N518AS
Service difficulty reports · 480
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 = 'N518AS' 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 = 'N518AS' 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 ASAA2020102033397Control Panel · intermittentALITUDE PRESELECT ON MCP INTERMITTENT. GROUNDED-YES. NO LOGGED FAULTS FCC 1 & 2. REBOOTED MCP-SYSTEM TESTS GOOD, REF B737-800 AMM 22-00-01-730-801.SDR ASAA2020100633290Overheat Sensor · faultedAPU DET INOPERABLE LIGHT ILLUMINATED MOMENTARILY IN FLIGHT. GROUNDED-YES. ACCOMPLISHED B737-800 FIM 26-10 TASK 802, NO FAULTS LOGGED. REPLACED M1925, REF B737-800 AMM 26-15-01-400-801. OPERATIONS NORMAL, REF B737-800 AMM 26-15-00-710-801. AIRCRAFT RETURNESDR ASAA2020093033259Actuator · faultyPACK LIGHT ILLUM DURING RECALL. RESETS W/ MASTER CAUTION RESET. GROUNDED-YES. RELEASED PER MEL 21-32B. RT PACK PRIM CONTROLLER AUTHORIZED BY SEAMC RON. PERFORMED ZONE TEMP CONTROL BITE TEST, NR 2 ZTC FAULTED THE RT RAM AIR DOOR ACTUATOR. A/C HAS HISTORY SDR ASAA2020092133212Warning Light · false activationRT PACK LITE ILLUMINATES ON RECALL LIGHT GOES OUT WITH MASTER CAUTION RESET. GROUNDED-YES. BITE CK SHOWS NR 2 CONTROLLER RAM ACT ON BIT + PREV FLT, BUT VERIFIES GO. ACCOMPLISHED THE PACK/ZONE TEMPERATURE CONTROLLER BITE TEST, REF B737-800 AMM 21-51-00-700-8SDR ASAA2020082753090Cdu · defectiveFO'S MCDU RIGHT SIDE OF SCREEN IS PIXELATED. GROUNDED - YES. REPLACED MCDU, REF B737-800 AMM 34-61-01.SDR ASAA2020081753028Flange · damagedPREVIOUS REPORT OF FILIFORM DEBRIS FOUND IN NR 1 ENGINE AFT SUMP MCD SCAVENGE SCREEN. GROUNDED - YES. REMOVED TURBINE REAR FRAME OIL INLET COVER, REF B737-800 AMM TASK 72-56-00-000-802-F00. COMPLETED STEPS 1,2 AND 3 OF TSR. MEASURED LPT SHAFT ASSY SEAL TOOSDR ASAA2020081753026Receptacle · looseEMERGENCY EXIT LIGHT AT 25ABC IS INOPERABLE. GROUNDED - YES. RELAMPED EMERGENCY EXIT LIGHT, NO HELP. NO POWER AND GROUND AT LIGHT. RESECURED LOOSE PLUG D11344 AT 25ABC OVERHEAD BIN.SDR ASAA2020033132578Window · delaminatedON TAXI L2 WINDOW STARTED TO FORM BUBBLES/MELT/DELAM NO MASTER CAUTION OR OVERHEAT LIGHT. GROUNDED - YES. WHCU BITE SHOWS NO CURRENT FAULTS FOUND LEFT SIDE WINDOW. WHCU ON WRONG TAP. ADJUSTED TO PROPER TAP FOR NEW WINDOW TO BE INSTALLED, REF WDM 30-41-12. REMOSDR ASAA2020021873197Circuit Breaker · trippedRT SIDE WINDOW HEAT CAUTION. DID NOT CLEAR AFTER RUNNING CHECKLIST. GROUNDED - YES. FOUND C/B C228 OPEN. GVI ACCESSIBLE WIRING, NO FAULTS FOUND, REF B737-800 WDM 30-41-11. REF B737-800 AMM 20-60-01, RESET C/B. OPERATED WINDOW HEAT. C/B REMAINS SET, WINDOW HEATSDR ASAA2020012982006Bulb · inoperativeL2 DOOR EXTERIOR EMERGENCY LIGHT INOP. GROUNDED - YES. RELAMPED L2 DOOR EXTERIOR LIGHT EMERGENCY LIGHT REF B737-800 AMM 33-51-04. OPS CHECK GOOD.SDR ASAA2019120631524Warning Light · illuminatedAFTER ENGINE START, ON MASTER RECALL CONT CAB ZONE TEMP LIGHT ILLUMINATES. EXTINGUISHES ON RESET. GROUNDED - YES. UNABLE TO DUPLICATE DEFECT - MASTER CAUTION RECALL SHOWS NO ZONE TEMP LIGHTS. BITE TEST OF PACK/ZONE TEMP CONTROLLERS NR 1 AND 2 SHOWS NO FAULTS ASDR ASAA2019120311486Warning Message · false activationHF #1 SHOWS FAIL MESSAGE. GROUNDED - YES. CYCLED C/B'S - SYS RESTORED AND CKS NML REF B737-800 FIM 23-11 TASK 802. COMM & BITE CK GOOD. GND VERIFICATION SUCCESSFUL.SDR ASAA2019112071380Terminal · looseUPON SHUTDOWN, NOTICED ENGINE #2 ENG VALVE CLOSED LIGHT IS ILLUMINATED BRIGHT, NOT DIM. GROUNDED - YES. REF TSR 704433 FOR TROUBLESHOOTING. SUSPECT #2 ENGINE HMU. REMOVED AND REPLACED #2 ENG HMU PER T/C N8473000 & T/C N8473001 FAULT REMAIN ABNORMAL SHUT DOWN ASDR ASAA201910231080Warning Message · false activationHF1 RADIO DISPLAYS FAIL MESSAGE. GROUNDED - YES. PERFORMED HF COMMUNICATION SYST BITE PROCEDURES B737-800 FIM TASK 23-11-00-810-801. FAIL MSG. EXTINGUISHED. NO FAULT NOTED.SDR ASAA2019102203171Warning Light · false activationCONT CABIN ZONE TEMP ON RECALL. LT GOES OUT ON MASTER CAUTION RESET. GROUNDED - YES. ACCOMPLISHED B737-800 AMM 21-61-00. PACK/ZONE TEMPERATURE CONTROLLER BITE TEST. GROUND VERIFICATION TEST PASSED. LIGHT NO LONGER DISPLAY BEFORE AND AFTER RECALL IS PRESSED. OPSDR ASAA2019101093971Warning Message · false indicationHF RADIO #2 DISPLAYS FAIL. GROUNDED - YES. BITE TESTED #2 HF TRANSCEIVER REF B737-800 AMM 23-11-21. OPS CHECK GOOD. FAIL NO LONGER DISPLAYED ON RADIO TUNING PANELS.SDR ASAA2019100293874Shutoff Valve · out of limitsAFTER SHUTDOWN ENG 2 NORMALLY, ENG VALVE CLOSED ANNUNCIATOR REMAINED BRIGHT. ACFT GROUNDED. REPLACED NR 2 HMU HPSOV SWITCH REF B737-800 AMM 73-21-09-000-801-F00 & 73-21-09-400-801-F00. OP'S CHECK GOOD REF PP TEST #12 & #13 REF AMM 71-00-00-800-811-F00.SDR ASAA2019092830857Warning System · false activationAFTER SHUTTING DOWN ENGINE #2 NORMALLY, ENGINE VALVE CLOSED ANNUNCIATOR REMAINED BRIGHT. GROUNDED - YES. CYCLED #2 FUEL CUTOFF - #2 ENGINE VALVE CLOSED LIGHT WENT DIM. OPS CHECKS NORMAL.SDR ASAA2019092730856Lever · out of position#2 ENG VALVE CLOSED LIGHT REMAINS BRIGHT BLUE WITH ENGINE SHUT DOWN. GROUNDED - YES. FOUND START LEVER OUT OF DETENT. CYCLED LEVER LIGHT EXTINQUISHED. OPS CHECK OK ON ENGINE RUN REF TO B737-800 AMM 71-00-00. OK FOR SERVICE.SDR ASAA2019082730510Brake · faulted#2 ENGINE HAS HISTORY OF DELAYED SHUTDOWN WITH HPSOV LIGHT REMAINING BRIGHT. GROUNDED - YES. REMOVED AND REPLACED ENG START BRAKE ASSY REF B737-800 AMM 76-11-10. OPS NORMAL. IGNITION OPS NORMAL REF AMM 74-00-00.SDR ASAA2019081203374Connector · unsecureWHILE SHUTTING DOWN ENGINE NR 2, START LEVER TO CUTOFF, THE ENGINE CONTINUED RUNNING. START LEVER WAS MOVED OUT OF CUTOFF, AND RETURNED, AND THE ENGINE SHUT DOWN. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 73-06 TASK 804. FOUND NR 2 ENG HMU HPSOV CANNON PLUG NOSDR ASAA201908052288Control Valve · failedL PACK CAUTION LIGHT ON RECALL DOES RESET. GROUNDED - YES. PERFORMED L/H PZTC BITE REF B737-800 AMM 21-51-00. FOUND TCV FAULT LIGHT ON BIT AND ALL PREV FLT. IN VERIFY L/H TCV IS VERY LOUD. REMOVED AND REPLACED L/H TEMP CONTROL VALVE REF B737-800 AMM 21-51-10. SDR ASAA2019080213271Actuator · failedUPON ETOPS EXTERIOR WALK FOUND R/H RAM DOOR FULL CLOSED. GROUNDED - YES. PERFORMED PACK ZONE TEMP CONTROL BITE PER B737-800 AMM 21-61-00-700-806-002. R/H RAM AIR DOOR ACTUATOR IS BAD. REMOVED RAM AIR DOOR ACTUATOR PER AMM 21-51-21-000-801. INSTALLED RAM AIR DOSDR ASAA2019072330158Satcom · lockedSATCOM LOCKUP AFTER POWER TRANSFER. GROUNDED - YES. QRH COMPLETED. RESTORED NORMAL OPERATIONS.SDR ASAA2019072230162Display · malfunctionedFO'S BLANKED AND RESET DEADING TOP OF CLIMB. THE SCREEN WAS BLANK, ALL ADVISORY LIGHTS, AND THE EXC LIGHT ILLUMINATED. NO VTK FLAGS WERE VISIBLE ON EITHER X10 AND THE MCDU REBOOTED ITSELF IN 2-3 MINUTES. SUBSEQUENTLY IT FUNCTIONED THE DURATION OF THE FLIGHT. GSDR ASAA2019070429958Eec · faulted#1 ENG S/N 896974 HAS LONG TIME FAULT 73-20171 "INTERNAL EEC FAULT". DEFERRED PER T/C 78273000. GROUNDED - YES. REMOVED AND REPLACED EEC ON #1 ENGINE PER AMM 73-21-60/401, OPERATIONAL TEST PASSED. NO FAULTS FOUND GROUND VERIFICATION SUCCESSFUL.SDR ASAA2019070329917Hmu · faultedRIGHT SIDE ENG VALVE CLOSED LIGHT ILLUMINATED BRIGHT BLUE DURING PREFLIGHT BEFORE START. GROUNDED - YES. PERFORMED FIM 73-06 TASK 804, DISCONNECTED CONNECTOR DP1203, CONFIRMED PROPER OPERATION OF FIRE CONTROL PANEL SWITCH S9 AND PROPER OPERATION OF THE #2 ENGISDR ASAA2019062929875Apu · overtempAPU CT5ATP TEMPERATURE CONTINUES TO BE ABOVE THE ESTABLISHED APU ON DEMAND THRESHOLD. REMOVE APU FOR USE ON NONE ETOPS TAIL. GROUNDED - YES. REMOVED AND REPLACED APU REF AMM 49-11-00-400-803 OPS AND LEAK CHECK GOOD.SDR ASAA2019062729873Unknown · malfunctionedCREW REPORT VTK FLAG ON CAPT ND AFTER LANDING WAS ON FOR 10 SECONDS THEN WENT AWAY. GROUNDED - YES. FMC 1 LOGGED ONE GROUND FAULT, PGM FAULT. COMPLETED FIM 34-61 TASK 807. HARDWARE/ SOFTWARE RESET. NO FAULTS. OK FOR SERVICE.SDR ASAA2019062649819Compensator · failedNR 2 MAIN TANK FUEL QUANTITY INDICATION SYSTEM FAILS SYSTEM TEST IAW AMM TASK 28-41-00-730-801. GROUNDED - YES. PERFORMED TANK UNIT AND COMP TEST REF B737-800 AMM TASK 28-41-21-710-801. COMPENSATOR FAILS AT 60.58 PICO FARADS. ALL TANK UNITS READ GOOD. REMOVED SDR ASAA2019061069629Warning Light · illuminatedRIGHT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. GROUNDED - YES. TURNED OFF AND BACK ON AFTER COOLING PER B737 QRH STAYED EXTINGUISHED.SDR ASAA2019051729419Bracket · crackedAFT CARGO COMPARTMENT FS 867 LBL 18 BRACKET 149A8109 - 114 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED BRACKET IAW SRM 51 40 02 0G 0 7D.SDR ASAA2019050929533Channel · corrodedAFT CARGO LT TRANSITION PANEL HAS CORR AT STA 724-787. GROUNDED - YES. REPAIRED LT TRANSITION PANEL (ZEE CHANNEL) IAW SRM 53 00 53 2R 6 W 1.0 O .063 R 0 L 1.0 D .063.SDR ASAA2019050929422Shield · corrodedAFT CARGO R/S SHEILD AT STA 767-794 HAS CORR ON BOTTOM SIDE. GROUNDED - YES. REMOVED CORR AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53 60 15 1A 1 REMOVED AND REPLACED SHIELD IAW SRM 51 40 02 0G 0 W .5 O .050 R .040 L 1.5 D .010.SDR ASAA2019050929421Intercostal · corrodedAFT CARGO R/S BAFFLE AT STA 747-767 HAS CORR ON BOTTOM SIDE. GROUNDED - YES. REMOVED AND REPLACED BAFFLE (INTERCOSTAL ZEE) IAW SRM 51 40 05 0G 0 AND SRM 51 40 02 0G 0 W .5 O .032 R .020 L 1.2 D .012.SDR ASAA2019050929420Transition Panel · corrodedAFT CARGO RT TRANSITION PANEL HAS CORR AT STA 727-767. GROUNDED - YES. REPAIRED RT TRANSITION PANEL IAW SRM 53 00 53 2R 6 W .8 O .040 R 0 L 1.2 D .040.SDR ASAA2019050729532Intercostal · crackedINTERCOSTAL AT STA 312-328 LBL 33 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED 1EA. INTERCOSTAL AT STA 312-328 LBL 33 IAW SRM 51 40 02 0G 0 PG 6 STEP D.SDR ASAA2019050329531Skin · crackedLT HORIZ LOWR SKIN CRACKED AT STA 101.9, 37 IN. AFT OF FRONT SPAR. GROUNDED - YES. REPAIRED CRACK ON LT HORIZ.LOWER SKIN AT STA 101.9 37" AFT OF FRONT SPAR IAW SRM 55 10 01 2R 11, PG 3 STEP 4 THIS IS A CAT. B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTALSDR ASAA2019050329530Skin · crackedLT HORIZ LWR SKIN CRACKED AT STA 100 AT REAR SPAR. GROUNDED - YES. REPAIRED CRACK ON LT HORIZ. LOWER SKIN AT STA 100 AT REAR SPAR IAW SRM 55 10 01 2R 11, PG 3 STEP 4 THIS IS A CAT. B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTAL FLT. CYCLES WITH AN INSPESDR ASAA2019050329529Skin · crackedLT HORIZ LWR SKIN CRACKED AT STA 129.5, 34 IN. AFT OF FRONT SPAR. GROUNDED - YES. REPAIRED CRACK ON LT HORIZ.LOWER SKIN AT STA 129.5 34" AFT OF FRONT SPAR IAW SRM 55 10 01 2R 11, PG 3 STEP 4 THIS IS A CAT. B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTAL SDR ASAA2019050329528Skin · crackedRT HORIZ. LWR SKIN HAS A CRACK AT STA 136, 32 IN. AFT OF FRONT SPAR. GROUNDED - YES. REPAIRED CRACK ON RT HORIZ.LOWER SKIN AT STA 136. 32" AFT OF FRONT SPAR IAW SRM 55 10 01 2R 11, PG 3 STEP 4 THIS IS A CAT. B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTASDR ASAA2019050329527Skin · crackedRT HORIZ. LWR SKIN HAS A CRACK AT STA 147, 9 IN. AFT OF FRONT SPAR. GROUNDED - YES. REPAIRED CRACK ON RT HORIZ. LOWER SKIN AT STA 147 9" AFT OF FRONT SPARIAW SRM 55 10 01 2R 11, PG 3 STEP 4 THIS IS A CAT. B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTAL FSDR ASAA2019050329526Skin · crackedRT HORIZ LWR SKIN HAS A CRACK AT STA 167, 31 IN AFT OF FRONT SPAR. GROUNDED - YES. REPAIRED CRACK ON RT HORIZ. LOWER SKIN AT STA 167.31" AFT OF FRONT SPARIAW SRM 55 10 01 2R 11, PG 3 STEP 4 THIS IS A CAT. B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTAL FSDR ASAA2019041738997Hmu · faultedON ENG. #2 LONG TIME FAULT 73-31162 " THE MECHANICAL OVERSPEED PROTECTION SIGNAL IS OUT OF RANGE" DEFERRED PER T/C 78273000. GROUNDED - YES. REMOVED AND REPLACED #2 ENG HMU IAW ASA T/C # N8473000 AND T/C # N8473001.SDR ASAA2019040858902Knob · defectiveAIR TEMPERATURE SOURCE SELECTOR KNOB WON'T PROPERLY SEAT AT VARIOUS ZONE SELECTIONS. GROUNDED - YES. TROUBLESHOT TO DEFECTIVE TEMP SOURCE SELECT SWITCH (S-1) P5-17 CABIN TEMP PANEL. REMOVED & REPLACED P5-17 TEMP CONTROL MODULE REF B737-800 AMM 21-61-15, GROUNDSDR ASAA201904018823Hf Comm · malfunctioned#1 HF WILL NOT TRANSMIT. GROUNDED - YES. RESET C/B PER B737-800 AMM 20-60-01. PERFORMED HF COMMUNICATION SYSTEM BITE PROCEDURE PER B737-800 FIM 23-11-TASK 801, BITE TEST GOOD NO FAULTS, OPS CHECK HF TRANSCEIVER OPS TEST GOOD OK FOR SERVICE, GROUND VERIFICATIONSDR ASAA2019032428773Transceiver · inoperativeNUMBER 1 HF RADIO HAS NO SOUND OR SIDETONE. GROUNDED - YES. WENT TO BITE NR 1 HF TRANSCEIVER, FOUND NR 1 HF TRANSCEIVER INOP. R & R NR 1 HF TRANSCEIVER, REF AMM 23-11-21-000-801/400-801. PERFORMED NR 2 HF BITE TEST AND OPS CHECK. NR 1 HF OPS NORMAL.SDR ASAA2019022628311Coupler · failed#2 HF RADIO FAILED ENROUTE. GROUNDED - YES. PERFORMED HF2 BITE WITH NO FAULTS FOUND CW B737-800 FIM 23-11 TASK 806 AND WAS UNABLE TO ESTABLISH 2 WAY COMMUNICATION. PLACED HF2 ON MEL 23-11A. REMOVED AND REPLACED HF#2 COUPLER IAW B737 800 AMM 23 11 61. ACCOMPLISSDR ASAA201902128147Display · malfunctionedPRIOR TO PUSH BACK F/O'S NAV DISPLAY MAP LIGHT ILLUMINATED F/O LOST ROUTE, CAPTAIN'S OK. GROUNDED - YES. ACCOMPLISHED RESET OF FMC SYS. NO FAULTS EVIDENT. REF B737-800 FIM TASK 34-61.SDR ASAA2019020628104Valve · faultedCONTROL CAB SINGLE CHANNEL ZONE TEMP FAILURE LIGHT ILLUMINATED ON RECALL AND EXTINGUISHED ON RESET. GROUNDED - YES. NR 2 PZTC BITE FREV FLT SHOWS FLT DECK TRIM VALVE FAULT, RESET FAULT. VERIFIED BOTH PACKS OPS CHECKED NORMAL ON GND WITHOUT FAULTS. NR 1 AND NR
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