N483AS

Service difficulty reports · 179

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 = 'N483AS' 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 ASAA2016112718844Warning Light · illuminatedRIGHT AIR CONDITIONING PACK LIGHT LIGHT ILLUMINATED. RAN QRH LIGHT WOULD NO RESET. ALSO WOULD NOT RESET WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED RIGHT PACK TEMP CONTROL BITE, IAW FIM 21-62 TASK 801, RIGHT PACK LOGGED TCV FAULT. PERFORMED FIM 21-62 Nov 27, 2016 · N483AS · Boeing 737990ER · Cabin Cooling SystemSDR ASAA2016111318653Warning Light · false activationDURING CLIMB OUT, RIGHT PACK LIGHT ILLUMINATED. THE PACK LIGHT EXTINGUISHED WHEN THE MASTER CAUTION SYSTEM IS RESET. ACFT GROUNDED. PERFORMED BITE TEST IAW FIM 21-53 TASK 810 AND OPS TEST IAW AMM 21-00-00. OPS CHECKED GOOD.Nov 13, 2016 · N483AS · Boeing 737990ER · Cabin Cooling SystemSDR ASAA2016101018258Eec · failedFLIGHT CREW REPORTS CDS FAULT DISPLAYED ON OUTBOARD DISPLAY UNITS. ACFT GROUNDED. DEU 1 & 2 CURRENT STATUS SHOWS FAULT 31-65030 EEC DATA DISAGREE. NR 2 ENGINE EEC RECENT FAULTS SHOWS CH B EEC DATA NOT AVAILABLE WITH FAULT CODE 73-10102 INTERNAL EEC FAULT. REMOct 10, 2016 · N483AS · Boeing 737990ER · Fuel Controlling SystemSDR ASAA2016081817763Sensor · failedAPU OIL AT CDU INDICATES LOW. ACFT GROUNDED. VERIFIED OIL LEVEL AT APU FULL, PERFORMED FIM 49-90, TASK 804. FOUND MESSAGE NR 49-91227. R & R OIL QTY SENSOR, REF AMM 49-94-11. NO FURTHER FAULTS OR DEFECTS NOTED, OPS CHECK NORMAL.Aug 18, 2016 · N483AS · Boeing 737990ER · APU Oil SystemSDR ASAA2016081717737Controller · failedON PRESSURIZATION PANEL AUTO FAIL AND ALTN LIGHT ILLUMINATED WITH SELECTOR KNOB IN AUTO POSITION. ACFT GROUNDED. R & R NR 2 CABIN PRESSURE CONTROLLER IAW AMM 21-31-01. OPS CHECKS GOOD IAW AMM 21-31-00-700-802.Aug 17, 2016 · N483AS · Boeing 737990ER · Cabin Pressure ControllerSDR ASAA2016080217595Transmitter · failedWHILE PERFORMING LWMP TRAINING, DFCS LIBRARY TEST NR 31 FAILS FOR CHANNEL B SPOILER POSITION SENSOR 9 AND DFCS SENSOR VALUES SHOWS NO INPUT TO FCC-B FROM SPOILER NR 9 POSITION SENSOR. ACFT GROUNDED. REF WDM 22-11-31-4 AT M930 SPOILER 9 POSITION SENSOR, SWAPPAug 2, 2016 · N483AS · Boeing 737990ER · Autopilot SystemSDR ASAA2016071217351Sensor · failedDURING CHECK, FOUND CDU APU OIL QUANTITY SAYS ADD OIL, APU SIGHT GLASS WAS FULL. ACFT GROUNDED. REMOVED AND REPLACED APU OIL LEVEL SENSOR, IAW AMM 49-94-11. OPS CHECKED GOOD. LEAK CHECKED GOOD.Jul 12, 2016 · N483AS · Boeing 737990ER · APU Oil SystemSDR ASAA2016062817191Autopilot Sys · malfunctionedAUTOPILOTS A & B WILL NOT ENGAGE. ACFT GROUNDED. DFCS CURRENT STATUS TEST SHOWED NO FAULTS. FLIGHT FAULT REVIEW SHOWS NO FAULTS. SHOOK OUT FLIGHT CONTROLS AND RAN LAND VERIFY TEST 3 SEPARATE TIMES WITH NO DISCREPANCIES NOTED. AUTOPILOT SYS ENGAGES AND OPSJun 28, 2016 · N483AS · Boeing 737990ER · Autopilot SystemSDR ASAA2016061917086Oil Cooler · failedIN FLIGHT, SOURCE OFF, GEN OFF BUS AND DRIVE LIGHT CAME ON SIMULTANEOUSLY, AT FL 350. CREW EXECUTED CHECKLIST, SOURCE OFF, 6.9 AND DRIVE, 6.3. WIRED GENERATOR DRIVE DISCONNECT SWITCH WAS BROKEN TO HOLD SWITCH IN, DISCONNECT, POSITION IAW 6.3. APU WAS STARTEJun 19, 2016 · N483AS · Boeing 737990ER · AC Generator-AlternatorSDR ASAA2016042916567Warning Light · false activationP-5 PANEL ELEC LIGHT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED FIM 24-34, TASK 802 AND 24-31, TASK 801. FAULT LIGHT RESET. INTERMITTENT FAULT. GROUND VERIFICATION TEST GOOD.Apr 29, 2016 · N483AS · Boeing 737990ER · DC Generating SystemSDR ASAA2016040716321Wire · burnedDURING TAXI, ELECTRIC LIGHT ILLUMINATED FOLLOWED BY CABIN LIGHTS FAILURE. ACFT GROUNDED. R & R R607, NO HELP. WHILE T/S USING SSM 24-51-11 PAGE 103, SHEET 2 FOUND BURNED TERMINAL RINGS AND WIRES ON B-PHASE. REMOVED POWER DISTRIBUTION PANEL P91 IAW AMM 24-2Apr 7, 2016 · N483AS · Boeing 737990ER · Electrical Power System WiringSDR ASAA2016040616260Wire · failedRIGHT PACK LIGHT ILLUMINATED ON RECALL, EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED BITE CHECK, REF AMM 21-61-00, OPS NORMAL. SUSPECT FAULTS CAUSED DUE TO P-91 WIRING FAILURE.Apr 6, 2016 · N483AS · Boeing 737990ER · Air Conditioning System WiringSDR ASAA2016032416087Control Panel · failedLEFT SIDE OF MCP PANEL BACKLIGHTING INOPERATIVE. ACFT GROUNDED. VERIFIED, ADJUSTING FACE PLATE DID NOT FIX ISSUE. R & R MODE CONTROL PANEL REF AMM 22-11-34. INSTALLATION TEST PASSED. ACCOMPLISHED ADDITIONAL TESTING DFCS LRU INTERFACE TEST FOR MCP NR 32, LMar 24, 2016 · N483AS · Boeing 737990ER · Autopilot SystemSDR ASAA2016031315892Converter · failedBURNED WIRE ODOR IN ELECTRONIC EQUIPMENT BAY. ACFT GROUNDED. CONDUCTED GVI OF ELECTRONIC EQUIPMENT BAY. ODOR APPEARS TO BE AT P91 OR APU START CONVERTER UNIT. OPENED P91 INSPECTED WIRES & CIRCUIT BREAKERS & RELAYS, FOUND NO DEFECTS. OPENED FLOOR PANEL TO INSMar 13, 2016 · N483AS · Boeing 737990ER · APU Start/Ignition SystemSDR ASAA2016022315644Circuit Breaker · trippedABORTED ENGINE NR 2 START. WITH 25 PERCENT N2 START LEVER WAS AT IDLE AND INITIAL FUEL FLOW WENT TO .2 AND THEN ROLLED BACK TO ZERO. SPAR VALVE CLOSED LIGHT ILLUMINATED AT THE SAME TIME. AT GATE NR 2 ENGINE LT IGNITION C/B WAS FOUND TRIPPED. ACFT GROUNDED. FFeb 23, 2016 · N483AS · Boeing 737990ER · Ignition Power SupplySDR ASAA2016012314967Warning Message · false activationFMC DISAGREE ON BOTH FMCS AT GATE. ACFT GROUNDED. PERFORMED QRH AND BOTH FMCS RESET.Jan 23, 2016 · N483AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2016010314628Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMC RESTORED NORMAL.Jan 3, 2016 · N483AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2015123114600Fmc · failedAT FL350 VTK ILLUMINATED ON NR 1 MAP DISPLAY AND BOTH FMC'S WENT BLANK THEN TO MENU. AFTER APPROXIMATELY 1 MINUTE SYS WENT BACK TO NORMAL AND OPERATED NORMALLY. ACFT GROUNDED. LEFT FMC FAULT LOGGED IN FLT, LEG 6 ONLY. ACCOMPLISHED LT FMC GROUND VERIFICATION TDec 31, 2015 · N483AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2015122014357Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMC DISAGREE NO LONGER DISPLAYED.Dec 20, 2015 · N483AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2015121614294Filter · dirtyF/A REPORTS ROWS 13 AND 14 HAVE NO AIR AIRVENTS, OVERHEAD WORKING AND AREA IS WARM. WE MOVED FORWARD CABIN CONTROL TO FULL COLD, SUPPLY DUCT SHOWING 10 DEGREE C. FWD PASSENGER CABIN SHOWING 20 DEGREE C. WE DIDN`T MOVE TRIM AIR TO OFF, IT STAYED ON. DUE TO CDec 16, 2015 · N483AS · Boeing 737990ER · Cabin Temperature Control SystemSDR ASAA2015102913570Transmitter · failedNR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED DURING TAXI IN. ACFT GROUNDED. PERFORMED ELECTRONIC ENGINE CONTROL BITE 73-00, TASK 801. RECENT HISTORY FAULT SHOWS FLTS X+1 W/79-31121 DUAL CHANNEL. MAINTENANCE MESSAGE OF OIL FILTER SIGNAL DISAGREE. OIL FILTOct 29, 2015 · N483AS · Boeing 737990ER · Engine Oil Distribution (Airframe Furnished)SDR ASAA2015101313496Start Valve · failedDURING START OF ENGINE NR 2, THE "START VALVE OPEN" REMAINED ILLUMINATED AFTER THE COMPLETION OF THE ENGINE START SEQUENCE. ALL ENGINE START PARAMETERS WERE NORMAL. ACFT GROUNDED. ELECTRONIC ENGINE CONTROL & DEU BITE GOOD WITH NO FAULTS LOGGED IAW FIM 80-07,Oct 13, 2015 · N483AS · Boeing 737990ER · Engine Start Valves/ControlsSDR ASAA2015101113470Transmitter · failedDURING TAXI OUT, LT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED ABOUT 10 SECS, THEN WENT OUT. LT ENGINE OIL PRESSURE 23-26, OIL TEMP WAS 76, OIL QTY 16-17. ACFT GROUNDED. PERFORMED ELECTRONIC ENGINE CONTROL BITE, MSG 79-31121, OIL FILTER SIGNAL DISAGREE. ACCOct 11, 2015 · N483AS · Boeing 737990ER · Turbine Engine Oil SystemSDR ASAA2015100713400Transmitter · failedNR 1 OIL FILTER BYPASS LIGHT ILLUMINATED AFTER LANDING. ACFT GROUNDED. ACCOMPLISHED FIM TASK 79-05, TASK 817, REPLACED OIL FILTER SCAVENGE CLOGGING TRANSMITTER, REF AMM 79-21-07. REPLACED SCAVANGE OIL FILTER IAW AMM 79-21-06. FOR PRECAUTIONARY MEASURE REPLAOct 7, 2015 · N483AS · Boeing 737990ER · Turbine Engine Oil SystemSDR ASAA2015100713399Warning Light · false activationNR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED ALONG WITH ENGINE NR 1 3-PACK FLASHING DURING TAXI OUT. ACFT GROUNDED. NR 1 ENGINE FMCS CDU SHOWS FAULT CODE 79-31121, THE OIL FILTER SIGNALS DISAGREE. ACCOMPLISHED FIM 79-05, TASK 817. REMOVED SCAVENGE OIL FOct 7, 2015 · N483AS · Boeing 737990ER · Turbine Engine Oil SystemSDR ASAA2015100613370Fmc · failedLEFT FMC FAILURE. ACFT GROUNDED. REPLACED LT FMC IAW MM 34-61-02-400-801. SOFTWARE CROSS LOADED FROM RT FMC. FMC OPS CHECKED NORMAL, IAW MM 34-61-00.Oct 6, 2015 · N483AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2015092313178Warning Message · false activationFMC DISAGREE. ACFT GROUNDED. FOLLOWED QRH, RESET, FMC OPS NORMAL REF FIM 34-61, TASK 835.Sep 23, 2015 · N483AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2015092313177Warning Message · false activationFMC DISAGREE MESSAGE DISPLAYED ON THE GROUND. ACFT GROUNDED. ACCOMPLISHED QRH. OPS NORMAL. INTERMITTENT FAULT REF MM 34-61.Sep 23, 2015 · N483AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2015092013136Warning Message · false activationFMC DISAGREE LIGHT. ACFT GROUNDED. FOLLOWED QRH, RESET.Sep 20, 2015 · N483AS · Boeing 737990ER · Flight Management Computing Hardware System
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