N587AS

Service difficulty reports · 482

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 = 'N587AS' 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 ASAA2014070308442Warning Light · false activationDURING CRUISE FLIGHT, THE FMC P/RST LIGHT ILLUMINATED ALONG WITH VTK ON CAPTAINS ND. PERFORMED FMC FAIL CHECKLIST IN QRH AND DETERMINED THAT THE LT FMC FAILED. BEARING/DISTANCE INFORMATION FOR LT FMC DID NOT RETURN. CONTINUED WITH FMC SWITCH BOTH ON "RIGHT". Jul 3, 2014 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014062708374Warning Message · illuminatedELECTRICAL LIGHT ILLUMINATED ON THE OVERHEAD PANEL AMP METER & VOLT. MASTER CAUTION ON 6 PACK & OVERHEAD. ACFT GROUNDED. ACCOMPLISHED FIM 24-31-00-810-801. SPCU INOPERATIVE FAULT STORED. RAN FIM 24-34 TASK 802. FAULT CLEARED NO HISTORY. GROUND VERIFICATJun 27, 2014 · N587AS · Boeing 737890 · Electrical Power SystemSDR ASAA2014052907986Warning Light · false activationRIGHT ENGINE "COWL VALVE OPEN" LIGHT STAYED ILLUMINATED AFTER ANTI-ICE WAS TURNED OFF. ACFT GROUNDED. RAN NR 2 RT ENG AND PERFORMED ENG COWL ANTI-ICE OPS TEST IAW AMM 30-21-00-710-80. ALL TESTS NORMAL. NO FAULTS FOUND.May 29, 2014 · N587AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2014050907723Oil Cooler · leakingAPU HAS A HISTORY OF OIL SERVICING CURRENT OIL CONSUMPTION IS HIGHER THAN EXPECTED GROUNDED. C/W FIM TASK 49-95-00-810-801. FOUND APU TO BE LEAKING FROM AFT DRAIN. FOUND OIL COOLER LEAKING ON SHUTDOWN. REPLACED THE APU OIL COOLER, REF AMM 49-91-41/401. NOMay 9, 2014 · N587AS · Boeing 737890 · APU Oil SystemSDR ASAA2014033107379Control Panel · malfunctionedMODE CONTROL PANEL IS BLANK. ACFT GROUNDED. CYCLED MCP DC1 AND DC2 CIRCUIT BREAKERS. MCP RETURNED TO NORMAL. NO HISTORY. MODE CONTROL PANEL BITES NORMAL IAW GRP 32-22-11-34/501. LAND VERIFY TESTS NORMAL BITE GRP 49 22-11-00/201. HGS SENSOR TEST NORMAL REMar 31, 2014 · N587AS · Boeing 737890 · Autopilot SystemSDR ASAA2014032307281Lamp · inoperativeEMERGENCY LIGHT EXTERIOR SLIDE LIGHT ADJACENT TO LT FORWARD OVERWING EXIT IS INOPERATIVE. ACFT GROUNDED. REPLACED LAMP AND TESTED L1210 OVERWING ESCAPE LIGHT IAW MM 33-51-04-960-801. OPS NORMAL.Mar 23, 2014 · N587AS · Boeing 737890 · Emergency LightingSDR ASAA2014022106936Actuator · faultedLEFT PACK ANNUNCIATION ON MASTER CAUTION RECALL DURING DECENT. ANNUNCIATION EXTINGUISHED ON MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISH PACK - ZONE TEMP. CONTROLLER BITE TEST, NR 1 CONTROLLER SHOWS FAULT FOR LT RAM AIR ACTUATOR IAW MM 21-61-00-700-806-Feb 21, 2014 · N587AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014021906918Lens · crackedLAV G LOWER EMERGENCY LIGHT LENS, CRACKED. ACFT GROUNDED.Feb 19, 2014 · N587AS · Boeing 737890 · Emergency LightingSDR ASAA2014021906914Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. PERFORMED RESET ON CPC NR 1 AND RAN PRESSURIZATION SYS GROUND TEST WITH NO FURTHER FAULTS NOTED IAW AMM 21-31-00-700-802.Feb 19, 2014 · N587AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014021706859Fuse · failedBOTH OVERWING FWD LOWER EXIT LIGHTS ARE INOPERATIVE. ACFT GROUNDED. R & R FUSES ON BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD IAW AMM 33-51-06.Feb 17, 2014 · N587AS · Boeing 737890 · Emergency LightingSDR ASAA2014012406773Seat Track · crackedSTA 727B, SEAT TRACK, LBL 45.50 INBD FLANGE IS CRACKED AT FASTENER HOLE. ACFT GROUNDED. REPAIRED IAW REO G17114, REV A AND EA SB737-53-1296, NG-104.Jan 24, 2014 · N587AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2014012406772Seat Track · crackedBS 727B, SEAT TRACK RBL 45.50 INBD AND OTBD FLANGES ARE CRACKED AT FASTENER HOLE. ACFT GROUNDED. REPAIRED IAW REO G17114, REV A AND EA SB737-53-1296-NG-104.Jan 24, 2014 · N587AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2014010912365Valve · malfunctionedNR 2 ENGINE SPAR VALVE CLOSED LIGHT ILLUMINATED. ENG INDICATES NORMAL. ACFT GROUNDED. GROUND VERIFICATION CHECK PASSES. ACCOMPLISHED MMEL 28-22 RESTORATION FUEL SPAR VALVE CLOSED LIGHT OPS NORMAL. ACCOMPLISHED FIM 28-22, TASK 812 & FIM 28-22, TASK 810 BOTH Jan 9, 2014 · N587AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2014010112294Transmitter · faultedTWICE ON ILS, LOC AND G/S CAPTURED, ACFT NOSED OR PITCHED DOWN EXCESSIVELY. VISUAL CHECK END OF RUNWAY G/S TRANSMITTER WAS NOT BLOCKED, AUTOPILOT. ACFT GROUNDED. C REW VERBAL INFO -A/P DID NOT DISCONNECT ON EITHER TIME. CREW DISCONNECTED A/P. NO FLT FAULTJan 1, 2014 · N587AS · Boeing 737890 · Autopilot SystemSDR ASAA2013112696549Transceiver · malfunctionedHF NR 1 RADIO DOES NOT TRANSMIT. AIRCRAFT GROUNDED. ACCOMPLISHED FIM 23-11 TASK 806. MADE SUCCESSFUL HF NR 1 PLANE TO PLANE AND TRANSMIT AND RECEIVE COMMUNICATIONS FROM BOTH CAPT AND F/O POSITIONS. OPS NORMAL. HF 1 TRANSCEIVER BITE CHECKED NORMAL REF FIM 2Nov 26, 2013 · N587AS · Boeing 737890 · HF Communications SystemSDR ASAA2013112196486Engine · hung startNR 2 ENGINE WOULD NOT START WITH IGNITION IN LT OR RT POSITION. EGT WOULD GO NO HIGHER THAN 180 DEG. HUNG START. ACFT GROUNDED. ACCOMPLISHED FIM TASK 73-00-801, NO FAULTS FOUND. IAW FIM TASK 80-05-806 PERFORMED GVI OF NR 2 ENGINE, NO DEFECTS NOTED. STANov 21, 2013 · N587AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2013110496297Warning Message · false activationAPU BITE TEST INOPERATIVE, CHECK APU OR ECU INTERFACE MESSAGE DISPLAYED ON CDU. ACFT GROUNDED. CYCLED ACFT POWER, APU BITE BACK TO NORMAL. ACCOMPLISHED APU CURRENT STATUS CHECK & NO FAULTS IN HISTORY. CHECKED NORMAL IAW 49-61-00. NO HISTORY 30 DAYS & SEAMNov 4, 2013 · N587AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2013092696072Battery Pack · no testDURING T/C 7823307, EMERGENCY LIGHT BATTERY PACKS FAILED OPS CHECK. ACFT GROUNDED. R & R BATTERY PACK IAW MM 33-51-06.Sep 26, 2013 · N587AS · Boeing 737890 · Emergency LightingSDR ASAA2013081795822Warning Light · false activationON RECALL, CONT CABIN ZONE TEMP LIGHT ILLUMIINATED. RAN QRC AND LIGHT STAYED ON. ACFT GROUNDED. FLT DECK TRIM VALVE FAULT NR 2 ZONE TEMP CONTROLLER. RESET AND TESTS NORMAL IAW FIM 21-61, TASK 801. GROUND VERIFICATION SUCCESSFUL.Aug 17, 2013 · N587AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013080795753Circuit Breaker · trippedAFCS SYS A ENGAGE INTERLINK CIRCUIT BREAKER FOUND TRIPPED. ACFT GROUNDED.Aug 7, 2013 · N587AS · Boeing 737890 · Autopilot SystemSDR ASAA2013061595114Spinner · damagedNR 1 ENGINE INLET SPINNER FRONT CONE MISSING PAINT AND ANODIZED COATING. ACFT GROUNDED. NR 1 ENGINE R & R INLET SPINNER FRONT CONE IAW TC 78472002.Jun 15, 2013 · N587AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2013061595113Shim · wornNR 1 ENGINE, TWENTY FOUR FAN BLADE SHIMS WORN. ACFT GROUNDED. R & R SHIMS IAW T/C 78472002.Jun 15, 2013 · N587AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2013061495103Unknown · unknownFMC DISAGREE. ACFT GROUNDED. ACCOMPLISHED FMC DISAGREE CHECKLIST 11.2. OPS NORMAL.Jun 14, 2013 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013061395115Switch · failedRT ENG VALVE LT - CAME ON DURING FLIGHT (BRIGHT). ACFT GROUNDED. RAN NR2 ENG, ENG VALVE LT FLICKERED THEN WENT OUT, RANG OUT SW DP1207 ON HMU. FOUND HPSOV SW TO BE BAD WDM 76-21-21. REPLACED NR 2 ENG HPSOV SW REF MM 73-21-09. OPS CK GOOD GROUND VERIFICATIJun 13, 2013 · N587AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2013060895038Terminal · brokenOVERHEAT DETECTOR FAULT LIGHT ENGINE NR 2. ACFT GROUNDED. REPAIRED BROKEN TERMINAL MW0326. REF SWPM20-30-11, WDM26-11-11, AMM 26-11-00. GROUND VERIFICATION SUCCESSFUL.Jun 8, 2013 · N587AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2013050994779Sliding Window · dislodgedFOS NR 2 WINDOW FELL OFF WHEN TRYING TO CLOSE. ACFT GROUNDED. REINSTALLED NR 2 FOS SLIDING WINDOW REF MM 56-12-11. OPS NORMAL, OK FOR SERVICE.May 9, 2013 · N587AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA2013050894748Warning Light · false activationZONE TEMP CONT CAB ILLUMINATED ON RECALL. ACFT GROUNDED. TESTED RT PACK/ZONE CONTROLLER IAW FIM 21-62, TASK 801. FOUND A FAULT LIGHT FOR THE CONTROL CABIN TEMP VALVE. RESET PACK/ZONE CONTROLLER AND RETESTED 3 TIMES. NO FURTHER FAULT INDICATED. ALSO, DID NMay 8, 2013 · N587AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013040894397Hinge · lack of lubeRIGHT PACK AND MASTER CAUTION LIGHTS ILLUMINATED ON CLIMBOUT (APPROX 11,000). PERFORMED QRH PROCEDURE - SELECTED WARMER TEMP. PACK RESET OK. NO FAULTS LOGGED ON ZONE TEMP CONT, HOWEVER NOTICED RT RAM AIR DEFLECTOR DOOR REMAINS DEPLOYED DURING CYCLE/TEST. FApr 8, 2013 · N587AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013030794107A/C Pack · malfunctionedON CLIMB OUT, RT PACK TRIPPED, RESET PACK IAW QRH. RT PACK TRIPPED A SECOND TIME AND REMAINED OFF FOR THE REMAINDER OF FLIGHT IAW QRH. UNABLE TO DUPLICATE.Mar 7, 2013 · N587AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013030694114Fuel Cell · contaminatedON DESCENT AT 6000 FT, THE IMBALANCE LIGHT ILLUMINATED. FUEL STATE WAS 7.62 LT MAIN, 5.56 CTR, 8.62 RT MAIN. CROSSFEED TO BALANCE WORKED. NO LOW PRESSURE BOOST PUMP LIGHTS ILLUMINATED. REMOVED ICE AND RESIDUAL WATER FROM NR 2 FUEL TANK. R & R NR 2 F/Q Mar 6, 2013 · N587AS · Boeing 737890 · Fuel StorageSDR ASAA2013030294045Hmu · unstableWHILE CLIMBING THROUGH HIGH 20S AT 3201/.792 COST INDEX 45, FUEL HAD DEVELOPED A 600 LBS IMBALANCE WITH LT SIDE HEAVY. TURNED LT CENTER PUMP OFF, CROSSFEED CLOSED AND ALL OTHER BOOST PUMPS ON. ABOUT 4 MINUTES LATER AT ABOUT 33,000 LEFT ENGINE VARIED AT MODERMar 2, 2013 · N587AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA2013020693839Control Panel · crackedRADAR CONTROL PANEL CRACKED AROUIND IDNT BUTTON. REPLACED RADAR CONTROL PANEL, REF M/M 34-43-91. TESTS NORMAL.Feb 6, 2013 · N587AS · Boeing 737890 · Weather Radar SystemSDR ASAA2013010793631Warning Light · false activationON CLIMBOUT, RT PACK LIGHT ILLUMINATED. FOLLOWED QRH AND LIGHT RESET WITH THE TRIP RESET BUTTON. OPERATED NORMALLY THEREAFTER. ACCOMPLISHED FIM TASK 21-52, TASK 821. PACK OPERATES NORMAL. PACK OPERATED NORMALLY THROUGHOUT FLIGHT, SUCCESFUL GROUND VERIFICJan 7, 2013 · N587AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013010493617Unknown · unknownWEATHER RADAR SPOKING IN ALL MODES. ACCOMPLISHED WEATHER RADAR SYS, OPS TEST. NO DEFECT. GROUND VERIFICATION SUCCESSFUL. REF AMM 34-43-00-710-802-001.Jan 4, 2013 · N587AS · Boeing 737890 · Weather Radar SystemSDR ASAA2012111893314Warning Light · false activationON SHUTDOWN, AMBER SPEED TRIM FAIL ANNUNCIATOR ILLUMINATED. AFTER CREW REALIGNED IRUS, SPEED TRIM LIGHT WENT OFF. PERFROMED DFCS BITE IAW SIM 22-11, TASK 801 AND FIM 22-13, TASK 817. NO DEFECTS NOTED. PERFORMED STAB/SPEED TRIM BITE TEST 14 WITH NO FAULTS FONov 18, 2012 · N587AS · Boeing 737890 · Auto Flight SystemSDR ASAA2012102593192Warning Light · false activationAFTER STARTING TAXI RECEIVED FMC DISAGREE LIGHT. PERFORMED QRH CHECK LIST. FAULT CLEARED.Oct 25, 2012 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012091592884Warning Light · false activationAUTOLAND APPROACH WARNING IN FLARE & LINED UP 20 TO THE RT OF CENTERLINE. HEADINGS FFR SHOWED RADAR ALTIMETER INVALID FOR LAST FLT, DFCS RECORDED NO FAULT. PERFORMED LAND VERIFY AND HGS SYS TEST REF MM 22-00-01-730-801 ALL TEST PASSED.Sep 1, 2012 · N587AS · Boeing 737890 · Autopilot SystemSDR ASAA2012090192805Fmc · false activationFMC DISAGREE ANNUNCIATED. ACFT GROUNDED. PULLED AND RESET FMSC CMPTR 1 &2 CIRCUIT BREAKERS IAW QRH FMC DISAGREE CHECKLIST PROCEDURE.Sep 1, 2012 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012072992631Warning Light · false activationFMC DISAGREE MESSAGE DISPLAYED. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE AND FMC DISAGREE MESSAGE NO LONGER DISPLAYED. BOTH SYSTEMS OPS CHECKED GOOD IAW AMM 34-61-00.Jul 2, 2012 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012071692552Warning Message · false activationON TAXI OUT GOT FMC DISAGREE MESSAGE. ACFT GROUNDED. RESET SUCCESSFUL IAW FMC/QRH PROCEDURES. OPS NORMAL.Jul 1, 2012 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511665Warning Message · illuminatedFMC DISAGREE MESSAGE DISPLAYED AFTER ENGINE START. QRH PROCEDURE ACCOMPLISHED. MESSAGE CLEARED.Jun 9, 2012 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511670Lens · dislodgedOVERHEAD EXIT SIGN NEAR ROW 16 FELL OFF. FOUND EXIT LENS OFF SECURED LENS BY SNAPPING ONTO RETAINING TABS . TABS FULLY ENGAGED IN HOLES. LIGHT OPS CHECKED GOOD.Jun 7, 2012 · N587AS · Boeing 737890 · Emergency LightingSDR ASAA2012062792438Idg · failedNR 2 CSD DRIVE LIGHT ILLUMINATED WHILE AT GATE AND NR 1 CSD DRIVE LIGHT NOT ILLUMINATED. CONFIRMED NR 1 ENGINE DRIVE LIGHT DOES NOT ILLUMINATE WITH ENGINE OFF. LIGHT DOES PRESS TO TEST. CHARGE PRESSURE SWITCH IN IDG IS READING OPEN THROUGH PINS 5/6 OF DP120Jun 2, 2012 · N587AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA12511622Actuator · failedSPAR VALVE CLOSED LIGHT ILLUMINATED BRIGHT BLUE. QRH PROCEDURE ACCOMPLISHED LIGHT REMAINS ON WITH START LEVER IN IDLE POSITION. SYS REPORTED IS NR 1 SIDE AND THERE WERE NO OTHER PROBLEMS NR1 ENGINE RAN FINE IAW PILOT PASS DOWN.) ACFT GROUNDED. WHEN ACCOMPLISJun 2, 2012 · N587AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA12511554Transceiver · failedRADAR TILT SEEMS TO SLOWLY DRIFT DOWN AFTER ABOUT 10 MINUTES OF USE. TILT UP HAS LITTLE EFFECT ON TOTALLY GREEN SCREEN IE +5 AT FL 380 IN CLEAR SCREEN. ALL GREEN TILT ON OR OFF WX T MAP NO CHANGE TURNING RADAR OFF FOR 5 MINS THEN ON. RADAR WILL WORK AGAIN BMay 13, 2012 · N587AS · Boeing 737890 · Weather Radar SystemSDR ASAA12511520Radar · malfunctionedWEATHER RADAR UNRELIABLE. WORKS NORMALLY FOR A WHILE THEN PAINTS SOLID GROUND CONTACT FOR 320 NM (IN RANGE REGARDLESS OF TILT POSITION) THEN CYCLES BACK TO NORMAL OPERATION. COULD NOT DUPLICATE. OPS CHECKED NORMAL AND GROUND CLUTTER SUPPERSSION TEST REF MM 34May 6, 2012 · N587AS · Boeing 737890 · Weather Radar SystemSDR ASAA12511522Warning Message · illuminatedAFTER PUSH BACK AND INITIAL TAXI, FMC DISAGREE ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. OPS NORMAL.May 6, 2012 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511499Track · lack of lubeL2 WINDOW HANDLE BINDS WHEN CLOSING. ACFT GROUNDED. CLEANED L2 WINDOW TRACKS IAW SOPM 20-30-03. LUBED L2 WINDOW TRACKS IAW NG AMM 12-25-81-600-801. OPS CHECK OF L2 WINDOW GOOD IAW AMM 56-12-11-710-803.May 2, 2012 · N587AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA12511498Arm · out of adjustR1 DOOR HANDLE BINDS WHEN CLOSING. ACFT GROUNDED. ADJUSTED GUIDE ARM IAW MM 52-41-00.May 2, 2012 · N587AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA12511484Skin · gougedFUSELAGE SKIN GOUGED BETWEEN STA 727G - 727F AT STRINGER 23 LEFT. ACFT GROUNDED. FOUND GOUGE TO BE OUT OF LIMITS IAW SRM 53-00-01. REMOVED AFT CARGO COMPARTMENT LT SIDEWALL PANEL IAW NG AMM 25-52-06-000-801. REMOVED DAMAGED AREA OF SKIN FABRICATED 1 EA REPAIMay 1, 2012 · N587AS · Boeing 737890 · Fuselage Main, Plate/Skin
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