N570AS
Service difficulty reports · 547
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 = 'N570AS' 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 = 'N570AS' 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 ASAA2020022643273Anti-Ice Valve · inoperativeON TAXI OUT FOUND WING ANTI-ICE CB POPPED IT WORK IN ON PREFLIGHT REST & RT WING ANTI-ICE LT ILLUMINATED. GROUNDED - YES. VERIFIED RT WING ANTI ICE VALVE INOP AFTER RESETTING CB. REMOVED AND REPLACED ANTI-ICE VALVE RT WING REF B737-800 AMM 30-11-11 LEAK CHECK SDR ASAA2020010631784Unknown · malfunctionedBOTH NAV DISPLAY SHOW PHANTOM RADAR RETURNS AT THE 10:00 AND 02:00 O'CLOCK POSITION. THE PHANTOM DISPLAYS INCREASE IN SIZE AS THE MILEAGE SCALE IS REDUCED. THE PHANTOM DISPLAY SHOWS UP BOTH IN THE AUTO AND MANUAL MODE. THE PHANTOM DISPLAYS FADE AWAY IN THE MANSDR ASAA2020010331759Radar · malfunctionedRADAR DISPLAY ACCURATELY SHOWS RETURNS - NO FAILURES NOTED. RADAR DISPLAY ALSO SHOWS TWO "PHANTOM RETURNS" AT APPROXIMATELY 10:00 AND 2:00 O'CLOCK POSITION IN BOTH "AUTO" AND OUT OF AUTO MODE. THE TWO PHANTOM RETURNS SHOW UP ON MULTIPLE RANGE SELECTIONS. OTHERSDR ASAA2019122423689Warning Light · false activationRIGHT PACK LIGHT ON MASTER RECALL RESET EXTINGUISHES LIGHT. GROUNDED - YES. PERFORMED PACK TEMP CONTROL BITE FIM 21-62- TASK 801. CHECKED MASTER CAUTION RECALL AND NO PACK LIGHT ILLUMINATED. NO FAULTS NOTED.SDR ASAA2019122423688Sensor · dirtyCONT CAB ZONE TEMP LIGHT MASTER CAUTION RECALL LIGHT EXTINGUISHED WHEN RESET. GROUNDED - YES. CLEANED CAB ZONE FILTER AND RECHECKED MASTER CAUTION RECALL, NO CAB ZONE TEMP LIGHT NOTED. PACK TEMP CONTROL BITE FIM 21-62 TASK 801 AND NO FAULTS NOTED.SDR ASAA2019122081661Start Valve · inoperativeAFTER THE #2 ENGINE WAS STARTED AND STABLE THE "START VALVE OPEN" "OIL FILTER BYPASS" AND "LOW OIL PRESSURE" AMBER INDICATIONS FLASHED, ENGINE WAS SHUT DOWN , "START VALVE OPEN" REMAINED ILLUMINATED PERFORMED ALTERNATE DEACTIVATION PROCEDURES. GROUNDED - YES. SDR ASAA2019122081660Pin · shearedL1 DOOR DIFFICULT TO OPEN, FOUND GUIDE ARM PIN SCREW SHEARED OFF. GROUNDED - YES. REMOVE & REPLACE UPPER RADIUS LINK PIN , KEYWASHER & SCREW REF B737-800 AMM 52-11-21-000-802 & 52-11-21-400-802 L1 DOOR.SDR ASAA2019121641604Warning Light · false activationON PREFLIGHT, FOUND ELEC LIGHT ILLUMINATED. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 24-31 TASK 801 INTERMITTENT BATTERY CHARGER FAULT. FAULT CLEARED.SDR ASAA2019121103568Blade · wornREF T/C #78472010 CFM56-7 FAN BLADE LUBRICATION. #2 ENG FOUND 2 BLADES #7 AND #20 HAVE MISSING CU-NI-IN COATING BEYOND LIMITS OF AREA X ON CONCAVE T/E SIDE. GROUNDED - YES. REPLACED 2 PAIRS OF BLADES #7/#19 AND #8/ #20 ON ENG #2 PER T/C 78472010.SDR ASAA2019121301587Safety Wire · brokenLEFT HAND PACK RAM AIR ACTUATOR IS HOWLING. GROUNDED - YES. FOUND LEFT RAM AIR ACTUATOR ROD END JAMNUT SAFETY WIRE BROKEN AND JAMNUT CONTACTING ACTUATOR BODY. ADJUSTED RAM AIR ACTUATOR REF B737-800 AMM 21-51-21 OP CK GOOD.SDR ASAA2019112101391Fmc · failedFO'S FMC FAILED IN FLIGHT. GROUNDED - YES. ACCOMPLISHED FMC OP TEST PER B737-800 AMM 34-61-00. NO FAULTS NOTED. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2019100763928Director · malfunctionedAT CRUISE ALTITUDE 350 FOR APPROX 10 MIN BOTH FLIGHT DIRECTOR DISPLAYS DISAPPEARED, A AUTOPILOT DISENGAGED, BOTH HEADING BUS DISPLAYS & SPEED BUG DISPLAYS ON DU'S LOCKED UP. RAN MCP LOCK UP CHECKLIST INCLUDING CIRCUIT BREAKER RESET -NO EFFECT. AFTER APPROX 15 SDR ASAA2019092630839Unknown · malfunctionedRADAR SHOWS GHOST RETURNS AT 70 DEGREES LEFT AND RIGHT OF CENTERLINE AT ABOUT THE 4 TO 6 NM RANGE. GHOST RETURNS APPEAR IN BOTH WX & WX+T MODES, IN AUTO AND MANUAL TILT, SHOWS ON BOTH CAPT AND F/O SIDE. GROUNDED - YES. REMOVED & REPLACED (WXR) WEATHER RADAR R/SDR ASAA2019082620473Autopilot Sys · malfunctionedON CLIMBOUT THRU FLT LVL190 AUTOPILOT A DISENGAGED & WOULD NO IMMEDIATELY RE ENGAGE. LNAV + VNAV MCP LIGHTS ALSO EXTINGUISHED AND WOULD NOT DIM. REENGAGE FLT DIRECTOR BARS BOTH SIDES WENT AWAY. RECYCLED FLT DIRECTOR FEW TIMES. EVENTUALLY LNAV, VNAV, FLT DIRECTSDR ASAA2019081530420Bolt · missingBOLT MISSING FROM #1 ENG AFT EXHAUST FLANGE AND IS LAYING INSIDE THE EXHAUST CONE. GROUNDED - YES. INSPECTED AREA AND NO OTHER DEFECTS NOTED REMOVED BOLT. INSTALLED NEW BOLT IN #1 AFT EXHAUST FLANGE AND RE-TORQUED ALONG WITH ALL REMAINING BOLTS. REF AMM 72-56-SDR ASAA2019081263368Warning Light · illuminatedDURING APU START FAULT LIGHT ILLUMINATED. ONE REATTEMPT AND FAULT LIGHT ILLUMINATED AGAIN. GROUNDED - YES. ON DEFERRAL.SDR ASAA2019072330167Filter · seizedREF L/P 11951092 MCD & SCAVENGE OIL FILTER INSPECTION - WHILE REMOVING SCAVENGE FILTER BOWL ON #2 ENGINE, THE FILTER BOWL SEIZED AND COULD NOT BE REMOVED. GROUNDED - YES. REMOVED AND REPLACED SCAVENGE OIL FILTER ASSY REF AMM 79-21-04. ACCOMPLISHED POWERPLANT TSDR ASAA2019071530078Transceiver · intermittentWHEN #1 HF RADIO SELECTED FAIL APPEARS IN BOTH THE ACTIVE AND STANDBY RADIO TUNING PANEL DISPLAYS. GROUNDED - YES. INITIAL EVAL OPS NORMAL, WITH HF1 SELECTED NO FAIL INDICATIONS, BITE TEST PASS. DUE TO PREVIOUS HISTORY REPLACED HF1 TRANSCEIVER AMM 23-11-21, INSDR ASAA2019070629936Unknown · malfunctionedUPON CHECKING IN WIN KZAK RTU DISPLAYS "FAIL" FOR HF RADIO. GROUNDED - YES. ACCOMP HF TRANSCEIVER BITE TEST OF #1 TEST PASS REF AMM 21-11-00-740-003 ACCOMP HF COMMUNICATION TEST HF #1, TEST PASS REF AMM 23-11-00-730-001 ALSO ACCOMP. ACCOMP TEST, TEST PASS. REFSDR ASAA2019070529952Nut Plate · damagedDURING FAN LUBE ON #1 ENG, IT WAS FOUND THAT AFT SPINNER CONE HAS A BAD NUT-PLATE. GROUNDED - YES. REMOVED AND REPLACED #1 ENG AFT SPINNER CONE AND SWAPPED ALL 36 BALANCE SCREWS IAW AMM 71-00-00-750-802-F00, 14.F.(12)(C)1). ALL BALANCE SCREWS ARE P07 OR P14. ASDR ASAA2019062759825Hf Comm · unknownHF #1 AT CRUISE. NO TX OR RCV. GROUNDED - YES. COULD NOT DUPLICATE DEFECT. #1 HF OPS NRML REF B737-800 AMM 23-11-00. XMIT & RECV OPS NRML, NO "FAIL" (W/ SFO ARINC).SDR ASAA2019062539806Autopilot Sys · malfunctionedCAPTAIN SIDE AUTOPILOT AUTO-DISENGAGED AT FL 370. WOULD NOT REENGAGE. ALSO LOST LEFT FLIGHT DIRECTOR. CAPTAIN SIDE HEADING BUG STAYED FROZEN ON LAST SELECTED HEADING. ALL CIRCUIT BREAKERS IN. RT (FO) SIDE AUTOPILOT FD AND DISPLAY ALL FUNCTION NORMALLY. AFTER ASDR ASAA2019062029804Nozzle · damaged#2 ENGINE: WHILE ACCOMPLISHING T/C 78472020, FOUND 1 HPT NOZZLE SEGMENT TO HAVE A .010" BURN THROUGH HOLE. SEGMENT IS DIRECTLY BEHIND BORO PORT S-15. THIS CONDITION IS PERMITTED PER ABOVE TASK CARD REF STEP 3.B. (6) (B)2), BUT, REQUIRES A REDUCED INTERVAL REINSDR ASAA2019062199776Warning Light · false activationFLIGHT CREW REPORTED ELECT LIGHT ILLUMINATED. GROUNDED - YES. PERFORMED FIM 24-31 TASK 801. FAULT LIGHT DIMINISHED, NO OTHER FAULTS NOTED AT THIS TIME.SDR ASAA2019061129663Display · malfunctionedVTK FLAG APPEARED ON FO'S MFD AND DISAPPEARED 30 SECONDS LATER. DURING THAT TIME WE LOST LNAV/VNAV CAPABILITY AND THE AUTOPILOT REVERTED TO CWS. AFTER 30 SECONDS AND WHEN VTK/FLAG DISAPPEARED WE WERE ABLE TO REENGAGE FO'S AUTOPILOT ALONG WITH VNAV/LNAV. GROUNDSDR ASAA201906129676Wire Harness · damagedFOUND #1 ENG LONG TIME FAULT 73-10811 THE T12 SIGNAL IS OUT OF RANGE. GROUNDED - YES. EEC TEST SHOWS FAULT MESSAGE 73-10811. REF B737-800 AMM 73-21-05-200-801-F00, FOUND T12 SENSOR J7 HARNESS CONNECTOR HAD FALLEN OFF OF J7 RECEPTACLE. THREADS ON RECEPTACLE ENDSDR ASAA2019052029404Indicator · inoperativeFUELER REPORTS #2 REFUEL QUANTITY INDICATOR INOP. GROUNDED - YES. REMOVED, REPLACED AND TESTED #2 REFUEL QUANTITY INDICATOR REF AMM 28-41-61. OPS NORMAL.SDR ASAA2019051229288Unknown · malfunctionedFORWARD CABIN HEAT DOES NOT FUNCTION PROPERLY. THE FORWARD CABIN REMAINS COLD AT 20C, WITH THE FORWARD SUPPLY DUCT TEMPERATURE AT 20C. AS THE FORWARD TEMPERATURE CONTROL KNOB IS ROTATED VERY GRADUALLY CLOCKWISE, THERE IS NO RESPONSE IN THE FORWARD SUPPLY DUCT SDR ASAA2019050129217Unknown · malfunctionedCA FLIGHT DIRECTOR BARS INOP. GROUNDED - YES. ACCOMPLISHED AMM 22-00-01-730-807. ALL TEST PASS NO OTHER RELATED FAULTS.SDR ASAA201904128962Lens · detachedEMERGENCY EXIT SIGN AT OVERWING EXIT FELL OFF. GROUNDED - YES. REATTACHED EMERGENCY EXIT LENS COVER REF B737-800 AMM TASK 33-51-01, OK.SDR ASAA2019041072891Controller · malfunctionedPRIMARY CONT CABIN ZONE TEMP LIGHT ON. GROUNDED - YES. CONT CABIN ZONE TEMP LIGHT ACTIVE ON RECALL, #2 PACK ZONE TEMP CONTROLLER SHOWS FLT DECK TRIM VALVE FOR PREVIOUS FLT, GREEN FOR VERIFY. RESET CONTROLLER, RAN PACKS, PZTC BITE SHOWS 3 GREEN BOTH CONTROLLERSSDR ASAA201904028849Control Panel · inoperativeCAPTAINS COURSE SELECTOR IS INOP ALL MODES. GROUNDED - YES. REMOVED & REPLACED MCP. OP CK NORMAL. REF B737-800 AMM 22-11-34-000-801 & 22-11-34-400-801. BITE GROUPS 32, 49 & 70.SDR ASAA201904028850Warning Message · false activationDURING FLIGHT FOUND DC BUSS INDICATION - SW HOT BAT CIRCUIT BREAKER POPPED. GROUNDED - YES. INSPECTED BEHIND C/B PANEL - NO DEFECTS NOTED. RESET C/B PERFORMED DC SYSTEM OPS TEST REF B737-800 AMM 24-31-00 OPS CHECK NORMAL.SDR ASAA2019040198818Controller · malfunctionedFWD CABIN CONTROLLER NOT CONTROLLING TEMPERATURE. CONTROLLER DOES NOT RESPOND TO KNOB MOVEMENTS UNTIL A POINT THEN DUCT TEMP GOES FROM 18 DEGREES TO 60-70 DEGREES, WITH LITTLE RESPONSE BETWEEN THAT RANGE. GROUNDED - YES. RESET SYSTEM, RAN BOTH PACKS, TEMPERATUSDR ASAA2019032428772Control Panel · malfunctionedMCP HEADING DISPLAY WINDOW IS CORRUPTED. GROUNDED - YES. REMOVED AND REPLACED MCP REF AMM 22-11-34. MODE CONTROL PANEL INSTALLATION TEST PASSED REF AMM 22-11-34-740-801.SDR ASAA2019031828664Filter · cloggedFWD CABIN CONTROL RHEOSTAT NOT WORKING PROPERLY. VERY LITTLE HEAT IS PRODUCED UNTIL KNOB PASSES 4 O'CLOCK POSITION THEN ONCE HEAT IS INITIATED, IT RUNS TO FULL HOT. GROUNDED - YES. FOUND BOTH CABIN TEMP SENSOR FILTERS CLOGGED. CLEANED BOTH REF AMM 21-61-06. ADSDR ASAA2019030528498Selector · faultedFWD CAB ZONE TEMP LIGHT ILLUMINATED ON RECALL. THE LIGHT EXTINGUISHES WITH MASTER CAUTION RESET. GROUNDED - YES. ACCOMPLISHED PZTC BITE. NR 1 CONTROLLER SHOWED " BACKUP ZONE SELECTOR" FAULT. DUE TO HISTORY, REMOVED, REPLACED, AND TESTED FWD ZONE SELECTOR IAW MSDR ASAA2019022728386Battery Pack · defectiveM1676 RT FWD BULL NOSE AND RT FWD OVERWING LIGHTS WILL NOT CHARGE GROUNDED - YES. REPLACED BATTERY PACK AND OPS CKD GOOD.SDR ASAA2019022628385Battery Pack · defectiveFWD OVERWING AND OUTSIDE OVERWING BATTERY PACK WOULD NOT CHARGE. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK. OPS GOODSDR ASAA2019021428408Bulkhead · crackedACCESS AND OVER SIZE BS 540 BULKHEAD LOWER CHORD FASTENER HOLE LT SIDE SHOWING CRACK INDICATION. GROUNDED - YES. REPAIRED BS540 LT LOWER CHORD IAW EA 800-53EA-21262.SDR ASAA2019021128252Floorbeam · corrodedAFT WET AREA STA 947.5 HAS AREA OF CORR AT LBL 53. GROUNDED - YES. REPAIRED FLOORBEAM UPPER FLANGE IAW SRM 53 70 51 2R 5 W 1" O .180 R .138 L 1" D .042".SDR ASAA2019020828388Intercostal · corrodedFWD WET AREA BS270 HAS AREAS OF CORROSION LBL 12 TO RBL 12. GROUNDED - YES. REMOVED CORR FROM FWD WET AREA BS 270 BETWEEN LBL 12 AND RBL 12, FOUND TO BE OUT OF LIMITS IAW SRM 53 10 51 1A 1 REPAIRED BS 270 BETWEEN LBL 12 AND RBL 12 IAW EA 800 53EA 21263 W 1 O .SDR ASAA2019020828273Floorbeam · corrodedAFT WET AREA CORR ON STA 986 FLOORBEAM UPPER FLANGE LBL 21 TO RBL 43. GROUNDED - YES. REPAIRED 986 FLOORBEAM IAW SRM 53 70 51 2R 6 W 1" O .150" R .122' L 4" D .028".SDR ASAA2019020828272Floorbeam · corrodedAFT WET AREA STA 947.5 FLOORBEAM UPPER FLANGE HAS AREAS OF CORR AT APPROX LBL5. GROUNDED - YES. REPAIRED FLOORBEAM AND INSTALLED ALL REPAIR PARTS ON UPPER FLANGE IAW SRM 53 70 51 2R 6 W 2" O .180" R .154" L 1" D .026".SDR ASAA2019020828271Pressure Panel · crackedUPON NDT INSPECTION FOUND CRACK IN O/B BAY OF LT PRESSURE WEB. GROUNDED - YES. REPAIRED LT PRESSURE WEB IAW SRM 51 10 10 2R 3 REPAIR 3 ALTERNATIVE 2.SDR ASAA2019020828182Intercostal · crackedFWD WET AREA FORMED INTERCOSTAL STA 312 TO 328 LBL 45.5 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED DAMAGED INTERCOSTAL AT FWD WET AREA STA 312 TO 328 LBL 45.5 IAW SRM 51 40 02 0G 0.SDR ASAA2019020828180Pressure Panel · crackedUPON NDT INSPECTION FOUND CRACK IN O/B BAY OF RT PRESSURE WEB. GROUNDED - YES. REPAIRED RT PRESSURE WEB IAW SRM 57 10 10 2R 3 REPAIR 3 ALTERNATIVE 2.SDR ASAA2019020628270Door Sill · corrodedFWD CARGO DOORWAY LOWER SILL WEB IS CORRODED. GROUNDED - YES. REMOVED CORR ON FWD CARGO DOORWAY LOWER SILL WEB FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED SILL WEB IAW SRM 53 30 15 1A 1 FIG 103, 51 40 02 0G 0 W 2 O .080 R 63 L 4 D .017.SDR ASAA2019022538291Angle · crackedFWD PIT STA 500H L/H FWD BAFFLE CLIP CRACKED. GROUNDED - YES. REMOVED AND REPLACED FWD PIT STA 500 L/H FWD BAFFLE CLIP IAW B737 800 SRM 51 40 02 0G 0.SDR ASAA2019020328179Fitting · crackedFWD PIT STA 500H RT AFT BAFFLE CLIP CRACKED. GROUNDED - YES. REMOVED AND REPLACED FWD PIT STA 500H RT AFT BAFFLE CLIP IAW SRM 51 40 02 0G 0.
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