N519AS

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 = 'N519AS' 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 ASAA1058234Filter · obstructedSTARTED APU NORMALLY, WAITED APPROX 30 TO 60 SECONDS TO CONNECT APU GEN, IMMEDIATELY AFTER CONNECTING APU GEN IT DROPPED OFF LINE & APU AUTO SHUTDOWN W/APU FAULT LIGHT ILLUMINATED. STARTED APU RUN FOR ABOUT 60 SEC NORMALLY THEN AUTO SHUT DOWN WITH FAULT LIGHTAug 27, 2010 · N519AS · Boeing 737890 · APU Oil SystemSDR ASAA1057918Idg · failedLEFT GEN DRIVE LIGHT ILLUM IN FLT. FOLLOWED QRH PROCEDURE. LEFT GEN DRIVE DISCONNECTED. REPLACED NR 1 ENG IDG PER M/M 24 11 11. GEN DRIVE & BUSS OFF LIGHT RELAMPED. OPS CHECK GOOD PER M/M 24 11 00.Jun 10, 2010 · N519AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1057895Unknown · malfunctionedLEFT PACK LIGHT ILLUMINATED ON RECALL. QRH WAS ACCOMPLISHED AND LIGHT EXTINGUISHED AFTER RESET. PERFORMED PACK / ZONE TEMPERATURE CONTROLLER BITE CHECK NO FAULTS NOTED PER AMM 21 62 00 810 801. CREW REPORTED NO PACK LIGHT ON RECALL. GROUND VERIFICATION COMJun 4, 2010 · N519AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1057851Transceiver · malfunctionedWX RADAR "SPOKING" AFTER 5 TO 6 SPOKES PER SWEEP GROUNDED YES. CONFIRMED REMOVED & REPLACED WX RADAR TRANSCEIVER REF MM 34 43 41 000 801 / 400 801. OPS NML PER SAME. ETOPS GROUND VERIFICATION GOOD.May 21, 2010 · N519AS · Boeing 737890 · Weather Radar SystemSDR ASAA1057718Valve · failedCLIMBING THRU FL 330 DISCOVERED SPLIT OF 23SPI. AT FL370 LEFT DUCT IS 43PSI RIGHT IS 21PSI. N1 AT 91 PERCENT N2 AT 94.4 SAT= 44C TAT= 16C. ENGINES ARE MATCHED PARAMETERS OTHER THAN DUCT PRESSURE. PRESSURIZATION NORMAL. DUCT PRESSURES CONVERGED TO SAME PREApr 19, 2010 · N519AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1057652Spinner · damagedWHILE ACCOMPLISHING FAN LUBE ON NR 1 ENG FOUND NOSE SPINNER FRONT CONE MISSING ANODIZED COATING. REMOVED AND INSTALLED SERVICEABLE NOSE CONE IAW TASK CARD 78472002 FAN BLADE LUBRICATION.Apr 3, 2010 · N519AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA1057627Shutoff Valve · defectiveDURING CLIMB WITH ENGINES AT FULL POWER HAD A BLEED AIR DUCT PRESSURE DIFFERENCE OF 23 PSI. LEFT DUCT PRESSURE WAS 43 PSI THE RIGHT WAS 20 PSI. INITIAL TESTS GOOD EXCEPT FOUND PRSOV MOVEMENT VERY STIFF WHEN USING WRENCH. REMOVED AND REPLACED PRSOV IAW AMM 3Mar 31, 2010 · N519AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1057551Warning System · activatedCONTROL CAB ZONE TEMP LIGHT ILLUMINATES DURING RECALL.Mar 18, 2010 · N519AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1057542Ring · nickedNR 2 ENGINE FWD ANODIZED RING NICKED AT 10 O’CLOCK POSITION. INSPECTED FAN CASE AND FOUND TO BE WITHIN REPAIRABLE LIMITS PER AMM 72 24 01 200 801 F00. REPAIRED SMALL NICK PER AMM 72 24 01 200 801 F00 PARA F, OK FOR CONTINUED SERVICE.Mar 15, 2010 · N519AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA1057534Fmc · malfunctionedINFO ONLY: FMC DISAGREE ILLUMINATED ON TAXI OUT IN SEA. CHECKLIST 11.2 COMPLIED WITH FMC RE-PROGRAMMED WITHOUT FURTHER INCIDENCE. INFO NOTED GROUND VERIFICATION ACCOMP. FMCS SENSOR STATUS ON BOTH CHECK NORMAL REF M/M 36 61 00 710 801.Mar 13, 2010 · N519AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1057532Warning System · malfunctionedON TAXI FROM SEA ZONE TEMP FOR CONT CAB ILLUMINATED ON RECALL. PROCEDURES FOR FLIGHT CREW PLACARD FOLLOWED FOR MEL 21 21F. SEA MAINTENANCE NOTIFIED. COULD NOT DUPLICATE DEFECT. OPERATED BOTH PACKS AND PERFORMED BITE CHECK'S ON BOTH CONTROLLERS BOTH SHOW "GMar 13, 2010 · N519AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1057473Circuit Breaker · openPRE DEPARTURE LEFT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. VERIFIED DISCREPANCY. FOUND CB OPEN FOR LEFT SIDE WINDOW HEAT CONTROL. INSPECTED AND RESET CB PER MM 20 60 01. TESTED WINDOW HEAT REF MM 30 41 11. TESTS OK. BITE TEST NO FAULTS. GROUND TESTFeb 26, 2010 · N519AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0957148Servo · disconnectedA/T DISCONNECTED ON CLIMBOUT & WOULD NOT RE-CONNECT. REMOVED AND REPLACED AUTOTHROTTLE SERVO MOTOR NR 1 PER MM 22 31 91 020 801 / MM 22 31 91 400 801. PERFORMED AUTOTHROTTLE CURRENT STATUS TEST PER MM 22 31 91 400 801 AND SERVO MOTOR TEST PER MM 22 31 00 710Dec 15, 2009 · N519AS · Boeing 737890 · Auto Throttle SystemSDR ASAA0957018Anti-Ice Valve · failedAT TOP OF DESCENT FL380 SELECTED ENGINE ANTI ICE ON THE NR 1 COWL VALVE OPEN LIGHT REMAINED BRIGHT WITH AMBER TAI INDICATION ON THE ENGINE INSTRUMENT DISPLAY, QRC PROCEDURE COMPLETED COWL VALVE DID FINALLY OPEN JUST PRIOR TO ENGINE SHUTDOWN, NORMAL INDICATION.Nov 16, 2009 · N519AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA0957006Autothrottle Sys · malfunctionedAUTO THROTTLES DISENGAGED ON CLIMB-OUT WOULD NOT REENGAGE. ACFT GROUNDED. RESET SYSTEM OPS CHECK GOOD IAW FIM 22-11 TASK 802 LRU REPLACEMENT TEST FOR AUTOTHROTTLES. CHECKED HISTORY BACK TO AUGUST 1 2009 AND FOUND NO OTHER AUTOTHROTTLE WRITE UPS.Nov 13, 2009 · N519AS · Boeing 737890 · Auto Throttle SystemSDR ASAA0956797Warning Message · illuminatedFMC DISAGREE DISPLAYED F/O'S SIDE ON THE GROUND. ACFT GROUNDED. FLIGHT CREW PERFORMED QRH PROCEDURE. OPS NORMAL.Oct 13, 2009 · N519AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0956795Warning System · malfunctionedAT TOP OF DESCENT RECEIVED SINGLE FMC OPS IN BOTH SCRATCHPADS ACCOMPLISHED QRH PROCEDURE. FMC BOTH ON CPT. GROUNDED YES. ACCOMPLISHED FIM TASK 34 61 00 810 807 FMC HARDWARE/SOFTWARE FAULTS INITIAL EVALUATION. ALSO PERFORMED FMC SYSTEM OPERATIONAL TEST REF Oct 12, 2009 · N519AS · Boeing 737890 · Central WarningSDR ASAA0956376Pressure Switch · failedLEFT FUEL FILTER BY PASS LIGHT ILLUMINATED AFTER LANDING LIGHT WENT OFF WHEN ENGINE SHUT DOWN. PERFORMED FIM TASK 73 31 00 810 802 F00 FOUND DIFFERENTIAL PRESSURE SWITCH OPEN. REMOVED AND REPLACED NR 1 ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH PER M/M Aug 5, 2009 · N519AS · Boeing 737890 · Fuel Pressure SensorSDR ASAA0956360Eec · faultedACQUIRED FAULT ON EEC BITE TEST ON NR 1 ENG. FAULT CODE 73 31071 ON NR 1 ENG FUEL FILTER SIGNALS DISAGREE. ACCOMPLISHED T/C 78273000 ENGINE FMC CDU FAULTS. NO FAULTS LOGGED. OPS NORMAL.Aug 2, 2009 · N519AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA0956006Cam · lack of lubeF/A REPORTS L1 DOOR HARD TO OPEN AND CLOSE. FOUND L1 DOOR UPPER CAM DRY OF LUBRICANT. APPLIED LUBRICANT AT L1 DOOR UPPER CAM. OPS CHECK NORMAL IAW AMM 52 11 00.Jun 22, 2009 · N519AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA0955802Door · lack of lubeL1 DOOR DIFFICULT TO OPEN FROM INSIDE. CHECKED AND LUBED NR 1 LEFT DOOR PER M/M 52 10 00, OK FOR SERVICE.May 31, 2009 · N519AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA0955617Servo · failedAUTOTHROTTLES WILL NOT STAY ENGAGED. KICK OFF SHORTLY AFTER ENGAGEMENT. GROUNDED YES. PERFORMED FIM 22 31 TASK 805 CURENT STATUS BITE GOOD BUT A/T INTERACTIVE/SERVO MOTOR TEST FAILS LT THROTTLE WILL NOT DRIVE. ASM 1 AT FAULT. REMOVED/INSTALLED ASM 1 REF. MM 22May 13, 2009 · N519AS · Boeing 737890 · Auto Throttle SystemSDR ASAA0955423Module · faultyAFTER START PACK (L) LIGHT ILLUMINATED WOULD NOT RESET WITH MASTER CAUTION RESET. PERFORMED FIM TASK 21 62 00 810 830 BECAUSE OF TCV FAULT FOR LEFT PACK ON CONTROLLER BITE. REPLACED LT PACK TCV. TCV INSTALLATION TEST PASSED NO DUCT LEAKS FOUND. NO FAULTS OApr 30, 2009 · N519AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA0955165Guide Arm · faultyF/A REPORTS YELLOW GUST LOCK ON L1 DOOR DIFFICULT TO PRESS TO CLOSE THE DOOR. REMOVED & REPLACED GUIDE ARM ASSY. ADJUSTED GUIDE ARM. DISCONNECTED SNUBBER FROM DOOR, NO HELP. RECONNECTED SNUBBER TO DOOR. REMOVED L1 DOOR GUIDE ARM. REMOVED SIDEWALL PANELS Apr 16, 2009 · N519AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA0954994Trim Motor · failedDURING CLIMBOUT BOTH CAPT & F/O ELECTRIC TRIM SWITCHES WOULDN’T TRIM NOSE DOWN INITIALLY, LEFT FLAPS AT 1 DEG TO STAY SLOW AND AVOID NEARLY MORE NOSE DOWN TRIM. ACCOMPLISHED QRH FOR STABILIZER TRIM INOP. AFTER MANUALLY TRIMMING, RETRACTED FLAPS TO DO AFTER TMar 29, 2009 · N519AS · Boeing 737890 · Stabilizer ActuatorSDR ASAA0954971Warning System · malfunctionedWHEN FLAPS RETRACTED TO UP FROM 1 DEG SPEED TRIM FAIL LIGHT ILLUMINATED WENT OUT AFTER FLAPS REACHED UP. DFGS BITE TESTS PASS ALL TEST PER FIM TASK 22 11 00 810 801. OPS NORMAL.Mar 29, 2009 · N519AS · Boeing 737890 · Autopilot SystemSDR ASAA0954855Outflow Valve · malfunctionedAUTO PRESSURIZATION FAIL SWITCHED TO ALT. FOUND FAULT ON CABIN PRESS CONT NR 2 FLIGHT LEG OO CODE O78 OFU LRU FAIL 38214. VERIFIED P/N 4063 19972 01AA WITH SEAMC. REMOVED AND REPLACED AFT OUTFLOW VALVE REF MM 21 31 03 19382. DFPC BITE TEST GOOD, PRESSURIZAMar 20, 2009 · N519AS · Boeing 737890 · Pressure Regulator/Outflow ValveSDR ASAA0954826Paint · missingNR 2 ENGINE FRONT SPINNER MISSING BLACK ANTI EROSION PAINT. REPLACEMENT OF NR 2 ENGINE FRONT SPINNER DEFERRED UNTIL NEXT C-CHECK PER MM 72 21 01 200 801, SEAMC NOTIFIED.Mar 15, 2009 · N519AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA0954678Warning System · activatedBLUE MAINT LIGHT ILLUMINATED ON APU AFTER START. PERFORMED APU BITE PROCEDURE PER FIM TASK 49 60 00 810 801, FOUND MESSAGE 49 91227 LOW OIL QUANTITY. PERFORMED LOW OIL QUANTITY FAULT ISOLATION PER FIM TASK 49 50 00 810 804. FOUND OIL .5 QTS LOW NO OTHER FAUMar 9, 2009 · N519AS · Boeing 737890 · APU Oil SystemSDR ASAA0954670Control Valve · faultyON TAXI OUT N1 RPM VALUES WERE SPLIT BY .7 (NR 1 ENG 86.1 NR 2 ENG 86.8). N1 CARROTS WERE ALSO SPLIT. LEFT PACK VALVE FAILED TO OPEN TWICE WHILE OPERATING. PERFORMED FLOW CONTROL & SHUTOFF VALVE TEST REF MM 21 51 01 STEP G, ALL TESTS GOOD. PERFORMED ENG RUMar 6, 2009 · N519AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA0954638Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL NOT ENGAGE. COULD NOT DUPLICATE. REF FIM 22 31/810 & 817 INFLT FAULT REVIEW SHOWED NR 22 31671 & 72 FAULTS ON DEFECT RELATED FLT LEG. A/T CURRENT STATUS CHECK NORMAL NO FAULTS. FAULT IS INTERMITTENT PER FIM TASK 817. ALSO PERFORMED DFCS Mar 4, 2009 · N519AS · Boeing 737890 · Auto Throttle SystemSDR ASAA0954635Unknown · malfunctionedFMC DISAGREE IN CDU SCRATCH PAD. FOLLOWED QRH. RESET C/B. PERFORMED FMCS OPERATIONAL TEST PER M/M 34 61 00 710 801. ALL TESTS NORMAL SOFTWARE VERIFIED.Mar 3, 2009 · N519AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0954633Autoland Sys · malfunctionedCAT III APPROACH AND AUTOLAND. AIRCRAFT LANDED OUT OF LIMITS TO LEFT SIDE OF RUNWAY. GP NR 20 FFR OF DFCS A & B & HGS SHOWS NO FAULTS LAST FLT. GP NR 49 LAND VERIFY OF DFCS PASSES. HGS SYS TEST PASSES REF MM 34 36 00. A/C REMAINS CAT IIIA AUTOLAND & HGS QMar 2, 2009 · N519AS · Boeing 737890 · Autopilot SystemSDR ASAA0954439Switch · unknownAFTER LIFTOFF WING ANTI ICE SWITCH DID NOT MOVE TO OFF POSITION. SWITCH HAD TO BE MANUALLY POSITIONED OFF. PERFORMED PSEU BITE CHECK, NO RELEVANT FAULTS NOTED. PERFORMED WING ANTI ICING OPERATIONAL TEST IAW M/M 30 11 00 710 801, OPS CHECKS GOOD. PULLED ANDFeb 16, 2009 · N519AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA0954429Sensor · faultyCONT CABIN ZONE TEMP LIGHT ILLUM ON MASTER CAUTION RECALL. PERFORMED TEMP CONTROLLER BITE CHECK REF MM 21 61 00 CONTROL CABIN TEMP SENSOR FAULTED. REPLACED CONTROL CABIN TEMP SENSOR REF MM 21 61 10. TEMP CONTROLLER BITE CHECK GROUND VERIFIED OK REF MM 21 61Feb 13, 2009 · N519AS · Boeing 737890 · Cabin Temperature Sensor
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