N590AS
Service difficulty reports · 440
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 = 'N590AS' 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 = 'N590AS' 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 ASAA2013011193655Sensor · failedRT PACK CAUTION LIGHT ILLUMINATED DURING CLIMB, RESET ONCE, THEN PACK LIGHT ILLUMINATED AGAIN. RT RAM DOOR FULL OPEN LIGHT ILLUMINATED DURING CLIMB AND CRUISE AT FL300 WITH FLAPS UP. ACCOMPLISHED FIM TASK 21-53, TASK 818, STEPS A.-E.(3)(A). COULD NOT DUPLICSDR ASAA2013010593618Unknown · unknownRT BLEED TRIPPED TWICE, FL 390 EARLY IN FLIGHT. RESET TWICE THEN OPS NORMAL. ACCOMPLISHED ENG BLEED TRIP FIM TASK 36-10-TASK 809. NO DEFECTS NOTED AT THIS TIME. NO HISTORY IN 90 DAYS. VERIFICATION FLIGHT SATISFACTORY.SDR ASAA2012121193440Battery · inoperativeMAIN BATTERY AND AUX BATTERY SHOW A CONSTANT 3 AMP CHARGE DURING FLIGHT. REPLACED MAIN BATT IAW MM 24-36-11. REPLACED AUX BATTERY IAW MM 24-31-11. NO FAULTS NOTED. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2012120293393Warning Light · false activationFMC DISAGREE ON GROUND. FOLLOWED QRH, DISAGREE RESOLVED.SDR ASAA2012110593246Overheat Sensor · malfunctionedIN FLT, RT WING BODY OVERHEAT ILLUMINATED AND RAN CHECK LIST. REPLACED M371 AND M269 OVERHEAT SENSOR ELEMENTS, REF MM 26-18-02. OPS CHECKS NORMAL IAW SAME. RAN RT ENGINE WITH RIGHT BLEED AND PACK ON, NO FAULTS FOUND.SDR ASAA2012110293223Module · inoperativeAPU BLEED SWITCH ROTATES, LOCKING DETENT NOT ALIGNED. R & R AIR CONDITIONING MODULE ASSY IAW NG AMM 21-25-02-400-801 AND 36-21-02-600-02. OPS CHECKED GOOD.SDR ASAA2012103193219Keyboard · stuckFIRST OFFICER`S FMC KEYPAD L6 BUTTON STICKY. ACFT GROUNDED. R & R F/O FMC KEYBOARD & OPS CHECKED GOOD IAW AMM 34-61-01-400-801.SDR ASAA2012102193208Floorbeam · corrodedFWD CARGO FLOORBEAM AFT BULKHEAD FS 500I. R & R FLOORBEAM IAW SRM 51-40-02.SDR ASAA2012102193207Floor Panel · corrodedFWD CARGO BAY, FLOOR PANEL 120DF HAS LIGHT CORROSION AROUND THE EDGES. FOUND CORROSION TO BE OUT OF LIMITS ON FLOOR PANEL IAW SRM 53-00-53. FABRICATED NEW FLOOR PANEL IAW DWG 453A1610-20.SDR ASAA2012102193169Floor Panel · corrodedFWD CARGO BAY FLOOR PANEL 120AF HAS CORROSION AT FWD EDGE. FOUND CORROSION ON PANEL TO BE OUT OF LIMITS WITH MORE THAN 3" IN DIAMETER IAW SRM 53-00-53. FABRICATED NEW PANEL IAW DWG 453 A 1610-14 REVE AND SRM 51-40-02.SDR ASAA2012090492827Fastener · looseNR 2 ENG INLET HAS 15 LOOSE FASTENERS ON LIPSKIN, BETWEEN 2 & 10 O`CLOCK POSITION. R & R FASTENERS IAW SRM 51-40-02 REF CMM 71-11-22.SDR ASAA2012092992969Detector · failedAPU FIRE TEST FAILED. ACFT GROUNDED. PERFORMED BITE TEST 26-10-00-810-802. RECEIVED TAILPIPE DETECTOR FAULT. REPLACED APU OVERHEAT DETECTOR ASSY. OPS CK GOOD. REF AMM 26-15-01.SDR ASAA2012080392662Panel · damagedNR 1 ENGINE INLET AND FAN BLADES DETAILED INSPECTION FOUND ONE SCREW MISSING AND NUTPLATE MISSING AT 6 O`CLOCK POS ENGINE NOSE COWL LWR VENT PANEL (M). APPLICABLE HOLE IS OVERSIZED & PULLED THRU. R & R WITH NEW PANEL IAW SRM 51-40-02 AND SEALED IAW SRM 51-20-SDR ASAA2012080392667Bleed Valve · failedPRESSURIZATION DUCT, PRESSURE IS 18 PSI, N1 97 IN CLIMB. IN CRUISE N1 87.5 LT DUCT PRESSURE 20 PSI. RT DUCT PRESSURE 36 PSI. DURING DESCENT THROUGH 30,000 FT, N1 37 BOTH LT & RT DUCT PRESS 19 PSI. ACCOMPLISHED T/C NG-36WC-00001 FOR NR1 ENG BLEED AIR SYS HEASDR ASAA2012080392661Bolt · damagedNR 1 ENG INLET AND FAN BLADES DURING DETAILED INSPECTION, FOUND ONE SCREW LOOSE, AND APPEARS TO BE SHANKED OUT WITH DAMAGE TO FASTENER COUNTERSINK, AT 2:30 O`CLOCK POS, ALF (M), IN ENGINE NOSE COWLING. REMOVED FASTENER AND COUNTER SINK WASHER AND REPLACED WISDR ASAA2012081792734Sensor · failedNR 2 BLEED TRIP OFF LIGHT ILLUMINATED DURING DECENT WITH THROTTLES REDUCED POWER, NR 1 DUCT 30 PSI, NR 2 DUCT DUCT 12PSI. RAN QRH, COULD NOT RESET. ACFT GROUNDED. COMPLIED WITH PRECOOLER CONTROL VALVE HEALTH CHECK, OPS NORMAL IAW 36-12-00-700-802. R & R NR SDR ASAA2012081192689Warning Light · false activationELECTRIC FAULT LIGHT ILLUMINATED DURING POWER UP. ACFT GROUNDED. PERFORMED ELECTRIC LIGHT MESSAGE LIGHT CHECK IAW FIM 24-31-00. SPCU INOPERATIVE I CODE FAULT. CODE CLEARED, NO FURTHER DEFECTS NOTED.SDR ASAA2012072592608Acoustic Panel · damagedNR 2 ENGINE, FAN ACOUSTICAL PANEL AT 1100 POSITION, LOWER CENTER BOLT HAS PULLED THROUGH PANEL. ACFT GROUNDED. R & R NR 2 ENG FAN ACOUSTICAL PANEL 1100 POS, REF AMM 72-23-07.SDR ASAA2012071892560Keyboard · wornCAPTAIN'S FMC KEYBOARD WORN. REMOVED & INSTALLED CAPTAIN'S FMC CDU KEYBOARD ASSY. OPS NORMAL REF SAME MM.SDR ASAA2012062792434Connector · damagedSEVERAL EMERGENCY LIGHTS RT AFT PORTION OF ACFT ARE INOPERATIVE. FOUND GROUND PIN FOR UNIT M1672 PULLED OUT OF BLOCK GD3889, RESECURED GROUND PIN, OPS CHECK GOOD IAW AMM 33-51-00.SDR ASAA2012062192400Lens · looseCOVER OF EXIT SIGN CAME LOSE FROM SIGN ON CABIN OVERHEAD AT MID CABIN. ACFT GROUNDED. REINSTALLED COVER EXIT MID CABIN.SDR ASAA12511623Warning Light · illuminated"FMC DISAGREE" DISPLAYED IN BOTH FMC CDU'S. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. NORMAL OPS RESTORED.SDR ASAA12511597Fmc · malfunctionedWHILE TAXIING TO THE GATE AFTER LANDING, FMC DISAGREE LIGHT CAME ON. ACFT GROUNDED. RESET NR 2, FMC OPS RESTORED, FMC DISAGREE LT OFF. BITE CHECKED OK IAW MM 34-61-01. GROUND VERIFICATION OF ETOPS SIGNIFICANT SYS OK. ACFT OK FOR SERVICESDR ASAA12511585Control Valve · malfunctionedRT BLEED TRIP OFF LIGHT ILLUMINATED AT TOP OF DESCENT RESET IAW QRH PROCEDURE. ACFT GROUNDED. ACCOMPLISHED T/C NR NG 36WC 00001. FOUND NR 2 ENG PRSOV HARD TO OPEN & CLOSE & NR 2 ENG PRECOOLER CONTROL VALVE DOES NOT FUNCTION PROPERLY. REPLACED NR 2 ENG PRSOVSDR ASAA12511475Fmc · unknownF/O FMC INTERMITTENTLY WOULD NOT ALLOW TO BRING UP FIX TO TOP (D TO FIX). ACFT GROUNDED. OPS CHECK OF FMC GOOD ALL KEY INPUTS OPS NO FAULTS. SYS OPS NORMAL. REF MM 34-61-00.SDR ASAA12511382Fmc · malfunctionedDURING TAXI OUT, FMC DISAGREE MESSAGE ILLUMINATED ON NAV DISPLAYS. PERFORMED QRH PROCEDURE AND NORMAL OPS WAS RESTORED.SDR ASAA12511358Control Unit · malfunctionedR2 WINDOW HEAT "ON" LIGHT GOES ON & OFF WITH WINDOW BELOW OPERATING TEMP. VERIFIED WINDOW HEAT FILM & SENSOR RESISTANCE GOOD PER 30-41-21. REPLACED WINDSHIELD HEAT CONTROL UNIT PER 30-41-11. SYS OPS CHECKED NORMAL.SDR ASAA12511287Unknown · malfunctionedAUTOTHROTTLES ARMED FOR TAKEOFF TOGA BUTTON PUSHED A/T DISARMED RE-ARMED PRESSED TOGA A/T DISARMED AGAIN. PERFORMED AUTOTHROTTLE BITE PROCEDURE PER RIM TASK 22 31 00 810 801. LEG 01 AND 03 LOGGED MSG 22 31687. ACCOMPLISHED FIM TASK 22 32 00 810 819. AUTOTHSDR ASAA12511246Unknown · malfunctionedDUAL "FMC FAIL" ANNUNCIATED ON BOTH ND'S ON GROUND SAN. ACCOMPLISHED QRH. OPS NORMAL.SDR ASAA12511157Unknown · malfunctionedRECEIVED FMC DISAGREE MESSAGE ON SCRATCH PAD. RAN QRH PROCEDURE. RESET FMC AND IT WENT AWAY.SDR ASAA12511060Transceiver · inoperativeNR 1 HF RADIO INOP. PERF HF NR 1 FAULT ISOLATION PER 23 11 00 810 803. CONFIRMED NR 1 HF TRANSCEIVER INOP. REPLACED NR 1 HF TRANSCEIVER PER 23 11 00 810 803/400 801, OPS CHECK NORMAL PER SAME.SDR ASAA12510895Unknown · malfunctionedFMC DISAGREE ON TAXI OUT AT PDX. ACCOMPLISHED QRH PROCEDURE. LIGHT EXTINGUISHED.SDR ASAA11510858Battery Pack · failedREF T/C 78233001: EMERGENCY LIGHT BATTERY PACKS M1672 & M1675 FAILS CAPACITY CHECK. REF WDM 33 51 12 & 33 51 14. REPLACED AND TESTED EMERGENCY LIGHT BATTERY PACKS M1675 & M1675 PER MM 33 51 06 960 805, OPS NORMAL.SDR ASAA11510750Switch · faultyNR 2 ENG START SWITCH DID NOT SWITCH OFF AT 56 PERCENT. REPLACED NR 2 ENGINE START SWITCH PER M/M 80 11 00, OPS CHECKS GOOD PER SAME.SDR ASAA11510593Unknown · malfunctionedAFTER START CHECKLIST AFTER PUSHING RECALL MASTER CAUTION LIGHT AND A/C LIGHT (CONT CABIN ZONE TEMP) REMAINED ILLUMINATED. QRH COMPLETED. A/C LIGHT GOES OUT AFTER PUSHING MASTER CAUTION RESET. SEAMC CONTACTED. NR 2 CONTROLLER LOGGED FLT DECK TRIM VALVE FAULSDR ASAA11510487Switch · failedDURING NR 1 ENG START ENGINE START SW FAILED TO TURN OFF AUTOMATICALLY AND START VALVE REMAIN OPEN AND FLASHING BEYOND 56 PERCENT N2. REPLACED NR 1 ENGINE START SWITCH REF WDM 80 11 11. NR 1 ENGINE START SWITCH TEST NML REF MM 80 11 00.SDR ASAA11510475Window · faultyL SIDE WINDOW OVHT DURING FLIGHT. WOULD NOT RESET PER QRH. REPLACED CAPTS NR 2 OPEN ABLE WINDOW PER MM 56 12 11 400 801. ACCOMPLISHED OPS & FUNCTIONAL CHECKS NO DEFECTS NOTED. WINDOW HEAT OPS TEST GOOD PER MM 30 41 00 710 80. ACCOMPLISHED FLT DECK NR 2 WISDR ASAA11510474Unknown · malfunctionedCAPTAINS NR 2 WINDOW HOT TO TOUCH NO OVERHEAT LIGHT. MEASURED RESISTANCE FOR CAPT'S SLIDER WINDOW TEMP SENSOR (STBY) AND HEATER ELEMENT REF WDM 30 41 12 AND MM 30 41 21. ALL VALUES WITHIN LIMITS. CAPT'S SLIDER WINDOW HEAT OPS NORMAL REF MM 30 41 00.SDR ASAA11510471Unknown · malfunctionedLEFT SIDE WINDOW OVERHEAT LT ON TURNED OFF THEN BACK ON AND OVERHEAT LT AGAIN. WHCU BITE SHOWS SENSOR FAULT. SWAPPED TO SPARE SENSOR AT WINDOW PER FIM 30 41 TASK 811. OPS CHECK FAIL. WHCU BITE NOW SHOWS P5 9 FAULT. SENSOR FAULT CLEARED. SWAPPED WHCU WITHSDR ASAA11510425Valve · failedFOLLOW UP TO RECENT RIGHT PNEUMATICS BLEED TRIP IN FLIGHT. PRECOOLER VALVE FAILED TO OPEN PROPERLY WOULD BARELY MOVE OFF FULL CLOSED DOWN TO 3 PSI AND WOULD ONLY OPEN PROPERLY AT 1 PSI. REPLACED PRECOOLER VALVE PER MM 36 12 02. VERIFIED CORRECT OPERATION PRSDR ASAA11510415Valve · malfunctionedRIGHT BLEED TRIP OFF LIGHT ON INFLIGHT. RESET PER QRH. FOUND RIGHT HIGH STAGE VALVE NOT CLOSING FULLY. CHANGED OUT NR 2 HIGH STAGE VLV SEE 36 11 06 000 801 AND 36 11 06 400 801 AND 71 00 00 700 821 F00. LEAK CHECK GOOD.SDR ASAA11510363Drive Unit · defectiveRADAR IMAGE ON CAL/MAX OR 3 WITH STAB ON IS "SPOKING". IMAGE SPOKES IN ALL QUADS OF SCREEN. REPLACED WEATHER RADAR ANT DRIVE UNIT PER M/M 34 43 11. PERFORMED WXR SYSTEM OPS TEST, OPS TEST GOOD.SDR ASAA11510326Transceiver · failedPAST "'RP" WX RADAR "WX FAIL" ANNUNCIATED ON ND. IN TEST MODE "PWS FAIL AND WX FAIL" ANNUNCIATED. THE REST OF FLIGHT RADAR WAS INTERMITTANT. WX WAS VFR EN ROUTE. FAILURE OCCURED IN ETOPS AIRSPACE. REPLACED WEATHER RADAR TRANSCEIVER PER M/M 34 43 41. PERFOSDR ASAA11510324Unknown · malfunctionedWX FAIL AND PWS FAIL MESSAGES DISPLAYED WITH RADAR FAILURE. RESTORED WX RADAR SYSTEM REF AMM 34 43 00 710. SYS OPS NORMAL GROUND VERIFICATION OF SYSTEM CHECKS OK.SDR ASAA11510195Unknown · malfunctionedFMC DISAGREE LIGHT ON TAXI OUT. PERFORMED QRH PROCEDURE. RESTORED FMC OPS TO NORMAL.SDR ASAA1150101Control Valve · malfunctionedLEVEL AT 380 "BLEED TRIP OFF" LIGHT ILLUMINATED. TRIP RESET BUTTON EXTINGUISHED LIGHT (RIGHT PACK). REPLACED PRE COOLER CONTROL VALVE AND PRSOV REF MM 36 12 02 400 801 AND 36 11 04 400 801. ENG BLEED AIR SYS HEALTH CK REF MM 36 11 00 700 801 STEPS G (1) (8)SDR ASAA11510080Regulator · defectiveDURING CLIMBOUT PASSED FL 370 WITH THE WING ANTI ICE OFF RIGHT BLEED TRIP OFF LT ILLUMINATED. RAN QRH PROCEDURE DURING CLIMB & LIGHT WENT OUT. LIGHT RE-ILLUMINATED 30 SECONDS LATER. RAN QRH PROCEDURE AGAIN AT CRUISE WITH REDUCED POWER SETTING & LIGHT WENT OSDR ASAA11510063Warning System · intermittentAT TOP OF CLIMB FL350 WITH WING ANTI ICE OFF THE RIGHT BLEED TRIP ILLUMINATED. WENT OUT AFTER RESET. ACCOMPLISHED FIM TASK 36 10 00 810 801 NO FAULTS NOTED. PERFORMED GROUND VERIFICATION TEST PER FIM TASK 36 10 00 810 801 GROUND VERIFICATION SUCCESSFUL. NOSDR ASAA1159985Unknown · malfunctionedAUTOLAND TOUCHED DOWN APPX IN LINE WITH LEFT HASH MARK OF RUNWAY WHILE CORRECTING TO THE RIGHT. PERF'D DFCS CURRENT STATUS TEST REF AMM 22 11 00 NO FAULTS BUT FLIGHT FAULT REVIEW REVEALED BOTH A/P'S WITH "VOR/LOC BEAM ANOMALY DETECTED" DURING APPCH/FLARE. ACSDR ASAA1159760Control Panel · lockedFIRST OFFICER'S FMC CONTROL PANEL IS LOCKED UP ON POS REF PAGE 2. INFORMATION INPUT BUTTONS DO NOT RESPOND TO INPUT. C/W FIM TASK 34 61 00 SYSTEM GROUND FUNCTION CHECK GOOD. NO FAULTS NOTED.
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