N413AS
Service difficulty reports · 359
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 = 'N413AS' 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 = 'N413AS' 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 ASAA2018022423685Fuel Nozzle · malfunctionedAPU CT5ATP EGT TREND DATA SHOWS EGT HAS SHIFTED ABOVE THE MAINTENANCE THRESHOLD OF 593 WITH A HIGH OF 608 DEGREES BEEN RECORD APU HAS PREVIOUS HISTORY OF HIGH CT5ATP. GROUNDED - YES. ACCOMPLISHED APU BITE PROCEDURE PER B737-900 FIM 49-60 TASK 801. NO RECENT FSDR ASAA2018021723612Wire Harness · shortedFMC REPORTED A LONG TIME FAULT CODE 75-10822, THE T25 SIGNAL IS OUT OF RANGE ON THE NR 2 ENGINE. ACFT GROUNDED. FOUND ACTIVE T25 SENSOR FAULTS 75-10822, 75-10802, AND 75-20802 ON LEGS 2 AND 3. INPUT MONITORING OF THE T25 SENSOR SHOWED DASHES FOR CHANNEL BSDR ASAA2018021723611Wire Harness · faultedFMC REPORTED A SHORT TIME FAULT CODE 75-30802, T25, SIGNALS DISAGREE. ACFT GROUNDED. REMOVED AND REPLACED THE WIRE HARNESS IAW AMM 73-21-06-400-802-F00.SDR ASAA2018021223508Idg · failedDURING APPROACH, THE NR 1 SOURCE OFF & GEN OFF BUSS LIGHTS ILLUMINATED. COMPLIED WITH QRH, LIGHTS REMAINED ILLUMINATED. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 IDG IAW AMM 24-11-11, AND 24-11-11-080-801. FILTERS WERE CLEAN FROM CONTAMINATION. OPS CHECSDR ASAA2018020423439Probe · faultedMESSAGE 77-10842, THE TOP RIGHT EGT SIGNAL T495S1 IS OUT OF RANGE ON THE NR 2 ENGINE. FLIGHT LEGS 1-10. ACFT GROUNDED. REMOVED & REPLACED THE T49.5 S1 SENSOR. OPS CHECKED GOOD IAW AMM 77-21-01/401. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2018012123279Sensor · faultyFOUND NR 2 ENGINE, ECONOMIC FAULT, MAINT MESSAGE 77-10842 THE TOP RIGHT EGT SIGNAL IS OUT OF RANGE. REMOVED & REPLACED TOP RIGHT EGT SENSOR (S4) REF AMM 77-21-01/401. OPS GOOD. GROUND VERIFICATION SUCCESSFUL. CLEARS PLT.SDR ASAA2018012123238Display · frozenRIGHT MCDU IS LOCKED UP/FROZEN. GROUNDED - YES. CYCLED POWER & OPS CHECKS NORMAL PER AMM 34-61-01.SDR ASAA2018010823114Fault Message · false activationNR 2 ENGINE SHOWS A SHORT TERM FAULT 75-30802. THE T25 SIGNALS DISAGREE. ACFT GROUNDED. PERFORMED T/C 78273000, VERIFIED THE NR 2 ENGINE HAVE NO FAULTS MESSAGES PRESENT ON THE LAST 3 FLT LEGS. IAW 75-33 TASK 805 THE NR 2 ENGINE EEC BITE GROUND TESTS PASSED WSDR ASAA2017122923058Sensor · faultyWHILE PREFORMING T/C 78273000, FOUND FAULT 75-20822 "THE T25 SIGNAL IS OUT OF RANGE" LONG TIME FAULT DEFER PER T/C 78273000. GROUNDED - YES. REMOVED AND REPLACED T25 SENSOR REF AMM 73-21-02, OPS CHECK NORMAL. THIS CLEARS PLT.SDR ASAA2017122923057Sensor · faultyWHILE PREFORMING T/C 78273000 FOUND SHORT TIME FAULT 75-30802 "T25 SIGNALS DISAGREE" DEFERRED PER T/C 78273000 ON NR 2 ENGINE. GROUNDED - YES. REMOVED AND REPLACED T25 SENSOR REF AMM 73-21-02,OPS CHECK NORMAL. PLT CLEARED.SDR ASAA2017122422998Bypass Switch · failedON FINAL, RECEIVED A FUEL FILTER BYPASS CAUTION LIGHT FOR THE NR 2 ENGINE. FUEL FILTER HOUSING DRAINED WITH NO CONTAMINATES NOTED. DRAIN PLUG REINSTALLED AND LEAK CHECKS OK. REMOVED & REPLACED THE NR 2 ENGINE FUEL FILTER, NO DAMAGE OR CONTAMINATION NOTED. RSDR ASAA2017122422985Satcom · malfunctionedSATCOM NOT WORKING, CAN MAKE AND RECEIVE CALLS BUT CANNOT HEAR ANYTHING. RECEIVER CAN HEAR THE TRANSMISSIONS. ACCOMPLISHED FIM 23-15 TASK 801. OPS CHECKED NORMAL. NO FAULTS. ACFT GROUNDED.SDR ASAA2017121322879Control Valve · faulted"CONT CAB" ZONE TEMP LIGHT ILLUMINATES ON RECALL AND EXTINGUISHES WITH MASTER CAUTION RESET. GROUNDED - YES. REMOVED AND REPLACED FLT DECK TCV REF B737-900 AMM 21-61-21-400-801, BITE TEST ON THE PACK/ZONE TEMP CONTROLLERS OK. LEAK CHECK OK. A/C RELEASED FROM MSDR ASAA2017121022840Blade · damaged#2 ENG # 24 BLADE PLATFORM AFT LUG DAMAGE MARKS. GROUNDED - YES. EXAMINED PLATFORM IAW B-737- 900 AMM 72-21-02-210-006-F00 FOUND OUT OF LIMITS. REMOVED AND REPLACED 24 PLATFORMS ON #2 ENG IAW ASA MTX TASK CARD 78472002.SDR ASAA2017111622632Exciter · malfunctionedAFTER LANDING APU WOULD NOT START, FAULT LIGHT CAME ON. ACFT GROUNDED. REMOVED & REPLACED APU EXCITER, IGNITION UNIT IAW AMM 49-41-31. OPS CHECKED NORMAL.SDR ASAA2017110922528Oil System · lowWHEN TOWING TO GATE APU BLUE MAINTENANCE LIGHT ILLUMINATED. GROUNDED - YES. UPON FURTHER INSPECTION DETERMINED BLUE MAINTENANCE LIGHT WAS FOR LOW OIL QUANITY. SERVICED APU OIL TO PROPER LEVEL REF AMM 12-13-31. ACCOMPLISIHED APU OIL LEVEL INSPECTION OIL SIGHT GSDR ASAA2017101922251Actuator · faultedLEFT PACK LIGHT ILLUMINATED ON RECALL. EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFOMED BITE CHECK OF THE NR 1 AND 2 ZONE TEMP CONTROLLERS. FOUND THE NR 1 CONTROLLER FAULT FOR LEFT RAM ACTUATOR FAULT IAW FIM 21-62, 801. REMOVED AND REPLACEDSDR ASAA2017101822236Actuator · faultedAFTER ENGINE START & RECALL, A PACK LIGHT ILLUMINATED. DOES NOT RESET WITH CHECKLIST. ACFT GROUNDED. RAM AIR ACTUATOR FAULT ON ZONE TEMP CONTROLLER NR 1. RESET & BITE TESTED NORMAL IAW FIM 31-62, TASK 801.SDR ASAA2017101422194Warning Light · false activationZONE TEMP CONTROL CABIN LIGHT ILLUMINATED DURING TAXI AND RESET. ACFT GROUNDED. ACCOMPLISHED A PACK TEMP CONTROL BITE IAW FIM 21-62, TASK 801. FOUND THE NR 2 CONTROLLER SHOWS FLT DECK TRIM VALVE FAULTED. ACCOMPLISHED VERIFY TEST, NO CURRENT FAULTS. RESET FSDR ASAA2017100622136Fmc · failedRIGHT FMC INOPERATIVE. ACFT GROUNDED. ON INITIAL EVALUATION, FOUND THE RT FMC INOPERATIVE. FMC VALID LIGHT NOT ILLUMINATED. CYCLED THE CIRCUIT BREAKER AND SYSTEM RESTORED. ACCOMPLISHED FMC LT AND RT FAULT DOWNLOAD. AFTER FAULT DOWNLOAD, RT FMC FAILED AGAISDR ASAA2017092822090Fmc · failedRIGHT FMC FAILED MOMENTARILY, THEN RECOVERED. VTK ON FIRST OFFICER`S MAP DISPLAY AND LOST LNAV. RAN QRH, RECOVERED BEFORE MOVING FMC SOURCE SELECT SWITCH. ACFT GROUNDED. PERFORMED FMCS BITE AND FOUND TWO FAULTS ON FLIGHT LEG. RT FMC WATCHDOG TIMER AND RSDR ASAA2017092622048Fmc · malfunctionedAT CRUISE RIGHT FMC FAILED. SELECTED BOTH ON LEFT, CONTINUED FLIGHT WITH BOTH ON LEFT. CONTINUED FLIGHT WITH BOTH ON LEFT SUCCESSFULLY. GROUNDED - YES. RETURNED FMC SELECTOR SWITCH TO NORMAL. PERFORMED TROUBLESHOOTING PER FIM 34-61 TASK 807. RIGHT FMC RESTOREDSDR ASAA2017090821868Oil Cooler · leakingDURING A WALK AROUND, FOUND OIL BEHIND IDG AIR/OIL COOLER IN TR IN NR 2 ENGINE. ACFT GROUNDED. FOUND THE NR 2 IDG TO BE LOW AND HAD A HISTORY OF EXCESSIVE SERVICING. REMOVED AND REPLACED NR 2 IDG AIR/OIL COOLER IAW AMM 24-11-21. OPS AND LEAK CHECKED GOOD.SDR ASAA2017082521720Connector · looseAFTER SWITCHING NR 1 ENGINE ANTI-ICE SWITCH TO OFF, 10 MINUTES LATER COWL ANTI-ICE LIGHT ILLUMINATED DIM AFTER SELECTING SWITCH BACK TO OFF. ACFT GROUNDED. FOUND THE NR 1 TAI VALVE CONNECTOR PLUG VERY LOOSE. REMOVED AND INSPECTED THE CONNECTOR AND RECEPTACLSDR ASAA2017080821567Warning Message · false activationECS TEMPERATURE INDICATIONS SHOW ERRONEOUS READINGS FOR ALL SEVEN POSITIONS. ALL SEVEN INDICATIONS SHOW WELL BELOW 20C. FLIGHT ATTENDANT REPORTED NORMAL TEMPERATURE IN BOTH FWD & AFT CABIN WITH THE INACCURATE READINGS. ACFT GROUNDED. CYCLED AIR TEMP SWITCH FSDR ASAA2017080321538Circuit Breaker · trippedCLIMBING THROUGH 27,000 FT, MASTER CAUTION AND CAPTAIN`S PITOT PROBE HEAT AMBER LIGHT ILLUMINATED. ACFT GROUNDED. FOUND HEATERS CAPTAIN`S PITOT CIRCUIT BREAKER ON P18-3 PANEL TRIPPED. RESET THE CIRCUIT BREAKER IAW AMM 20-60-01-860-801. CAPTAIN`S PITOT HEATESDR ASAA2017072921507Unknown · failedCONDUCTED BLEEDS OFF TAKEOFF FOR KSAN CONDITIONS. UTILIZED NO ENGINE BLEED TAKEOFF PROCEDURES. APPROX ONE MINUTE AFTER DOING AFTER TAKEOFF PROCDURES NR 2 BLEED TRIP OFF LIGHT CAME ON. APPLIED BLEED TRIP OFF QRH PROCEDURES. BLEED TRIP OFF LIGHT EXTINGUISHED FORSDR ASAA2017071921419Battery · failedMAIN BATTERY SHOWS CONSTANT 2 AMP CHARGE. ACFT GROUNDED. REMOVED AND REPLACED MAIN AND AUXILIARY BATTERIES IAW AMM 24-31-11. GROUND VERIFICATION GOOD.SDR ASAA2017071721403Fmc · malfunctionedRIGHT FMC FAILED. ACFT GROUNDED. PERFORMED FIM 34-61, TASK 836, & RT FMC RESTORED. GROUND FUNCTIONAL TEST OF RT FMC PASSED IAW AMM 34-61-00-710/801.SDR ASAA2017071121345Shutoff Valve · leakingDURING ACCOMPLISHMENT OF BLEED AIR HEALTH CHECK T/C NG-36WC-00001, FOUND THE NR 1 ENGINE PRSOV LEAKING AT DIAPHRAGM SPLIT LINE. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE PRSOV IAW AMM 36-11-04. LEAK & OPS CHECKED GOOD. T/C NG-36WC-00001 CHECKED GOOSDR ASAA2017060320942Autoland Sys · malfunctionedWHILE PERFORMING AN AUTOLAND-HGS APPROACH FOR THE APPROACH SURVEY, RECEIVED A APPROACH WARNING BELOW 50 FT. REASON IS UNKNOWN. DISCONNECTED AND LANDED. ACFT GROUNDED. RESET SYSTEM AND RAN LAND VERIFY TEST IAW AMM 22-11-00/201, OPS CHECKED GOOD.SDR ASAA2017060120932Display · malfunctionedFMC DISAGREE INDICATION ON BOTH CAPTAIN`S & FIRST OFFICER`S NAVIGATIONAL DISPLAY THROUGHOUT FINAL APPROACH. CLEARED UPON LANDING. ACFT GROUNDED. PERFORMED A CIRCUIT BREAKER RESET IAW FIM 34-61, TASK 835 MESSAGE DID NOT SHOW UP. SYSTEM OPERATES NORMAL.SDR ASAA2017042820568Control Valve · failedBLEED TRIP OFF ON ROTATION. RAN QRH ONCE CLEANED UP. BLEED RESET MOMENTARILY THEN TRIPPED AGAIN. RIGHT BLEED PSI INDICATED EQUAL 0 DURING BLEED TRIP. GROUNDED - YES. AIR TURNBACK - PERFORMED ENGINE BLEED HEALTH CHECK PER AMM 36-11-00, HEALTH CHECK GOOD. PERFORSDR ASAA2017042320523Regulator · failedAFTER ROTATION, THE BLEED TRIP OFF LIGHT ILLUMINATED ON THE NR 2 ENGINE. FOLLOWED QRH AND LIGHT DID RESET FOR 10 SECONDS AND CAME BACK ON, DISCUSSED WITH MAINTENANCE CONTROL AND TRIED ANOTHER RESET AT FL 340 AFTER 5 MINUTES AT CRUISE POWER, RESET WORKED. ACFTSDR ASAA2017032120239Harness · damagedNR 2 ENGINE RIGHT SIDE CORE AREA J9 HARNESS AT 1:00 POSITION HAS DAMAGE TO OUTER CLOTH SHEATH MEASURING 1.10 INCHES LONG 3 INCHES FROM T3 SENSOR CONNECTOR DP0905. NO DAMAGE TO METALLIC SHEATH NOTED. ACFT GROUNDED. REMOVED T3 SENSOR CONNECTOR DP0905 FROM T3 SESDR ASAA2017032120238Wire Harness · damagedNR 2 ENGINE RIGHT SIDE CORE AREA F10 HARNESS AT 1 O`CLOCK POSITION HAS DAMAGE TO OUTER CLOTH SHEATH MEASURING 1 INCH LONG, 2.5 INCHES FROM T3 SENSOR CONNECTOR DP1005. NO DAMAGE TO METALLIC SHEATH NOTED. ACFT GROUNDED. REPAIRED AFFECTED AREA IAW AMM 70-70-SDR ASAA2017032120235Wire Harness · damagedNR 2 ENGINE, LEFT SIDE CORE AREA MW0326 HARNESS AT 11:00 POSITION HAS THREE AREAS OF DAMAGE. FIRST AREA HAS THE HARNESS SHIELD SHEATH COMPLETELY MISSING IN A SIX INCH AREA BETWEEN TO CLAMPS BELOW PRECOOLER. SECOND AREA HAS DAMAGE TO OUTER SHIELD SHEATH 2.30 INSDR ASAA2017032120234Wire Harness · damagedNR 2 ENGINE, RIGHT SIDE CORE AREA MW0325 HARNESS AT 3:00 POSITION SIX INCHES FORWARD OF RIGHT CORE DETECTOR LOOP HAS 5 INCHES OF HARNESS SHIELD SHEATH MISSING BEHIND PNEUMATIC DUCT. ACFT GROUNDED. REMOVED & REPLACED FIRE DETECTION HARNESS IAW AMM 26-11-02. ESDR ASAA2017011619406Actuator · malfunctionedALL THREE ZONE TEMP LIGHTS ON AT THE SAME TIME, NO CONTROL OF ALL THREE TEMPS. LIGHTS EXTINGUISH ON MASTER RECALL. ACFT GROUNDED. REMOVED AND REPLACED THE RT RAM AIR DOOR ACTUATOR IAW AMM 21-51-21. PERFORMED BONDING RESISTANCE CHECK. PERFORMED RT RAM AIR INSDR ASAA2017011119358Indicator · failedBOTH FWD AND AFT CABIN TEMP GAUGES FOR SUPPLY DUCT AND PACK READINGS ABNORMALLY LOW, 10 DEG C TEMP CONTROLS OPERATED NORMALLY. GROUNDED - YES. ACCOMPLISHED T/S PER FIM 21-61 TASK 857. NO DEFECTS NOTED. REMOVED AND REPLACED P5-17 TEMPERATURE CONTROL MODULE IAW SDR ASAA2016120318917Fmc · faultedRIGHT FMC FAILED. IAW QRH PUT BOTH FMC'S ON LEFT SIDE. ACFT GROUNDED. RIGHT FMC BITE SHOWED FMC-R FAULT "ETHERNET-2 WRAP" LOGGED AS AN INTERMITTENT FAULT FOR 8 OF THE LAST 10 LEGS. FAULT IS NOT DEFINED IN FAULT ISOLATION MANUAL. REMOVED AND REPLACED RIGHT FLIGSDR ASAA2016120118909Valve · failedCOCKPIT AIR TEMP GAUGE DOES NOT ACCURATELY REFLECT THE TEMPERATURE SUPPLY DUCT, PAX CABIN, PACK TEMPS ALL READING AT OR BELOW 10 DEG C. F/A REPORTED CABIN TEMP OK OR SLIGHTLY WARM. ACFT GROUNDED. REMOVED & REPLACED THE TEMPERATURE CONTROL MODULE, IAW AMM 21-6SDR ASAA2016111318654Autothrottle Sys · malfunctionedAUTOTHROTTLES WILL NOT ENGAGE IN FLIGHT. ACFT GROUNDED. AUTOTHROTTLE BITE CHECKED IAW FIM 22-31 TASK 801 SHOWED FAULT 22-31687 ASM-1 LOGGED TWICE FOR LEG 9. PERFORMED TROUBLESHOOTING FOR FAULT 22-31687 IAW FIM 22-32 TASK 819 - AUTOTHROTTLE SERVO MOTOR TEST PASDR ASAA2016110918630Fmc · failedRIGHT FMC FAILED INFLIGHT. GROUNDED - YES. REPLACED RIGHT FMC COMPUTER. REF AMM 34-61-02/401. 4 C/B'S OPENED, TAGGED, TAGS REMOVED, AND 4 C/B'S CLOSED. INSTALLATION TESTS PASS. GROUND VERIFICATION SUCCESSFUL SEAMC DARREN NOTIFIED.SDR ASAA2016110718593Fmc · malfunctionedNR 2 FMC DISPLAYED VTK ON NR 2 DU. ACFT GROUNDED. PERFORMED FIM 34-61 TASK 807. AFTER NR 2 FMC RESET VTK NOT PRESENT ON F/O'S DU. ALL INDCATIONS NORMAL.SDR ASAA2016101518343Fmc · malfunctionedAFTER LANDING, BOTH FMCS BLANKED FOR APPROXIMATELY 15 SECONDS, BOTH FMCS RESTARTED NORMALLY WITHOUT ANY INPUT FROM PILOTS. ACFT GROUNDED. ACCOMPLISHED SYSTEM OPS CHECK IAW AMM 34-61-00, OPS NORMAL. NO HISTORY 30 DAYS.SDR ASAA2016101218315Door · bindingL1 DOOR VERY DIFFICULT TO OPEN. ACFT GROUNDED. ACCOMPLISHED GVI OF L1 DOOR. DOOR MECHANISM OPS CHECKS NORMAL. FOUND DOOR CREAKING WHEN MOVING TO FULL OPEN POSITION. LUBED UPPER/LOWER DOOR HINGES IAW AMM 12-25-11. OPS CHECKED NORMAL.SDR ASAA2016083117872Fan · obstructedON AIR TEMP CONTROLLER PANEL, FORWARD CABIN WAS VERY ERRATIC. TEMPERATURE WAS CONTROLLER BUT WOULD HAVE SEVERE TEMPERATURE SWINGS WITH VERY LITTLE MOVEMENT POSITION OF CONTROL KNOB. TEMP WAS ALMOST UNBEARABLE ACCORDING TO FAS, TOO HOT. CONTROLLER TO "OFF" ASDR ASAA2016081017706Channel · corrodedAFT CARGO BAY, RT TRANSITION PANEL IS CORRODED AT BS 727L. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-00-53, AND FOUND TO BE OUT OF LIMITS. REMOVED THE TRANSITION PANEL IAW SRM 53-00-53 AND FABRICATED NEW CHANNEL SIDEPLATE AND SPLICE SIDEPLATE IAW SRM 53-SDR ASAA2016072317472Keyboard · damagedLEFT MCDU, LINE SELECT KEYS 4L AND 5L COVER TORN FROM USE. ACFT GROUNDED. REPLACED MCDU KEYBOARD ASSEMBLY IAW AMM 34-61-00. OPS CHECKED OK.
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