N593AS
Service difficulty reports · 521
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 = 'N593AS' 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 = 'N593AS' 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 ASAA2016103118528Valve · failedFWD PACK CONTROLLER WAS INOPERATIVE, DUCT TEMP WAS STUCK ON 14, WOULD NOT MOVE REGARDLESS OF TEMP CONTROLLER POSITION. ACFT GROUNDED. PERFORMED PACK TEMP CONTROL BITE IAW FIM 21-62-801. TRIM VALVE ZONE FAULT ON NR 2 CONTROLLER. DURING TROUBLESHOOTING FOUND SDR ASAA2016103018517Valve · failedFWD CABIN ZONE TEMP, GOES OUT WITH RECALL. GROUNDED, YES. PERFORMED BITE TEST OF PACK/ZONE TEMP CONTROLLER. FOUND FAULT, ZONE TRIM VALVE ON NR 2 CONTROLLER WILL NOT CLEAR. REMOVED AND REPLACED FWD CABIN TRIM VALVE, REF AMM 21-61-21. BITE CHECK GOOD. LEAKSDR ASAA2016102418470Actuator · failedRIGHT PACK LIGHT ILLUMINATED, RESET WITH TRIP RESET AND LIGHT EXTINGUISHED MOMENTARILY, THEN ILLUMINATE AGAIN, ISOLATED TO SINGLE PACK OPERATION. ACFT GROUNDED. REMOVED AND REPLACED RIGHT RAM AIR INLET ACTUATOR IAW AMM 21-51-21/401. RAM AIR ACTUATOR INSTALLASDR ASAA2016092018084Coupler · dirtyREF LOG PAGE 11584611, FVR FAILED DUE TO BOTH HF RADIOS LOW END INOPERATIVE. ACFT GROUNDED. REF TSR817982: CLEANED AND RESEALED COUPLER TRAY AND ANTENNA BONDING POINTS. ACCOMPLISHED HF 1 AND HF 2 OPS AND SYSTEM TEST, REF AMM 23-11-00-710-801 AND AMM 23-11-0SDR ASAA2016091518046Coupler · failedCOULD NOT TRANSMIT HF2 FREQUENCIES 6.640 AND 11.342 FROM CAPTAIN'S OR F/O'S RADIO PANEL. ACFT GROUNDED. COULD NOT ISOLATE FAULT TO NR 1 COUPLER BY REMOVING POWER FROM SYS 1 AND TRANSMITTING ON NR 2 PER ENGINEERING NOTE IN PREVIOUS T/S. DUE TO HISTORY REPLACSDR ASAA2016090818006Coupler · failedUNABLE TO TRANSMIT ON EITHER HF RADIO, TRIED MULTIPLE HF FREQUENCIES. WHEN TRANSMITTING, CONTINUOUS SIDE TONE. RECEIVED HF OK. ACFT GROUNDED. TRIED HEADSET AND MICROPHONE AT FACE OF BOTH HF R/TS. ABLE TO RECEIVE, UNABLE TO TRANSMIT BOTH SIDES. REMOVED BOSDR ASAA2016081817847Web · corrodedAFT CARGO THRESHOLD WEB IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW IAW SRM 53-11-52-020-801. FABRICATED NEW THRESHOLD WEB IAW DWG 146A8123 REV-. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02, AND DWG 146A8340 REV-.SDR ASAA2016081817840Transition Panel · corrodedAFT CARGO LT TRANSITION PANEL HAS CORROSION FROM BS 727B TO 727I. ACFT GROUNDED. INSTALLED A NEW TRANSITION PANEL IAW DWG 146A7500 REV- AND B737-800 SRM 53-00-53-2R-5.SDR ASAA2016081817839Transition Panel · crackedAFT CARGO RT TRANSITION PANEL HAS CRACKS AND CORROSION BS 727C TO 767. ACFT GROUNDED. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 51-40-02, DWG 146A7502, AND SRM 53-00-53-2R5.SDR ASAA2016081817837Transition Panel · corrodedFWD CARGO LT TRANSITION PANEL IS PUNCTURED AT BS 500G. ACFT GROUNDED. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 51-00-53-2R-5SDR ASAA2016081817836Transition Panel · corrodedFWD CARGO RT TRANSITION PANEL IS PUNCTURED AT BS 500A+18. ACFT GROUNDED. REMOVED AND REPLACED THE TRANSITION PANEL IAW DWG 143A7500 REV- AND SRM 53-00-53-2R-5.SDR ASAA2016081879722Floor Support · corrodedAFT PIT FLOOR SUPPORT, BS 767+4, RBR 13.84 IS CORRODED. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .070, REMOVED .014 REMAINING MATERIAL IS .056 FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 DETAIL-D/FFIG 103 USED UT GAGE T8225V REPAIRED FSDR ASAA2016081717830Floor Support · corrodedAFT PIT FLOOR SUPPORT, BS 767+4, RBR 13.84 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION ORIGINAL THICKNESS .070, REMOVED .014 REMAINING MATERIAL IS .056 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2, DETAIL-D/F FIG 103 USED UT GAGE T8225V, REPAIRED FLOOR SDR ASAA2016080717637Fmc · malfunctionedON DOWNWIND, FMC DISAGREE ILLUMINATED, RAN QRH, IT RESET. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE PER QRH. FMCS RESTORED NORMAL.SDR ASAA2016072517510Actuator · leakingFOUND NR 2 ENGINE RIGHT VSV LEAKING AT DRAIN BELOW THRESHOLD LIMITS. ACFT GROUNDED. R & R NR 2 ENGING OTBD ACTUATOR IAW AMM 75-31-01-400-802-F00. ACCOMPLISHED LEAK CHECK OF VSV ACTUATOR IAW AMM 75-31-01-790-801-F00. NO LEAKS NOTED. ACCOMPLISHED GROUND VERSDR ASAA2016072017444Actuator · failedWHILE PERFORMING T/C 78273000, FOUND MAINTENANCE MESSAGE 75-10452, THE VBV POSITION SIGNALS DISAGREE, FLIGHT LEG 2 SHORT TIME. ACFT GROUNDED. R & R NR 2 ENGINE RT VBV ACTUATOR, OPS CHECK & LEAK CHECK GOOD. NO FAULTS FOUND, REF AMM 75-32-02.SDR ASAA2016071817418Satcom · lockedSATCOM LOCKUP OCCURRED DURING POWER TRANSFER. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE IAW QRH. SATCOM OPS RESTORED NORMAL.SDR ASAA2016070617282Satcom · lockedSATCOM LOCK NOTED. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE PER QRH. SATCOM OPS RESTORED NORMAL.SDR ASAA2016070217238Engine · malfunctionedON DEPARTURE NR 2 EGT WENT AMBER WITH 27K BUMP POWER. THIS HAPPENED BRIEFLY DURING CLIMB. ACFT GROUNDED. ACCOMPLISHED FIM 71-06 TASK E04 EEC FOR NR 2 ENGINE, LOGGED NO FAULTS IN RECENT OR FAULT HISTORY. STEPS A THRU E (2) ACCOMPLISHED ABOVE. ACCOMPLISHED HPT SDR ASAA2016070217216Computer · faultedON DEPARTURE FROM HNL AUTOTHROTTLE TURNED OFF AND I WAS NOT ABLE TO REARM. GROUNDED - YES. A/T BITE CURRENT STATUS NO FAULTS. FLIGHT FAULTS REVIEW SHOWS NUMEROUS FAULTS LAST LEG ONLY MESSAGE 22-31543 A/T 28VDC INV. REPLACED FCC-A IAW AMM 22-11-33, INSTLN TESTSDR ASAA2016070117239Case · crackedWHILE ACCOMPLISHING NR 2 ENGINE INLET INSPECTION T/C 7847100, FOUND FAN CASE FLANGE B-1 CRACKED AT 11 O'CLOCK LOOKING FWD AT BRACKET FOR FIRE DETECTOR TRANSPONDER. ACFT GROUNDED. REPAIRED FAN CASE B-1 FLANGE IAW T/C SBCFM56-7B-72-0580-1, OPS AND LEAK CHECKEDSDR ASAA2016061217020Warning System · false activationWHILE PERFORMING T/C 78273000, FOUND MAINTENANCE MESSAGE 75-30452, THE VBV POSITION SIGNALS DISAGREE, FLIGHT LEG 9 SHORT TERM. ACFT GROUNDED. ACCOMPLISHED T/C 78273000, NO CURRENT FAULTS, OR FAULT HISTORY.SDR ASAA2016053116905Warning Light · false activationAUTO FAIL LIGHT & ALTN LIGHT ILLUMINATED ON PRESSURIZATION PANEL. ACFT GROUNDED. PERFORMED PRESS CONTROL MANUAL MODE TEST IAW AMM 21-31-00. ALL FAIL LIGHTS INDICATION NORMAL. NO FAULT LIGHTS NOTED. OK FOR CONTINUED SERVICE. FAULT OCCURRED AT POWER TRANSFER.SDR ASAA2016052816865Computer · failedAUTOTHROTTLE WILL NOT ENGAGE. ACFT GROUNDED. ACFT RELEASED IAW MEL 22-4B A/T SYS INOPERATIVE. A/T INFLT REVIEW SHOWED ON 3 FLTS A TOTAL OF 54 FAULTS OF A/T ENG 28VDC INV 22-31543, SUSPECT LRU FCC-A. PERFORMED FIM 22-31, TASK 802 AND 801. A/T BITE PROCEDURE SDR ASAA2016052716880Warning Light · illuminatedWHEN STARTING NR 1 ENGINE UPON RAISING START LEVER TO IDLE, THE ENGINE VALVE CLOSED, LIGHT REMAINED ILLUMINATED BRIGHT. ACFT GROUNDED. RESET HPSOV IND C/B NR 1 ENGINE. CHECKED, ENGINE VALVE CLOSED, LIGHT OPERATION IAW FIM 73-06, TASK 805. OPERATION NORMAL.SDR ASAA2016052616841Fire Loop · failedFOLLOW-UP TO RECENT HISTORY WITH NR 2 ENGINE FIRE WARNING LOOP A TEST FAIL. ACFT GROUNDED. R & R NR 2 CORE FIRE LOOP HARNESS MW0325, REF AMM 26-11-02. OPS CHECK OK.SDR ASAA2016052316832Eec · failedNR 2 ENGINE IGNITION SYS, R, SIDE FAILED TO START ENGINE LT IGNITION START ATTEMPT GOOD. ACFT GROUNDED. PERFORMED NR 2 ENGINE IGNITION SYS AUDIBLE TEST, REF AMM 74-00-00. NR 2 ENGINE RT IGNITION SYS CHANNEL B AUDIBLE TEST FAILED. PERFORMED FIM TASK 74-21, TASDR ASAA2016051616755Fire Loop · faultedNR 2 ENGINE FIRE LOOP "A" APPEARS TO HAVE A FAULT. ACFT GROUNDED. REF AMM TASK 26-10, TASK 801 INITIAL EVALUATION BITE TEST OF M279 MODULE NR 2 ENGINE A LOOP FAILED TO ILLUMINATE. CYCLED A/C POWER. CYCLED FIRE CONTROL HANDLE. FAULT CLEARED. RAN GROUND ENGINESDR ASAA2016050316643Eec · failedWHILE PERF T/C 78273000 FOUND NR 2 ENGINE W/ SHORT TIME FAULT 75-20452, THE VBV POS SIGNALS DISAGREE. ACFT GROUNDED. REPLACED NR 2 ENG ELECTRONIC ENGINE CONTROL. OPS CK GOOD. REF AMM 73-21-60 & B737-800, IPC 73-21-60-01A.SDR ASAA2016033116188Control Valve · failedRIGHT PACK TRIP. WILL NOT RESET. ACFT GROUNDED. ACCOMPLISHED BITE PROCEDURE OF ZONE/TEMP CONTROLLERS IAW FIM 21-62, TASK 801. NO DEFECTS NOTED IN ANY PORTION OF TEST. REMOVED PANEL 192BR, RAM AIR DUCT PANEL AND INSPECTED HEAT EXCHANGER FOR DEBRIS AND BLOCKAGSDR ASAA2016030715793Satcom · malfunctionedHAD NO SATCOM PROMPT ON MCDU. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE IAW QRH. SATCOM OPS NORMAL.SDR ASAA2016022415656Plate · out of positionPLATE COVERS ALTITUDE INTERVENTION BUTTON. ACFT GROUNDED. R & R MCP REF AMM 22-1-34, OPS CHECK NORMAL. ACCOMPLISHED MCP LWMP CHECKS REF LWMP CHECKLIST AMM 22-00-01, ALL TEST PASSED.SDR ASAA2016021915582Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED DURING CLIMBOUT. RAN QRH PROCEDURE, LIGHT RE-ILLUMINATED. ISOLATED PACK AND TURNED OFF. ACFT GROUNDED. RESET - INTERMITTENT FAULT IAW FIM 21-53, TASK 802. NO FAULTS EITHER ZONE TEMP CONTROLLER. RAN RT PACK ON APU FOR 20 MINUTSDR ASAA2016021615484Warning Message · false activationON TAXI OUT FMC DISAGREE ANNUNCIATED ON BOTH PILOTS CDU'S. ACFT GROUNDED. ACCOMPLISHED FMC RESET PROCEDURES IAW QRH. FMCS OPS NORMAL.SDR ASAA2016021015434Fuel Nozzle · deterioratedWHILE ACCOMPLISHING NR 2 ENGINE LEAK CHECK , NOTE THE ORANGE HEAT SHIELD FOR THE FUEL NOZZLE MANIFOLD AT THE 6:30 POSITION TO BE DETERIORATED. ACFT GROUNDED. R & R ORANGE HEAT SHIELD FOR THE FUEL NOZZLE MANIFOLD AT THE 6:30 POSITION REF AMM 73-11-04-400-805-SDR ASAA2016012915182Satcom · malfunctionedSATCOM INOPERATIVE. NO SELECTION IN FMC DISPATCH TRIED TO CALL WITH NO SUCCESS. ACFT GROUNDED. CYCLED THE SATCOM CIRCUIT BREAKER IAW THE QRH PROCEDURES. ACCOMPLISHED SATCOM VOICE TEST FOR OUTGOING CALL AND INCOMING CALL TO DISPATCH SYS 1 AND 2. AMM 23-15-00SDR ASAA2016012915075Sending Unit · failedREF TSR 817439, FOUND NR 2 FUEL QTY TANK UNIT CAPACITANCE OUT OF TOLERANCE. ACFT GROUNDED. ACCOMPLISHED SYS TEST OF NR 2 FUEL QTY INDICATING SYS IAW AMM 28-41-00-730-801. FOUND NR 2 TANK TOTAL CAPACITANCE AT 414 PICOFARADS AND OUT OF LIMITS. ACCOMPLISHED TASDR ASAA2016011914923Probe · out of limitsAT CRUISE, NOTICED THE MAIN TANK WOULD DECREASE 10 LBS EVERY 6 MINUTES. CONTACTED MAINTENANCE CONTROL. ALL 6 FUEL PUMPS ON WHEN THIS HAPPENED. FOLLOWED IAW MAINTENANCE CONTROL, PREVIOUS CREW ACTIONS ON DEC 24TH. TRANSFEED VALVE OPEN, CENTER TANK FUEL PUMPS OSDR ASAA2015122714505Starter · failedNR 1 ENGINE FAIL TO START NR N2, N1, ROTATION CYCLED BLEEDS V CB'S, V LIST. ACFT GROUNDED. REPLACED NR 1 ENGINE STARTER, REF MM 80-11-01-000-801. PERFORMED ENGINE RUN FOR NR 1, OP'S CHECK NORMAL NO LEAK NOTED.SDR ASAA2015122614446Shutoff Valve · malfunctionedRIGHT PACK TRIP LIGHT 30 MIN INTO FLT AT 33.0 PACK TEMP REACH 60 DEGREE C. RESET OK, THEN TRIP LIGHT ON AGAIN, ISOLATED PACK & RTB. ACFT GROUNDED. INSPECTED RT RAM AIR DUCTS, FOUND NO DEBRIS. RAN RT PACK, GOOD AIRFLOW OUT OF RT PACK RAM AIR EXHAUST DUCT OSDR ASAA2015122314469Engine · faultedNR 2 ENGINE HAS RECENT FAULT 73-31372 UPPER EGT SECTORS READ HIGH, ECONOMIC FAULT. ACFT GROUNDED.SDR ASAA2015122214428Autothrottle Sys · failedAUTOTHROTTLES WILL NOT ENGAGE. ACFT GROUNDED. A/T BITE CURRENT STATUS MESSAGE 22-31543, CH-A ARM FAULT. REPLACED FCC-A, INSTLN TEST PASSED REF AMM 22-11-33. A/T BITE CURRENT STATUS "NO FAULTS" AFTER FCC-A REPLACEMENT.SDR ASAA2015122214427Transmitter · failedAUTO LAND TEST FAILED, FAULT CODE 22-11159. ACFT GROUNDED. REPLACED THE NR 9 SPOILER POSITION SENSOR IAW AMM 22-11-27/401. SPOILER POSITION SENSOR NR 9, OPS CHECKS GOOD IAW SAME AMM REFERENCE.SDR ASAA2015122114383Exciter · failedAPU WILL NOT START. FAULT LIGHT ILLUMINATED. ACFT GROUNDED. APU BITE TEST SHOWS FAULT CODE 49-41180, IGNITION CIRCUIT SHOWS HIGH CURRENT. REPLACED THE APU IGNITION UNIT IAW AMM 49-41-31 AND FIM 49-40, TASK 804. OPS CHECK GOOD WITH 4 SUCCESSFUL STARTS.SDR ASAA2015121914330Apu · failedWHILE OPERATING LT PACK ON APU AIR SOURCE, FLIGHT CREW OBSERVED 2 DUCT PRESSURE SURGES, GROUND CREW ALSO REPORTED THE SOUND OF THE APU EXHAUST SURGE. ACFT GROUNDED. R & R THE APU IAW TASK CARD 78349010. APU OPS CHECK PASS, NO SURGE.SDR ASAA2015121814309Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED IN FLIGHT. FOLLOWED QRH PROCEDURE, WOULD NOT RESET. ACFT GROUNDED. PERFORMED PACK/ZONE TEMPERATURE CONTROLLER BITE TEST IAW AMM TASK 21-61-00-700-806-002. CHECKED GOOD WITH NO FAULTS.SDR ASAA2015121514277Satcom · false indicationSATCOM FAILURE. ACFT GROUNDED. RESET THE CIRCUIT BREAKER IAW QRH. NORMAL OPS.SDR ASAA2015121414263Autothrottle Sys · disengagedAUTO THROTTLE DISENGAGED ON ITS OWN AND WOULD NOT RE-ENGAGE. ACFT GROUNDED. PERFORMED AUTO THROTTLE BITE TEST REF AMM TASK 22-31-00-710-801, NO DEFECTS NOTED. PERFORMED DFGS BITE TEST GROUP NR 43, NO DEFECTS NOTED.SDR ASAA2015112614004Engine · faultedFOUND ECONOMIC FAULT CODE 73-31371 ON NR 1 ENGINE WHILE ACCOMPLISHING FMC CDU INTERROGATION FOR ENGINE FAULTS IAW T/C 782730000. ACFT GROUNDED.SDR ASAA2015112614003Engine · faultedFOUND ECONOMIC FAULT CODE 73-31372 ON NR 2 ENGINE WHILE ACCOMPLISHING FMC CDU INTERROGATION FOR ENGINE FAULTS IAW T/C 78273000. ACFT GROUNDED. ON DEFERRAL.
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