N569AS
Service difficulty reports · 514
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 = 'N569AS' 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 = 'N569AS' 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 ASAA2018012123249Fmc · malfunctionedBOTH FMC'S WENT OFF-LINE AFTER LANDING FMC PROMPT CAME BACK UP DURING TAXI IN. GROUNDED - YES. L AND R FMC LOGGED "PGM FAULT". PERFORMED FIM 34-61 TASK 807, CYCLED 2 CB'S. OPS NML PER SAME. NO HISTORY LAST 30 DAYS. ETOPS GROUND VERIFICATION TEST NML, REF FIM 3SDR ASAA2018011123162Anti-Ice Valve · failedWHEN ENGINE ANTI-ICE SELECTED, BRIGHT BLUE COWL VALVE LIGHT REMAINS BRIGHT WITH AMBER TAI INDICATION ON UPPER DISPLAY INTERMITTENT. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENG ANTI-ICE VALVE IAW AMM 30-21-11-400-9-801. OPS AND LEAK CHECKED NORMALSDR ASAA2017121922986Latch · brokenOVERWING EMERGENCY EXIT SIGN HANGING FROM THE CEILING ABOVE THE CENTER ISLE, THE SIGN HOUSING ACCESS PANEL LATCH IS BROKEN. ACFT GROUNDED. ACCOMPLISHED TEMPORARY REPAIR IAW EA 88-33EA-19666.SDR ASAA2017120922861Fault Message · illuminatedDURING ACCOMPLISHMENT OF T/C 78273000 #1 ENGINE HAS A SHORT TIME FAULT MSG 73-21281 EEC CHANNEL IS NOT ENERGIZED WITH THE ALTERNATOR VOLTAGE. GROUNDED - YES. UPON RECHECK OF T/C 78273000 - FOUND NO #1 ENGINE RECENT FAULTS AND FAULT HISTORY SHOWED DEFERRED FAULSDR ASAA2017120822835Bleed Valve · failedPERFORMED BLEED OFF TAKEOFF IN HNL. UPON CONFIGURING BLEEDS; #1 BLEED VALVE DID NOT OPEN. OPENED ISO VALVE TO CONFIRM #1 PACK OPERATION. L DUCT PRESS SHOWED ZERO W/PACK & BLEED SW ON W/ISO VALVE IN AUTO. ATTEMPTED NUMEROUS RECYCLES OF SWITCHES. CONTACTED MX CTSDR ASAA2017120522790Engine · faulted#2 ENGINE CODE 75-20802 T25 SIGNALS DISAGREE SHORT TERM FAULT. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 75-33 TASK 805 INITIAL EVALUATION. PERFORMED EEC BITE PER FIM 73-00 TASK 801 AND EEC TEST PER B737-800 AMM 73-21-00-700-804-F00. THERE ARE NO RECENT FAULTSSDR ASAA2017112522705Fault Code · false activationFOUND A NR 1 ENGINE FAULT CODE 73-11271, THE ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE, SHORT TERM FAULT, ACFT GROUNDED. PERFORMED TASK CARD 78237000. NO FAULTS FOUND IAW FIM 73-27, TASK 804. THIS IS AN INTERMITTENT FAULT.SDR ASAA2017111222550Starter · failedNO N2 ROTATION UPON STARTING NR 2 ENGINE. ABORTED START LIST ACCOMPLISHED. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 STARTER IAW AMM 80-11-01/401, OPS CHECKED GOOD.SDR ASAA2017102922341Oil System · lowBLUE APU MAINT LIGHT ILLUMINATED AFTER APU START. ACFT GROUNDED. SERVICED THE APU OIL IAW AMM 12-13-31.SDR ASAA2017101822252Static Inverter · warning lightELEC LIGHT ON. ACFT GROUNDED. PERFORMED ELEC LIGHT BITE PROCEDURE IAW FIM 24-31, TASK 801. LOGGED STATIC INVERTER INOP 1. PERFORMED A STATIC INVERTER INOPERATIVE PROCEDURE IAW FIM 24-34, TASK 801. FAULT RESET, DEFECT DEFINED AS AN INTERMITTENT FAULT. REPLASDR ASAA2017101622209Warning Light · false activationELECTRIC LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED BITE IAW FIM 24-31, TASK 801. LOGGED SPCU INOPERATIVE FAULT. PERFORMED FIM 24-34, TASK 802. FAULT RESET, CHECKED GOOD.SDR ASAA2017092121994Battery · dischargedBATTERY FOUND NOT CHARGING, VOLTAGE LOW. ACFT GROUNDED. REMOVED AND REPLACED TWO BATTERIES IAW AMM 24-31-11. A BATTERY TEST CHECKED NORMAL.SDR ASAA2017083021770Warning Light · illuminatedRED BOX SHOWED UP ON THE NR 1 ENGINE EGT DURING SHUTDOWN. NO EXCEEDANCES NOTED DURING FLIGHT. ACFT GROUNDED.SDR ASAA2017083021760Fault Message · unknownWHILE ACCOMPLISHING T/C 78273000, A MESSAGE FOR THE RT ENGINE, 75-20802 (T25 SIGNALS DISAGREE) SHORT TIME FAULT. ACFT GROUNDED. PERFORMED FIM 75-33 TASK 805, CHECKED RESISTANCE AT THE T 25 SENSOR. RESISTANCE CHECKED GOOD. CHECKED WIRING FROM CONNECTOR DP09SDR ASAA2017081321634Sensor · failedDUCT PRESSURE SPLIT. DURING CLIMB LEFT 17 PSI, RIGHT 48 PSI. DURING CRUISE, LEFT 20 PSI, RIGHT 43 PSI. ACFT GROUNDED. PERFORMED FIM 36-10 TASK 804. ALL STEPS CHECKED GOOD UP TO PAR F(29). PER STEP F(29)(B). REPLACED THE NR 1 ENGINE 450 THERMOSTAT, IAW SDR ASAA2017080621552Satcom · failedLOST SATCOM ENROUTE. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURES IAW QRH. SATCOM OPS RESTORED NORMAL.SDR ASAA2017080121514Fault Code · false activationFOUND FAULT 73-31372 FOR UPPER EGT SECTORS READING TOO HIGH ON THE NR 2 ENGINE DURING ACCOMPLISHMENT OF T/C 78273000. ACFT GROUNDED. PERFORMED TASK CARD 7827300, NO EGT FAULTS NOTED. PERFORMED FIM 73-11, TASK 801. CLEANED EGT CONNECTORS IAW AMM 77-21-00. SDR ASAA2017080121517Unknown · malfunctionedDURING FLARE, AIRCRAFT PITCHED DOWN AND REFLARED THEN DRIFTED RIGHT APPROX 35 FEET AS APPROACH WARNING IDICATED. MANUALLY TOOK OVER TO LAND. ACFT GROUNDED. SYS TESTED GOOD IAW AMM 22-00-01-730-807. NO HISTORY.SDR ASAA2017073021501Satcom · lockedSATCOM LOCKED UP, ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.SDR ASAA2017071621384Circuit Breaker · trippedL1 WINDOW OVERHEAT LIGHT ILLUMINATED IN FLIGHT. PERFORMED QRH BUT LIGHT REMAINS ILLUMINATED WHEN SWITCH IS ON. ACFT GROUNDED. FOUND CIRCUIT BREAKER TRIPPED ON P6-11, CIRCUIT BREAKER B-9. PERFORMED CIRCUIT BREAKER RESET PROCEDURES IAW AMM 20-60-01. NO DEFECTSSDR ASAA2017061421064Control Panel · failedAUTOPILOT ENGAGE SWITCH FOR CWS B IS INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED MCP IAW AMM 22-11-34. TESTED OK. IAW AMM 22-11-34-740-801. ACCOMPLISHED DFCS REPLACEMENT TEST FOR MCP BITE GRP 32 IAW AMM 22-11-33/401. ACCOMPLISHED LAND VERIFY BITE GRPSDR ASAA2017061121038Control Panel · intermittentHEADING KNOB WORKS INTERMITTENTLY. ACFT GROUNDED. REPLACED MASTER CONTROL PANEL. ACCOMPLISHED INSTALLATION TEST AND LLM TESTS. ALL PASS IAW AMM 22-11-34-400-801.SDR ASAA2017060921006Knob · looseHEADING SELECT KNOB WILL OCCASIONALLY NOT CHANGE DIGITS. MOVING OR PUSHING AND PULLING ON THE SELECTOR KNOB WILL START IT WORKING AGAIN. ACFT GROUNDED. HEADING KNOB ON MCP WAS SLIGHTLY LOOSE. TIGHTENED THE TWO SET SCREWS ON KNOB USING ALLEN WRENCH. KNOB OPS. SDR ASAA2017060921005Autopilot Sys · malfunctionedHEADING BUG STUCK ON 102 HEADING CAN NOT BE MOVED. ACFT GROUNDED. UNABLE TO DUPLICATE, HEADING DISPLAY ON MCP AND ND OPERATE NORMALLY IAW AMM 22-11-34.SDR ASAA2017032620316Control Unit · failedFOLLOW-UP TO R2 WINDOW HEAT POWER C/B TRIPS CAUSING DELAYS. GROUNDED - YES. REMOVED & REPLACED WHCU M320, REF AMM 30-41-11. OPS CHECK NORMAL.SDR ASAA2017032520257Circuit Breaker · openDURING PRE-FLIGHT FOUND CIRCUIT BREAKER FOR WINDOW HEAT RIGHT SIDE AC WAS FOUND OPEN. ACFT GROUNDED. RESET THE CIRCUIT BREAKER IAW AMM 20-60-01 AND OPS OK IAW AMM 30-41-00.SDR ASAA2017032320256Circuit Breaker · openR2 WINDOW OVERHEAT LIGHT ON. WON'T RESET, WINDOW FEELS COOL. ACFT GROUNDED. CIRCUIT BREAKER FOUND OPEN, RESET THE CIRCUIT BREAKER IAW AMM 20-60-01, AND WINDOW HEAT OPS NORMAL IAW AMM 30-41-00. NO HISTORY LAST 60 DAYS.SDR ASAA2017030220008Generator · failedNR 1 GENERATOR WILL NOT COME ONLINE AFTER ENGINE START. NO AC VOLTS OR FREQUENCIES ON THE NR 1 GEN WITH ENGINE RUNNING. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 GENERATOR IAW AMM 24-11-11-50.SDR ASAA2017020819811Support · corrodedAFT PIT FLOOR CROSS SUPPORT CORRODED BS 767 - BS 787. GROUNDED - YES. REMOVED CORROSION ORIGINAL MATERIAL .070 IAW BAC DRAWING 1466A9401 REV C. REMOVED .008 REMAINING .062. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. RECEIVED NEW TEE ASSEMBLY PART NUMBER 146A9SDR ASAA2017020727791Door Sill · corrodedAFT CARGO DOOR SILL CORRODED. GROUNDED - YES. REMOVED CORROSION AT AFT CARGO DOOR SILL WEB IAW SRM 53-00-15-1A ORIGINAL MAT .050 MAT REMOVED .017 FOUND TO BE OUT LIMITS IAW SRM 53-00-15-1A I RECEIVED NEW PART LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG # 453ASDR ASAA2017020719793Door Sill · corrodedAFT CARGO DOOR SILL CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT LIMITS IAW SRM 53-00-15-1A. NEW PART LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 453A8120 REV. INSTALLED THE NEW DOOR SILL IAW SRM 51-40-02 AND DWG 146A8340 REV.SDR ASAA2017020619829Transition Panel · corrodedAFT CARGO BAY RT TRANSITION PANEL HAS CORROSION FROM BS 727+4 - 767. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2, REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 51-40-02, SRM 51-40-02, 53-00-53-2R-5, DWG 146A7502 RSDR ASAA2017020619828Transition Panel · corrodedAFT CARGO BAY LT TRANSITION PANEL HAS CORROSION FROM BS 727+4 - 847. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW SRM 53-60-53-01-2 & DWG 146A7502 REV -. INSTALLED IAW SRM 51-40-02 & DWG 146A7502 REV - , 14SDR ASAA2017020619792Tee Fitting · corrodedAFT CARGO FLOOR TEE ASSY AT BS 727D IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2.SDR ASAA2017020219656Warning Light · false activationCONTROL CABIN ZONE TEMP AND LEFT PACK LIGHTS ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE TEST AND FOUND TCV FAIL ON LEFT CONTROLLER, RESET FAULT AND AND RETESTED WITH NO FAULT. OPERATED SYSTEM. CONT. CABIN ZONE TEMP AND LT PACK LISDR ASAA2017012819914Wire Harness · faultedNR 1 ENGINE SHOWS MESSAGES 75-10601 (TBV POSITION SIGNALS DISAGREE) SHORT TIME FAULT, 75-10591 (TBV POSITION SIGNALS DISAGREE) LONG TIME FAULT, AND 75-20601 (TBV POSITION SIGNALS DISAGREE), SHORT TIME FAULT. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINESDR ASAA2017012319527Starter · failedUNABLE TO START NR 1 ENGINE. START VALVE OPEN LIGHT ILUMINATED, NO ROTATION. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE STARTER IAW AMM 80-11-01. LEAK AND OPS CHECKED GOOD.SDR ASAA2017011519381Valve · wornENG 1 HIGH STAGE VALVE WORN. GROUNDED - YES. REMOVED AND REPLACED HIGH STAGE VALVE. OPS CK GOOD AND NO LEAKS NOTED REF AMM 36-11-06.SDR ASAA2017011419387Actuator · leakingNR 1 ENGINE LT VSV ACTUATOR LEAKING (AT 6:00 DRAIN) (8 DROPS PER MINUTE). GROUNDED - YES. REMOVED AND REPLACED NR 1 ENG LT VSV ACTUATOR. NO LEAKS NOTED OPS CK GOOD. REF AMM 75-31-01.SDR ASAA2017011419378Battery Pack · dischargedWHILE ACCOMPLISHING TASK CARD 78233001 LIGHTS FROM SEAT ROW 25 AFT ON LEFT SIDE OF AIRCRAFT AND CENTER AFT GALLEY LIGHT FAILED 15 MIN CHECK AFTER DEEP CYCLE OF BATTERIES. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK AT POWER SUPPLY M1673 AND M1672 REF AMMSDR ASAA2016123119223Actuator · leakingFUEL DRIPPING FROM THE NR 1 ENGINE RT VSV ACTUATOR DRAIN TUBE WITH ENGINE OPERATING. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE VSV ACTUATOR IAW AMM 75-31-01-000-802-F00 AND AMM 75-31-01-400-802-F00. ACCOMPLISHED ACTUATOR TESTS IAW TABLE TEST 3A, TESDR ASAA2016121219021Transceiver · failedNR 2 HF SHOWS FAILED. ACFT GROUNDED. NR 2 HF TRANSCEIVER HARD FAIL, NO BITE TEST. REMOVED & REPLACED IAW AMM 23-11-21, SYSTEM OPS CHECKED NORMALSDR ASAA2016120118908Warning Light · false activationCONTROL CABIN ZONE TEMP ANNUNCIATION ON MASTER CAUTION RECALL. ACFT GROUNDED. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST RESET, NO FAULTS FOUND IAW AMM 21-61-00-700-806-002.SDR ASAA2016111418685Warning Message · false activationWHILE ACCOMPLISHING TASK CARD 78273000, FOUND ENGINE FAULT CODE 75-20441 'THE VBV POSITION SIGNAL IS OUT OF RANGE' ON THE NR 1 ENGINE, THIS IS A LONG TERM FAULT. ACFT GROUNDED. NO FAULTS FOUND IN RECENT FAULTS OR FAULT HISTORY.SDR ASAA2016111118617Autopilot Sys · malfunctionedDESCENDING THROUGH FL245, AUTOPILOT DISENGAGED. A/C REMAINED LNAV/VNAV PATH AND I WAS ABLE TO RE-ENGAGE SUCCESSFULLY. GROUNDED - YES. BITE CHK DFCS, NO CURRENT FAULTS, OPS NORMAL, IAW FIM 22-11 TSK 801. PERFORMED B737-800 FIM 22-11 TASK 801 CURRENT STATUS TESTSDR ASAA2016111018628Sensor · faultedON ROTATION A/T KICKED OFF, FLIGHT DIRECTOR WENT AWAY MOMENTARILY, GOT EVERYTHING BACK AT APROX 15000. ON CAPT MFD LOST SPEED TAPE AIRPLANE CAME OUT OF LNAV VNAV. SYSTEM CAME BACK WE WERE ABLE TO SELECT LNAV VNAV AT APROX 24000 FT. AIRPLANE DROPPED INTO CONTROSDR ASAA2016110718636Eec · faultedFOUND NR 1 ENGINE FAULT, SHORT TIME, MESSAGE 75-30601. THE TBV POSITION SIGNALS DISAGREE. ACFT GROUNDED. ACCOMPLISHED FIM 75-23 TASK 803. FOUND EEC FAULT. PERFORMED FIM 75-23 TASK 802, REMOVED AND REPLACED EEC IAW AMM 73-21-60. OPS CHECKED NORMAL. ACCOMPLISHSDR ASAA2016103018518Satcom · lockedSATCOM LOCKUP. GROUNDED, YES. ACCOMPLISHED SATCOM RESET PROCEDURE PER QRH. SATCOM OPS RESTORED NORMAL..SDR ASAA2016101818392Autothrottle Sys · malfunctionedAUTOTHROTTLE DISENGAGED, WOULD NOT RE-ENGAGE. ACFT GROUNDED. PERFORMED AUTOTHROTTLE BITE/CURRENT STATUS CHECK AND FOUND NO CURRENT FAULTS. UNDER INFLIGHT FAULTS FOUND VARIOUS OCCURRENCES OF FAULT 22-31502 NO ASM DATA FOR ASM 2 ON FLIGHT LEG 17. PERFORMED FIMSDR ASAA2016101818396Battery Pack · dischargedEMERGENCY LIGHT BATTERY PACKS REQUIRE CHARGE. ACFT GROUNDED. CHARGED EMERGENCY LIGHT BATTERY PACKS FOR 90 MINUTES, IAW AMM 33-51-06.
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