N583AS
Service difficulty reports · 465
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 = 'N583AS' 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 = 'N583AS' 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 ASAA2021122536994Unknown · noneAFTER TAKEOFF FA'S REPORT NO WATER AND NO WASTE OPERATION. GROUNDED - YES. DIVERSION TIME 27 MINUTES. PERFORMED B737-800 FIM 38-10 TASK 803. NO SYSTEM FAULTS. HAD RAMP RESERVICE POTABLE WATER CORRECTLY (PREVIOUSLY SERVICED INCORRECTLY). GROUND CHECKED LAVS ANDSDR ASAA2021121936964Unknown · unknownL SIDE WINDOW OVERHEAT IN FLIGHT RAN QRH, OVERHEAT LIGHT STAYED ILLUMINATED. SWITCH LEFT IN OFF POSITION FOR REST OF FLIGHT. GROUNDED - YES. FOUND L2 WHCU SENSOR FAULT. SWAPPED TO SPARE SENSOR OP CK GOOD REF B737-800 FIM 38-41 TASK 811.SDR ASAA2021121736939Unknown · unknownFMC FAIL. F.O. FMC FAILED THEN RAN QRH. THIS CAUSED DUAL FMC FAILURE. FMC'S BOTH CAME BACK. CONTINUED NORMAL OPS. CAPT'S RNP/AND WAS 10/9.92, GPS L&R O.O. IRS - L 340/1.0. IRS - R 300/1.2. CPDLC WAS LOST. GROUNDED - YES. RESET SYSTEM AND TESTED FMCS 1&2, GROUNSDR ASAA2021120436806Blade · damagedWHILE ACCOMPLISHING T/C 78472010 FOUND BLADES 13,9,2,8,18,5,21 ON ENGINE #1 TO HAVE DAMAGE TO THE COATING THAT IS OUT OF LIMITS. GROUNDED - YES. REPLACED #1 ENGINE BLADES 1,2,5,6,8,9,13,14,18 AND 21 REF T/ 78472010.SDR ASAA2021120136774Platform · out of positionPER T/C 78472010 #2 FAN BLADE LUBE PLATFORM #14 P/N 340-001-817-0 NOT PAIRED 180 DEGREES APART. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE FAN BLADE PLATFORM #14 WITH P/N 340-001-816-0 REF TC 78472010.SDR ASAA2021120136773Spacer · debondedPER T/C 78472010 #2 FAN BLANE LUBE SPACERS #(1-12),13,AND (17-24) ELASTOMERS ARE DISBONDED. GROUNDED - YES. REMOVED AN REPLACED #2 ENG FAN BLADE SPACERS 1-12,13,17-24 PER TC 78472010.SDR ASAA2021112236686Sensor · inoperativeDURING AIR CONDITIONING - PRESSURIZATION CHECKS, WITH TRIM AIR ON, CONT CAB, FWD & AFT CABIN TEMP SELECTORS AT 12 O'CLOCK POSITION. CABIN TEMPS WERE 21*-27* C-NORMAL. LEFT PACK TEMP WAS 30*C AND RIGHT PACK TEMP WAS 0*C - BOTTOM OF GAUGE. WHEN FWD & AFT TEMP COSDR ASAA2021110636617Skin · crackedCRACKED INDICATION FOUND: L/H HORIZONTAL LOWER SKIN I/B OF STA.147.90, 16.5" AFT OF L/E, 2.150" FWD OF REPAIR DOUBLER, MARKED AT .320"L.DOT: A373 GROUNDED - YES. REPAIRED THE L/H HORIZONTAL LOWER SKIN AT APPROX. 147.9 USING DOUBLER MAT.100 2024-T3 AND FILLER SDR ASAA2021102536405Unknown · unknownAFTER LANDING DUAL FMC FAILURE FOR APPROXIMATELY 20 SECONDS. GROUNDED - YES. PERFROMRED B737-800 FIM 34-61TASK 801 FLIGHT MANAGEMENT COMPUTER SYSTEM BITE TEST PROCEDURE. LEFT FMC LOGGED "PGM FAULT ON GROUND LEG (G). THIS IS A SOFTWARE ANOMALY. BOTH LEFT & RIGHSDR ASAA2021100536186Unknown · unknown"ZONE TEMP" LIGHT ILLUMINATES ON RECALL. GROUNDED - YES. BITE CK SHOWS FLT DECK TRIM VALVE. CW B737-800 FIM 21-62 TASK 832. FAULT CLEARED NOT ACTIVE.SDR ASAA2021093036156Actuator · faultedDURING T/C 78273000 FOUND SHORT TIME FAULT 75-30542 ON ENGINE 2. GROUNDED - YES. REPLACED #2 ENG LEFT VBV ACTUATOR REF B737-800 AMM 75-32-02-400-801-F00 STEPS 3A-3H(7). PERFORMED IDLE LEAK CHECK AND ACTUATORS TEST. CHECK/TEST OK. REF AMM 75-32-02-400-801-F00 SSDR ASAA2021091735979Unknown · unknownWINDOW HEAT L SIDE OVERHEAT CAUTION DURING DESCENT THROUGH 10,000. GROUNDED - YES. RAN QRH AND OVERHEAT REMAINED EXTINGUISHED.SDR ASAA2021090435859Lamp · inoperativeOVERHEAD EMERGENCY EXIT LT @ ROW 1 IS INOP. GROUNDED - YES. RELAMPED ROW 1 EMERGENCY EXIT AREA LIGHT, OPS CHECKS OK. REF B737-800 AMM 33-51-03.SDR ASAA2021070435258Acm · seizedPACK TRIP OFF LIGHT ON TAXI OUT RESET AND CONTINUED TO OVERHEAT. GROUNDED - YES. PER B737-800 FIM 21-62 TASK 801 PERFORMED BITE OF PZTC 1 AND 2. NO FAULTS AND VERIFY PASSED. ATTEMPTED OPERATION OF LEFT PACK. PRESSURE SUPPLIED BUT ACM DID NOT TURN. REPLACED LT SDR ASAA2021061835228Compensator · inoperativeTECH SERVICES REQUEST FOLLOW-UP TO RECENT #2 FUEL QTY GROUNDED - YES. ACCOMPLISHED A TANK AND COMPENSATOR UNITS TEST PER B737-800 AMM 28-41-21-710-801 ON THE #2 TANK AND FOUND COMPENSATOR PROBE AND TANK UNITS 2, 5, AND 6 OUT OF LIMITS. REMOVED AND REPLACED COSDR ASAA2021061435096Lamp · inoperativeEMERGENCY LIGHT EXIT LOCATOR SIGN AT LEFT FORWARD OVERWING EXIT HAS SEVERAL LAMPS INOP. GROUNDED - YES. RELAMPED AND TESTER PER B737-800 AMM 3351-01-960-801 - OPS NORMAL.SDR ASAA2021051834852Fmc · failedAFTER LANDING ON TAXI BACK TO THE GATE THE CAPTAIN'S FMC FAILED THEN RESET BACK TO NORMAL WITHIN ABOUT 10 SECONDS. GROUNDED - YES. L/H FMC HAD PGM FAULT REBOOTED FMC & BITE CK OK. REF B737-800 FIM 34-61-00-860-801.SDR ASAA2020030932351Warning System · false activationON RECALL, RIGHT PACK LIGHT ILLUMINATED EXTINGUISHES WITH RESET OF MASTER CAUTION. GROUNDED - YES. FOUND RIGHT PACK ACTUATOR FAULT, A/C CHECKED AND RELEASED IAW MEL 21-32B, PRIMARY RIGHT PACK TEMP CONTROL INOP. PERFORMED PACK TEMP CONTROL BITE. NO FAULTS IN PRSDR ASAA2020030932392Spacer · debondedPER T/C 78472010 #1 ENGINE FAN BLADE LUBE SPACER 2,5,8,9,10,11,12,17, AND 21 ELASTOMERS ARE DISBONDED. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE FAN BLADE SPACER 9 TOTAL REF. T/C # 78472010SDR ASAA2020020632072Compensator · failedFUEL QUANTITY INITIALLY 40.8 TOTAL 8.64 / 23.5 / 8.64. LESS THAN 5 MIN AFTER ENGINE START QTY WAS 7.68 / 22.6 / 8.6 (#1 QTY DROPPED NEARLY 1000 POUNDS). NO OTHER ABNORMAL INDICATIONS. ALL 6 PUMPS ON. NOTE "TOTAL" FUEL ALSO DROPPED (MIRRORED THE LOSS #1 QTY INDSDR ASAA2020020422070Fuel Sys · malfunctionedMAIN TANK IMBALANCE OF 800# AT 4 HOURS INTO FLIGHT. LEFT TANK LOW. FUEL FLOW EVEN. BALANCED FUEL AT COMPLETION OF CENTER FUEL BURN. TANKS BURNED EVENLY UNTIL SEATTLE. GROUNDED - YES. FUELER REFUELED A/C 24.6 TOTAL FUEL ONBD. REFUEL DONE, NO PUMPS ON, CROSSFEEDSDR ASAA2020013082020Autothrottle Sys · disengagedAUTOTHROTTLE DISENGAGED AT 100 FT, UNABLE TO RE-ENGAGE THROUGHOUT FLIGHT. GROUNDED - YES. ACCOMPLISHED AUTOTHROTTLE BITE IAW FIM 22-31 TASK 801. ALL TESTS PASSED. ACCOMPLISHED LRU REPLACEMENT TEST FOR DFCS IAW AMM 22-11-00-740-815. ALL TESTS PASSED. ACCOMPLSDR ASAA2020011531861Unknown · malfunctionedWHEN CARGO TEST BUTTON IS PRESSED EXT FWD GREEN LIGHT DOES NOT ILLUMINATE. GROUNDED - YES. RAN FIM 26-16 TASK 806 AND INSPECTED FWD CARGO SMOKE DETECTORS NO FAULTS FOUND OPS TEST GOOD.SDR ASAA2020010331757Unknown · malfunctionedFWD CARGO EXT LIGHT DOES NOT ILLUMINATE DURING LIGHT TEST. GROUNDED - YES. PERFORMED B737-800 FIM 26-16-TASK 806. UPON INITIAL EVLAUATION CARGO FIRE CONTROL TEST CKS NORMAL. ALL REQURIED LIGHTS ILLUMINATE. NO OTHER DEFECTS NOTED.SDR ASAA2020010331761Unknown · malfunctionedAFTER LANDING, BOTH CDU'S BLANKED THEN CAME BACK ON "MENU" PAGE. NO FMC PROMPT FOR ABOUT 1 MIN. THEN IT CAME BACK. GROUNDED - YES. PERFORMED B737-800 FIM 34-61 TASK 801 AND FOUND FMC-L PGM FAULT. PERFORMED FIM 34-61 TASK 807 AND ALL NECESSARY PROMPTS SHOW. OPSSDR ASAA2019120971527Warning Message · false activationCONT CABIN ZONE TEMP LIGHT ILLUMINATED DURING RECALL. GROUNDED - YES. ACCOMPLISHED BIT CK ON BOTH CONTROLLERS B737-800 AMM 21-61-00, VERIFY GREEN LIGHT W/ NO REMAINING FAULTS.SDR ASAA2019112533435Valve · not closedF/A REPORTS NO POTABLE WATER FOR COFFEE MAKER OR SINKS. GROUNDED - YES. AIR TURNBACK - DIVERSION TIME 30 MINUTES - TROUBLESHOOT IN REF TO B737-800 FIM 38-10 TASK 803 FOUND FILL/OVERFLOW VALVE NOT CLOSING COMPLETELY AND LEAKING WHEN SERVICE DOOR CLOSED. REMOVSDR ASAA2019102331201Skin · crackedCRACK INDICATION NOTED BETWEEN AT STAB STA 138.70 AND STAB STA 147.90 APROX .5 IN LENGTH. LOCATION IS APOX 5 INCHS FROM CENTERLINE OF FWD ROW OF FASTNER AFT SPAR AND 2 INCH AFT SIDE FROM DOUBLER ON THE STA 147.90 END POINTS OF CRACK ARE IDENTIFIED IN RED MARKESDR ASAA2019102231205Floorbeam · corrodedFLOOR BEAM 986.5 APPROXIMATELY 4" FROM R/H INNER CHORD HAS CORROSION AROUND FASTENER HOLE. GROUNDED - YES. BLEND AND FOUND EDGE OF FASTENER HOLE TOO LARGE AMOUNT OF DAMAGE, ORIGINAL MATERIAL .150 MATERIAL REMOVED .072 REMAINING MATERIAL .078 FOUND TO BE OUT OFSDR ASAA2019091530703Elastomer · tornWHILE ACCOMPLISHING TC 78472010 FOUND THAT ALL THE PLATFORMS RUBBER ON #1 ENG IS RIPPING. GROUNDED - YES. REPLACED ALL PLATFORMS ON #1 ENG REF TC 78472010 FAN BLADE LUBE.SDR ASAA2019070829975Unknown · malfunctionedAT FLIGHT LEVEL 330, ONE CENTER TANK LOW PRESSURE ILLUMINATED. ASSOCIATED CENTER PUMP TURNED OFF AND CROSSFEED OPENED TO BALANCE FUEL. BOTH CTR PUMPS TURNED OFF AND CROSSFEED CLOSED. "FUEL IMBAL" ILLUMINATED WITH 1000 POUND IMBALANCE. CROSSFEED RE-OPENED AND FSDR ASAA2019061729715Connector · loose#2 ENG ANTI ICE COWL VALVE OPEN LIGHT ON THE FWD OVERHEAD PANEL CYCLES ON AND OFF WITHOUT SWITCH ACTUATION, HISTORY OF CONNECTOR DP1303 BEING FOUND LOOSE PRI 2 ETOPS SIGNIFICANT SYSTEM. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE HARNESS MW0313 IAW B737-800SDR ASAA2019060429585Connector · looseWITH ENGINE ANTI ICE OFF RT ENGINE COWL VALVE OPEN FLICKERS ON AND OFF. GROUNDED - YES. FOUND CANNON PLUG LOOSE TO TAI VALVE ON #2 ENG. REMOVED CANNON PLUG, INSPECTED, REINSTALLED CANNON PLUG, PERFORMED ENG RUN AND OPERATIONAL TEST GOOD. REF: B737-800 AMM CH. SDR ASAA2019051329333Connector · contaminatedENROUTE RT COWL VALVE OPEN BLUE LIGHT FLICKERING WITH ENG ANTI ICE SWITCH OFF. WHEN ENG ANTI ICE SWITCH SELECTED ON BRIGHT BLUE COWL OPEN LIGHT ILLUMINATED. LIGHT BRIGHT BLUE IN DESCENT REGARDLESS OF SWITCH POSITION. GROUNDED - YES. PERFORMED FIM 30-21 TASK 80SDR ASAA2019042929193Oil Cooler · leakingWHILE ACCOMPLISHING TSR FOR APU FREQUENT SERVICING FOUND A OIL LEAK NEAR THE AFT FITTING ON THE TURBINE SCAVENGE LINE. REF W/O 450930. GROUNDED - YES. REF FIM TASK 49-95 TASK 801 AND FOUND OIL COOLER LEAKING OIL COOLER REMOVED AND REPLACED OIL COOLER REF AMM 4SDR ASAA2019043099195Unknown · unknownENGINE CONTROL LIGHT ON #1 ENGINE AFTER START. EXTERNAL POWER FAILED ON PUSH. RELIED ON BATTERY POWER FOR APPROX. 15 MINUTES PRIOR TO STARTING ENGINE #1 AND ESTABLISHING AC ELECTRICAL POWER. GROUNDED - YES. THE AIRPLANE VOLTAGE INPUT TO EEC IS OUT OF RANGE. ASDR ASAA2019040188835Connector · damaged#2 ENGINE, CONNECTOR DP1103 AT GROUND WING THERMAL ANTI-ICE SOLENOID VALVE IS LOOSE. GROUNDED - YES. RESECURED #2 ENGINE CONNECTOR DP1103 BACKSHELL REF B737 SWPM 20-60-09.SDR ASAA2019022728391Warning System · false activationON RECALL CONT CAB ZONE TEMP LIGHT ILLUMINATED CLEARS ON RESET. GROUNDED - YES. FLIGHT PRIMARY TEMP CONT INOP. PERFORMED CABIN TEMP CONTROLLER BITE TEST PER AMM 21-61-00 SYSTEM OP CHECKS GOOD.SDR ASAA2019022518312Circuit Breaker · trippedSTANDBY POWER OFF LT ILLUMINATED IN FLIGHT ALSO NOTICED BATT BUS CB TRIPPED BEHIND FO SEAT SECT 2. GROUNDED - YES. RESET BUS SECTION 2 C/B REF B737-800 AMM 20-60-01-801, C/B REMAINS SET. PERFORMED OPS TEST OF THE STANDBY POWER SYS PER AMM 24-34-00-710-802 NO DSDR ASAA2019020528061Switch · inoperativeCREW REPORTS V/S MODE SELECT SWITCH LIGHT PARTIALLY INOP. GROUNDED - YES. REMOVED AND REPLACED DFCS MODE CONTROL PANEL PER AMM 22-11-34. PERFORMED MODE CONTROL PANEL INSTALLATION TEST PER AMM 22-11-34-740-801 AND DFCS GROUP 49 (LAND VERIFY) TEST PER AMM 22-11-SDR ASAA2019010327690Guide Arm · out of adjustL1 DOOR HARD TO LATCH CLOSED. GVI PERFORMED. FOUND UPPER INBOARD ROLLER LATCH DEEPLY GOUGED. GROUNDED - YES. FOUND L1 DOOR GUIDE ARM OUT OF ADJUSTMENT PER AMM 52-11-00-820-801.SDR ASAA2018112027090B-Nut · looseFUEL LEAKING AT 9 O’CLOCK STRUT ON NR 1 ENGINE. GROUNDED - YES. REMOVED 9:00 STRUT PANEL FOR ACCESS. SECURED & TORQUED, LOOSE VBV FUEL TUBE "B" NUT AT THE STRUT MOUNT, INSTALLED STRUT FAIRING AT THE 9 O’CLOCK POSITION, REF SHOP MANUAL 72-00-00 -ASSY 002. LEAK SDR ASAA2018112027083Heater · leakingNR 1 ENG FUEL HEATER SERVO LEAKING AT THE CAP. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENG SERVO FUEL HEATER REF AMM 73-11-07. OPS & LEAK CK GOOD.SDR ASAA2018111636857Warning Message · false activationAFTER START AND AFTER BLEED SWITCHES ON (AND PACK SWITCHES ON) WE HAD A "ZONE TEMP" LIGHT THAT CAME ON FOR THE CONTROL CABIN WITH MASTER CAUTION RECALL AND WENT OUT FO WITH RESET. GROUNDED - YES. INITIAL EVALUATION FOUND #2 PACK/ZONE TEMP CONTROLLER SHOWING FLSDR ASAA2018111126815Compensator · out of limitsPROBES F15, 2, AND 7 ARE OUT OF LIMITS IN THE NR 2 TANK. GROUNDED - YES. REMOVED AND REPLACED COMPENSATOR PROBE F15 AND TANK UNITS F2 AND F7 REF B737-28-41-21. NR 2 F/Q SYSTEM TEST GOOD REF AMM 28-41-00-730-801.SDR ASAA2018111126814Compensator · out of limitsPROBES F15, 6 9 AND 10 IN THE NR 1 TANK ARE OUT OF LIMITS. GROUNDED - YES. REMOVED AND REPLACED COMPENSATOR PROBE F15 AND TANK UNITS F6, F9 AND F10 REF B737-28-41-21. NR 1 F/Q SYSTEM TEST GOOD REF AMM 28-41-00-730-801.SDR ASAA2018110856740Nozzle · burnedWHILE ACCOMPLISHING TASK CARD 78477022, FOUND #1 ENG S/N 894763. 3 LPT NOZZLES TOTAL AT 4 O CLOCK, 7 O CLOCK, AND 10 O CLOCK POSITION WITH BURN MARKS AND MISSING MATERIAL. GROUNDED - YES. ON DEFERRAL.SDR ASAA2018092625263Apu · malfunctionedATTEMPTED TO START APU, GOT CLIMBING HIGH EGT WITH NO SUCCESSFUL START, WITH REVERBERATING NOISE. CURRENT CODE 49-94226. LOW OIL PRESSURE SWITCH SHOWS OPEN CIRCUIT, NO FAULT LIGHTS ILLUMINATED. GROUNDED - YES. VISUALLY INSP TAILCONE, NO DEFECTS NOTED. OIL LEVESDR ASAA2018090726037Exciter · failedENGINE NR 1 HUNG START WITH RIGHT IGNITER SELECTED. STARTED NORMALLY WITH LEFT IGNITER SELECTED. GROUNDED - YES. REMOVED & REPLACED EXCITER UNIT REF AMM 74-11-01. AUDIBLE CHECKED GOOD REF AMM 74-00-00. POWER IDLE CHECKED NORMAL REF AMM 71-00-00.SDR ASAA2018081925839Coupler · failedHF 2 WILL NOT TRANSMIT OR RECEIVE. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 HF ANTENNA COUPLER. OPS NORMAL IAW AMM 23-11-61-400-801.
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