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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASAA2012102593196Flow Divider · failedCSS FAILED WITH FAULT LIGHT AND AUTO SHUTDOWN AT FL 360. FAULT LIGHT EXTINGUISHED W/IN 5 MINUTES IAW START ATTEMPT. R & R FUEL FLOW DIVIDER AND SOLENOID VALVE REF AMM 49-31-15. OPS CHECK NORMAL.SDR ASAA2012102393168Apu · malfunctionedAPU FAILED FIRST START AT FL 320, WITH FAULT LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURE. FAULT LIGHT EXTINGUISHED AND SECOND APU START SUCCESSFUL. NOTE APU EGT HUNG AT APPROX 450 DEGREES WITH FAULT LIGHT ON FIRST ATTEMPT. TROUBLESHOT CDU - FOUND FAULT 49-41SDR ASAA2012102393167Valve · openRT COWL VALVE OPEN LIGHT REMAINED IN THE BRIGHT BLUE STATUS WITH THE SWITCH IN THE ON POSITION. R & R NR 2 ENGINE COWL VALVE IAW MM 30-21-11. RAN ENGINE, COWL VALVE OPERATES NORMAL.SDR ASAA2012092992966Control Panel · failedON CLIMBOUT HEADING SELECTOR & BUG INTERMITTENTLY FROZE (BUG DISPLAY ON PFD/ND WOULD NOT MOVE) DURING CRUISE HDG WINDOW WOULD INTERMITTENTLY MOVE ON ITS ON - WITHOUT PILOT INPUT (BUG DISPLAY ON PFD/ND WOULD FOLLOW HEADING WINDOW DISPLAY. ACFT GROUNDED. R & RSDR ASAA2012092892965Unknown · unknownHEADING BUG LOCKED ON HEADING 110 AIRBORNE. CYCLED BOTH F/D AND TURNED OFF AUTOPILOT WITH NO CHANGE ALT AND SPEED BUGS WORKED NORMAL. AFTER LANDING HEADING NOW SHOWS 117. ACFT GROUNDED. OPS CHECKED MODE CONTROL PANEL HEADING SELECTOR KNOB IAW AMM 22-11-34,SDR ASAA2012092092927Fuel Nozzle · faultedCOLD SOAK START(CSS) WAS INCOMPLETE. FIRST START ATTEMP FL390. FAULT LIGHT ILLUMINATED, WENT OUT AFTER 4 MINUTES. SECOND START ATTEMPT FL36.3 UNSUCCESSFUL WITH FAULT LIGHT ILLUMINATION. WENT OUT AT 4-5 MINUTE MARK. BUT ACFT HAD DESCENDED BELOW FL290. SUBSSDR ASAA2012080492660Connector · dirtyCSS FAILED WITH FAULT AUTO SHUTDOWN. FAULT LIGHT WENT OUT AFTER 3 MINUTES. FOUND FAULT CODE 49-41010 THAT WAS 2 STARTS OLD UNDER FAULT HISTORY. UNDER CURRENT STATUS THERE WAS NO FAILURES. STARTED APU 2 TIMES & NO DISCREPANCIES NOTED. ACCOMPLISHED FIM TASKSDR ASAA2012080392663Pressure Switch · failedRIGHT FUEL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT, ALL ENGINE PERIMETERS NORMAL. QRH 12.3 COMPLETED. ACCOMPLISHED FAULT ISOLATION PROCEDURE, DIFFERENTIAL PRESSURE SWITCH FAILED IN CLOGGED POSITION. R & R NR 2 ENG FUEL DIFFERENTIAL PRESSURE SWITCH REF AMSDR ASAA2012082392768Control Valve · failedLEFT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. R & R LT PACK TEMP CONTROL VALVE IAW AMM 21-51-10. OPS CHECKED NORMAL. LEAK CHECKED OK.SDR ASAA2012081792732Igniter · failedFIRST CSS OF APU RESULTED IN FAILED START AND APU FAULT LIGHT. ALTITUDE OF 37,000. FAULT LIGHT WENT OUT AFTER QRH PROCEDURE AND 3 MIN. SECOND CCS AT FL 350 WAS SUCCESSFUL. PERFORMED APU BITE TEST - FOUND CODE 49-41010 NO ACCELLERATION SHUTDOWN. PERFORMED SDR ASAA2012081192693Fuel Control · malfunctionedCREW REPORTED VIA ACARS MSG THAT APU WOULD NOT START AND FAULT LIGHT ILLUMINATED AT 33,000. APU STARTED ON 3RD ATTEMPT. ACFT GROUNDED. APU BITE SHOWS NO CURRENT FAULTS & MSG 49-41010 (NO ACCELERATION) FOR THE PREVIOUS 2 FAILED STARTS. (COLD SOAKED). APU BITSDR ASAA2012070792499Computer · failedFIRST OFFICER FMC FAIL FOLLOWED CHECKLIST UNABLE TO RESTORE RNP REMAINED 10.0 FOLLOWED BY 2.0 ANP 0.02. - VERIFIED DEFECT, R & R NR 2 FMC REF MM 34-61-02, OPS CK NORMAL.SDR ASAA2012070492469Sensor · malfunctionedNR 2 ENGINE VIBRATION INDICATION INTERMITTENTLY BLANKS NO INDICATION. ACFT GROUNDED. AVM LOGGED MULTIPLE N2 RPM SIGNAL LOSS NR 1 AND NR 2 ALSO LOGGED MULTIPLE ENG 2 N2 SIGNAL LOSS MAINT MSG 31-63160. R & R N2 SENSOR REF AMM 77-11-02, LEAK AND OPS CHECKED GOOSDR ASAA12511672Warning Light · illuminatedFMC DISAGREE. ACCOMPLISHED QRH PROCEDURE. OPS NORMAL.SDR ASAA2012061592340Apu · odorVERY STRONG DIRTY SOCK ODOR IN DESCENT. STARTED WHEN BELOW 10,000. R & R APU IAW T/C 78349010. OPS AND LEAK CHECK GOOD.SDR ASAA12511673Sensor · intermittentNR 2 VIBRATION INDICATION MISSING INTERMITTENTLY AFTER ENGINE START. GROUNDED, RAN NR 2 ENG NR 2 N2 AND NR 2 VIBE INDICATIONS WENT BLANK. VIBE MONITOR FAULTED N2 TACH LOSS NR 2 DEFAULTED 31-63160, NR 2 ENG RPM INVALID. REPLACED N2 SPEED SENSOR NR 2 ENG REF SDR ASAA2012062192402Warning Light · false activationFMC DISAGREE AT THE END OF RUNWAY. QRH PROCEDURE ACCOMPLISHED. OPS NORMAL.SDR ASAA2012062092388Warning Light · false activationBLUE MAINT LIGHT FOR APU ILLUMINATED AFTER APU START AND REMAINED ON. ACFT GROUNDED. CHECKED APU OIL QUANITY IAW AMM 12-13-31. OIL QUANTITY CHECKED GOOD. PERFORMED APU BITE CHECK IAW FIM TASK 49-60-810-801. NO CURRENT FAULT FOUND. RESTARTED APU MAINT LIGHTSDR ASAA12511624Warning Light · illuminatedON TAXI OUT FMC DISAGREE ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. OPS NORMAL.SDR ASAA2012061992380Wire Harness · failedNR 2 ENGINE ECM DATA SHOWS INTERMITTENT RECORDING OF CORE VIBRATION SENSOR. ACFT GROUNDED. ACCOMPLISHED BITE CHECK OF AVM. SELF TEST OK. FAULT HISTORY HAS 32 OCCURENCES OF N2 TACH LOSS E2. CHECKED RESISTANCE OF NR 2 ENG T422 N2 SPEED SENSOR. RESISTANCE OK.SDR ASAA12511494Fmc · malfunctionedFMC DISAGREE LIGHT CAME ON AFTER PUSH BACK. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. RESET SATISFACTORY.SDR ASAA12511436Idg · malfunctionedDURING SERVICE CHECK, FOUND NR 1 IDG DELTA P INDICATOR EXTENDED. PERFORMED FIM TASK 24-11-00 CHECKED HISTORY (FIRST) DPI RESET FOR IDG NR 1. TC 78273000 FMC/CDU COMPLETED. NO FAULTS. TC 78424000, IDG FILTER AND OIL CHANGE COMPLETED. NO DEFECTS. FIM TASK 24SDR ASAA12511420Actuator · failedFCC A FAILS SELF TEST. MESSAGE 22-11339 'R SENSOR EXC INV'. ACFT GROUNDED. REPLACED A/P AILERON A ACTUATOR IAW AMM 22-11-25-400-801, LEAK CHECKED GOOD IAW AMM 22-11-25-710-801. OPS CHECKED GOOD IAW AMM 22-11-25-710-801.SDR ASAA12511423Valve · failedNR 2 ENGINE PCV VALVE FAILED HEALTH CHECK. ACFT GROUNDED. REPLACED NR 2 ENG PCV IAW AMM 36-12-02. NR 2 ENG PCV DID NOT OPERATE DURING WING TAI SOLENOID VALVE TEST. REPLACED NR 2 ENG PCV AGAIN IAW AMM 36-12-02. OPS AND LEAK CHECKED GOOD.SDR ASAA12511117Fuel Nozzle · failedAPU CT5ATP EGT TREND DATA SHOWS EGT HAS SHIFTED ABOVE THE ESTABLISHED THRESHOLD. REMOVED AND REPLACED TEN FUEL NOZZLES AND SHROUDS REF MM 49-31-14. OPS AND LEAK CHECKED GOOD.SDR ASAA1251005Sensor · faultyAPU EGT (CT5ATP) TREND DATA SHOWS A SUDDEN SHIFT. INDICATION ERRORS ARE SUSPECT. REPLACED APU INLET TEMP SENSOR (T2) REF MM 49 61 31 000 801 AND 49 61 31 400 801.SDR ASAA12510951Paint · missingNR 1 ENGINE INLET SPINNER FRONT CONE MISSING MORE THAN 50 PERCENT OF WHITE ANTI EROSION PAINT. REMOVED AND REPLACED NR 1 ENGINE INLET SPINNER FRONT CONE REF T/C 78472002.SDR ASAA11510777Cdu · faultyBUTTON 5L INOP ON RT FMC. REPLACED F/O`S CDU OPS CHECK GOOD REF MM 34 61 01.SDR ASAA11510583Module · defectiveLED BURNED OUT ON PRESSURIZATION PANEL. INSTALLED CABIN PRESS CONTROL MOD PER MM 21 31 02 400 801. TEST OF MODULE PER MM 21 31 00 700 802 & MM21 31 00 710 801. ALL TEST OPS CHECK NORMAL.SDR ASAA11510578Keyboard · inoperativeUPPER LEFT QUADRANT OF COPILOT FMC MENU KEYS IS BURNED OUT. REPLACED AND TESTED F/O'S MCDU KEYBOARD PER MM 34 61 01 000 801 / MM 34 61 01 400 801, OPS NORMAL.SDR ASAA11510569Control Module · failedFLT ALT DISPLAY ON PRESS CONTROL PANEL IS BLANK. REPLACED CABIN PRESS CTL MODULE (CKPT OVHD) & PERF'D ALL REQ'D TESTS REF AMM 21 31 02, ALL OPS NORMAL. GROUND VERIFICATION TESTS SUCCESSFUL.SDR ASAA11510317Valve · malfunctionedAT CRUISE FL 350 (4+ HOUR CRUISE) L DUCT PRES 18 PSI / R DUCT PRES 40 PSI (L DUCT PRES APPEARS TO VARY BETWEEN 18 PSI AND 20 PSI). AT TOP OF DESCENT FIRST THROTTLE REDUCTION R DUCT PRES FLUXUATED AND REDUCED TO 19 PSI / AT THE SAME TIME L DUCT PRES STAYED SOLSDR ASAA11510262Unknown · malfunctionedSELECTING WX RADAR ON EITHER CAPTS OR F/O DISPLAY CAUSES TERR FAIL TO ILLUMINATE TURNING WX RADAR OFF TERR FAIL GOES AWAY AND TERR COMES UP ON BOTH ND'S TERR FAIL MSG COMES ON WHEN WX RADAR IS SELECTED AND TURNED ON. PERFORMED GPWS OPS TEST PER 34 46 00 710 8SDR ASAA11510241Servo · failedAUTOTHROTTLES DISENGAGE AFTER ENGAGEMENT. WHEN THROTTLES BEGIN TO MOVE ONLY NR 2 THROTTLE MOVES THEN DISENGAGES. ON DEFERRAL. A/T CURRENT STATUS SHOWS NO FAULTS, A/T SERVO TEST PASS. FFR SHOWS 11 FAULTS ON LEG 2 MESSAGE 22 31687 ASM NR 1 LEGS 3 40 NO FAULTSDR ASAA11510227Computer · malfunctionedAUTOTHROTTLE DISENGAGES AUTOMATICALLY FAULT CODE 223 130 00. T/S PER FIM FAULT CODE 223 130 00. CURRENT BITE PASSES NO FAULT. A/T SERVO TEST PASSES. PREVIOUS LEG FAULTS ASM 1 RATE MONITOR 4 TIMES ON 2ND FLT LEG. PER FIM 22 31 TASK 805 FCC A SHOULD BE REPLSDR ASAA11510178Autothrottle Sys · disengagedAUTOTHROTTLES DISENGAGED UNABLE TO RE ENGAGE. FFR LOGGED MSG22 31687 ASM 1FOR LAST LEG. CURRENT & SERVO TEST PASSED. DUE TO HISTORY REPLACED ASM 1 REF MM 22 31 93 OPS NORMAL. A/C REMAINS CAT IIIA AUTOLAND & HGS QUALIFIED STATUS SCREW REFLECT SAME.SDR ASAA11510154Control Valve · failedLEFT PACK VARIES 38 45 PSI RIGHT PACK APPROXIMATELY 23 PSI OBSERVED AT FLT LVL 38000 PER FLT CREW. PRECOOLER CONT VALVE FAILED HEALTH CHECK. REPLACED PRECOOLER CONT VALVE REF MM 36 12 02 400 801. INSTALLATION TEST PASSED. PERFORMED ENGINE BLEED AIR CROSSOVSDR ASAA11510132Servo · faultyAUTO THROTTLES FAILED AFTER T/O. SWITCH ONLY STAYS ENGAGED ABOUT 3 4 SEC. REF FIM:22 31/801 A/T LOGGED ON RELATED FLT LEG ASM1 FAULT AND SERVO MOTOR TEST INTERMITTENTLY FAILS ASM1 #22 31780. REPLACED NR 1 ASM REF MM 22 31 91, OPS CHECK NORMAL.SDR ASAA1159936Unknown · malfunctionedFMC DISAGREE DISPLAYED. ACCOMPLISHED FMC DISAGREE QRH CHECKLIST FMC DISAGREE MESSAGE NO LONGER DISPLAYED.SDR ASAA1159935Unknown · malfunctionedAUTO THROTTLES WILL NOT REMAIN ENGAGED. PERFORMED A/T BITE TEST FOUND F/C 22 31687 ASM NR 1 PER FTD 22 039 AND MT 22 039 CYCLED CB FOR AUTOTHROTTLE DC1. PERFORMED A/T SERVO MOTOR AND CURRENT STATUS TEST NO FAULTS. ALSO TORQUE MOTOR TEST NO FAULTS.SDR ASAA1159881Circuit Breaker · openLEFT FWD WINDOW OVERHEAT LIGHT ON CB WAS CHECKED IN ON PREFLIGHT FOUND DURING TROUBLESHOOT. FOUND CB P6 11 B9 WINDOW PWR HEAT LT FRT OPEN. RESET CB PER AMM 20 60 01 AND WDM 30 41 11. CB REMAINS SET L1 WINDOW OPS CHECK NORMAL REF AMM 30 41 11.SDR ASAA1159717Keyboard · inoperativeCAPT'S MCDU BUTTON L6 INOP. VERIFIED FAULT. REPLACED CAPT FMC KEY BOARD WITH SERVICABLE ONE. ACCOMP KEY BOARD TEST & CDU LAMP TEST BOTH TEST PASS REF M/M 34 61 01 400 801.SDR ASAA1159667Control Panel · damagedFOUND RADAR CONTROL PANEL TILT KNOB BROKEN. REPLACED RADAR CONTROL PANEL REF 34 43 91 AND 34 43 91 400 801. OPS CHECKED PER SAME.SDR ASAA1159644Control Panel · faultyON PDC FOUND ENG/APU FIRE EXTINGUISHER BULB LIGHT WORKS INTERMITTENTLY ON NR 1 SIDE WORKS OK ON NR 2. REPLACED ENGINE AND APU FIRE CONTROL PANEL IAW MM 26 00 01, OPS CHECK GOOD.SDR ASAA1159611Transceiver · failedPWS FAIL LIGHT OBSERVED ON BOTH SCREENS (FLIGHT DECK) DURING PREFLIGHT. REPLACED RADAR RECEIVER/TRANSMITTER PER MM 34 43 41, SYSTEM OP CHECKS GOOD PER MM 34 43 00.SDR ASAA1159558Unknown · malfunctionedFMC DISAGREE ON BOTH NDS DURING TAXI OUT AT KOA. RAN QRH PROCEDURE OPS NORMAL.SDR ASAA1159520Selector Panel · failedPRESSURIZATION CONTROLLER PANEL DISPLAY BLANK ON PREFLIGHT. REMOVED AND REPLACED CABIN PRESSURE SELECTOR PANEL PER MM 21 31 02 . SYSTEM TESTS NORMAL REF MM 21 31 02 400 801.SDR ASAA1159422Exciter · faultyNR 1 START ON APU NO LIGHT OFF WITH FAULT LIGHT ILLUMINATED. NR 2 START ON APU NO LIGHT OFF LOW OIL PRESS LIGHT ONLY ILLUMINATED. REPLACED APU IGNITER BOX. PER MM 49 41 31 000 AND 49 41 31 400. OPS CHECK GOOD.SDR ASAA1159346Unknown · malfunctionedFMC DISAGREE DISPLAYED. FOLLOWED QRH CLEARED ITSELF AFTER FOLLOWING QRH PROCEDURE. OPS NORMAL.SDR ASAA1159246Unknown · malfunctionedFMC DISAGREE LIGHT ON GROUND. RAN QRH CORRECTED PROBLEM.
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