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.

SDR ASAA2015021910729Start Valve · malfunctionedON WALK AROUND, NOTED LOUD RUSH OF AIR FROM NR 1 ENGINE LT SIDE AND OTBD FAN COWL VERY HOT. ACFT GROUNDED. PERFORMED MANUAL WRENCH CHECK ON STARTER VALVE, VERIFIED VALVE NOT FULLY CLOSING. R & R NR 1 ENGINE STARTER VALVE OPS AND LEAK CHECK GOOD REF MM 80-11Feb 19, 2015 · N570AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2015020310540Fault Code · activatedNR 1 ENGINE HAS MAINTENANCE MESSAGE FAULT 76-31361. THE START LEVER SIGNALS DISAGREE, LONG TERM FAULT. ACFT GROUNDED. OPENFeb 3, 2015 · N570AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2015012810461Control Panel · failedUNABLE TO DISCONNECT AUTOTHROTTLES FROM THRUST LEVERS. HAD TO DISCONNECT AUTOTHROTTLES WITH SWITCH ON MODE CONTROL PANEL. ACFT GROUNDED. REPLACED MODE CONTROL PANEL IAW MM 22-11-34. SYS OPS CHECKED GOOD IAW MM 22-11-34/501 AND HOUSING SENSOR TEST IAW MM 3Jan 28, 2015 · N570AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2015011410266Probe · dirtyNR 1 ENGINE EEC BITE SHOWS FAULT 77-10841, THE TOP RT EGT SIGNAL IS OUT OF RANGE. LOGGED FOR 4 OUT OF 10 LEGS. FAULT 77-10841 IS AN ECONOMIC LEVEL FAULT. ACFT GROUNDED. ACCOMPLISHED T/S FOR FAULT 77-10841 IAW FIM 77-21, TASK 801. EEC TEST IAW MM 73-21-00-Jan 14, 2015 · N570AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2014100609313Servo · leakingLEAK CHECK AFTER HMU CHANGE FOUND FUEL HEATER SERVO LEAKING FROM AROUND CAP, EVIDENCE SHOWS IT HAS BEEN LEAKING FOR AWHILE. CLASSIFIED AS CONTINUOUS. ACFT GROUNDED. REMOVED SERVO HEATER IAW MM 73-11-07-000-801-F00. INSTALLED SERVO FUEL HEATER IAW MM 73-11-0Oct 6, 2014 · N570AS · Boeing 737890 · Engine Fuel DistributionSDR ASAA2014100609298Hmu · warning lightNR 1 ENGINE VALVE CLOSED LIGHT IS ILLUMINATED, CLOSED. ACFT GROUNDED. REPLACED THE HMU IAW T/C'S N8473000 & N8473001. OPS & LK CK'S GOOD. OK FOR CONTINUED SERVICE.Oct 6, 2014 · N570AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2014100509304Indicator · failedCABIN TEMP GAUGE LIGHT BURNED OUT. ACFT GROUNDED. R & R CABIN TEMP INDICATOR IAW AMM TASK 21-61-32-000/400-801. OPS NORMAL INCLUDING INTEGRAL LIGHTING.Oct 5, 2014 · N570AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014092709230Warning Light · false activationON RECALL, A MASTER CAUTION AIR CONDITIONING WITH A PACK LIGHT ON LT SIDE PACK LIGHT DISAPPEARS ON RESET. ACFT GROUNDED. PERFORMED ZONE/TEMP CONTINUE BITE CHECK IAW MM 21-61-00. NR 1 CHECKED GOOD. NR 2 BITE SHOWED TCV. PREVIOUS FLT SHOWED TCV VERIFY PASSESep 27, 2014 · N570AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014092209203Switch · failedAFTER ENGINE SHUTDOWN NR1 ENGINE, ENG VALVE CLOSED LIGHT, STAYED BRIGHT BLUE. ACFT GROUNDED. R & R HPSOV SWITCH IAW AMM 73-21-09-000/400-801-F00. OPS NORMAL. 71-00-00-800-811-F00, TESTED GOOD.Sep 22, 2014 · N570AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2014092009182Connector · dirtyDIAGNOSTICS REPORTED NR 2 ENGINE TREND DATA SHOWS A SHIFT IN DELTA CRUISE AND TAKEOFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. ACFT GROUNDED. ACCOMPLISHED T49.5 + EGT SYSTEM INSPECTION IAW AMM 77-21-01. FOUND SLIGHT CONTAMINATION AT J10 CONNECTOR OF EEC,Sep 20, 2014 · N570AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA2014083009001Actuator · faultedNR 1 ENGINE FUEL SHUTOFF VALVE LIGHT ILLUMINATED BRIGHT BLUE. ACFT GROUNDED. ACCOMPLISHED FIM TASK 28-22, TASK 809. FAULT IS DETERMINED TO BE INTERMITTENT. REPLACED NR 1 ENGINE SPAR VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECKED NORMAL.Aug 30, 2014 · N570AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2014081908895Eec · malfunctionedNR 2 EEC WILL NOT ACCEPT EEC SOFTWARE UPGRADE 7BW. ACFT GROUNDED. REPLACED NR 2 EEC IAW AMM 73-12-60-000-801-F00 AND AMM 73-21-60-400-801-F00, OPS CHECK GOOD IAW AMM 73-21-00-840-801-F00, AMM 73-21-00-700-804-F00, 73-21-00-700-808-F00, AMM 71-00-00-700-807-FAug 19, 2014 · N570AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2014081508857Warning Message · activatedNR 1 ENGINE LOGGED FAULT 77-20871 ECONOMIC FAULT. ACFT GROUNDED. ACCOMPLISHED 50-HR, ONE TIME ACCOMPLISHMENT OF TASK CARD 78273000 FOR NR 1 ENGINE, NO CURRENT FAULTS & NO FAULT HISTORY LAST 11 FLIGHT LEGS.Aug 15, 2014 · N570AS · Boeing 737890 · Engine Indicating SystemSDR ASAA2014081308848Circuit Breaker · trippedDURING TAXI OUT, A LEFT CENTER TANK FUEL BOOST PUMP LIGHT ILLUMINATED WITH THE SWITCH ON. CENTER TANK FUEL WAS 2.11 LBS. ACFT GROUNDED. FOUND THE LT CENTER BOOST PUMP CIRCUIT BREAKER OPEN. REST CIRCUIT BREAKER IAW AMM 20-60-01-860-801 AND COMPLIED WITH FIMAug 13, 2014 · N570AS · Boeing 737890 · Fuel Boost PumpSDR ASAA2014071408555Battery · false indicationTHE P5-13 ELECTRIC PANEL SHOWING A HIGH AMP DRAW IN BATTERY & AUX BATTERY POSITION. ACFT GROUNDED. AMP INDICATION RETURNED TO NORMAL AFTER AN HOUR, PERFORMED BATTERY INSTALLATION TEST REF 24-31-11-400-802. OPS CHECED NORMAL.Jul 14, 2014 · N570AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2014070708477Warning Message · false activationFMC DISAGREE ANNUNCIATED. ACFT GROUNDED. RAN CHECK LIST RESET SUCCESSFUL.Jul 7, 2014 · N570AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014070108410Controller · failedRIGHT PACK LIGHT ILLUMIATED DURING RECALL & EXTINGUISHED. ACFT GROUNDED. R & R RIGHT PACK TEMP CONTROLLER AMM 21-61-20. OPS CHECKED NORMAL.Jul 1, 2014 · N570AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014062608364Warning Light · illuminatedRT PACK LIGHT ILLUMINATED UPON RECALL LIGHT OUT AFTER M/C RESET. ACFT GROUNDED. OPENJun 26, 2014 · N570AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014061908325Regulator · malfunctionedABNORMAL DUCT PRESSURE SPLIT DURING CLIMB, DELTA PSIG LESS THAN/EQUAL TO 20PSI, FL 280, LT PAC 30, PSI-R PAC 48, PSI. N1 98.9 CLIMB. FL 300, LT PAC 30, PSI-RT PAC 39 PSI-WENT TO 50 PSI THEN TO 48 PSI IN 10 SECONDS N1 99.7. FL 330, LT PAC 29 PSI-RT PAC 49, PSJun 19, 2014 · N570AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2014061608231Control Panel · failedHEADING SELECT BUG WILL NOT MOVE WHEN HEADING SELECT KNOB IS TURNED. ACFT GROUNDED. REPLACED MODE CONTROL PANEL IAW AMM 22-11-34-00-801 AND 22-11-34-400-801. ACCOMPLISHED MCP INSTALLATION TEST IAW AMM 22-11-34-740-801. ALL TESTS PASSED.Jun 16, 2014 · N570AS · Boeing 737890 · Autopilot SystemSDR ASAA2014051107769Apu · malfunctionedAPU WILL NOT START. ACFT GROUNDED. ACCOMPLISHED FIM TASK 49-40, TASK 803. STARTED APU SEVERAL TIMES WITH NO CURRENT 49-41012 FAULT. FAULT CORRECTED IAW FIM. CHECKED MAGNETIC DRAIN PLUG. NO DEBRIS NOTED. NO HISTORY ON CURRENT APU.May 11, 2014 · N570AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2014042507581Shim · wornNR 1 ENGINE FAN BLADE SHIMS 24 EA MOLYDAY COATING WORN AND BLADE PLATFORMS 24EA. HAVE TORN SEALS. ACFT GROUNDED. R & R 1 ENG FAN BLADE SHIMS, 24EA AND BLADE PLATFORMS, 24EA IAW T/C 78472002.Apr 25, 2014 · N570AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2014041807511Warning Message · false activationRT FMC NOT PROVIDING POSITION INFO IN FLIGHT. FMC-FMC VERIFY MESSAGE. ACFT GROUNDED. PERFORMED FMC SYS BITE IAW FIM 34-61, TASK 801. NO FAULTS FOUND. GROUND TEST PASSED. NO HISTORY 30 DAYS.Apr 18, 2014 · N570AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014030307061Lamp · failedEMERGENCY LIGHT HANDLE FLOODLIGHT AFT LAMP INOPERATIVE AT LT FORWARD OVERWING EXIT. ACFT GROUNDED. REPLACED LAMPS AND TESTED IAW MM 33-51-01-960-801. OPS NORMAL.Mar 3, 2014 · N570AS · Boeing 737890 · Emergency LightingSDR ASAA2014021006820Hf Comm · abnormalNR 1 HF RADIO GARBLED AND UNREADABLE DURING RECEPTION, TRANSMIT FUNCTION WORKS AND IS RECEIVED BY RADIO AS LOUD AND CLEAR. ACFT GROUNDED. PERFORMED HF NR 1 OPS CHECK IAW MM 23-11-00-710-801. PASSED, NO DEFECT NOTED. CREW REPORTED WORKED FINE IN FLIGHT. NO HIFeb 10, 2014 · N570AS · Boeing 737890 · HF Communications SystemSDR ASAA2014020506785Apu · unknownAPU CT5ATP ABOVE THRESHOLD. ACFT GROUNDED.Feb 5, 2014 · N570AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2013122512235Warning Message · false activationON GROUND, FMC SINGLE OPS MESSAGE. ACFT GROUNDED. RAN CHECKLIST IAW QRH, DUAL FMC OPS RESTORED.Dec 25, 2013 · N570AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013120896684Warning Message · false activationDURING TAXI, FMC DISAGREE ILLUMINATED ON SCRATCH PADS. ACFT GROUNDED. PERFORMED THE FMC DISAGREE QRH PROCEDURE, ESTABLISHED NORMAL FMC OPERATIONS.Dec 8, 2013 · N570AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013120896683Fmc · malfunctionedDURING CRUISE FLIGHT, SINGLE FMC OPERATION ANNUNCIATED ON SCRATCH PAD, FOLLOWED BY AMBER MAP FLAG ON F/O NAV DISPLAY. QRH FOLLOWED. NORMAL OPERATIONS RESTORED. ACFT GROUNDED. PERFORMED BITE TASK 34-61, TASK 801, TEST OK. AS PRECAUTIONARY R & R RT FMC. CRDec 8, 2013 · N570AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013120696646Actuator · faultedLEFT PACK LIGHT ON MASTER CAUTION RECALL LIGHT EXTINGUISHED ON MASTER CAUTION RESET. COMPLIED WITH QRH. ACFT GROUNDED. PERFORMED LT PACK/ZONE TEMP CONTROL BITE TEST, FOUND RAM AIR INLET ACTUATOR FAULT. REPLACED LT RAM AIR INLET ACTUATOR REF AMM 21-51-21. OPDec 6, 2013 · N570AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013120496601Control Valve · warning lightDURING FINAL APPROACH, LEFT PACK LIGHT ILLUMINATED. RESETS WITH MASTER CAUTION. ACFT GROUNDED. ACCOMPLISHED INTERROGATION OF BOTH LT & RT ZONE TEMP CONTROLLERS. LT ZONE TEMP CONTROLLER FAULTED TEMP CONTROL VALVE REF AMM 21-61-00. REMOVED TEMP CONTROL VALVDec 4, 2013 · N570AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013112596546Warning Light · illuminatedAMBER ZONE TEMP LIGHT ILLUMINATED AFTER START. FOLLOWED QRH, LIGHT EXTINGUISHED. LIGHT CAME BACK ON AT RECALL ON LANDING. AIRCRAFT GROUNDED. PERFORMED BITE CHECK OF PACK/ZONE TEMP CONTROLLERS 1 & 2 REF AMM 21-61-00. FLT DECK TRIM VALVE DISPLAYED ON NR 2 RENov 25, 2013 · N570AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013112596529Controller · false indicationPRESSURIZATION AUTOFAIL. ACFT GROUNDED. FOUND TWO FAULTS ON NR 2 PRESSURIZATION CONTROLLER. CONTROL PANEL FAULT AND SYSTEM WIRING. SUSPECTED FAULT INDUCED BY POWER TRANSFER. CYCLED NR 2 CONTROLLER POWER, NR 2 AUTO PRESSURIZATION. OPS NORMAL REF FIM 21-31Nov 25, 2013 · N570AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2013112296491Controller · faultedON RECALL, LEFT PACK LIGHT ILLUMINATED, EXTINGUISHES WHEN RECALL PRESSED AGAIN. ACFT GROUNDED. ACCOMPLISHED PACK-ZONE TEMP CONTROLLER BITE IAW MM 21-61-00-700-806-002. PREVIOUS FAULT LOGGED FOR LT RAM INLET ACTUATOR. RESET FAULT, OPS CHECKED GOOD, FAULT DOENov 22, 2013 · N570AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013092896075Controller · failedPRESSURIZATION MODE CONTROLLER LANDING ALT LCD HAS 1 DIGIT NOT FULLY ILLUMINATED. GROUNDED. REPLACED CABIN PRESSURE SELECTOR MODULE IAW MM 21-31-02. OPS CHECK GOOD.Sep 28, 2013 · N570AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA2013080495734Actuator · malfunctionedLEFT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. REPLACED LT RAM AIR INLET ACTUATOR IAW AMM 21-51-21. BITE TEST PASSED IAW AMM 21-61-00.Aug 4, 2013 · N570AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013073195711Control Valve · failedLEFT PACK LIGHT COMES ON WITH RECALL. EXTINGUISHES WITH RESET. ACFT GROUNDED. ACCOMPLISHED TASK 21-61-00-700-806-002 PACK/ ZONE TEMP CONTROLLER. BITE TEST ON NR 1 CONTROLLER LOGGED MULTIPLE FAULTS ON MULTIPLE SYS. SWAPPED NR 1 AND NR 2 CONTROLLERS. FAULTJul 31, 2013 · N570AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013072595679Warning Light · false activationNR 1 PACK LIGHT ILLUMINATED ON PRESS TO TEST. ACFT GROUNDED. PACK LIGHT WAS NOT ACTIVE DURING RECALL. NO FAULTS LOGGED ON EITHER ZONE TEMP BITE REF FIM 21-60 TASK 801.Jul 25, 2013 · N570AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013070695487Lever · malfunctionedCREW REPORTED NR 1 ENG HAS A DELAYED SHUTDOWN AFTER START LEVER IS POSITIONED TO CUTOFF. ACFT GROUNDED. PERFORMED NR 1 ING EEC BITE, IAW FIM TASK 73-00, TASK 801, MAINT MESSAGE 76-31361 LOGGED. LONG TERM FAULT. PERFORMED NORMAL ENG START/ STOP ON NR 1 ENGIJul 6, 2013 · N570AS · Boeing 737890 · Engine Starting SystemSDR ASAA2013070595481Wire · damagedWHILE ACCOMPLISHING TASK CARD 78273000, ENGINE 1 LOGGED LONG TERM FAULT 76-31361. THE START LEVER SIGNAL DISAGREE. ACFT GROUNDED. FOUND GROUND WIRE FROM PIN 15, D11288 TO GD800-DC NOT SEATED IN GROUND BLOCK, RECONNECTED AND TESTS GOOD REF WDM 76-21-11, AND Jul 5, 2013 · N570AS · Boeing 737890 · Engine Control System WiringSDR ASAA2013070395455Diaphragm · failedDUCT PRESSURE SPLIT IN CLIMB EXCEDED 20 PSI -CLIMB/CRUISE. FL 350 N1-101.9, DUCT PRESS L- 28, R-47. FL 390 N1-99.6, DUCT PRESS L-26, R-47. FL 400 N1-99.1, DUCT PRESS L-26, R-47. FL 400 N1-87.6, DUCT PRESS L-30, R-35. ACFT GROUNDED. PERFORMED T/C NG-36WC-000Jul 3, 2013 · N570AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013070395454Shutoff Valve · inoperativeDUCT PRESSURE SPLIT IN CLIMB FL 350 LT 26 PSI, RT 47 PSI. ACFT GROUNDED. R & R NR 1 ENGINE PRSOV IAW AMM 36-11-01. PERFORMED INSTALLATION TEST OK, REF 36-11-04.Jul 3, 2013 · N570AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013070295452Control Valve · inoperativeRT A/C PACK ON /OFF DISCRETE SHOWS ON WITH PACK SWITCH OFF. ACFT GROUNDED. REMOVED RT PACK FLOW CONTROL VALVE. REMOVED ACM REINSTALL NEW FLOW CONTROL AND REINSTALL ACM REF AMM 21-51-01 AND AMM 21-51-04. PERFORMED FLOW CONTROL VALVE INSTALLATION TEST AND ACMJul 2, 2013 · N570AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013070295451Counterweight · failedLT ENGINE VIBRATION AT CRUISE 1.1, N,86.1 LT & RT. ACFT GROUNDED. ACCOMPLISHED TEST 14B FAN TRIM BALANCE NR 1 ENGINE SOULTION POS 13, REMOVE P-14 INSTALLED P09, POS 15, REMOVED P-14 INSTALLED P09, POS 21. REMOVED P-08, INSTALLED P-14, POS 28. REMOVED P08 INJul 2, 2013 · N570AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2013061495153Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED BS 312 - BS 328, RBL 31. R & R FLOOR SUPPORT.Jun 14, 2013 · N570AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013061495151Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED, BS 344 - 360, LBL 12. R & R FLOOR SUPPORT.Jun 14, 2013 · N570AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013061495150Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED BS344 - 360, LBL 0. R & R FLOOR SUPPORT.Jun 14, 2013 · N570AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013061495147Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED, BS 312 - 328, LBL 46. R & R FLOOR SUPPORT.Jun 14, 2013 · N570AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013061395321Seat Track · wornMAIN CABIN SEAT TRACK AT STA .520 RBL 45 FOUND TO BE WORN, OUT OF LIMITS. REPAIRED SEAT TRACK REF SRM 53-00-52-2R-4, REPAIR 4.Jun 13, 2013 · N570AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2013061395320Seat Track · wornMAIN CABIN SEAT TRACK AT STA 520, RBL 24.75 FOUND TO BE WORN, OUT OF LIMITS. REPAIRED SEAT TRACK REF SRM 53-00-52-2R-4, REPAIR 4.Jun 13, 2013 · N570AS · Boeing 737890 · Fuselage, Seat/Cargo Attach Fittings
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