 2014 · N586AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2014022507150Web · corrodedAFT CARGO DOOR CUTOUT, LOWER SILL AREA, CORRODED. BS 790 - 840. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1, FIG 103, DET "D". R & R WEB IAW SRM 51-410-02.Feb 25, 2014 · N586AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014010112299Filter · cloggedWHILE PERFORMING W/C 78349012, APU LUBE MODULE AND LINES GV INSPECTION FOUND THE MAIN OIL FILTER CLOGGING. INDICATOR POPPED. ACFT GROUNDED. UNABLE TO RESET OIL FILTER CLOGGING INDICATOR. R & R OIL FILTER HOUSING CLOGGING INDICATOR, REF MM 49-91-13-000-801,Jan 1, 2014 · N586AS · Boeing 737890 · APU Oil SystemSDR ASAA2013112396505Exciter · failedFLT CREW REPORTS FAULT LIGHT ILLUMINATED ON APU START. ACFT GROUNDED. REPLACED STARTER IGNITION UNIT IAW AMM 49-41-31.Nov 23, 2013 · N586AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2013111796444Guide · out of rigF/A REPORTS L1 DOOR DIFFICULT TO CLOSE. ACFT GROUNDED. ON EVALUATION FOUND THE L1 DOOR AFT UPPER ROLLER NOT ENGAGING. R & R L1 DOOR GUIDE ARM IAW MM 52-11-21. RIG AND OPS TEST GOOD.Nov 17, 2013 · N586AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2013111596422Warning Light · illuminatedON RECALL ZONE TEMP CONT. CABIN LIGHT COMES ON. RESET THE MASTER CAUTION AND THE LIGHT GOES OUT. ACFT GROUNDED. NR 2 ZONE CONT LOGGED FLT DECK TRIM VALVE, FAULT CLEARED & TESTED NORMAL IAW 21-61-00.Nov 15, 2013 · N586AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013101096159Regulator · failedBLEED DUCT SPLIT 3500, FT L-45, PSI R-20, PSI N1 87.1, 18000 FT L-43 PSI R-20 PSI N1 98.0, FL330 FT L-32, PSI R-24, PSI N1 83.5, FL340 FT L-40 PSI R-22, PSI N1 85.2, TOD L-20 PSI R-20 PSI N1 38, 12000 FT L-45 PSI R-22, PSI N1 81, 18000 FT L-24 PSI R-24 PSI N1 Oct 10, 2013 · N586AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013100296095Wire Harness · brokenLEFT ENGINE CORE FIRE DETECTOR HARNESS (MW0326) HAS 2 BROKEN TERMINALS AT RT UPPER TERMINAL. ACFT GROUNDED. REPLACED MW0326 FIRE DETECTOR HARNESS FOR LT ENGINE. OPS TEST PASSES, REF AMM 26-11-02/401.Oct 2, 2013 · N586AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2013100196085Cover · unsecureR1 EXIT SIGN COVER FALLS OFF. ACFT GROUNDED. R & R R1 EXIT SIGN IAW AMM 33-27-00.Oct 1, 2013 · N586AS · Boeing 737890 · Emergency LightingSDR ASAA2013091695989Autopilot Sys · malfunctionedB- AUTOPILOT DISENGAGED DURING CRUISE FLIGHT, FOR NO APPARENT REASON. ENGAGED B- AUTOPILOT AND SYS WORKED NORMALLY FOR REMAINDER OF FLIGHT. ACFT GROUNDED. CONFIRMED DFCS LOGGED FAULT 22-11607 MCP FAULT ON AFFECTED LEG. PERFORMED FIM TASK 22-11 TASK 817. CHASep 16, 2013 · N586AS · Boeing 737890 · Autopilot SystemSDR ASAA2013090195912Autothrottle Sys · malfunctionedAUTOTHROTTLES WILL NOT STAY ENGAGED. ACFT GROUNDED. RESET SYS, GROUND FUNCTIONAL TEST GOOD IAW AMM 22-31-00-710-810 AND 22-31-00-710-802, NO HISTORY LAST 90 DAYS.Sep 1, 2013 · N586AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013082895896Warning Message · illuminatedFMS DISAGREE ON GROUND. ACFT GROUNDED. QRH FOLLOWED, FMC RESTORED.Aug 28, 2013 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013081995845Battery Pack · no testEMERGENCY LIGHTING BATTERY PACKS M1670 AND M1671 FAILED DEEP CYCLE TEST. ACFT GROUNDED. REPLACED M1670 AND M1671 EMERGENCY LIGHTING BATTERY PACKS REF MM33-51-06. OPS NORMAL.Aug 19, 2013 · N586AS · Boeing 737890 · Emergency LightingSDR ASAA2013081995844Fmc · false indicationFMC DISAGREE. ACFT GROUNDED. QRH FOLLOWED. FMC RESTORED.Aug 19, 2013 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013080995774Warning Message · false activationFMC DISAGREE CAUTION AND SCRATCH PAD MESSAGE ILLUMINATED DURING TAXI. ACFT GROUNDED. FOLLOWED QRH PROCEDURE. LIGHTS AND MESSAGE DEACTIVATED. FMC OPS NORMAL.Aug 9, 2013 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013080395729Control Panel · failedTHE MODE CONTROL PANEL AUTO PILOT CMD FOR AN AUTO PILOT SWITCH LIGHT ARE INOP. ACFT GROUNDED. REPLACED DFCS MCP IAW AMM REF 22-11-34-000-801/22-11-34-400-801. OPS CKS GOOD IAW AMM REF TASK 22-11-34-740-801. PERFORMED ADDITIONAL MINIMUM TESTS TO MAINTAIN ACAug 3, 2013 · N586AS · Boeing 737890 · Autopilot SystemSDR ASAA2013071395585Fmc · unknownFMC DISAGREE DISPLAYED DURING TAXI. ACFT GROUNDED. FOLLOWED QRH PROCEDURE AND FMC DISAGREE WAS CLEARED.Jul 13, 2013 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013070595479Fmc · malfunctionedCAPTAIN`S FLAG - RAN QRH, SINGLE FMC OPS, RT FMC OPS, F/O GOT FLAG ABOUT 10 MIN LATER. A/T LIM FLAG. NO SPEEDS ON TAPE. ACFT GROUNDED. PERFORMED FMC BITE CHECK, NO FAULTS NOTED. REF FIM TASK 34-61-801. REMOVED NR 1 FMC COMPUTER. INSPECTED PINS. NO DEFECTJul 5, 2013 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013060895041Transceiver · failedPWS FAIL ON BOTH ND. ACFT GROUNDED. WEATHER RADAR FAILED ILLUMINATED ON BOTH ND WHILE ENROUTE. REPLACED WEATHER TRANCEIVER, REF AMM 34-43-41. GROUND VERIFICATION SUCCESSFUL.Jun 8, 2013 · N586AS · Boeing 737890 · Weather Radar SystemSDR ASAA2013060294955Lens · dislodgedOVERHEAD EXIT SIGN COVER AT EMERGENCY EXIT ROWS FELL OFF. ACFT GROUNDED. REINSTALLED EXIT SIGN COVER.Jun 2, 2013 · N586AS · Boeing 737890 · Emergency LightingSDR ASAA2013030894113Indicator · activatedAPU OIL FILTER DELTA P INDICATOR HAS EXTENDED. R & R APU OIL FILTER REF MM-49-91-13. RESET DELTA P INDICATOR AND LEAK CHECK GOOD. PERFORMED TASK MM 49-91-13-600-801. INSPECTED MAGNETIC DRAIN PLUG, NO METAL FOUND.Mar 8, 2013 · N586AS · Boeing 737890 · APU Oil SystemSDR ASAA2013022694000Fuel Cell · contaminatedAT THE GATE IN OAK BOTH FUEL TANKS NR 1 & NR 2 READ 8.54 (FULL). DURING CLIMB NR 2 TANK INDICATED 8.18 (DROP OF APPROX 400 LBS) WHILE STILL BURNING FROM CENTER TANK. IMMEDIATELY UPON LEVEL OFF AT CRUISE ALT NR 2 TANK QTY STEADILY INCREASED TO 8.66. NR 1 FUELFeb 26, 2013 · N586AS · Boeing 737890 · Fuel StorageSDR ASAA2013022593992Control Valve · failedDURING CRUISE PNEUMATIC DUCT PRESSURE NEEDLE SPLIT WAS INTERMITTENTLY 25PSI ( LT 45 PSI & RT 20 PSI ). AT OTHER TIMES IT WAS AS LITTLE AS 10 PSI DIFFERENTIAL. ACCOMPLISHED NR 2 ENGINE BLEED AIR SYS HEALTH CHECK IAW T/C NG-36WC-00001. PRECOOLER CONTROL VALVE Feb 25, 2013 · N586AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013022593991Fuel Cell · contaminatedDURING CRUISE, WHILE STILL BURNING FROM CENTER TANK, RT WING TANK WAS NOTICED TO BE APPROX 400 LBS HIGHER THAN PREVIOUS READING PRIOR TO DEPARTING & AT CRUISE, I.E; 8.5 INCREASED TO 8.9. A SHORT TIME LATER, SIMILARLY, THE LT WING TANK WENT FROM APPROX 8.5 TO 8Feb 25, 2013 · N586AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2013022593990Indicator · false indicationDURING PREFLIGHT OUR FUEL QTY INDICATION WAS 38.1. 10 MINUTES LATER GETTING READY TO PUSHBACK FUEL INDICATION 37.6 (MINIMUM). APU HAD BEEN RUNNING ONLY 10 MINUTES, LT WING TANK 8.55, CENTER 20.88, RT WING TANK 8.16. PERFORMED OPS TEST OF FQIS SYS, REF AMM 28Feb 25, 2013 · N586AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2013021993952Shutoff Valve · failedAFTER DEPARTURE, DUCT PRESSURE INDICATED 55 PSI IN LT DUCT, 22PSI IN RT DUCT, GOT BETTER AS FLIGHT CONTINUED. REF MM 36-11-00-700-804, FOUND PRSOV BAD. REPLACED PRSOV REF MM 36-11-04-400-801. LEAK & OPS CHECKED GOOD. ACCOMPLISHED ENGINE BLEED AIR CROSSOVEFeb 19, 2013 · N586AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013020593831Warning Light · false activationDURING TAKE OFF WITH TOGO 90N1 BOTH EEC LIGHTS CAME ON. LOW SPEED ABORT OF ABOUT 50 KNOTS. RETURNED TO GATE. PERFORMED EEC BITE PROCEDURE FOR NR 1 & 2 ENGINES IAW FIM 73-00 TASK 801, NO FAULTS NOTED. ACCOMPLISHED FIM 73-05, TASK 811, NO DEFECTS FOUND. ACCFeb 5, 2013 · N586AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2013011193657Static Inverter · faultedELECTRIC LIGHT ILLUMINATED ON ELECTRICAL OVERHEAD PANEL. BITE TEST OF PANEL SHOWS FAULT STATIC INVERTER. R & R STATIC INVERTER REF. MM 24-34-21. TESTS OK. CLEARED FAULT AND TESTS OK REF 24-31-801.Jan 11, 2013 · N586AS · Boeing 737890 · DC Generating SystemSDR ASAA2012120793419Warning Light · false activationON TAXI OUT, FMC DISAGREE MESSAGE ON FMC. FOLLOWED QRH AND FMC DISAGREE DID NOT REAPPEAR.Dec 7, 2012 · N586AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012120593408Control Unit · faultedELEC LIGHT ILLUMINATED. SPCU FAULT DURING BITE. REPLACED SPCU IAW AMM 24-34-11. OPS CKD NORMAL.Dec 5, 2012 · N586AS · Boeing 737890 · DC Generating SystemSDR ASAA2012111393296Autothrottle Sys · malfunctionedDURING CRUISE FLIGHT, THE THRUST MODE DISPLAY INDICATED A/T LIMIT IN A WHITE BOX. DURING DESCENT, THE DISPLAY BECAME NORMAL GREEN CRUISE AS SOON AS THE A/T MODE CHANGED TO ARM. DURING LEVEL OFF, THE TMD AGAIN SWITCHED TO WHITE A/T LIMIT. ACCOMPLISHED FIM TASNov 13, 2012 · N586AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012110393249Apu · failedDURING MX TROUBLESHOOTING, CSS FAILED WITH FAULT LIGHT. R & R APU . ACCOMPLISHED APU START AND OPERATION IAW 49-11-00-860-801. NO LEAKS NOTED. APU OPS TESTED GOOD IAW AMM 49-11-00-701-801.Nov 3, 2012 · N586AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2012102893212Manifold · inoperativeAPU FAULT LIGHT ILLUMINATED DURING IN-FLIGHT START. EXTINGUISHED AFTER 5 MINUTES. SECOND ATTEMPT SUCCESSFUL. R & R PRIMARY FUEL MANIFOLD IAW MM 49-31-16, LEAK CHECKED GOOD. R & R INLET TEMP SENSOR IAW MM 49-61-31. APU OPS CHECKED GOOD.Oct 28, 2012 · N586AS · Boeing 737890 · APU Engine Fuel and Control
Back to N586AS