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 ASAA2013032694272Drive Unit · failedWEATHER RADAR FAIL FLAG ON ND. FAULT CODE 344-050-32. VERIFIED FAULT RT INOPERATIVE. REPLACED WEATHER RADAR TRANSCEIVER IAW MM 34-43-41. PERFORMED WEATHER RADAR GROUND CHECK, FAULTED ANTENNA IAW MM 34-43-00. REPLACED WEATHER RADAR ANTENNA DRIVE UNIT IAW AMMSDR ASAA2013031994197Warning Light · false activationRIGHT PACK LIGHT COMES ON DURING RECALL, EXTINGUISHES WHEN MASTER CAUTION REST. PERFORMED BITE TEST OF RT PACK/ZONE TEMP CONTROLLER REF MM 21-51-00-700-803. NO FAULTS NOTED AFTER SEVERAL TESTS. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2013022493985Control Valve · leakingRIGHT PACK LIGHT ILLUMINATED DURING RECALL. ACFT GROUNDED. CONFIRMED FAULT, NR 2 TEMP CONTROLLER LOGGED THIS PACK TCV. ACCOMPLISHED FIM 21-62 TASK 831 RT TEMP CONTROL VALVE - FAULT ISOLATION. FOUND TCV (V141) LOOKING OVERHEATED AND LEAKING OIL. REPLACED TCSDR ASAA2013011493687Shutoff Valve · wornLT ENG PRSOV STUCK OPEN WITH ENGINE OFF. PERFORMED TROUBLESHOOTING TASK 36-00-00-860-807, SECTION C, DETERMINED PRSOV VALVE TO BE WORN EXCESSIVELY. REMOVED PRSOV VALVE ON NR 1 ENGINE REF AMM 36-22-04-000-801. INSTALLED PRSOV VALVE ON NR 1 ENGINE REF AMM 36-SDR ASAA2013010193590Oil System · lowBLUE MAINTENANCE LIGHT ILLUMINATED AFTER APU START. FOUND MAINT MESSAGE 49-91277 OIL QTY LOW. SERVICED OIL TO FULL IAW MM 12-13-31. NO HISTORY LAST 30 DAYS. POSITIVE MAINT ACTION COMPLETED. OK FOR CONTINUED SERVICE.SDR ASAA2012122093506Starter Gen · inoperativeON TAXI IN, STARTED APU BOTH ENGINES RUNNING BATTERY DISCHARGE LIGHT ILLUMINATED FOR 30 SECONDS. DURING START SEQUENCE THE WENT OUT. ALSO OCCURRED IN GATE WITH GROUND POWER CONNECTED DURING START SEQUENCE. ACFT GROUNDED. UPON START, FOUND THAT BATTERY DISCHSDR ASAA2012112093361Fan · out of balanceNR 2 ENGINE VIBRATION INDICATE BETWEEN 1.9-2.0 AT 84-97 N1 CAUSING AN AUDIBLE AND TACTILE VIBRATION. VARYING THE RPM WILL CAUSE THE AUDIBLE AND TACTILE VIBRATION TO INCREASE FOR A PERIOD AND THEN SETTLE DOWN TO A LESSER VALUE. PERFORMED ONBOARD FAN TRIM BALSDR ASAA2012111993327Blade · lack of lubePILOT REPORTED THAT NR 2 ENGINE VIBRATION 2.4 - 2.6. DURING TAKEOFF AND CRUISE. ACCOMPLISHED WO 187681, FAN BLADE LUBE, BOROSCOPE & MX. ACCOMPLISHED VIBRATION SURVEY AMM 71-00-00-700-814-F00. ALL INDICATION WITHIN SERVICEABLE LIMITS.SDR ASAA2012100993095Start Valve · failedSTART VALVE OPEN, LIGHT ON NR 1 ENGINE REMAINS ILLUMINATED AFTER ENGINE START. ALL START INDICATIONS NORMAL. R & R NR 1 ENGINE START VALVE. OPS CHECKED GOOD. NO LEAKS NOTED. REF MM 80-11-03-000-801-F00, AND 71-00-00-700-809-F00.SDR ASAA2012080792678Start Valve · inoperativeON NR 1ENGINE START , STARTER VALVE TAKES 15 SECONDS TO OPEN. REMOVED AND INSTALLED NR 1 ENGINE START VALVE IAW AMM 80-11-03. OPS CHECKED START VALVE, VALVE OPENED IMMEDIATELY. LEAK CHECK GOOD.SDR ASAA2012081692735Regulator · failedNR 1 ENG BLEED AIR REGULATOR FAILED. OPS CHECK FOR FIRE CONTROL PANEL B/P. ACFT GROUNDED. R & R BAR IAW MM 36-11-03. OPS & LEAK CHECKED GOOD.SDR ASAA2012081092703Wire Harness · frayedENGINE OVERHEAT LIGHT FAILS TO ILLUMINATE DURING TEST. ACFT GROUNDED. PERFORMED TASK 26-10-00-810-801 NO FAULTS NOTED, CYCLED A/C POWER, NR 1 ENG OVERHEAT LIGHT TESTED NORMAL. AFTER STARTING NR 1 ENGINE, THE OVERHEAT DETECT LIGHT ILLUMINATED. AFTER APPROX SDR ASAA2012081392704Actuator · faultedRIGHT PACK LIGHT ILLUMINATED DURING RECALL CHECK. RT PACK LIGHT WENT OUT WHEN MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED FIM 21-62 TASK 801. FOUND RAM AIR ACTUATOR FAULT. RESET FAULT. BITE TEST GOOD.SDR ASAA2012081092694Eec · malfunctionedFOUND MESSAGE NR 73-11282 EEC CHANNEL IS NOT ENERGIZED WITH THE ALTERNATOR VOLTAGE ON ENGINE NR 2. ACFT GROUNDED. FOR ENGINE NR 2 ACCOMPLISHED FIM 73-27-00-810-805-F00. ONLY 1 OCCURRENCE OF THIS FAULT LOGGED IN FAULT HISTORY. AFTER ENGINE RUN AND EEC TEST, FSDR ASAA2012070292455Sensor · failedRIGHT RAM AIR DOOR OPEN LIGHT ON DURING FLT AT CRUISE ALTITUDE. SUBSEQUENT CLOSED AFTER APRROX 45 MINS. ACCOMPLISHED T/C 78121000, CLEANING OF PRIMARY AND SECONDARY HEAT EXCHANGERS. NO DEFECTS NOTED. R & R RT RAM AIR CONTROL TEMP SENSOR, T482, IAW AMM 21SDR ASAA2012071092520Warning Light · false activationON RECALL, RIGHT PACK LIGHT ILLUMINATED. CLEARS WITH MASTER CAUTION RESET. NR 2 CONTROLLER SHOWS RAM AIR ACT FAULT ON BIT AND PREVIOUS FLT TESTS. VERIFY TEST PASSED. RESET FAULT. FAULT DID NOT RETURN. BITE TEST NR 2 CONTROLLER GOOD. REF FIM 21-62/836. SDR ASAA2012062792432Warning Light · no indicationR1 WINDOW HEAT GREEN ON LIGHT, NOT ILLUMINATED. R1 WINDOW HEAT TESTED GOOD REF 30-41-00-710-801.SDR ASAA2012061892369Warning Light · false activationFMC DISAGREE MESSAGE ON TAXI. ACFT GROUNDED. ACCOMPLISHED QRH. OPS NORMAL.SDR ASAA2012061592348Warning Light · false activationZONE TEMP LIGHT ILLUMINATED MASTER CAUTION RESETS LIGHT, PRESS RECALL & LIGHT ILLUMINATES. ACFT GROUNDED. PERFORMED PACK ZONE TEMP CONTROLLER BITE CHECK IAW AMM 21-61-00-700-806-002. OPS CHECKED GOOD. DID NOT DUPLICATE ORIGINAL DISCREPANCY AND FOUND NO MAISDR ASAA2012061192339Accessory Unit · failedCLIMBING OUT THROUGH FL 350, NOTICED RIGHT RAM AIR DOOR FULL OPEN LIGHT ILLUMINATED. EXTINGUISHED SHORTLY AFTER LEVEL-OFF FL 370. ALL OTHER INDICATIONS NORMAL. RESTORED RIGHT RAM AIR DOOR MODULATION SYSTEM IAW AMM 21-00-00-440-802. TESTED RT RAM DOOR IAW AMSDR ASAA12511586Fire Warning · malfunctionedFIRE WARNING TEST FAIL, NO LIGHT, ENG 1 OVERHEAT AND NR 1 RED HANDLE LIGHT. ACFT GROUNDED. PERFORMED OPS TEST 26-11-00-710-801, STEP E. OPS NORMAL. PERFORMED BITE 26-10-00-810-801, NO FAULTS. NO RECENT HISTORY.SDR ASAA12511535Actuator · faultyDURING CLIMB AWAY FROM SEA THE RIGHT "RAM DOOR FULL OPEN" LIGHT STAYED ON THROUGH 11 500 THEN ONLY AT APPROXIAMETLY 32 000 IT CAME ON AGAIN TILL LEVEL OFF AT 36,000. IT EXTINGUISHED AND STAYED OUT THROUGHOUT CRUISE FLIGHT. LIGHT CAME ON BELOW 6,000 DURING DESCSDR ASAA12511483Unknown · unknownWHEN STARTING THE LT NR 1 ENGINE IT TAKES 5 SEC FOR THE START VALVE OPEN LIGHT TO COME ON AS WELL AS 5 SEC BEFORE N2 ROTATION HAS STARTED WHEN START SWITCH MOVES TO OFF IT TAKES THE SV OPEN LIGHT 4 SECONDS TO GO OUT. NEXT FLIGHT CREW PERFORMED NR 1 ENG START SDR ASAA12511425Warning Light · false activationRT RAM DOOR FULL OPEN LIGHT REMAINED ON THROUGHOUT CLIMB. LIGHT WENT OUT AFTER 10 MINUTES AT FL 360. ACFT GROUNDED. PERFORMED BITE CHECK OF BOTH PACK/ZONE TEMP CONTROLLERS AND FOUND NO FAULTS. COULD NOT DUPLICATE DISCREPANCY. REF AMM 21-61-00-700-806-002 SDR ASAA12511408Modulating Valve · faultedDURING MASTER CAUTION RECALL AFTER START ZONE TEMP (CONT CAB) ILLUMINATED. LIGHT EXTINGUISHED ON MASTER CAUTION RESET. ACFT GROUNDED. CHECKED CABIN TEMP CONTROLLERS FOR DEFECT ISOLATION. FOUND FLT DECK TRIM MOD VALVE FAULTED. COMPLETED VERIFY TEST REF MM 21SDR ASAA12511365Probe · faultyDIAGNOSTICS REPORTED NR 2 ENGINE TREND DATA CONTINUES TO SHOW A SHIFT IN DELTA CRUISE AND TAKE OFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. PREVIOUS MAINT EGT CONNECTOR CLEAN. NO FAULTS ON CURRENT FAULTS & FLIGHT FAULT HISTORY. ACCOMPLISHED AMM TASK 77-2SDR ASAA12511368Warning Light · illuminatedRIGHT RAM DOOR FULL OPEN LIGHT REMAINED ILLUMINATED THROUGHOUT CLIMB TO FLIGHT LEVEL 380. CREW NOTED THAT RAM AIR FULL OPEN LIGHT EXTINGUISHED AFTER REACHING CLIMB & OPERATED NORMALLY FOR REST OF FLIGHT. ACCOMPLISHED TEMP CONTROL BITE CHECK PER INSTRUCTIONS SDR ASAA12511284Actuator · malfunctionedIN CRUISE RAM DOOR FULL OPEN LIGHT ILLUMINATED BRIEFLY RIGHT PACK. REMOVED AND REPLACED RT RAM AIR ACT AMM REF 21 51 21, OPS NORMAL.SDR ASAA12511285Unknown · malfunctionedRIGHT PACK LIGHT CAME ON, ON RECALL AFTER QRH. RECALL PUSHED LIGHT CAME BACK ON. RESET CONTROLLERS AND OPS CHECKED IAW AMM 21 61 20, OPS CHECK GOOD. RAN PACKS FOR OVER TEN MINUTES AND CHECKED RECALL AFTERWARDS NO FAULTS NO HISTORY ON RT PACK LAST 10 DAYS.SDR ASAA12511270Indicator · defectiveCENTER FUEL QTY INDICATOR ON REFUELING PANEL IS BLANK. FQIS TEST PASSED. CYCLED PWR TO REFUEL PANEL NO HELP. COCKPIT INDICATION OK. PER AMM 28 41 61 400 801 INSTALLED SERVICEABLE FUEL QUANTITY INDICATOR AT REFUEL PANEL CENTER POSITION OPS NORMAL.SDR ASAA11510855Bleed Valve · failedON CLIMBOUT DUCT PRESSURE DIFFERENTIAL 22 PSI (R50PSI LT28PSI) CRUISE DIFFERENTAIL PRESSURE (10PSI RT40PSI LT 30PSI) A/C PRESSURISED NORMALLY. ACFT GROUNDED. ACCOMPLISHED LT ENGINE BLEED AIR SYSTEM HEALTH CHECK PER MM 36-11-00. FOUND BLEED AIR REGUALATOR ANSDR ASAA11510813Idg · failedAT GATE PRIOR TO PUSH NR 2 DRIVE LIGHT IS NOT ILLUMINATED WITH ENGINES NOT RUNNING. LIGHT PRESS TO TEST OPERATES NORMALLY. CONFIRMED NR 2 ENG DRIVE LIGHT NOT ILLUMINATED W/ ENGINE NOT RUNNING. REPLACED NR 2 ENG IDG W/ SERVICEABLE PER AMM TASK 24 11 11 400 8SDR ASAA1150797Actuator · malfunctionedLEFT PACK ILLUM ON APPROACH, FAULT CODE 215 250 41. REPLACED THE LEFT RAM AIR DOOR EXHAUST ACTUATOR PER AMM 21 51 21.SDR ASAA11510774Unknown · malfunctionedLT PACK LIGHT ILLUMINATED ON RECALL AFTER LANDING. BITE CHECK OF NR 1 TEMP CONTROLLER LOGGED RAM AIR ACTUATOR FAULT. CLEARED FAULT AND BITE CHECK GOOD OF NR 1 TEMP CONTROLLER. REF M/M 21 61 20.SDR ASAA11510779Wire Harness · damagedNR 1 ENGINE J9 HARNESS DIRECTLY BENEATH INBD T/R DUCT HOLD OPEN ACTUATOR HAS DAMAGED REPAIR AT BEND OF HARNESS. REPLACED NR 1 ENG J9 HARNESS REF AMM 73 21 06, OPS NML PER SAME.SDR ASAA1058584Guide Arm · out of adjustFOUND L1 DOOR NOT PARALLEL WITH DOOR CUTOUT IN FINAL STAGES OF CLOSING MAKING DOOR DIFFICULT TO CLOSE ADJ. L1 DOOR GUIDE ARM ADJUSTMENT PER B737 800 MM 52 11 00 820 801 STEP H PAGES 2 AND 3. DOOR NOW CLOSES NORMALLY.SDR ASAA1057446Structure · wornECS HIGH PRESSURE DOOR LATCH WEAR ON LOWER CHORD BLENDED DAMAGED AREA ON UPPER SURFACE OF LOWER CHORD AND INSTALLED REPAIR STRAP & FILLER IAW ASA EA 800 53EA 02944.
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