N513AS
Service difficulty reports · 437
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 = 'N513AS' 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 = 'N513AS' 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 ASAA2021062335158Autopilot Sys · faultedBOTH A/P'S WOULD NOT ENGAGE. GROUNDED - YES. DIVERSION TIME 27 MINUTES - ADVISED FLIGHT CREW STAB TRIM SWITCH IN CUT-OFF POSITION. ACCOMPLISHED REQUIRED TESTS REF B737-800 AMM 22-11-00 OPS CHECK GOOD CAT IIIA AUTOLAND & HGS QUALIFIED.SDR ASAA2021061335090Ecu · faultedDURING T/C 78273000, #1 ENG SHOWS SHORT TIME FAULT MSG 73-21281. EEC TEST SHOWS CHANNEL A INOP ON BOTH NORMAL AND ALT MODE. DURING FIM 73-27 TASK 805 EEC SHOWED INTERNAL FAULT MSG 73-20101. #1 ENG REQ EEC REPLACEMENT. GROUNDED - YES. REMOVED AND REPLACED #1 ENSDR ASAA2021052434908Fmc · faultedWE GOT AN FMC DISAGREE MESSAGE ON THE SCRATCH PAD IT CLEARED ITSELF BEFORE REACHING THE GATE. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 34-61 TASK 836 FMCS OPS CHECK NORMAL.SDR ASAA2021051734831Sensor · inoperativeWHILE PERFORMING T.C. # 08031001, AEVM DISPLAYED MSG "N1 TACHO LOSS E1," ON LEGS 0, 1, AND 2. SYSTEM TEST OK. GROUNDED - YES. REMOVED AND REPLACED N1 SPEED SENSOR PER B737-800 AMM 77-11-01-400-801-F00. OPS AND LEAK CHECK GOOD. NO FAULTS LOGGED.SDR ASAA2021050134718Idg · failedAFTER ENGINE START GEN 1 WOULD NOT COME ON LINE. NO FREQ'S OR VOLTS NOTED ON PANEL. GROUNDED - YES. R/R #1 ENG IDG NO LEAKS NOTED. REF B737-800 AMM 24-11-11. OPS CHECK GOOD. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2021042434654Fmc · failedRIGHT FMC FAILED IN FLIGHT VTK AND MAP APPEARED ON RIGHT NAV DISPLAY AFTER 20 SECONDS THE FMC RETURNED TO NORMAL OPS FOR REMAINDER OF THE FLIGHT. GROUNDED - YES. ACCOMPLISED FMCS OPS TEST B737-800 AMM 34-61-00 NO FAULTS FOUND OPS TEST NORMAL.SDR ASAA2021040934543Fmc · malfunctionedVTK AND MAP FLAGS ON RIGHT ND, SINGLE FMC OPERATION SCRATCHPAD MESSAGE ON BOTH MCDU'S. GROUNDED - YES. PERFORMED B737-800 FIM 34-61 TASK 836, NO MORE MESSAGES ON ND FMC RH OK.SDR ASAA2021031234337Oil Cooler · leakingFOLLOWUP FOR MORE THAN DESIRED APU OIL CONSUMPTION. GROUNDED - YES. REMOVED & REPLACED APU OIL COOLER, ALONG WITH OIL COOLER RETURN TUBE, WHICH WAS FOUND TO HAVE A BENT LOCK TAB. LEAK CHECK OK. REF B737-800 AMM 49-91-41.SDR ASAA2021022434187Fmc · malfunctionedON DESCENT VTK ON F/O'S DU FOR ABOUT 30 SECONDS. GROUNDED - YES. PERFORMED B737-800 FIM 34-61 TASK 836, FMC RESET OPS NORMAL FAULT INTERMITTENT.SDR ASAA2021021834151Fmc · failed3 SEPARATE OCCASIONS, FO NAV DISPLAY SHOWED MAP AND VTK WITH ASSOCIATED FMC ALERT LIGHT ILLUMINATION INDICATING RIGHT FMC FAILURE EACH TIME IT RESOLVED BEFORE ACCOMPLISHING, QRH. GROUNDED - YES. NR 2 FMC OPS NORMAL, COULD NOT DUPLICATE, NO HISTORY.SDR ASAA2021021534112Warning Light · false activationAFTER ENGINE START ELEC LIGHT ILLUMINATED. COMPLETED QRH PROCEDURES. GROUNDED - YES. PERFORMED BITE CK REF B737-800 FIM 24-31 TASK 801. LOGGED AUX BAT CHGR, STAT INV & SPCU INOP. RESET FAULTS. FAULTS CLEARED AND IS OK FOR SERVICE.SDR ASAA2021021134095Fmc · malfunctionedRT PED DISPLAYED VTK AT 4000 FT QRH RESTORED. GROUNDED - YES. PERFORMED FMCS RESET PER B737-800 FIM 34-51-TASK 836 OPS CHECK NORMAL.SDR ASAA2021011933908Sliding Window · out of rigCOPILOT R2 WINDOW/ESCAPE HATCH WILL NOT OPEN. GROUNDED-YES. R2 WINDOW OPENED AND VERIFIED VERY HARD TO OPEN/CLOSE, REF B737-800 AMM 56-12-11-720-801. VERIFIED WINDOW HEAT TAP ON TB5014 FOR H16 CODE IS AT TERM 1, REF B737-800 WDM 30-11-11 A. PERFORMED R2 WISDR ASAA2021011233879Sensor · inoperativeW/O 1860663 DUE T/C NG-36WC-00001 ISSUED REF L/P 60041478 CONTINUATION TROUBLE SHOOTING FOR LEFT BLEED AIR DUCT PRESSURE LOW. GROUNDED-YES. W/O 1860663 T/C NG-36WC-00001 COMPLETED, LEFT BLEED AIR DUCT PRESSURE STILL LOW. PER TECH SERVICE INSPECTED 5TH STAGESDR ASAA2021010633850Sensor · faultedWINDOW HEAT RIGHT SIDE OVERHEAT ILLUMINATED TURNED OFF COOLED/RESET, PER CHECKLIST AFTER WHICH THE OVERHEAT LIGHT ILLUMINATED AGAIN SWITCH TURNED OFF. GROUNDED-YES. REMOVED AND REPLACED R2 WINDOW. OPERATIONS TEST/LEAK CHECK GOOD, REF B737-800 AMM 56-12-11. SDR ASAA2021010333811Control Unit · inoperativeR2 WINDSHIELD OVERHEAT ANNUNCIATOR ON. GROUNDED-YES. REPLACED WHCU, REF B737-800 AMM 30-41-11.SDR ASAA2021010333810Warning Light · false activationR2 WINDSHIELD OVERHEAT LIGHT ILLUMINATES SHORTLY AFTER T/O RAN QRH. LIGHT STAYED EXTINGUISHED. GROUNDED-YES. RAN QRH RESET PROCEDURE. LIGHT STAYED EXTINGUISHED.SDR ASAA2020122933789Warning Light · false activationR2 WINDOW OVERHEAT LIGHT ILLUMINATED. GROUNDED-YES. RAN QRM, LIGHT WENT OUT STAYED OUT.SDR ASAA2020122433757Fmc · failedRIGHT FMC FAILED TWO TIMES, ONCE JUST AFTER LEVEL OFF AND AGAIN DURING APPROACH. RECOVERED ITSELF. GROUNDED-YES. ACCOMPLISHED GVI FMCS CMPTR 2 C/B WIRING BEHIND P6-1, REF B737-800 WDM 34-61-11. REMOVED FMC 2 & CHECKED D3261C, PIN 7 & 8 SHOWS 0 OHM TO GROUNSDR ASAA2020121533697Control Valve · failedAT CRUISE FL 380 LEFT PACK DUCT PRESS 6 PSI RIGHT IS 40 PSI ON CLIMB OUT RIGHT 42 PSI LEFT 5 PSI. GROUNDED-YES. C/W NR 1 ENGINE BLEED AIR HEALTH CHECK T/C NG-36WC-00001, FOUND PRECOOLER CONTROL VALVE FAILED CONTROL PRESS CHECK. REMOVED & REPLACED NR 1 ENGINSDR ASAA2020121133678Fmc · failedRIGHT FMC FAILED IN FLIGHT AT FL400. GROUNDED-YES. FOUND NUMEROUS INSTANCES OF "FMC DATA INV" AND "NO FMC DATA" LOGGED IN CHANNEL B OF DFCS FAULT REVIEW ON THIS FLIGHT. REPLACED THE NR 2 FMC, PER B737-800 AMM 34-61-02/401. OPERATIONS CHECKS GOOD, PER SAME. SDR ASAA2020112433640Skin · crackedLT HORIZONTAL LOWER SKIN HAS A CRACK AT STA 129.5 10 FWD OF TRAILING EDGE. GROUNDED-YES. REPAIRED LT HORIZ LOWER SKIN AT STA 129.5, IAW 737-800 SRM 55-10-01-2R-11 REPAIR 11. THIS IS A CAT B REPAIR REQUIRES INSPECTION AT THRESHOLD OF 56,000 TOTAL FLIGHT CYCLSDR ASAA2020091163160Check Valve · bindingREF TC AD20201651-NG-36-2, NR 2 ENG 5TH STG BLEED AIR CHECK VALVE FAILS INSP ON STEP NR 4. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG 5TH STG BLEED AIR VALVE, REF T/C AD20201651-NG-36-2. OPS CHECKED AND LEAK CHECKED GOOD.SDR ASAA2020081833039Oil Cooler · leakingNR 2 ENGINE HAS REPORTS OF EXCESS OIL ADDED AFTER 15 MINUTE IDLE RUN WHILE AIRCRAFT IS IN ACTIVE STORAGE. PREVIOUS MAINTENANCE ACCOMPLISHED FOR SIMILAR REPORT: ANTI LEAK VALVE REPLACED, LUBE MODULE REPLACED, GEARBOX CHECKED FOR OIL HIDING. GROUNDED - YES. BSDR ASAA2020052832764Valve · leakingDUE TO RECENT REPORT OF 7 QUARTS OIL ADD TO THE NR 2 ENGINE WHILE THE A/C IS IN STORAGE. IT IS SUSPECTED THAT THE ENGINE MAY BE OVER-SERVICED DUE TO A LEAKING ANTI-LEAK VALVE AND LUBE UNIT SCAVENGE ABILITY. GROUNDED - YES. REMOVED AND REPLACED OIL ANTI-LEAK SDR ASAA2020033132576Warning System · activatedRIGHT WINDOW 2 OVERHEAT LIGHT ILLUMINATED DESCENDING THROUGH 12,000'. GROUNDED - YES. QRH RAN, LIGHT EXTINGUISHED.SDR ASAA2020032332496Warning System · false activationWINDOW HEAT RIGHT SIDE "OVERHEAT" LIGHT ON AT LEVEL OFF. GROUNDED - YES. FOLLOWED QRH, AFTER COOLING PERIOD LIGHT STAYED EXTINGUISHED FOR REMAINDER OF FLIGHT. OPS NORMAL.SDR ASAA2020032032475Idg · faultyAT FL400FL GEN 1 SOURCE LIGHT OFF BUS BUS AND DRIVE ILLUMINATED. RAN SOURCE OFF THEN DRIVE OFF QRH, DISCONNECTED GEN 1 VIA SWITCH, STARTED APU AND PUT IT ON BUS. GROUNDED - YES. FOUND #I ENG IDG DPI EXTENDED. WHILE PERFORMING DPI CHECK REF 12-13-21-200-802. FOSDR ASAA2020031732444Computer · failedVTK DISPLAYED ON CAPTAINS ND DURING LANDING ROLL. GROUNDED - YES. REPLACED #1 FMC COMPUTER, REF B737-800 AMM 34-61-02. OPERATIONAL TEST NORMAL.SDR ASAA2020021833190Computer · failedAUTOTHROTTLES WOULD NOT ENGAGE. GROUNDED - YES. A/T BITE SHOWS NUMEROUS FAULT MSG #22-31543 "A/T ENG 28VDC". ACCOMPLISHED B737-800 FIM 22-31 TASK 802 FAULT ISOLATION. REMOVED & REPLACED FCC-A REF B737-800 AMM 22-11-33. ACCOMPLISHED DFCS LRU REPLACEMENT TEST (GSDR ASAA202002132174Autothrottle Sys · disconnectedAUTOTHROTTLE DISENGAGED ON FINAL APPROACH WOULD NOT REARM. GROUNDED - YES. A/T BITE SHOWS MULTIPLE A/T ENG 28 VDC INV MSG 22-31543 LAST LEG. ACCOMPLISHED CURRENT STATUS BITE REF B737-800 FIM 22-31 TASK 801. OPS NORMAL REF SAME.SDR ASAA2020012861992Start Valve · faultedNR 2 ENGINE 2 START VALVE WOULD NOT OPEN WITH THE NR 2 SWITCH IN GROUND. GROUNDED - YES. EXCERCISED THE NR 2 START VALVE IAW AMM 71-00-00, ENGINE STARTED NORMALLY DEFECTS CLEARED. TSR704679 REMOVED AND REPLACED THE NR 2 ENGINE START VALVE IAW AMM 80-11-0SDR ASAA2020012171912Control Unit · failedR2 WINDOW OVERHEAT LIGHT ON IN CRUISE. LIGHT WENT OUT AFTER QRH. GROUNDED - YES. RERACKED L/H WINDOW HEAT CONTROL UNIT. T/S AND OPS / BITE CK NML PER B737-800 AMM 30-41-11. C/W CORD INSPECTION PER AMM 30-41-00-200-801 CKS NORMAL. OK FOR SERVICE. AFTER SUBSEQUESDR ASAA2020011031819Unknown · malfunctionedGREEN A/T ARM LIGHT INOP. GROUNDED - YES. PERFORMED AUTOTHROTTLE SYS OPERATIONAL TEST REF B737-800 AMM 22-31-00-710-801. A/T ARM LIGHT AND OPS TESTS NORMAL.SDR ASAA2020010131758Warning System · false activationAFTER TAKE-OFF RIGHT SIDE WINDOW HEAT OVERHEAT LIGHT. GROUNDED - YES. RESET PER QRH. AS PRECAUTINARY ACCOMPLISHED WINDOW HEAT CONTROL BITE B737-800 AMM 30-41-11 NO FAULTS FOUND OPS CHECK NORMAL.SDR ASAA2019112653446Display · malfunctionedVTK ON FO ND. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 34-61 TASK 836. RESET 4 C/B. OPS TEST GOOD. GROUND VERIFICATION TEST GOOD.SDR ASAA2019103081167Actuator · failedLEFT PACK LT ILLUMINATED ON RECALL. GROUNDED - YES. PERFORMED BITE CHECK PER B737-800 AMM 21-61-00. LEFT P2TC SHOWS CURRENT FAULT FOR RAM AIR ACT & UNABLE TO CLEAR. PER TECH SERVICE NOTE, DUE TO HISTORY OF INSTALLED ACT FAILURE, REMOVE & REPLACED LEFT RAM AIR SDR ASAA2019102971153Warning Light · false activationDURING DESCENT CHECKLIST, LEFT PACK LIGHT ILLUMINATED DURING RECALL AND EXTINGUISHED WITH MASTER CAUTION. GROUNDED - YES. PERFORMED PACK TEMP CONTROL BITE REF B737-800 FIM 21-62 TASK 801 RESET CONTROLLERS AND NO FAULTS PRESENT. RAN PACKS, LEFT PACK LIGHT REMAISDR ASAA2019102931151Warning Light · false activationDURING DESCENT CHECKLIST, LEFT PACK LIGHT ILLUMINATED WITH RECALL. PACK LIGHT EXTINGUISHED WITH MASTER CAUTION RESET. GROUNDED - YES. FOUND PACK TEMP CONTROLLER BITE PROCEDURE ON BOTH CONTROLLERS PER B737-800 FIM 21-62 TASK 801. REST CONTROLLERS & NO FAULTS FOSDR ASAA2019102873115Actuator · faultyFOUND RAM AIR ACTUATOR FAULT ON L/H PACK ZONE TEMP CONTROLLER. GROUNDED - YES. REMOVED AND REPLACED L/H RAM AIR INLET ACTUATOR PER B737-800 AMM 21-51-21. THIS CLEARS CORRECTED FAULT ON L/H PACK ZONE TEMP CONTROLLER.SDR ASAA2019102831093Warning Light · false activationCONT CAB ZONE TEMP LIGHT ILLUMINATES ON RECALL. LIGHT EXTINGUISHES ON MASTER CAUTION SYSTEM RESET. GROUNDED - YES. ACCOMPLISHED BITE TEST ON LEFT AND RIGHT PACK ZONE TEMP CONTROLLERS PER B737-800 AMM 21-61-00. FAULT RESET. RAN PACKS FOR 30 MINUTES. NO FAULTS FSDR ASAA2019102183049Computer · faultedAUTO THROTTLE DISENGAGED AND WILL NOT RE-ENGAGE. GROUNDED - YES. RELEASED PER MEL 22-4B AUTO THROTTLE SYSTEM INOP. ACCOMPLISHED A/T SYSTEM TEST REF B737-800 AMM 22-31-00-710-802. ALL TESTS PASSED. DUE TO FAULT HISTORY, REMOVED & REPLACED FCC-A REF AMM 22-11-33SDR ASAA2019102153033Motor · failedAFT #1 MAIN FUEL PUMP "LOW PRESSURE" LIGHT ILLUMINATED ON CLIMB AND REMAINED AT CRUISE. THE TANK HAD 8500 LBS IN IT. GROUNDED - YES. REPLACE #1 AFT MOTOR IMPELLER BOOST PUMP. CLOSED 1 EA CIRCUIT BREAKER. GROUND VERIFICATION TEST SUCCESSFUL.SDR ASAA2019101193986Circuit Breaker · open#1 AFT MAIN FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED AT TOP OF DESCENT. GROUNDED - YES. PERFORMED B737-800 FIM TASK 28-22-00-810-803 FOUND C/B D-1 P92 OPEN, RESET PER B737-800 AMM 28-22TASK 814 OPS CHECKS NORMAL.SDR ASAA2019092830845Pump · overpressuredHYDRAULIC SYSTEM B PRESSURE SLOWLY INCREASED FROM 3030 PSI TO 3480 PSI OVER A 3 HR. PERIOD AT CRUISE FL 370. GROUNDED - YES. REMOVED AND REPLACED #2 ENG HYD PUMP REF B737-800 AMM 29-11-11/401, HYD FILTERS B SYS PRESS MODULE REF AMM 29-11-71/401, RETURN FILTER SDR ASAA2019082753506Autothrottle Sys · malfunctionedAUTOTHROTTLES INOP. GROUNDED - YES. OPERATIONAL TEST PER B737-800 AMM 22-31-00-710-801, OPS TEST GOOD. ACCOMPLISHED AUTOLAND VERIFY TEST PER AMM 22-11-00-700-801. TEST PASS. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2019082743504Controller · failedCREW REPORTS, AFTER ENGINE START, ON THE RECALL ITEM THE LEFT PACK LIGHT ILLUMINATED AS EXPECTED. WHEN MASTER CAUTION RESET BUTTON WAS PUSHED THE LEFT PACK LIGHT DID NOT EXTINGUISH. GROUNDED - YES. REPLACED NR 2 PACK TEMP CONTROLLER IAW AMM 21-61-20. FAULT CLSDR ASAA2019082743503Warning Message · false activationAFTER ENGINE START ON THE RECALL ITEM THE LEFT PACK LIGHT CAME ON AS EXPECTED GIVEN MEL 21-32B. WHEN MASTER CAUTION RESET BUTTON WAS PUSHED THE LEFT PACK LIGHT DID NOT EXTINGUISH. GROUNDED - YES. PERFORMED BITE TEST, REF B737-800 FIM 21-62 TASK 801 FAULT LH PRSDR ASAA2019082633469Warning Light · false activationLEFT PACK LIGHT ILLUMINATED UPON RECALL GOES OUT UPON RESET. GROUNDED - YES. RESET #1 PACK CONTROLLER FAULT HISTORY AND VERIFIED NO ACTIVE FAULTS IAW B737-800 AMM 21-51-00. OPERATED #1 PACK IAW AMM 36-00-00 WITH APU BLEED. NO FAULTS\LEAKS NOTED. PERFORMED SECOSDR ASAA2019072730199Warning System · false activationPACK LIGHT ILLUMINATES DURING RECALL AND EXTINGUISHES WHEN RESET. GROUNDED - YES. ACOMPLISHED BITE PER FIM 21-61 TASK 801. FOUND "TCV" FAULT ON #1 CONTROLLER. AFTER BITE FAULT CLEARED. OP CHECK GOOD PER AMM TASK 21-61-00-700-807-002.
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