N587AS
Service difficulty reports · 482
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 = 'N587AS' 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 = 'N587AS' 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 ASAA2021080435621Autoland Sys · faultedATTEMPTED AUTOLAND & HGS AIII, DEVELOPED A HIGH SINK RATE AND DID NOT FLARE. THEN APP/WARN IN THE HUD. DISCONNECTED A/P A/T AND LANDED MANUALLY. GROUNDED - YES. CHECKED FOUND HGS APCH WARN FOR LEG 6 AIRSPEED EXCEEDANCE. HGS SYSTEM TEST PASSED REF HGS 4000 SSM SDR ASAA2021072135507Probe · failedTEMP PROBE ANTI - ICE MASTER CAUTION ILLUMINATED IN CRUISE. INDICATIONS NORMAL. GROUNDED - YES. REMOVED AND REPLACED TAT PROBE IAW B737-800 AMM 34-21-06. OPS CHECK OKAY.SDR ASAA2021071535433Packing · failed#2 ENG HAS EXCESSIVE AMOUNT OF OIL DRIPPING FROM BOTTOM OF THE FAN COWL. GROUNDED - YES. PERFORMED IDLE RUN LEAK CHECK ON #2 ENG FOUND OIL LEAK FROM QAD ADAPTOR STARTER REF B737-800 MM 71-00-00. REPLACED BOTH PACKINGS ON STARTER REF AMM 80-11-01. IDLE LEAK CHKSDR ASAA2021071535405Housing · damagedMID CABIN EXIT SIGN LENS COVER HAS FALLEN OFF. GROUNDED - YES. (RESOLVED ON W/O: 1879171 TASKCARD: N/R-00001 ) REMOVED AND REPLACED MID CABIN EXIT SIGN LIGHT ASSY PER B737-800 AMM 33-51-01. OPS CHECK GOOD. THIS CLEARS PLT, SEAMC JAKE NOTIFIED.SDR ASAA2021061535102Sensor · inoperativeEQUIP COOLING FAN ALTN LT. ON. GROUNDED - YES. DIVERSION TIME 31 MINUTES - REF LP 60175101 EQUIP COOLING EXH. NORM INOP AS WELL. FOUND EQUIP COOLING EXH LOW FLOW SENSOR COMPLETELY CLOGGED CAUSING BOTH NORM & ALT TO FAIL. VERIFIED BOTH FANS ARE RUNNING - AFTER SDR ASAA2021051834855Starter · failedNO ROTATION WHEN TRYING TO START #1 ENG. GROUNDED - YES. ATTEMPTED MANUAL START VALVE ACTUATION FROM GROUND START VALVE MOVES FREELY AS REQUIRED,CKD START VALVE CIRCUIT BREAKERS ALL SET NO POPPED BREAKERS SUSPECT BAD STARTER REF B737-800 FIM 80-07 TASK 802. RESDR ASAA2021032134335Display · inoperativeCAPTAINS MCDU SCREEN BLANKED, WARNING LIGHT CAME ON, AND BIT MESSAGE DISPLAYED ON SCREEN. SEQUENCED AT LEAST 10 CYCLES. NO ASSOCIATED MAP OR VTK WARNING ON CDU'S. GROUNDED - YES. REMOVED, REPLACED, AND TESTED CAPTAIN'S MCDU PER B737-800 MM 34-61-01-000-802 / ASDR ASAA2021031834333Fmc · not reportedFMC L RECYCLED RESET TEST 8 TO 10 TIMES WORKED PROPERLY AFTER FINAL RESET. GROUNDED - YES. RESET FMC PER FIM TASK 34-61 TSK 836 OPS CHECK OK.SDR ASAA2020080642991Computer · malfunctionedL NAV WOULD NOT ENGAGE . SELECTED A DIFFERENT DEPARTURE L NAV ENGAGED. GROUNDED - YES. PERFORMED FIM 22-11 TASK 830, VERIFIED CORRECT FLIGHT PLAN WAS ENTERED. L NAV NOW ENGAGES, NO FURTHER MAINT ACTION REQUIRED VERIFICATION SUCCESSFUL.SDR ASAA2020072832943Terminal · looseACCOMPLISHED TROUBLESHOOTING RECOMMENDATIONS PER TSR705030 FOR HISTORY OF #1 ENGINE B LOOP NOT TESTING PROPERLY AND CAUSING DELAYS. RESISTANCE CHECK OF ENG 1 LOOP B FROM CONNECTOR D1002. CHECKS WITHIN LIMITS. REF B737-800 FIM 26-10 TASK 805. RIGHT CORE DETECTOSDR ASAA2020072072907Fire Detector · no test#1 ENGINE FIRE LIGHT FAILS TEST. TEST OK WITH "A" SELECTED . GROUNDED - YES. PERFORMED B737-800 FIM 26-10 TASK 801 WITH NO FAULTS AND OPS NORMAL. PERFORMED GVI OF FAN & CORE # 1 ENGINE LOOP WITH NO DEFECTS NOTED. PLACARDS REMOVED.SDR ASAA2020071632914Seal · broken#2 ENGINE OIL CAP SEAL BROKEN. GROUNDED - YES. REPLACED #2 ENGINE OIL CAP PACKING. OK FOR SERVICE.SDR ASAA2020070632862Unknown · malfunctionedNR 1 ENGINE FIRE LOOP B WILL NOT TEST. GROUNDED - YES. NR 1 ENGINE FIRE LOOP B INOP. ACCOMPLISHED FIM 26-10 TASK 801. OPS CHECK NORMAL. UNABLE TO DUPLICATE. MOVED LOOP SELECTOR SWITCH BACK TO NORMAL POSITION. REMOVED MEL.SDR ASAA2020070132856Modulating Valve · malfunctionedON RECALL CONT CAB ZONE TEMP LIGHT ILLUMINATES. EXTINGUISHES WITH RESET. NO TEMPERATURE FLUCTUATIONS. GROUNDED - YES. PERFORMED BITE CHECK, FOUND FLT DECK TRIM VALVE BAD. REMOVED AND REPLACED FLT DECK TRIM VALVE, REF AMM 21-61-21. OP CHECK GOOD.SDR ASAA2020061832813Valve · leakingNR 1 ENG HPT ACC LEAKING 4 DROPS PER MIN. GROUNDED - YES. REMOVED AND REPLACED THE NR 1 ENG HPT ACC VALVE IAW AMM 75-21-01-000-801-F00, & AMM 75-21-01-400-801-F00. LEAK CHECKED GOOD AND ACTUATOR TEST C/W -OPS NORMAL.SDR ASAA2020061103792Indicator · brokenNO 1 ENG LUBRICATION UNIT CLOGGING INDICATOR GLASS BOWL BROKEN. GROUNDED - YES. REMOVED AND REPLACED NO 1 ENG LUBRICATION UNIT CLOGGING INDICATOR GLASS BOWL REF B737-800 CMM 79-21-16 PG 302 & 305 STEP 4 I 1 & 2 AND PGS 703,706 & 709 STEPS 4.C. 26&27.SDR ASAA2020051632737Valve · leakingNR 1 ENGINE HAS A DRAIN LEAKING FUEL. FOUND HPTACC VALVE DRAIN AT 4 DROPS PER MINUTE. ALLOWABLE LIMITS LESS THAN 90 DPM. GROUNDED - YES. REMOVED AND REPLACED THE NR 1 ENG HPTACC VALVE IAW AMM 75-21-01-000-801-F00, & AMM 75-21-01-400-801-F00. LEAK CHECKED C/SDR ASAA2020051632729Hmu · leakingFUEL LEAKING CONTINUOUSLY FROM #1 ENGINE HMU DRAIN LINE. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE HMU REF T/C N8473001SDR ASAA2020051832728Pump · leakingFUEL LEAK, #1 ENGINE, AT THE PUMP/HMU MATING SURFACE. GROUNDED - YES. REMOVED AND REPLACED FUEL PUMP REF B737-800 AMM TASK 73-11-11-400-801-F00 3.A THRU 6.SDR ASAA2020051832727Bolt · missing#1 ENG EXHAUST CONE FLANGE MISSING ON BOLT @ 3 O'CLOCK POSITION. GROUNDED - YES. FOUND AND REINSTALLED BOLT AT 3 O'CLOCK POSITION ON THE #1 ENG EXHAUST FLANGE REF B737-800 AMM 72-56-00-400-801-F00.SDR ASAA2020033032690Fuel Line · damaged#1 ENGINE INLET AND FAN BLADES - DETAILED INSPT. FOUND FUEL LINE FROM IDG OIL COOLER HAS DAMAGED OUTER RUBBER COVER TORN. GROUNDED - YES. REMOVED AND REPLACED IDG OIL COOLER FUEL LINE P/N 340-016-251-0. REF B737-800 AMM 73-11-06-000-801-F00. AMM 73-11-01-000-8SDR ASAA2020032632559Fastener · looseREF T/C 78472000 #1 ENGINE INLET AND FAN BLADES- DETAILED INSPT. FOUND R/H MIDDLE FASTENER AND #6 STRUT PANEL DAMAGED DUE TO FASTENER BEING LOOSE. (M) ALF. GROUNDED - YES. REMOVED AND REPLACED #6 STRUT PANEL PN:340-084-003-0 REF B737-800 AMM 72-23-07.SDR ASAA2020032332499Light · inoperativeEMERGENCY LIGHT EXIT LOCATOR SIGN AT RIGHT AFT OVERWING EXIT HAS MULTIPLE LAMPS INOP. GROUNDED - YES. RELAMPED AND TESTED PER B737-800 MM 33-51-01-960-801 - OPS NORMAL.SDR ASAA2020030932353Wire Harness · broken#1 ENG "A" LOOP INOP. GROUNDED - YES. CONFIRMED FAULT, #1 ENGINE A-LOOP WILL NOT TEST. FOUND R/T CORE FIRE DETECTOR HARNESS (MW0315) TERMINAL LUG BROKEN AT THE DETECTOR, TOO SHORT TO REPAIR WIRING. REMOVED & REPLACED MW0315 CORE FIRE DETECTION HARNESS (A-LOOP)SDR ASAA2020021132159Engine · malfunctionedNO. 1 ENGINE WOULD NOT LIGHT OFF RIGHT OR LEFT IGN. GROUNDED - YES. FOUND 3 C/B OUT. ACCOMPLISHED C/B. RESET PROCEDURE. NO DEFECTS NOTED. REF B737-800 AMM 20-60-01. ACCOMPLISHED ELECTRICAL CONTROL AND INDICATION TEST FOR #1 ENGINE FUEL SPAR VALVE. TEST PASSED.SDR ASAA2020011331831Wire · brokenNR 1 ENG A LOOP INOP. GROUNDED - YES. ACCOMPLISHED FIRE DETECTION CONTROL MODULE BITE TEST PER FIM 26-10 TASK 801. PERFORMED VISUAL INSPECTION OF FIRE LOOPS AND HARNESSES FOUND RT CORE A LOOP WIRE BROKEN AT TERMINAL LUG. REPLACED TERMINAL PER AMM 26-11-002-960SDR ASAA2020010331777Coupler · faultedETOPS VERIFICATION FLIGHT FOR HF1 UNSATISFACTORY- HF1 TESTED WITH SFO RADIO ARINC AND THEY REPORTED THAT OUR TRANSMISSIONS WERE WEAK AND UNREADABLE. TESTED ON MULTIPLE FREQUENCIES. SENSITIVITY WAS SET TO 100- HF1 TUNING TOOK SLIGHTLY LONGER THAN NORMAL AS WELLSDR ASAA2019122391675Hf Comm · malfunctionedUNABLE TO TRANSMIT ON HF1. GROUNDED - YES. CYCLED POWER TO HF1 OPS RESTORED AND CHECKS OKAY REF B737-800 FIM 23-11 TASK 806 + 801SDR ASAA2019121973641Transceiver · failedHF #1 WILL TUNE & RECEIVE BUT WILL NOT TRANSMIT VOICE. GROUNDED - YES. R&R #1 HF TRANSCEIVER REF AMM 23-11-21 GROUND VERIFICATION NMLSDR ASAA201912031490Display · malfunctionedMAP FLAG ON FIRST OFFICERS INBOARD DISPLAY UNIT. GROUNDED - YES. PERFORMED SYSTEM RESET PER B737-800 FIM 34-61 TASK 836 & CYCLED POWER TO SYSTEM PER B737-800 AMM 20-60-05 OPS CHECK NORMAL.SDR ASAA2019112191390Radar · malfunctionedRADAR ONLY SWEEPS FROM LEFT TO RIGHT ON BOTH SIDES. CAPT RADAR BLANKS FOR 1 SECOND EACH SWEEP. GROUNDED - YES. COULD NOT DUPLICATE. OPS CHECK WX RADAR GOOD. REF B737-800 AMM 34-43-00.SDR ASAA2019111841356Transmitter · malfunctionedUNABLE TO TRANSMIT ON HF 1 WHEN TUNING SIDETONE LAST FOR ABOUT 5 SECONDS RECEIVING WORKS AND SELCAL FUNCTIONS NORMALLY. GROUNDED - YES. PERFORMED OPS TEST OF HF COMM SYS IAW B737-800 AMM 23-11-00-710-801 OPS CHECK AND GROUND VERIFICATION SUCCESSFUL.SDR ASAA2019103081169Indicator · malfunctionedFUELER REPORTS #1 FUEL GAUGE AT FUELING PANEL IS BLINKING. GROUNDED - YES. REMOVE AND REPLACED #1 FUEL QTY INDICATOR PER B737-800 AMM 28-41-61. OPS CHECK GOOD. CHP 5 ALTERNATE DEACTIVATION TABLE 3 ITEM 1 USED. REVERSE ALTERNATE DEACTIVATION.SDR ASAA2019082930585Unknown · malfunctionedREFUELER REPORT THAT THEY ARE UNABLE TO ADD FUEL TO TANK #1. GROUNDED - YES. PERFORMED FQIS BITE CHECK, NO CURRENT FAULTS NOTED, PERFORMED FUEL QUANTITY COMPARISON CHECK IAW AMM 28-41-00, NO DEFECTS NOTED, #1 TANK FOUND TO BE FULLY FUELED.SDR ASAA2019082623462Battery Pack · dischargedEMERGENCY LIGHT SIGNS AT L2 DOOR AREA ARE INOP. GROUNDED - YES. REMOVED AND REPLACED PERFORMED SUCCESSFUL SYSTEM OP CHECK ON EMERGENCY POWER SUPPLY M1673 IAW B737NG AMM 33-31-06-960-805.SDR ASAA2019082623461Power Supply · inoperativeEMERGENCY LIGHT SIGNS AR R1 DOOR AREA ARE INOP. GROUNDED - YES. REMOVED & REPLACED EMER, LIGHT PWR SUPPLY M1674, OPS CHECKS GOOD ALL R1 LIGHTS IAW 737NG AMM 33-51-06-960-805.SDR ASAA2019082623460Power Supply · inoperativeEMERGENCY LIGHT SIGNS AR R1 DOOR AREA ARE INOP. GROUNDED - YES. REMOVED & REPLACED EMER, LIGHT PWR SUPPLY M1674, OPS CHECKS GOOD ALL R1 LIGHTS IAW 737NG AMM 33-51-06-960-805.SDR ASAA2019082623459Battery Pack · failedEXTERIOR EMERGENCY LIGHT AT LH FWD OVERWING DOOR AREA IS INOP. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK IAW B737-NG AMM 33-51-06-960-805. OPS CHECK GOOD.SDR ASAA201908230448Battery Pack · faultedEMERGENCY EXIT O/W LIGHTS OUT GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK AND CHARGER.SDR ASAA201908230447Power Supply · inoperativeEMERGENCY LIGHT SIGN AT R1 DOOR AREA INOP GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M1674 S/N 36074, OPS CHECKED GOOD ALL R1 LIGHTS IAW B737-800 AMM 33-51-06-960-805.SDR ASAA201908230446Battery Pack · inoperativeEMERGENCY LIGHT SIGN AT L2 DOOR AREA INOP. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M1673 S/N 66253. PERFORMED SUCCESSFUL OP CHECK ON EMERGENCY POWER SUPPLY M1673 IAW B737-800 AMM 33-51-06-960-805.SDR ASAA2019080843331Floorbeam · crackedMAIN CABIN, PANEL BREAK SUPPORT CHANNEL CRACKED AT STA 540 BL0-LBL24. GROUNDED - YES. REMOVED AND REPLACED PANEL BREAK AT STA 540 BL 0 - LB L 24 IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A0060 REV-.SDR ASAA2019080643308Floor Support · crackedMAIN CABIN FLOOR SUPPORT INTERCOSTAL AT STA 312-328 LBL46 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL IAW B737-800 SRM 51-40-02. REMOVED DOT A621 REF BAC DWG 141A5400 REV "-".SDR ASAA2019081923407Floorbeam · corrodedAFT CABIN FLOOR SUPPORT CORRODED BS 947, BL 5L - BL 10R. GROUNDED - YES. REMOVED DAMAGE AND CHECKED LIMITS ORIGINAL THICKNESS .180 REMAINING 0.151,REMOVED 0.029. OUT OF LIMITS IAW B737-800 SRM 53-70-51. CUT OUT DAMAGE ANDINSTALLED "T" CHORD REPAIR STA 947 LBL SDR ASAA201908123349Floor Support · crackedCRACKS ON CABIN FLOOR SUPPORT ANGLE AT STA. 380-400, LBO 14 GROUNDED - YES. REMOVED AND REPLACED UPPER CHORD IAW BAC DWG 143A5400 AND B737-800 SRM 51-40-02SDR ASAA201908123348Fitting · corrodedL1 DOOR AFT GIRT BAR MOUNT FITTING HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED TIEDOWN FITTING P/N 141A5220-4 PO. 951405.2 IAW B737-800 SRM 51-40-02 AND AMM 20-50-11 TOOL # T8482Q DUE 11/14/2019SDR ASAA201908123347Fitting · corrodedL1 DOOR FWD GIRT BAR MOUNT FITTING HAS CORROSION GROUNDED - YES. REMOVED AND REPLACED TIEDOWN FITTING P/N 141A5220-2 PO. 951405.1 IAW B737-800 SRM 51-40-02 AND AMM 20-50-11 TOOL # T8482Q DUE 11/14/2019SDR ASAA201908123345Channel · corrodedL1 DOOR MOP SILL HAS MULTIPLE AREAS CHAFED FROM FLOOR PANEL INSERTS. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS OF .090, REMAINING THICKNESS OF .062, MAT LOSS OF .028 USING TOOL T8225G DETERMINED TO BE OUT OF LIMITS IAW B737-800 SRM 53-10-15, RECEIVSDR ASAA2019082213437Failsafe · dentedFUSELAGE FRAME, STATION 325.6 STRINGER 25L LBL 40, HAS FAIL SAFE ANGLTHAT IS DENTED. GROUNDED - YES. REMOVED AND REPLACED FUSELAGE FRAME, STA 325.6 STR 25L LBL 40 FAIL SAFE CHORD PER B737 DWG 141A1360 REV.- AND B737-800 SRM 51-40-02.SDR ASAA2019080193401Skin · gougedMAIN CABIN AFT GALLEY SERVICE DOOR CUTOUT FWD FRAME EXTERNAL SKIN EDGE GOUGED JUST ABOVE UPPER TORQUE TUBE MOUNT. GROUNDED - YES. REMOVED AND REPLACED SKIN CORNER 147A3110-6 REF B737-800 SRM 51-40-02 AND BAC DWG 147A0020 REV -.
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