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 ASAA2019072230157Warning System · false activationLEFT PACK LT ILLUMINATES ON RECALL. GROUNDED - YES. BITE AND VERIFY NO FAULTS.SDR ASAA2019071430054Wire Harness · damagedPER T/C N8420001 - RIGHT ENGINE HARNESS INSPECTION FOUND ENG J9 + J10 HARNESS DAMAGE AT T3 SENSOR CONN'S. GROUNDED - YES. REMOVED AND REPLACED J9 HARNESS ON #2 ENGINE REF AMM 73-21-06. FOR J10 HARNESS REPLACEMENT REF L/P 11973793. EEC DISCRETES TEST GOOD REF ASDR ASAA2019071430053Wire Harness · tornPER T/C N8420001 RIGHT ENGINE HARNESS INSPECTION FOUND BLACK BRAID TORN AT CJ10 DISCONNECT. DAMAGED BRAID IS ON THE J10 HARNESS. GROUNDED - YES. REMOVED AND REPLACED J10 HARNESS IAW AMM 73-21-06. FOR ALL HARNESS TESTS REF L/P 11973794, ALL TESTS PASSED.SDR ASAA201905319492Engine · crackedWHILE ACCOMPLISHING T/C 78472022 AT STAGE 1 LPT INSPECTION FOUND 1 FULL CRACK, 1 HOLE .0267 INCH SQUARE, 4 MULTI CRACKS (ON 1 AIRFOIL) AND 4 RADIAL CRACKS (ON 1 AIRFOIL) PER AMM 72-00-00-200-811-F00 FIG. 634. CONTINUE IN SERVICE LIMIT OF 25 CYCLES FOR #2 EMG. SDR ASAA2019052729487Wire Harness · intermittentAPU HAS HISTORY OF FAULT CODE 49-31171 WITH NO STARTS ON LANDING. GROUNDED - YES. ACCOMPLISHED FIM 49-31 TASK 808 STEP F.(4) CONTINUITY FROM CONNECTOR D3599B PIN A9 TO P23 PIN 1 IS GOOD REF WDM 49-62-12 P23 PIN 2 TO GROUND IS GOOD. P23 PIN 3 GROUND IS INTERMITSDR ASAA2019052529488Filter Element · cloggedWHILE PERFORMING INSPECTION ON THE APU FOUND OIL FILTER INDICATOR FOR THE LUBE FILTER HOUSING EXTENDED OUT. GROUNDED - YES. REMOVED AND REPLACED LUBE FILTER ELEMENT PER AMM 49-91-12 AND REMOVED AND REPLACED OIL FILTER INDICATOR PER AMM 49-91-13 OPS CHECK GOOD.SDR ASAA2019052029426Warning System · false activationCONT CAB ZONE TEMP LIGHT ILLUMINATED ON RECALL. EXTINGUISHED WITH MASTER CAUTION RESET. GROUNDED - YES. BITE CK FOUND FLT. DECK TEMP SENSOR FAULT ON PREV FLT. BITE CK OF BOTH ACC CONTROLS TEST NML. NO PRESENT FAULT. OPS CK NML. OK FOR SVC..SDR ASAA2019051829386Seal · leaking#1 ENGINE OIL CONSUMPTION TREND DATA SHOWS CONSUMPTION RATES TO BE GREATER THAN EXPECTED. GROUNDED - YES. UPON INSPECTION AFTER ENGINE RUN LEAK CHECK FOUND OIL LEAKING ON #1 ENGINE FROM IDG/AGB DRAIN. FOUND TO BE OUT OF LIMITS (MORE THAN ONE DROP IN 3 MINUTES)SDR ASAA2019051829376Idg · leakingDURING IDLE LEAK CHECK OF #1 ENGINE. FOUND OIL LEAKING FROM IDG VALVE CAP PLATE. GROUNDED - YES. REMOVED #1 ENGINE IDG IAW AMM 24-11-11-000-801. INSTALLED A SERVICEABLE IDG IAW AMM 24-11-11-400-801 PARA 3A THRU 3H. ACCOMPLISHED AMM 24-11-11-400-801 PARA 3.I. TSDR ASAA2019051729384Warning System · false activationPER INBOUND FLT CREW APU FAULT LT ILLUMINATED ON APU RESTART. GROUNDED - YES. PERFORMED APU BITE TEST REF FIM 49-60 TASK 801. FOUND MX MESSAGE 49-31171. PERFORMED FIM 49-31 TASK 808 WAITED 30 MIN AND RESTARTED APU START WAS NORMAL. NO MESSAGE ON CURRENT STATUSSDR ASAA2019051229317Warning System · false activationDURING TAXI IN TRIED STARTING APU RECEIVED APU FAULT LIGHT. GROUNDED - YES. APU WAS CONTINUOUS RUN IN FLIGHT. CREW TURNED OFF PRIOR TO TOP OF DESCENT. APU START ATTEMPTS WAS AFTER LANDING. NO SECOND ATTEMPT MADE. APU BITE ACCOMPLISHED. CODE 49-31171 DISPLAYED.SDR ASAA2019051129289Control Panel · defectiveDIGITS ARE DIFFICULT TO READ ON CAPTAINS COURSE DISPLAY ON THE MODE CONTROL PANEL. GROUNDED - YES. REMOVED AND REPLACED MCP PER AMM 22-11-34. PERFORMED INSTALLATION TEST OF MCP PER AMM 22-11-34-740-801. PERFORMED LRU REPLACEMENT TEST FOR MCP BITE TEST GROUP #3SDR ASAA2019042629173Wire Harness · damagedWHILE INSTALLING RH VSV, (ENG #2) FOUND DAMAGED WIRES. GROUNDED - YES. REPLACED J9 AND J10 HARNESS. ALL OPS NML. ALL TEST PASS, REF B737-800 AMM 73-21-06, 71-00-00. GROUND VERIFICATION SAT.SDR ASAA201904295171Switch · inoperativeWHEN INTERROGATING THE FMC CDU FOR ENGINE FAULTS FOUND ENGINE NBR 2 MSG NBR 73-31072 THE FUEL FILTER SIGNALS DISAGREE. GROUNDED - YES. REMOVED AND REPLACED FUEL FILTER DIFF PRESSURE SWITCH REF B737-800 AMM 73-34-01. OPS CHECKS AND LEAK CHECK GOOD.SDR ASAA2019042639142Filter · abnormal#2 FUEL FILTER BYPASS LIGHT ILLUMINATED AFTER ENGINE START. GROUNDED - YES. REMOVED AND REPLACED #2 ENG FUEL FILTER, DRAIN PLUG O-RING, AND RE-SAFETIED DRAIN PLUG IAW B737-800 AMM 73-11-02. ACCOMPLISHED GROUND VERIFICATION, PERFORMED IDLE ENG RUN OF #2 ENG, NOSDR ASAA2019042639139Control Valve · stuckRT PACK LIGHT ON UPON MASTER CAUTION RECALL LIGHT EXTINGUISHES UPON MASTER CAUTION RESET. GROUNDED - YES. REF L/P 11972111, TCV 2 (V141) FAILED BITE TEST. REMOVED & REPLACED TCV 2 REF B737-800 AMM 21-51-10. ACCOMPLISHED PACK-ZONE TEMP CONTROLLER BITE TEST REF SDR ASAA2019042639136Control Valve · stuckWITH MASTER CAUTION RECALL: # 2 PACK LIGHT REMAIN ON AFTER MASTER CAUTION RESET BUTTON PUSHED. GROUNDED - YES. CONFIRMED FAULT, BOTH #1 & #2 PACK-ZONE TEMP CONTROLLER BITE TEST FAILS TCV 2 (V141), WILL NOT RESET FAULT. FOUND TCV 2 FROZEN. REMOVED & REPLACED TCSDR ASAA2019042029085Actuator · leakingWHILE PERFORMING IDLE RUN CHECK ON ENG #2, FOUND LEFT VSV LEAKING. GROUNDED - YES. REMOVED AND REPLACED VSV ACTUATOR IAW B737-800 AMM TASK 75-31-01. LEAK AND OPS CHECKS GOOD. THIS CLEARS PLT.SDR ASAA2019042392986Actuator · leakingWHILE PERFORMING IDLE RUN CHECK ON ENG # 2 FOUND RIGHT VSV LEAKING. GROUNDED - YES. REMOVED AND REPLACED #2 ENG RIGHT VSV ACT IAW AMM 75-31-01. LEAK AND OPS CHECKS GOOD. THIS CLEARS PLT.SDR ASAA2019041879025A/C Pack · faultedR/H PACK LT W/ MC RECALL, GOES OUT W/ RESET. GROUNDED - YES. BITE CHECKED #2 ZTC - FAULTED TCV. PERF B737-800 FIM 21-62 TASK 831. VERIFY TEST PASSED. FAULT RESETS. RAN L/H & R/H PACKS W/ NO DEFECTS NOTED. ETOPS GND VERIFICATION TEST SUCCESSFUL.SDR ASAA201904158975Fmc · warning lightFMC DISAGREE LIGHT CAME ON DURING TAXI OUT. GROUNDED - YES. ACCOMPLISHED RESET PROCEDURE PER QRH. FMCS RESTORED NORMAL.SDR ASAA2019041088948Lens · brokenFA REPORTS EXIT SIGN BROKEN OFF BY R2 DOOR. GROUNDED - YES. INSTALLED NEW EXIT SIGN COVER.SDR ASAA201904028852Anti-Ice Valve · failedR/H ENG ANTI-ICE WILL NOT TURN OFF, LIGHT IS BRIGHT BLUE WITH SWITCH IN OFF POSITION. GROUNDED - YES. REMOVED AND REPLACED #2 ENG TAI VALVE, LEAK CHECK AND ENGINE RUN OPS CHECK GOOD REF B737-800 AMM 30-21-11-400-801.SDR ASAA2019032428774Warning System · false activationHF 1 SHOW FAIL IN BOTH THE ACTIVE & STANDBY WINDOWS, HOWEVER WE WERE ABLE TO TRANSMIT & RECEIVE. GROUNDED - YES. REF FIM 23-11 TASK 801. PERFORMED NR 1 HF BITE TEST NO FAULTS FOUND. TEST PASSED. AS PRECAUTIONARY R&R NR 1 HF TRANSCEIVER. REF AMM 23-11-21-000-80SDR ASAA2019030528479Unknown · malfunctionedHF NR 1 FAIL, CYCLED POWER OP CHECK NORMAL. GROUNDED - YES. UNABLE TO DUPLICATE HF NR 1 ISSUES. OPS CHECK GOOD.SDR ASAA2019030328432Sign · unsecureMID CABIN OVERWING EMERGENCY EXIT SIGN FELL OFF CEILING. GROUNDED - YES. REPLACED MISSING HARDWARE AND MOUNTED EMERGENCY EXIT SIGN.SDR ASAA2019022728395Unknown · abnormalAUTO THROTTLE WILL NOT ARM. GROUNDED - YES. ACCOMPLISHED AUTOTHROTTLE SYSTEM TEST AMM TASK 22-31-00-710-802. ALL TESTS PASS. ACCOMPLISHED LRU REPLACEMENT TEST FOR FCC A & FCC B. ALL TESTS PASS. REF AMM 22-11-00-740-815. ACCOMPLISHED LAND VERIFY TEST. ALL TESTSSDR ASAA2019021928263Warning System · false activationNR 2 ENG BLUE COWL VALVE OPEN LITE AND NR 2 ENG AMBER TAI LITE REMAIN ILLUMINATED WITH ENG A/I SWITCH IN OFF POSITION. DURING DESCENT BOTH LIGHTS EXTINGUISHED AND OPS NORMAL TO SHUTDOWN. GROUNDED - YES. VERIFIED NR 2 ENG COWL ANTI-ICE & COWL VALVE OPEN LIGHTS SDR ASAA2019021728206Sign · unsecureTHE EXIT SIGN NEAR R-2 DOOR NEEDS TO BE REPLACED. IT WILL NOT STAY ATTACHED TO THE WALL. GROUNDED - YES. REMOVED AND REPLACED EMER LIGHT BASE ASSY ON R-2 DOOR (LOWER LIGHT ASSY) IAW AMM 33-51-01. OPS CHECK GOOD. OK FOR SERVICE.SDR ASAA2019012127894Unknown · malfunctionedHF NR 1 PANEL 'FAIL' SHOWN ON BOTH FREQUENCY INDICATORS. SYSTEMS HANDBOOK NOTES POSSIBLE TRANSCEIVER FAILURE. NOTE BOTH HF RADIOS VOICE AND SELCAL CHECK GOOD. NA ACTUAL PROBLEMS NOTED DURING USE. GROUNDED - YES. RESET POWER TO HF SYSTEM. PERFORMED BITE PROCEDUSDR ASAA2019011227800Not Reported · malfunctionedWHILE PERFORMING TASK CARD, FOUND FAULT MSG NR: 73-31072 THE FUEL FILTER SIGNALS DISAGREE NR 2 ENG LONGTIME. GROUNDED - YES. FAULT DEFERRED PER T/C 78273000 FOR 450 FLT HRS. WHILE PERFORMING CDU FAULT CHECK. NO FAULTS NOTED ON NR 2 ENG. THIS CLEARS "PLT".SDR ASAA2018111327094Fitting · crackedFWD CARGO AFT BAFFLE CLIP STA 500H RT IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP IAW SRM 51 40 05 0G 0.SDR ASAA2018110827097Baffle · crackedFWD PIT BAFFLE RT SIDE STA 500D - 500E IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO BAFFLE RT STA 500D - 500E IAW SRM 51 40 05 0G 0 AND SRM 51 40 02 0G 0.SDR ASAA2018110727096Fitting · crackedFWD CARGO COMP BAFFLE CLIP AT STA 500H IS CRACKED RT SIDE. GROUNDED - YES. REMOVED/REPLACED FWD BAFFLE CARGO CLIP AT STA 500H RT SIDE IAW SRM 51 40 50 0G 0 AND SRM 51 40 02 0G 0.SDR ASAA2018110727093Fitting · crackedFWD CARGO COMP BAFFLE CLIP AT STA 500H IS CRACKED, LT SIDE. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO BAFFLE CLIP AT STA 500H LT SIDE IAW SRM 51 40 05 0G 0 AND SRM 51 40 02 0G 0.SDR ASAA2018113067149Skin · crackedLEFT HORIZ LOWER SKIN IS CRACKED AT RIB STA 184.70 APPROX 10" FROM REAR SPAR. GROUNDED - YES. REPAIRED L/H HORIZ STAB SKIN IAW 737 800 SRM 55 10 01 2R 11 REPAIR IS A CATEGORY B WITH AN INSP. THRESHOLD OF 56,000 CYCLES AND REINSPECT EVERY 9,000 CYCLES.SDR ASAA2018110627095Floorbeam · corrodedFLOORBEAM AT STA 986 HAS CORR ON SCREW HOLE AT RBL 64. GROUNDED - YES. REPAIRED FLOORBEAM AT STA 986, RBL 24, IAW SRM 53 70 57 2R 6, STEP 4 W 1 O .150 R .120 L 1" D .030.SDR ASAA2018113057148Skin · crackedRIGHT HORIZ STAB LOWER SKIN IS CRACKED AT STA 167.10 APPROX 8" FWD OF AFT SPAR. GROUNDED - YES. REPAIRED R/H HORIZ. STAB SKIN IAW 737 800 SRM 55 10 01 2R 11 REPAIR IS A CATEGORY B WITH INSP. THRESHOLD OF 56,000 CYCLES AND REINSPECT EVERY 9,000 CYCLES.SDR ASAA2018110527092Support Angle · corrodedAFT CARGO COMP RT FLOOR SUPPORT ANGLE FROM STA 767 TO 787 HAS CORR. GROUNDED - YES. REMOVED CORR FROM AFT CARGO COMPT. RT FLOOR SUPPORT ANGLE FROM STA 767 TO 787, FOUND TO BE OUT OF LIMITS IAW SRM 53 60 15 1A 1 FIG 103 DETAIL D, REMOVED AND REPLACED AFT CARGO SDR ASAA2018110527047Channel · corrodedAFT CARGO COMP LT Z CHANNEL FROM STA 727A TO 787 HAS MULTIPLE AREAS OF CORR. GROUNDED - YES. REMOVED AND REPLACED LT Z CHANNEL FROM STA 727 TO 847 IAW SRM 53 00 53 2R 6 W .5 O .040 R 0 L 1.1 D .040.SDR ASAA2018110527039Channel · corrodedAFT CARGO COMP RT Z CHANNEL FROM STA 727A TO 767 HAS MULTIPLE AREAS OF CORR. GROUNDED - YES. REMOVED AND REPLACED RT Z CHANNEL FROM STA 727 TO 767 IAW SRM 53 00 53 2R 6 W 0.5 O .040 R .020 L 1.2 D .020.SDR ASAA2018110527038Channel · corrodedAFT CARGO COMP FLOOR SUPPORT CHANNEL ON FRAME 767 HAS CORROSION. GROUNDED - YES. REMOVED CORR AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53 60 15 A 1. REMOVED AND REPLACED CHANNEL (WEB) IAW SRM 51 40 02 0G 0 W 0.5 O .050 R .040 L 1 D .010.SDR ASAA2018091426088Unknown · malfunctionedA/T DISENGAGED INFLIGHT WOULD NOT REENGAGE. GROUNDED - YES. CHECKED THE A/T FAULT HISTORY AND FOUND FAULT 22-31687 (ASM1) RECORDED ON TWO LEGS ON 9/10/18. PERFORMED FIM 22-31 TASK 805 WITH NO ACTIVE FAULTS NOTED. PERFORMED AN A/T OP-TEST PER AMM 22-31-00-710-8SDR ASAA2018080225645Anti-Ice Valve · stuckNR 2 ENGINE ANTI-ICE COWL VALVE WAS STUCK IN THE OPEN POSITION. ACFT GROUNDED. INSPECTED THE NR 2 ENG ANTI-ICE VALVE. ACCOMPLISHED INITAL OPS CHECKS IAW AMM 30-21-00. BOTH APU AND ENG SOURCE NORMAL. INDICATION VALVE OPS CHECKED OKAY.SDR ASAA2018080025625Fault Message · false indicationAFTER LANDING CAPTAIN'S INBOARD DU WAS GETTING INTERMITTEN VTK FLAG. GROUNDED - YES. PERFORMED FIM 34-61 TASK 801. NO FAULTS NOTED FIM TASK 34-61 TASK 836 LIST VTK FLAG AS NUISANCE FAULT AND A/C REBOOTED AND CLEARED W/ NO FAULTS NOTED.SDR ASAA2018072125525Engine · dirtyON TAKEOFF FROM LAS AT GEAR RETRACTION NOTICED NR 1 ENG EGT GAUGE RED INDICATING 917 DEG C. REDUCED POWER ON ENGINE TO APPROX 97% N1 AND EGT RETURNED TO NORMAL. 27K BUMP TO, 32 DEG C AT KLAS. GROUNDED - YES. ACCOMPLISHED NR 1 ENGINE GAS PATH WASH WITH WATER RESDR ASAA2018062195141Autopilot Sys · malfunctionedAUTOPILOT A DISCONNECTED DURING CRUISE, WITH ALL OTHER INDICATIONS NORMAL. AUTOPILOT A WAS ENGAGED BUT DISCONNECTED EARLY DURING DESCENT, AUTOPILOT B USED FOR REMAINDER OF FLIGHT. ACFT GROUNDED. FLIGHT FAULT REVIEW LOGGED MCP DATA INV, MESSAGE 22-11607, ASDR ASAA2018061225065Paint · missingWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 1 ENG T/C 78472002, FOUND FRONT SPINNER WITH MISSING PAINT. GROUNDED - YES. ON DEFERRAL.SDR ASAA2018061225044Shim · wornWHILE ACCOMPLISHING FAN BLADE LUBE T/C 78472002, ON NR 1 ENGINE FOUND ALL SHIMS WORN INTO PARENT MATERIAL. GROUNDED - YES. REMOVED AND REPLACED ALL FAN BLADE SHIMS ON NR 1 ENGINE, REF AMM 72-21-02/401.SDR ASAA2018061225043Blade · wornWHILE ACCOMPLISHING FAN BLADE LUBE, T/C 78472002 ON NR 1 ENG FOUND 4 EA BLADES 6, 7,13,14 WITH CU-NI-IN COATING WORN BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED FAN BLADES 1 2 6 7 13 14, AND 18 REF AMM 72-12-02-401 AND T/C 78472002.
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