N586AS
Service difficulty reports · 485
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 = 'N586AS' 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 = 'N586AS' 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 ASAA2021071535416Window · failedON CLIMB OUT ABOVE 10,000 (PROBABLY) CRACKING / POPPING SOUND COMING FROM L-1 WINDOW.. NOISE CONTINUED TO 20,000 LEVEL OFF AND THROUGH DECENT INTO LAX.. AFTER LANDING NOTICED A PIECE OF WINDOW SEALANT HANGING DOWN FROM TOP OF WINDOW.. GROUNDED - YES. REMOVED MSDR ASAA2021071035337Control Panel · faultedSHORTLY AFTER T/O LOUD CLICKING SOUND COMING FROM MCP PANEL. RAPID CLICKING LASTED APPROX 2MIN. AUTO PILOT B & AUTO THROTTLE ON. ALL OTHER INDICATIONS NORMAL. TURNED OFF AUTO B & AUTO THROTTLE, LATER CLICKING RETURNED BUT MUCH SLOWER, LASTED COUPLE MINUTES. THSDR ASAA2021060835086Wire Harness · pulledFIRE DETECTION #1 ENG "B" LOOP WON'T TEST ("A" LOOP OK). GROUNDED - YES. FOUND RING TERMINAL ON AFT RIGHT LOOP PULLED OUT. REMOVED AND REPLACED HARNESS MW326 REF B737-800 AMM 26-11-02. OPS NORMAL REF AMM 26-11-00.SDR ASAA2021052934983Pressure Switch · faultyWHILE ACCOMPLISHING T/C 78273000 #2 ENG CODE 73-31072 LONG TIME FAULT THE FUEL FILTER SIGNALS DISAGREE. GROUNDED - YES. REMOVED AND REPLACED #2 ENG FUEL FILTER DIFFERENTIAL PRESSURE SWITCH PER B737-800 AMM 73-34-01. OPS TEST NORMAL. LEAK TEST GOOD.SDR ASAA2021052834974Packing · leakingWHILE ACCOMPLISHING LEAK CHECK OF #2 ENG FUEL FILTER, FOUND FUEL LEAKING FROM FUEL HEATER SERVO COVER. GROUNDED - YES. REMOVED AND REPLACED O-RING ON #2 ENG FUEL HEATER SERVO REF CMM 73-11-77, LEAK CHECK FAILED. FUEL NO LONGER LEAKING FROM SERVO COVER O-RING. SDR ASAA2021052734975Pressure Switch · faultyAFTER LANDING RIGHT FUEL FILTER BYPASS LIGHT ILLUMINATED. GROUNDED - YES. REF TSR 710868 REMOVED AND REPLACED #2 ENG. FUEL FILTER DIFFERENTIAL PRESSURE SWITCH IAW B737-800 AMM 73-34-01SDR ASAA2021052234892Charger · inoperativeLEFT AFT OVERWING EXIT, EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE. GROUNDED - YES. REMOVED AND REPLACED M1670 BATTERY PACK AND CHARGER ASSY. LIGHT CONNECTED TO CHARGER ASSY TEST GOOD IAW B737-800 AMM 33-51-06-960-806.SDR ASAA2021051034891Skin · dentedLH FUSELAGE UPPER LOBE EXTERNAL SKIN HAS A DEEP DENT, BS 500F - BS 500G,S-5L. GROUNDED - YES. EVALUATED DENT ON THE FUSELAGE SKIN AT STA 500J+10, STR-5L, LBL 33 MEASUREDW=0.690" Y= 0.097, W/Y=7.113 FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-01-1A-1 FIGURSDR ASAA2021050834849Skin · crackedCRACK FOUND ON THE LOWER SKIN OF THE RIGH HAND SIDE HORIZONTAL STABILIZER BETWEEN STAB STA. 92.70 AND 101.90. CRACK LOCATION, LENGTH AND ENDSMARKED IN RED. GROUNDED - YES. REMOVED DAMAGE AND ACCOMPLSIHED REPAIR PER B737-800 AMM 55-10-01-2R-11REPAIR 11 ON R/H HSDR ASAA2021050834848Skin · crackedCRACK FOUND ON THE LOWER SKIN OF THE LEFT HORIZONTAL STABILIZER BETWEEN STAB STA. 129.50 AND 138.70 PROX. .75" LONG. GROUNDED - YES. REMOVED DAMAGE AND ACCOMPLISHED REPAIR IAW B737-800 AMM 55-10-01-2R-11REPAIR 11 ON L/H HORIZONTAL STABILIZER.SDR ASAA2021050534890Skin · corrodedLEFT AFT FUSELAGE SKIN, VACUUM WASTE VENT EXHAUST OPENING CORRODED. GROUNDED - YES. REMOVE CORROSION BY BLENDING ON THE FUSELAGE SKIN AT STA 917, BETWEEN STR-21L AND STR-22L, ORIGINAL THICKNESS 0.125", REMOVED 0.100", REMAININGTHICKNESS 0.025" FOUND TO BE OUT SDR ASAA2021041434573Contactor · intermittentDURING AFTER START FLOW #2 ENGINE GENERATOR DOES NOT REMAIN ENGAGED AND SOURCE LIGHT ILLUMINATES. GROUNDED - YES. #2 GCU SHOWS IDG FAULT, RESET FAULT AND STAYED CLEAR. OPERATED #2 ENG IDG AND THE IDG TRIPPED OFF ONCE. AFTER THAT, CYCLED IDG MULTIPLE TIMES ON ASDR ASAA2021040534518Indicator · false indicationWHILE TOTAL FUEL QUANTITY AND FUEL FLOWS APPREARED NORMAL, RIGHT FUEL QUANTITY SLOWLY PROGRESSED TO READ 600 POUNDS LOWER THAN LEFT TANK. AS CENTER TANK QUANTITY WAS EXHAUSTED TANKS READ 8.59/0.00/7.92. FUEL WAS THEN BALANCED WITH NO SUBSEQUENT ISSUES. GROUNDESDR ASAA2021032334382Fmc · malfunctionedON APPROACH FMC #2 SWITCHED AUTOMATICALLY TO ROUTE TLOD: SCRATCHPAD MESSAGE SINGLE FMC OPERATION. AFTER LANDING AND TAXI TO GATE SCRATCHPAD MESSAGE OF FMC DISAGREE. GROUNDED - YES. COULD NOT DUPLICATE BOTH FMC'S OPS NORMAL.SDR ASAA2021021034071Modulating Valve · faultedAFTER START ON RECALL GOT MASTER CAUTION, CONT CABIN ZONE TEMP. EXTINGUISHED WITH RESET. GROUNDED - YES. REMOVED AND REPLACED CONTROL CABIN TRIM MODULATING VALVE IAW B737-800 AMM 21-61-21-000-801 AND AMM 21-61-21-400-801, ETOPS GROUND FUNCTIONAL CHECK GOOD IAWSDR ASAA2021020734058Warning Light · false activationCONT CAB ZONE TEMP LIGHT ILLUMINATED ON RECALL CLEARS WITH MASTER CAUTION RESET. GROUNDED - YES. PERFORMED PZTC BITE REF B737-800 TASK 21-61-00-700-808-001. FOUND FLT DECK TRIM VALVE FAULT LOGGED ON #2 PZTC. CLEARED FAULT. RAN LEFT AND RT PACKS FOR HALF HOUR. SDR ASAA2020122533766Bracket · looseDURING J9 HARNESS CHANGE, FOUND BRACKET THAT HOLDS J9 TO 3 O'CLOCK STRUT LOOSE UNDER RIVETS. GROUNDED-YES. REMOVED AND REPLACED BRACKET AND FASTENERS, BRACKET IS SECURE IN PLACE, REF B737-800 SRM 51-40-02. NO OTHER DEFECTS NOTED.SDR ASAA2020121133686Spinner · damagedNR 2 ENGINE FRONT SPINNER COATING OUT OF LIMITS. GROUNDED-YES. REMOVED AND REPLACED NR 2 ENGINE FWD SPINNER, REF T/C 78472010.SDR ASAA2020112833606Autothrottle Sys · malfunctionedAUTOTHROTTLE KICKED OFF WHEN SELECTED TOGA ON T/O AND WOULD NOT REMAIN ENGAGED IN FLIGHT LONGER THAN A COUPLE SECONDS. GROUNDED-YES. A/T LOGGED MSG 22-31687. PERFORMED B737-800 FIM 22-32 TASK 819. A/T SYSTEM SERVO AND BITE NORMAL, OK FOR SERVICE.SDR ASAA2020111133534Power Supply · inoperativeROW 16 AND 17 HAVE MULTIPLE OVERWING EXIT SIGNS INOPERABLE. GROUNDED-YES. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY, REF B737-800 AMM 33-51-06. ACCOMPLISHED OPERATIONS TEST, REF AMM 33-51-06, WITH NO FAULTS FOUND.SDR ASAA2020103033447Modulating Valve · inoperativeZONE TEMP ANNUNCIATOR LIGHTS UP (ABOVE CONT CAB) ON MASTER RECALL, BUT TURNS OFF WHEN MASTER CAUTION IS RESET. GROUNDED-YES. REPLACED CONTROL CABIN TCV, PER B737-800 AMM 21-61-21-000-801, GREEN GO LIGHT ILLUMINATED.SDR ASAA2020092433217Switchpack · inoperativeNR 1 ENGINE T/R LIGHT ON. GROUNDED-YES. REMOVED AND REPLACED LT AUTOTHROTTLE SWITCHPACK ASSEMBLY, IAW B737-800 AMM 76-11-07-020-802-F00 AND 76-11-07-400-802-F00. OPS CHECK GOOD, IAW B737-800 AMM 76-11-07-400-802-F00 PARAGRAPH I.SDR ASAA2020032332492Warning System · false activationAFTER START CONT CAB ZONE TEMP ILLUMINATED. LIGHT RESETS WITH MC RESET. GROUNDED - YES. #2 ZTC LOGGED FLT DECK TRIM VALVE - BITE TESTS GOOD - FAULT RESET.SDR ASAA2020031832458Bolt · brokenBOLT BROKE OFF ON THE #1 ENG OIL INLET COVER BOLT #4. GROUNDED - YES. REMOVED REMNANT OF BROKEN BOLT FROM #1 ENG OIL INLET COVER BOLT #4 USING STANDARD INDUSTRY PRACTICES, 03/16/2020.SDR ASAA2020031732438Engine · oil consumptionPASSING THROUGH 15000 FEET WE RECEIVED REVERSE VIDEO LOW ENGINE OIL QUANTITY AT 4 QUARTS. WE RAN QRH AND RETURNED TO PDX. OIL QUANTITY INCREASED TO 6 QUARTS ON DESCENT AND APPROACH. IT THEN DROPPED TO 3 QUARTS ON FINAL APPROACH. OIL TEMP ENTIRE TIME NEVER GOT SDR ASAA2020031132427Pump · low pressureAFTER LEVEL FL340, TURNED CTR FUEL PUMPS ON AND RIGHT CTR PUMP SHOWED CONTINUOUS LOW PRESSURE WITH 1.0K POUNDS OF FUEL IN CENTER TANK. GROUNDED - YES. REMOVED AND REPLACED RIGHT CENTER PUMP REF B737-800 AMM 28-22-41-000-801/400.SDR ASAA2020030932395Warning System · activatedDURING TASK CARD 78273000 FOUND FAULT 75-30412 THE HPTACC POSITION SIGNALS DISAGREE ECONOMIC FAULT DEFERRED PER TASK CARD 78273000. GROUNDED - YES. DEFERRED PER T/C 78273000 WITHIN 500 HRS. RECHECK ACCOMPLISHED PER T/C 78273000, #2 ENG S/N: 896459 STILL SHOWINSDR ASAA2020022732325Satcom · malfunctionedDISPATCH REQUESTED SATCOM TEST: SATCOM INOP. GROUNDED - YES. PERFORMED SATCOM LOCK UP PROCEDURE CKLIST: SATCOM OPS CHECKS NORMAL.SDR ASAA2020022643275Sign · detachedEMERGENCY EXIT SIGN CAME OFF EMERGENCY EXIT ROW. GROUNDED - YES. REINSTALLED EMERGENCY EXIT SIGN COVER ON EMERGENCY EXIT ROW REF B737-800 AMM 33-51-01.SDR ASAA2020013072015Blade · damagedLEFT PACK TRIP LIGHT CAME ON WHEN TRYING TO USE APU FOR A/C ON THE GROUND. IT WOULD NOT RESET WITH MASTER CAUTION. GROUNDED - YES. CONFIRMED FAULT. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE TEST BOTH LEFT & RIGHT SIDE REF B737-800 AMM 21-61-00-700-806-002, NSDR ASAA2020010831801Warning System · false activationLEFT PACK LIGHT ON WHEN RECALL IS PUSHED. PACK LIGHT EXTINGUISHES WHEN MASTER CAUTION RESET IS PUSHED. GROUNDED - YES. TROUBLE SHOT PER B737-800 FIM 21-53 TASK 821. APPEARS TO HAVE BEEN AN INTERMITTENT FAULT. PAC TEMP CONTROLLER VERIFICATION CHECK SHOWS NO CURSDR ASAA2020010231751Eec · faultyENGINE 1 ALTERNATE POWER CHANEL B CIRCUIT BREAKER POPPED. GROUNDED - YES. MSG 73-10131 & 73-11281, COMPARED RESISTANCE CHECKS A & B AT ALTERNATOR & J7 & J8 AT EEC, NO DEFECTS NOTED REF B737-800 FIM 73-27 TASK 804. AS SOON AS EEC BITE IS INITIATED CH B C/B POPSSDR ASAA2019120961528Warning Message · false activationCONTROL CAB ZONE TEMP ILLUMINATES ON RECALL. EXTINGUISHERS ON RESET. GROUNDED - YES. RELEASED PER MEL 21-21G FLT DECK PRIMARY TEMP CONTROL INOP. REF B737-800 FIM 21-61-00. TEMP CONTROLLER SHOWS NO FAULTS. REF B737-800 AMM 21-61-06-100-801. CLEANED CONTROL CABISDR ASAA201912031487Hf Comm · malfunctionedCANNOT TRANSMIT ON HF1. GROUNDED - YES. REF B737-800 FIM 23-11 TASK 801, PERFORMED #1 HF BITE TEST. BITE TEST PASSED, NO FAULTS. REF FIM 23-11-806, PERFORMED #1 HF OPS CHECK. #1 HF OPS NORMAL. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2019112513431Fmc · inoperativeLEFT FMC INOP. VTK AND MAP ON CAPT SIDE NO LEFT FMC ON POS SHIFT 3/3. GROUNDED - YES. RAN B737-800 FIM TASK 31-61 TASK 836. CYCLE PWR TO L/H FMC. OPS RESTORED AND CKS OK. REF SAME.SDR ASAA2019102853134Sign · missingEXIT SIGN MISSING R2 DOOR. GROUNDED - YES. REMOVED AND REPLACED EXIT SIGN AT R2 DOOR AS REQUIRED. OPS NORMAL, NO OTHER DEFECTS FOUND AT THIS TIME. GOOD FOR SERVICE. REF AMM 11-31-01.SDR ASAA2019102213174Connector · disconnectedFUEL TEMP GAUGE INOP. GROUNDED - YES. FOUND FUEL TEMP INDICATOR CONNECTOR D616 DISCONNECTED. RECONNECTED D616 AND FUEL TEMP IND OPS NORMAL. CONNECTOR LOCKING FUNCTION OPS NORMAL. PERFORMED A GVI OF P5-2 PANEL CONNECTORS, NO DEFECTS NOTED.SDR ASAA2019100863960Eec · failedDURING FADEC SYSTEM TEST, TEST 12 ACTUATOR TEST FAILS DISPLAY LPTACC DEMAND AND POS SIGNALS DISAGREES MAINT MSG 75-20532. GROUNDED - YES. REPLACED #2 ENGINE EEC PER B737-800 AMM 73-21-60, FADEC SYSTEM TESTS PASS. RAN TEST 12 ACTUATOR TEST. NO FAULTS NOTED.SDR ASAA2019100733934Lens · brokenRT FWD GALLEY EXIT LIGHT COVER BROKEN. GROUNDED - YES. REPLACED FWD GALLEY EXIT LIGHT PER B737-800 AMM 33-51-01 OPS CHECKED GOOD.SDR ASAA2019082230491Warning Light · false activationENGINE CONTROL #2 LIGHT ON PRIOR TO TAKEOFF. LIGHT STAYED ON UNTIL ENGINE SHUT DOWN. GROUNDED - YES. PERFORMED EEC BITE REF B737-800 FIM 73-00 TASK 801. FOUND FAULT 75-2052. PERFORMED DRY MOTOR AND ACTUATOR TEST REF 71-00-00-700-807-FOO. TEST PASSED . FOUND TOSDR ASAA2019082623485Hmu · failedENGINE CONTROL #2 LIGHT ON WHEN TAXING THE RUNWAY FOR TAKEOFF. LIGHT STAYED ON UNTIL ENGINE SHUT DOWN. ALL OTHER ENGINE INDICATIONS NORMAL. OCCURRED IN SAME LOCATION AS PREVIOUS WRITE-UP. GROUNDED - YES. PERFORMED EEC BITE REF B737-800 FIM 73-00 TASK 801. FOUNSDR ASAA2019071630087Spinner · scratched#1 ENG FRONT SPINNER CONE HAS PAINT MISSING, LOOKS LIKE SCRATCH. GROUNDED - YES. REMOVED & REPLACED OUTER NOSE CONE ASSY. REF AMM 72-21-01.SDR ASAA2019070629938Pcu · failed"ELEC" LIGHT ANNUNCIATED AFTER ENGINE START. GROUNDED - YES. ACCOMPLISHED ELE LT BITE REF FIM 24-31 TASK 801, SPCU LOGGED AND WILL NOT CLEAR. REMOVED AND REPLACED SPCU REF AMM 24-34-11 ALL OPS CKD NML. OPENED/RESET 1 EA CB J9. RAN BOTH ENGINES WITH NO FURTHER SDR ASAA2019062929862Warning System · false activationFOLLOWING THE AFTER START CHECKLIST, THE ELEC LIGHT ON THE OVERHEAD PANEL REMAINED ILLUMINATED. GROUNDED - YES. FOUND FAULT SPCU PERFORMED FIM 24-34 TASK 802 TEST IS NORMAL, FAULT CLEARED. ACFT OK FOR SERVICE.SDR ASAA2019052629483Unknown · malfunctionedFMC DISAGREE - VERTICAL LIGHT ILLUMINATED THREE TIME FROM 30 MILES TO 10 MILES FROM KSEA. GROUNDED - YES. FMC'S OP NORMAL - NO DEFECTS FOUND.SDR ASAA2019052429471Warning System · false activationLEFT PACK LIGHT ILLUMINATES WITH MASTER RECALL CHECK PACK LIGHT EXTINGUISHES WITH MASTER CAUTION RESET. GROUNDED - YES. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE LEFT PACK TCV FAULT LOGGED .VERIFY & RESET OK WITH NO FURTHER DISCREPENCIES .NO HISTORY LAST 30 SDR ASAA2019050829268Unknown · malfunctionedINTERMITTENT ILLUMINATION OF "SINGLE FMC OPERATION" ON TAXI IN. GROUNDED - YES. DID FMC BITE REF FIM 34-61 TASK 801. ON FAULT REVIEW BOTH FMC SHOWED SEVERAL LT MMR FAULTS. INPUTTING 300 SHOWED LOC DEV RATE. TROUBLESHOT REF FIM 34-31 TASK 801. NO FAULTS NOTED. SDR ASAA2019050329239Unknown · malfunctionedLEFT FORWARD WINDOW HEAT OVERHEAT ILLUMINATED. WOULD NOT RESET PER QRH PROCEDURE. GROUNDED - YES. FOUND LEFT FRONT WINDOW HEAT POWER C/B POPPED. RESET SAME C/B. LT FRONT WINDOW HEAT SYSTEM OPS CHECK GOOD. REF AMM 30-41-00-710-801.SDR ASAA2019043029209Module · failedTEMP OUTPUT OF RT AND LEFT PAC IS NOT THE SAME IN NORMAL CRUISE FLIGHT (BOTH PACKS AUTO, TRIM AIR ON) OUTPUT OF RIGHT PACK IS NORMAL AT 20'C. BUT OUTPUT OF LEFT PACK IS 32'C -34'C ALSO TEMP INDICATION VARIES WHEN SELECT KNOB IS MOVED SLIGHTLY IN THE DETENT. RESDR ASAA201904018832Blade · damagedPER T/C 78472010 #2 ENGINE FAN LUBE #6 BLADE MISSING CU-NI MATERIAL MORE THAN LIMIT. GROUNDED - YES. REMOVED AND REPLACED #6 BLADE AND #18 BLADE PAIR REF T/C 78472010.
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