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 ASAA2018021923600Sign · detachedRAMP REPORTED AN EMERGENCY EXIT SIGN DETACHED AT ROW 16 ABC LT SIDE. ACFT GROUNDED. REMOVED & REPLACED THE SIGN IAW AMM 33-51-01-960-802. CHECKED GOOD. OPS NORMAL.SDR ASAA2018020623433Servo Motor · faultedAUTO THROTTLE WILL NOT STAY CONNECTED. AUTO THROTTLE CHECKED OK. ACFT GROUNDED. AUTO THROTTLE IN FLT REVIEW SHOWED NUMEROUS ASM-2 RATE MONITOR FAULTS. IAW AMM 22-31-91, REMOVED & REPLACED ASM-2 . OPS CHECKED NORMAL IAW AMM. AUTO THROTTLE CURRENT STATUSDR ASAA2018020123354Fcu · faultedAPU WITH A FAILED CSS ATTEMPTS WITH FAULT CODE 49-31016. ACFT GROUNDED. REMOVED AND REPLACED THE APU FUEL CONTROL UNIT IAW AMM 49-31-11. OPS & LEAK CHECKED NORMAL.SDR ASAA2018012923334Starter Gen · failedCSS FAILED AT 380, 360, 300 FAULT. ACFT GROUNDED. PERFORMED BITE AND RECEIVED A FAULT CODE 49-31016 OVER TEMP SHUTDOWN. PERFORMED INSTALLATION TEST FOR STARTER GENERATOR IAW AMM 49-41-21, OPS CHECK GOOD.SDR ASAA2018012723323Oil Filter · warning lightFAULT LIGHT ILLUMINATED WHEN STARTING APU, AUTOMATICALLY SHUT DOWN. RESTART ATTEMPTED AFTER 5 MINUTES, FAULT LIGHT RETURNED. ACFT GROUNDED. FOUND APU OIL FILTER DPI TRIPPED. COMPLIED WITH AMM 49-91-13-600-801 INSPECTED MAGNETIC DRAIN PLUG, NO DEFECTS NOTESDR ASAA2018011223148Warning Light · false activationILLUMINATION OF CONTROL CABIN ZONE TEMP LIGHT ON MASTER CAUTION RECALL. LIGHT EXTINGUISHED WHEN MASTER CAUTION SYSTEM IS RESET. ACFT GROUNDED. PERFORMED THE PACK/ZONE TEMP CONTROLLER BITE TEST IAW AMM 21-51-00-700-803. ONE INTERMITTENT FAULT FOUND FOR THE SDR ASAA2018011123149Cabin Pressure · false indicationDIFFERENTIAL PRESSURE HOLDING STEADY AT 8.5 PSI IN AMBER WHILE CRUISING AT FL 380, SHOWING APP 6800 FT CABIN ALTITUDE. ACFT GROUNDED. ACCOMPLISHED FIM 21-33 TASK 803, ALL CHECKED NORMAL.SDR ASAA2017123023034Hinge · dislodgedLEFT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. PERFORMED A LEFT PACK TEMP CONTROLLER BITE IAW AMM 21-61-00-700-806-002. FOUND THE INLET RAM ACTUATOR FAULTED ONE TIME.CLEARED THE FAULT AND PERFORMED THE BITE AGAIN. NO FAULTS FOUND. INSPECTED THE LEFSDR ASAA2017110622470Control Valve · failedZONE TEMP LIGHT ILLUMINATED JUST AFTER LEVEL OFF AT FL350. LIGHT EXTINGUISHED WHEN MASTER CAUTION BUTTON PUSHED. ACCOMPLISHED QRH PROCEDURES. (CONT CAB ZONE LIGHT). ACFT GROUNDED. PERFORMED FIM 21-62 ,TASK 848, REMOVED AND REPLACED CONTROL CABIN TRIM VALVE IASDR ASAA2017110422419Warning Light · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON MASTER CAUTION CHECK. CANCELLED ON RESET. ACFT GROUNDED. PERFORMED CABIN TEMP CONTROLLER BITE PROCEDURE. CLEARED FLIGHT DECK TRIM VALVE FAULT. RAN PACK, FAULT DID NOT RETURN IAW AMM 21-61-00. RECALL CHECKED GOOD.SDR ASAA2017110322424Computer · failedDURING CRUISE AT FL 370, CAPTAIN`S FLIGHT DIRECTOR CAUTION LIGHT ILLUMINATED. PRESSING MASTER CAUTION, LIGHT ILLUMINATED SPEED TRIM FAIL AND CAUTION LIGHT REMAINED ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED ACT DEATIVATION IAW CH 5 TABLE 3 ITEM 1. REMOVED ANSDR ASAA2017102722347Switch · failedON DEPARTURE, AUTOTHROTTLE FAILED, WILL NOT REARM. ACFT GROUNDED. REPLACED THE CO-PILOT`S AUTOTHROTTLE DISENGAGE SWITCH IAW AMM 22-31-51-400-801. REPLACED THE PILOT`S AUTOTHROTTLE DISENGAGE SWITCH, OPS NORMAL IAW AMM 22-31-51-400-801. ACCOMPLISHED AN AUTOSDR ASAA2017102622356Valve · failedLEFT BLEED TRIP OFF LIGHT ILLUMINATED INFLIGHT. RESET WITH THE TRIP RESET BUTTON PUSHED IAW QRH. ACFT GROUNDED. PERFORMED FIM 36-10, TASK 801. FAILED STEP F.2.C. FOUND HIGH STAGE VALVE NOT CLOSING COMPLETELY. REMOVED AND REPLACED THE NR 1 ENGINE HIGH STAGSDR ASAA2017091821980Control Panel · faultedAUTOTHROTTLE DISENGAGED UNCOMMANDED ON DESCENT AND WOULD NOT RE-ENGAGE. ACFT GROUNDED. AUTOTHROTTLES LOGGED FAULT MESSAGE 22-31543, ENG 28 VDC INV, FAULT IS LOGGED IN PREVIOUS A/T DEFECTS. OPS CHECKED THE AUTOTHROTTLE DISCONNECT SWITCHES, NO FAULT NOTED. REMSDR ASAA2017090921856Controller · malfunctionedON DESCENT CHECKLIST, PRESSED RECALL, ZONE TEMP FOR CONTROL CABIN ILLUMINATED, RAN CHECKLIST. ZONE TEMP FOR CONTROL CABIN RESET ON MASTER CAUTION. ACFT GROUNDED. CONTROLLER LOGGED TRIM VALVE FAULT, ACCOMPLISHED PACK / ZONE TEMP CONTROLLER BITE TEST PROCEDURSDR ASAA2017090721837Pin · out of positionWHILE ACCOMPLISHING T/C SBCFM56-7B-72-0986-1, FOUND THE 9 O'CLOCK ANTI-ROTATION PIN AT THE THIRD STAGE SEGMENT SEAT HAD ROTATED, GREATER THAN 45 DEGREES AND LESS THAN 90 DEGREES, THE PIN HAD ALSO MIGRATED. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE SDR ASAA2017090521821Actuator · faultedLEFT PACK LIGHT ON OVERHEAD PANEL. RECALL THEN PUSHING MST CAUTION EXTINGUISHES THE LIGHTS. ACFT GROUNDED. PERFORMED LT TEMP CONTROLLER BITE AND FOUND LT RAM AIR ACTUATOR FAULT ACTIVE. REPLACED THE LT RAM AIR ACTUATOR IAW AMM 21-51-21/401. OPS CHECKED GOOSDR ASAA2017090421815Computer · faultedAUTOTHROTTLE WILL NOT ARM FOR TAKEOFF. ACFT GROUNDED. AUTOTHROTTLE FAULT HISTORY LOGGED, MX MESSAGE 22-31543 ON FLIGHT LEG 08. DURING CURRENT STATUS TEST, AUTOTHROTTLE WOULD NOT ARM WITH MX MESSAGE 22-31541. REPLACED FCC A IAW FIM 22-31 TASK 802. ALL INSTALSDR ASAA2017083021767Warning Light · false activationRECALL CHECK SHOWS LEFT PACK LIGHT ON, IT DOES RESET. ACFT GROUNDED. PERFORMED FIM 21-61, TASK 801, CABIN TEMP CONTROLLER BITE PROCEDURE. CHECKED GOOD. ALL TEST LIGHTS ARE GREEN. OPS NORMAL.SDR ASAA2017082721714Computer · failedAUTO THROTTLE INITIALLY ARMED, THEN DISCONNECTED WHILE TAKING ACTIVE RUNWAY AND UNABLE TO REARM AUTOTHROTTLE. ACFT GROUNDED. REMOVED & REPLACED FCC-A IAW AMM 22-11-33-00-801/-400-801, RESPECTIVELY. PERFORMED AMM TASK 22-31-00-710-801. AUTOTHROTTLE SYS CHECKSDR ASAA2017082521729Transmitter · leakingWHILE ACCOMPLISHING IDLE LEAK CHECK ON #2 ENGINE FOUND FUEL FLOW TRANSMITTER LEAKING. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG FUEL FLOW TRANSMITTER REF AMM 73-31-01. LEAK & OPS TEST GOOD.SDR ASAA2017082421727Pin · missingWHILE ACCOMPLISHING T/C SBCFM56-7B-72-0986-1 ON THE NR 2 ENGINE FOUND STAGE 3 VSV SLAB HEAD PIN AT 9 O'CLOCK POSITON MISSING OUT OF SEGMENT. ACFT GROUNDED. REPLACED THE NR 2 ENGINE.SDR ASAA2017080621544Fault Code · false activationFOUND MESSAGE 75-30452, SHORT TIME FAULT, NR 2 ENGINE VBV POSITION SIGNALS DISAGREE. ACFT GROUNDED. FAULT IS NOT PRESENT IN FAULT HISTORY OR RECENT FAULTS. ACTUATORS TESTS PASSED IAW FIM 75-32/803.SDR ASAA2017080421537Compensator · out of toleranceWHILE ACCOMPLISHING T/C NG-28FCD-18088-1, FOUND PROBES F15, F1 AND F10 TO BE OUT OF TOLERANCE. ACFT GROUNDED. REMOVED AND REPLACED PROBE IAW AMM 28-41-21-400-801. R & R PROBE F1 AND F15 IAW AMM 28-41-21-400-801.SDR ASAA2017072821498Warning Message · false activationMAINTENANCE MESSAGE 75-10441, NR 1 ENGINE, THE VBV POSITION SIGNAL IS OUT OF RANGE. ACFT GROUNDED. ACCOMPLISHED T/C 78273000, FAULT IS NO LONGER ACTIVE.SDR ASAA2017072821497Warning Message · false activationNR 1 ENGINE, VBV POSITION SIGNALS DISAGREE. ACFT GROUNDED. TROUBLESHOT IAW FIM 75-32 TASK 803. NO DEFECTS NOTED. COULD NOT GET MESSAGE TO APPEAR DURING NR 1 EEC BITE TEST OR ACTUATORS TEST. AIRCRAFT RELEASED FROM PLT.SDR ASAA2017072521469Control Valve · no testNR 1 BLEED TRIP LIGHT ILLUMINATED PASSING 17000 FT MSL. NO DUCT PRESSURE SPLIT NOTED PRIOR TO LIGHT. BLEED TRIP RESET WAS SUCCESSFUL FOR APPROXIMATELY 5 MINUTES. BLEED TRIP LIGHT ILLUMINATED AGAIN PASSING 21000 T MSL. IAW QRH CHECKLIST, TURNED NR 1 PACK OFFSDR ASAA2017072421462Engine · damagedWHILE ACCOMP T/C SBCFM56-7B-72-0986-1 FOUND STAGE 3 VSV SLAB HEAD PIN AT THE 9 OCLOCK POSITION, ROTATED 90 DEGREE AND MIGRATING OUT OF SEGMENT. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE IAW TC 78471000 AND 78471001.SDR ASAA2017071121336Autoland Sys · malfunctionedHGS /AUTOLAND UNSUCCESSFUL. ACFT GROUNDED. ACCOMPLISHED DFCS BITE FIM 22-11, TASK 801. FOUND FAULTS 22-11208 AND 22-11822. ACCOMPLISHED LT & RT FMC BITE FIM 34-61, TASK 801. NO FAULTS FOUND. ACCOMPLISHED SPEED/STAB TRIM BITE LIBRARY TEST 32. ALL TESTS PASSSDR ASAA2017070921337Coupler · failedCAN'T TRANSMIT OR RECEIVE ON NR 1 HF. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 HF COUPLER IAW AMM 23-11-61.SDR ASAA2017070921315Transceiver · failedUNABLE TO TRANSMIT ON HF NR 1. ACFT GROUNDED. R & R NR 1 TRANSCEIVER IAW AMM 23-11-21.SDR ASAA2017070521290Engine · faultedFOUND THE NR 2 ENGINE LONG TIME FAULT MESSAGE 74-31312 , NR 2 DEU IGNITER DATA IS NOT CORRECT. ACFT GROUNDED. ACCOMPLISHED T/C 78273000, FAULT IS NO LONGER ACTIVE.SDR ASAA2017070321251Fuel Nozzle · out of limitsNR 1 ENGINE, RECEIVED AN ECONOMIC FAULT CODE OF 73-31371, UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. ACCOMPLISHED REPLACEMENT OF TOP 11 NOZZLES IAW EA PWRPL-73CMPT-07267-2. RAN ENGINE, NO RECENT FAULTS NOTED AFTER EEC BITE CHECK.SDR ASAA2017062021157Autothrottle Sys · failedJUST AFTER TOP OF DESCENT, AUTOPILOT A AND AUTOTHROTTLES DISENGAGED ON THEIR OWN. AUTOPILOT A WOULD REENGAGE JUST FINE, BUT AUTOTHROTTLES WOULD NOT FOR REMAINDER OF FLIGHT. ACFT GROUNDED. REMOVED & REPLACED AUTOTHROTTLE SERVO MOTOR IAW AMM 22-31-91-000-801SDR ASAA2017061021024Fault Code · false activationNR 2 ENGINE SHORT TERM FAULT LOGGED. MESSAGE NUMBER 75-30452 THE VBV POSITION SIGNALS DISAGREE. ACFT GROUNDED. CHECKED THE NR 2 ENGINE EEC BITE FAULTS, NO FAULTS FOUND IN RECENT OR HISTORY FOR NR 2 ENGINE. PERFORMED INITIAL EVALUATION IAW FIM 75-32 TASK 803.SDR ASAA2017052520864Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN APPEARED TO HAVE TWO CRACKS. ACFT GROUNDED. VERIFIED THE CRACK INDICATIONS IAW NDT 51-00-00, PART 6. REMOVED THE DAMAGE, FABRICATED A DOUBLER, AND INSTALLED. REPAIRED IAW SRM 55-10-01-2R-11.SDR ASAA2017050520648Idg · failedAFTER START WITH NR 1 GENERATOR ON APU, SWAPPED GEN TO NR 1 ENGINE AND NR 1 GEN BUSS SOURCE OFF LIGHT CAME ON. ACFT GROUNDED. REMOVED FILTERS FROM REMOVED IDG, NO CONTAMINATION NOTED IAW AMM 24-11-11. REMOVED AND REPLACED THE NR 1 IDG IAW AMM 24-11-11. LEAK SDR ASAA2017050420634Warning System · malfunctionedGEN NR 1 BUS FAIL ON NR 1 ENG START UP. GROUNDED - YES. ACCOMP NR 1 GCU BITE FOUND FAULT GCU/ APB FAULT RESET NR 1 GCU. OPEN P91 AND ACCOMP GVI NO DEFECTS OF GCB NR 1 (C801) CLOSED P91. CYCLED C/B AT P6-4 F-10. ACCOMP OPS TEST FOR A/C GENERATION AND CONTROL SYSDR ASAA2017042520535Light · inoperativeR2 DOOR SLIDE/EMERGENCY EXIT LIGHT INOP. GROUNDED - YES. RELAMPED R2 DOOR SLIDE/EMERGENCY EXIT LIGHT, REF AMM 33-51-04-960-801. OPS CHECKS GOOD.SDR ASAA2017042020507Indicator · inoperativeFUELER REPORTS NR 1 WING REFUELING GAGE AT WING INOP - BLANK. GROUNDED - YES. REMOVED AND REPLACED NR 1 WING REFUELING GAGE PER AMM 28-41-61, OPS CHECK GOOD . CLEARED MEL 28-12B.SDR ASAA2017020419664Satcom · malfunctionedSATCOM, UNABLE TO CALL OUT ON BOTH SAT 1 & SAT 2. TO ANY DISPATCH DESK. CALL OUT TO MEDLINK SUCCESSFUL. RECEIVE CALL FROM DISPATCH ALSO SUCCESSFUL. ACFT GROUNDED. ACCOMPLISHED SATCOM TEST IAW AMM 23-15-00. GENERAL DIRECTORY DISPATCH A-F CALLS RECEIVE "THIS NUSDR ASAA2017012519575Bleed Valve · faultyWHILE ACCOMPLISHING T/C 78273000 FOUND FAULT NR 2 ENG. FAULT 75-10452 THE VBV POS SIGNALS DISAGREE, AND 75-20452 THE VBV POS SIGNALS DISAGREE, ON 7 FLT LEGS. SHORT TERM FAULT. REF LOGPAGE 11754523, WHILE ACCOMPLISHING INITIAL EVALUATION OF VBV POSITION SIGNALSSDR ASAA2017012219973Probe · out of limitsWHILE ACCOMPLISHING T/C 78273000 A FAULT CODE APPEARED ON THE NR 1 ENGINE 73-31371 UPPER EGT SECTORS READING HIGH, ECONOMIC FAULT. ACFT GROUNDED. PERFORMED FIM 73-11 TASK 801. PERFORMED AMM 77-21-01. INSPECTED AND FOUND S3 AND S4 EGT PROBES OUT OF LIMITS. REMSDR ASAA2017011919475Control Valve · failedDURING CLIMB OUT, CONTROL CABN ZONE TEMP ILLUMINATED BUT EXTINGUISHED WITH MASTER CAUTION RESET. PERFORMED QRH ITEMS TO POINT WHETHER IT STATES, "NO FURTHER ACTION REQUIRED". ACFT GROUNDED. REPLACED THE CONTROL CABIN TRIM VALVE (V143) IAW AMM TASK 21-61-21-40SDR ASAA2017011519416Eec · faultedNR 2 ENGINE HAD SHORT TIME FAULT 75-30452 - THE VBV POSITION SIGNALS DISAGREE. ACFT GROUNDED. ACCOMPLISHED TROUBLESHOOTING IAW FIM 75-32 TASK 803. INITIAL EVALUATION AND FAULT ISOLATION FOUND NO DEFECTS. EEC TESTS INDICATED NO FAULTS. DUE TO EXTENSIVE HISTORSDR ASAA2017010919291Connector · dirtyDURING COMPLETION OF T/C 78273000 FOUND MAINT MESSAGES #75-10452 AND #75-20452 "THE VBV POSITION SIGNALS DISAGREE" SHORT TIME FAULT, #2 ENGINE ESN 896-367. GROUNDED - YES. ACCOMPLISHED T/S FOR FAULT 75-10452 (AND 75-20452, REF LOGPAGE 11612951) PER B737-800 FISDR ASAA2016122519143Bulb · failedEMERGENCY LIGHT EXIT LOCATOR SIGN AT LEFT FORWARD OVERWING EXIT HAS MULTIPLE LAMPS INOPERATIVE, ALSO AT LEFT AFT OVERWING EXIT AND EMERGENCY LIGHT EXIT LOCATOR SIGN AT R-2 DOOR. ACFT GROUNDED. REPLACED THE LAMPS AND TESTED IAW AMM 33-51-01-960-801. OPS NORMASDR ASAA2016122319154Engine · faultedWHILE PERFORMING T/C 78273000, FOUND NR 2 ENGINE SHORT TERM FAULT CODE 75-30452. THE VBV POSITION SIGNALS DISAGREE. ACFT GROUNDED. ACCOMPLISHED T/C FOR NR 2 ENGINE FAULT 75-30452 IAW FIM 75-32 TASK 803. INITIAL EVALUATION TEST 12 - ACTUATORS TEST IAW AMM 71SDR ASAA2016112019303Probe · failedWHILE ACCOMPLISHING TASK CARD 78273000 FOUND ECONOMIC FAULT 73-31371, UPPER EGT SECTORS READING HIGH ON NR 1 ENGINE. ACFT GROUNDED. REMOVED AND REPLACED T49.5 PROBE S1 IAW AMM 77-21-01-000-801 F00 AND 77-21-01-400-801-F00. ACCOMPLISHED EEC TEST IAW AMM 73-21-SDR ASAA2016112018769O-Ring · failedTBV TARGETED REPLACEMENT. DURING LEAK CHECK FOUND PHP CAP ON FUEL PUMP LEAKING. ACFT GROUNDED. REPLACED THE O-RING ON PHP PLUG, TORQUED PER CMM 73-11-15 ITEM 4. L. ACCOMPLISHED LEAK CHECK, NO LEAKS NOTED.
Back to N593AS