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 ASAA2017041320460Probe · out of limitsFQIS - NR 1 TANK AND COMPENSATOR UNITS TESTING, FOUND FUEL PROBES NR 1, 4, 5, 6, 7, 8, 9, & 10 OUT OF LIMITS. GROUNDED - YES. REMOVED AND REPLACED TANK UNITS NR 1, 4, 5, 6, AND 7, REF AMM 28-41-21-000-801 AND AMM 28-41-21-400-801. REMOVED & REPLACED TANK PROBESDR ASAA2017041320459Probe · out of limitsWHILE ACCOMPLISHING T/C NG-28FCD-18090-1, FQIS, NR 2 TANK & COMPENSATOR UNITS TESTING, FOUND FUEL PROBES NR 2, 4, 5, & 8 OUT OF LIMITS. ACFT GROUNDED. REMOVED & REPLACED THE FUEL PROBES IAW AMM 28-41-21. ACCOMPLISHED FQIS SYSTEM TEST IAW AMM 28-41-00. OPS SDR ASAA2017041120435Pressure Switch · failedCRUISE ALTITUDE (FL350) RECEIVED A MASTER CAUTION WITH NR 2 FILTER BYPASS LIGHT. ACFT GROUNDED REMOVED AND REPLACED THE NR 2 FUEL FILTER DIFFERENTIAL PRESSURE SWITCH IAW AMM 73-34-01. OPS TEST AND LEAK CHECKED GOOD.SDR ASAA2017032520260Battery Pack · inoperativeEMERGENCY EXIT LIGHT AFT OF R1 DOOR INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW WDM 33-51-12 AND AMM 33-51-06. OPS CHECKED GOOD.SDR ASAA2017030119979Warning Light · false activationCONTROL CABIN ZONE TEMP ILLUMINATED ON RECALL. ACFT GROUNDED. ACCOMPLISHED PACK TEMP CONTROL BITE IAW FIM 21-62 TASK 901. FOUND FLT DECK TRIM VALVE FAULT. ACCOMPLISHED VERIFY TEST, VERIFIED NORMAL. RESET FAULT, FLT DECK TEMP CONTROL OPS NORMAL.SDR ASAA2017022719963Sensor · failedAPU OIL LEVEL BITE CHECK IS UNKNOWN, MAINT MESSAGE 49-94304. OIL LEVEL SENSOR CIRCUIT FAILURE. ACFT GROUNDED. REMOVED AND REPLACED THE APU OIL LEVEL SENSOR IAW AMM 49-94-11-000-801, AND AMM 49-94-11-400-801, RAN APU FOR 5 MINUTES TWICE FOR OIL LEAKS, NO LEASDR ASAA2017020619727Shim · wornALL NR 1 ENGINE FAN BLADES SHIMS WORN. GROUNDED - YES. REPLACED ALL NR 1 ENGINE FAN BLADES SHIMS PER T/C 78472002.SDR ASAA2017020419672Rod End · worn#1 ENG LOWER STARTER DUCT FWD ROD-END ASSY & BRACKET WORN. ACFT GROUNDED. REPLACED ROD END ASSY & BRACKET.SDR ASAA2017013119628Idg · failedLOST LEFT ENGINE GENERATOR AFTER TAKEOFF. FOLLOWED QRH. APU COVERED LEFT BUSS. ACFT GROUNDED. REMOVED AND REPLACED THE IDG IAW AMM 24-11-11.SDR ASAA2016123019220Link · bindingFWD ENTRY DOOR IS BINDING AND WILL NOT FULLY OPEN. GROUNDED - YES. PARTIALLY REMOVED L1 DOOR UPPER HINGE SPIGOT. REMOVED AND REPLACED LOWER RADIUS LINK AT UPPER HINGE, REF AMM 52-11-21. REINSTALLED L1 DOOR UPPER HINGE SPIGOT, REF AMM 52-11-41 AND 52-11-00-400-SDR ASAA2016122919218Shutoff Valve · failedDUCT PRESSURE SPLIT, GREATER THAN 20 PSI AT FL 370. LEFT DUCT 40 PSI , RIGHT DUCT 14 PSI , N1'S APPROXIMATELY 80%. GROUNDED - YES. REPLACED NR 2 ENGINE PRESSURE REGULATOR BLEED SHUTOFF VALVE PER AMM 36-11-04-400-801 PERFORMED HEALTH CHECK PER AMM 36-11-700-804SDR ASAA2016121119004Warning Light · false activationZONE TEMP CONT CAB LIGHT ILLUMINATES ON MASTER CAUTION RECALL AND EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. ZONE TEMP CONT 2 BITE FAILS FLIGHT DECK TRIM VALVE. OPERATED FLIGHT DECK TEMPERATURE CONTROL, BITE CHECK TRIM AIR VALVE AND CABIN TEMP CONTROSDR ASAA2016121119003Warning Light · false activationWHILE PERFORMING ETOPS PDC FOUND CONTROL CABIN ZONE TEMP LIGHT ILLUMINATED. ABLE TO RESET. ACFT GROUNDED. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE TEST IAW AMM TASK 21-61-00-700-806--002 ON BOTH CONTROLLERS. NO FAULTS NOTED. NO FAULT LAST FLIGHT. OPS CHECK SDR ASAA2016113018895Fmc · malfunctionedACFT EXPERIENCED INTERMITTENT FMC FAILURES. INITIALLY FMC-L FAILED WITH VTK DISPLAYED ON ND CAPTAINS SIDE AND NO FMC PROMPT ON BOTH CDUS THEN FMC-R FAILED DISPLAYING VTK ON F/O ND. BOTH FMC'S RECOVERED + FAILED SEVERAL TIMES. FINALLY, BOTH FMC'S RECOVERED WITHSDR ASAA2016102818503Compensator · failedCHECKED DRY CAPACITANCE OF NR 2 TANK. ACFT GROUNDED. ACCOMPLISHED FQIS SYSTEM TEST, DRY CAL AND FOUND NR 2 TANK CAPACITANCE HIGH AT 407.5 AND COMP PROBE CAP HIGH AT 59.4 IAW AMM 28-41-00-730-801. ACCOMPLISHED TANK AND COMP UNITS TEST AND FOUND COMP PROBE F15SDR ASAA2016102618487Check Valve · missingCENTER FUEL TANK AND CENTER PUMPS ON. RT FUEL QUANTITY DECREASED BY APPROXIMATELY 200 PPH. AFTER CENTER TANK DEPLETED, WING TANKS REMAINED SLIGHTLY IMBALANCED UNTIL CORRECTED. ACFT GROUNDED. ACCOMPLISHED BOTH ENGINE IDLE RUN, WITH ALL SIX BOOST PUMPS ON, FUELSDR ASAA2016101718378Autothrottle Sys · malfunctionedAUTOTHROTTLES WILL NOT ENGAGE. ACFT GROUNDED. ACCOMPLISHED FIM 22-31 TASK 801, WITH ONE FAULT NOTED ON LEG 2, NO OTHER FAULTS NOTED. CURRENT STATUS TEST PASSED, AND SERVO MOTOR TEST PASSED. AUTOTHROTTLE SYSTEM OPS NORMAL, IAW FIM 22-31 TASK 801.SDR ASAA2016100618233Control Valve · faultedAFTER START, RECEIVED A ZONE TEMP LIGHT FOR THE COCKPIT, RAN CHECKLIST, STILL HAD THE LIGHT ON RECALL, EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED ZONE TEMP CONTROLLER NR 1 AND 2 BITE CHECK. FOUND TCV FAULT ON NR 1 CONTROLLER. R & R THSDR ASAA2016100318197Autothrottle Sys · malfunctionedAUTOTHOTTLE WOULD NOT ARM ON GROUND, BUT AFTER CYCLING A FEW TIMES IT WORKED. IT FAILED AGAIN AND IN FLIGHT THE A/T ARM SWITCHED TO OFF POSITION ALONG WITH THE RED A/T LIGHT ILLUMINATED. COULD NOT RESET. ACFT GROUNDED. PERFORMED FIM TASK 22-31-801 TASK. OPS SDR ASAA2016092718139Proximity Sensor · failedNR 7 LE FLAP TRANSIT LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT. NO ROLL FELT. SPEED TAPES, AUDIO WARNINGS, FMC COMPUTATIONS AFFECTED. OVERHEAD LE DEVICE NR 7 AMBER TRANSIT LIGHT ALSO ILLUMINATED INTERMITTENTLY. AIR TURNBACK. ACFT GROUNDED. RESET (1) C/B STALSDR ASAA2016092018085Idg · failedNR 2 DRIVE LIGHT EXTINGUISHED WITH ENGINE SHUTOFF. ACFT GROUNDED. R & R NR 2 IDG, REF AMM 24-11-11. NO LEAKS. OPS CHECK GOOD.SDR ASAA2016091418014Warning Light · illuminatedBOTH CTR TANK FUEL PUMP LIGHTS REMAIN ON WITH PUMPS ON. ACFT GROUNDED. PERFORMED FIM 28-22 TASK 801 & 802. CTR TANK FUELED TO 14000 LBS & PUMPS REPRIMED. BOTH CTR TANK BOOST PUMPS OPS NORMAL. ALL GROUND FUNCTIONAL TESTS PASSED.SDR ASAA2016072817556Sliding Window · failedL2 SIDE WINDOW OVERHEAT WARNING ILLUMINATED DURING DESCENT. ACCOMPLISHED QRC, OPS NORMAL. ACFT GROUNDED. REMOVED AND REPLACED THE L2 SLIDING WINDOW IAW AMM 56-12-11. OPS CHECKED GOOD. HANDLE FORCE ADJUSTMENT GOOD IAW AMM 56-12-11, STEP. 6. CABIN PRESSURESDR ASAA2016072617525Sign · detachedMID CABIN OVERHEAD EXIT SIGN DETACHED. ACFT GROUNDED. ATTACHED THE EXIT SIGN, OPS CHECKED NORMAL.SDR ASAA2016070717302Control Valve · failedRIGHT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL, EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. REPLACED RT A/C PACK TEMP CONTROL VALVE IAW AMM 21-51-10.SDR ASAA2016062017100Sensor · failedLEFT FORWARD WINDOW OVERHEAT LIGHT ILLUMINATED. ACFT GROUNDED. WINDOW SENSOR FAULTED MULTIPLE TIMES ON LT FORWARD WINDOW HEAT CONTROLLER. SWITCHED WINDOW SENSOR SWITCH TO SPARE POSITION IAW AMM 30-41-00. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2016062017098Control Panel · failedCLICKING NOSE HEARD FROM AROUND MCP SEEMED TO ONLY MAKE NOSE WHILE IN CLOUDS WE WERE AT FL360, -45 DEGREES CELSIUS. ACFT GROUNDED. REPLACED MCP PANEL IAW AMM 22-11-34-401, RAN LAND VERIFY TEST IAW AMM 21-11-00-201 AND HGS IAW AMM 34-36-00. ACFT REMAINS HGS ASDR ASAA2016061617056Actuator · failedLEFT PACK LIGHT ILLUMINATED ON RECALL; EXTINGUISHES UPON MASTER CAUTION RESET. ACFT GROUNDED. CONFIRMED DEFECT, BITE OF LT PACK ZONE TEMP CONTROL IAW FIM 21-62, TASK 801 SHOWED RAM AIR ACTUATOR FAULT. ACCOMPLISHED T/S FOR RAM AIR ACTUATOR FAULT IAW FIM 21-SDR ASAA2016061517050Unknown · unknownFMC'S DUMPED AFTER LANDING. ACARS DID NOT DUMP. ALL C/B'S CHECKED IN. ACFT GROUNDED. PERFORMED FIM TASK 34-61, TASK 807, NO FAULTS FOUND.SDR ASAA2016061417036Warning System · false activationCONTROLLER CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. RAN RTS CHECK OF ZONE TEMP CONTROLLER. RESET FAULT OF COCKPIT TRIM AIR VALVE, REF
AMM 21-61-20-400-801. OPS NORMAL. ZONE TEMP LIGHT IN COCKPIT DOES NOT ILLUMINATE ON RECALL.SDR ASAA2016060917008Panel · looseREF T/C 78472000, NR 1 ENGINE, 4-5 O`CLOCK AFT LOOKING FWD, LPTACC SCOOP FAN DUCT PANEL. AFT 2 FASTENERS ARE PULLED THROUGH PANEL. ACFT GROUNDED. R & R NR 1 ENGINE FAN DUCT PANEL, REF AMM 72-23-07.SDR ASAA2016052516851Fmc · malfunctionedAFTER LANDING BOTH FMCS DUMPED ALL INFORMATION, FMC PROMPT DISAPPEARED FOR A FEW SECONDS AND THEN CAME BACK. ACFT GROUNDED. ACCOMPLISHED LT AND RT FMC BITE, REF FIM 34-61-00-810-801, NO FAULTS FOUND. ACCOMPLISHED LT AND RT FMCS SYS TEST REF AMM 34-61-00. SYSDR ASAA2016052516845Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON RECALL, EXTINGUISHED WHEN RESET. ACFT GROUNDED. VERIFIED DISCREPANCY. PERFORMED LT PZTC BITE, REF AMM 21-51-00. FOUND RAM AIR ACTUATOR FAULT LOGGED ONE TIME. RESET FAULT. ACCOMPLISHED RAM AIR ACTUATOR INSTALL TEST, REF AMM 21-SDR ASAA2016051716779Warning Light · false activationON RECALL, AIR CONDITION-ZONE TEMP LIGHT ILLUINATED. RAN QRH. LIGHT RESET ON MASTER CAUTION SYS RESET. SYSTEM OPS NORMAL. GROUNDED. NR 2 PZTC LOGGED FLIGHT DECK TRIM VALVE. COULD NOT DUPLICATE MALFUNCTION. PZTC BITE CHECK NORMAL SEVERAL TIMES. DURING BITESDR ASAA2016051516746Fuel Nozzle · failedWHILE ACCOMPLISHING T/C 78273000 FOUND ECONOMIC FAULT 73-31371 NR 1 ENGINE, UPPER EGT SECTOR READING HIGH. ACFT GROUNDED. R & R UPPER HALF FUEL NOZZLES AT NR 1 ENGINE IAW T/C PWRPL-73CMPT-07267-2. LEAK CHECK OK-NO FAULTS NOTED.SDR ASAA2016050516658Probe · shortedDIAGNOSTICS REPORTS NR 2 ENGINE TREND DATA SHOWS EGT SCATTER AND DECREASE IN HOT DAY MARGIN. ALL OTHER PARAMETERS NORMAL. EGT INDICATION ERRORS ARE SUSPECT. ACFT GROUNDED. GAINED ACCESS TO INPUT MONITORING PAGE FOR ENGINE NR 2 EGT T49.5 BEFORE CLEANING. T49.SDR ASAA2016043016596Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL NOT ENGAGE. ACFT GROUNDED. ACCOMPLISHED AUTOTHROTTLE BITE IAW FIM 22-32, TASK 810. ALL TESTS PASSED.SDR ASAA2016042216504Shim · damagedNR 2 ENGINE FAN BLADE SHIMS MISSING MOLYDAG COATING. ACFT GROUNDED. REPLACED ALL 24 SHIMS, PN 340-252-307-0 ON NR 2 ENG REF T/C 78472002.SDR ASAA2016041716437Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. CONTROLLER LOGGED TCV FAULT, ACCOMPLISHED BOTH TEMP CONTROLLERS BITE TEST IAW AMM TASK 21-51-00 AND FAULT CLEARED. BOTH CONTROLLERS BITE CHECK OPS CHECK GOOD, NO EXISTING FAULT.SDR ASAA2016041716435Light · unknownF/A REPORTS EMERGENCY EXIT SIGN LIGHT INOPERATIVE ROW 16. ACFT GROUNDED. COULD NOT REPLICATE EMERGENCY EXIT SIGN FAULT. OPS CHECK WAS GOOD.SDR ASAA2016031015863Control Panel · malfunctionedMCP BLANK ON PREFLIGHT. ACFT GROUNDED. RESET 9 C/B. MCP R2 REF AMM 22-11-34. ACCOMPLISHED MCP INSTALL TEST IAW AMM 22-11-34-740-001. SYS OPS NORMAL. ALL TESTS PASSED. PROBLEM OCCURRED AT POWER TRANSFER. BOTH APU AND GROUND POWER OK.SDR ASAA2016030315762Satcom · failedTO CALL MEDLINK, SAT-2 ATTEMPT FAILED. ACFT GROUNDED. TESTED SATCOM IAW AMM 23-15-00 SYS, OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME.SDR ASAA2016022015589Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMCS RESTORED NORMAL.SDR ASAA2016021815592Probe · faultedWHILE ACCOMPLISHING T/C 78273000, FOUND NR 1 ENGINE ECONOMIC FAULT 73-31371, UPPER EGT SECTOR READING HIGH. ACFT GROUNDED. PERFORMED FIM 73-11 TASK 801 UPPER EGT SECTORS READING HIGH. VERIFIED DISCREPANCY NR 1 ENGINE SHOWS FAULT 72-31371. INSPECTED T49.5 RESDR ASAA2016021515451Warning Light · false activationAFTER ENGINE START RT PACK ANNUNCIATION ON MASTER CAUTION RECALL. ACFT GROUNDED. ACCOMPLISHED PACKS BITE CHECK, NO FAULTS NOTED, RESET PACKS CONTROL BOX IAW AMM 21-61-00.SDR ASAA2016020315379Skin · crackedCRACK INDICATION FOUND ON LT LOWER HORIZONTAL SKIN: NR 2, INBD AT STABILIZER BS 147.9 INBD OF INBD ROW OF RIVETS, 15.25" FWD OF AFT SPAR, MARKED, 1.450"L. ACFT GROUNDED. REMOVE DAMAGE AND ACCOMPLISHED DOUBLER REPAIR IAW SRM 55-10-01-2R-11, FIG 204.SDR ASAA2016020315368Skin · crackedCRACK INDICATION FOUND ON LT LOWER HORIZONTAL SKIN: NR 1, INBD AT STABILIZER BS 101.9, INBD OF INBD ROW OF RIVETS, 9" FWD OF AFT SPAR, MARKED .800"L. ACFT GROUNDED. REMOVED DAMAGE AND ACCOMPLISHED DOUBLER REPAIR IAW SRM 55-10-01-2R-11, FIG 204, REPAIR 11 ISSDR ASAA2016020215344Support · dentedAFT CARGO COMPARTMENT LT TRANSITION PANEL HAS A DENT AT BS 727H+2. ACFT GROUNDED. EVALUATED DENT IN AFT CARGO COMPARTMENT. LEFT TRANSITION PANEL AT BS 727H+2. W/Y = .7/.108-6.48, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED ZEE CHANNEL AND SPLICESDR ASAA2016020115359Channel · corrodedAFT CARGO COMPARTMENT LEFT ZEE CHANNEL SIDEPLATE BS 727D-BS LBL 21.0 CORRODED AROUND FASTENER HOLES AT PREVIOUS BLENDOUT LOCATIONS. BS 727D-BS 767, LBL 21.0 - LBL 21.0, STR 25L-25L. ACFT GROUNDED. REMOVED CORROSION ON AFT CARGO COMPARTMENT LT ZEE CHANNEL SIDSDR ASAA2016020115333Floor Panel · puncturedAFT CARGO COMPARTMENT FLOOR PANEL 140BF HAS A PUNCTURE. ACFT GROUNDED. FABRICATED NEW AFT CARGO COMPARTMENT FLOOR PANEL 140BF IAW DWG 453A2610, REV E & SRM 51-20-01.
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