N570AS

Service difficulty reports · 553

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 ASAA0957047Idg · malfunctionedENGINE NR 1 DRIVE LIGHT NOT ILLUMINATED DURING PREFLIGHT LIGHTS TEST AND PRESS TO TEST ARE NORMAL. TROUBLESHOT NR 1 ENG IDG RE-ENGATED IDG. RAN ENG IDG OPS CHECK NORMAL. REF AMM 24 11 00 700 802.Nov 20, 2009 · N570AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0957014Valve · faultedAFTER ENGINE STARTS WHILE PERFORMING AFTER START CHECK LIST ON RECALL ZONE TEMP CONT CAB ILLUMINATED: LIGHT EXTINGUISHED WITH MASTER CAUTION RESET. PERFORMED PROCEDURES AND CALLED MX CONTROL GROUNDED YES. PERFORMED BITE CHECK VERIFIED FAULT ON ZONE TEMP CONTNov 14, 2009 · N570AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0956648Unknown · malfunctionedIN DESCENT THRU 14000 WHILE IN VNAV/LNAV DESCENT AUTO WAS DOING NORMAL TRIMMING BUT MAKING A CLICK CLACK NOISE ON EACH ROTATION DISENGAGES TRIM WORKED SMOOTHLY NO NOISE, NORMAL AT 7000 RE-MESSAGE AUTOPILOT IT TRIMMED SMALL AMOUNTS USED BUT SAME CLICK CLACK NOISep 19, 2009 · N570AS · Boeing 737890 · Autopilot SystemSDR ASAA0956429Circuit Breaker · openFOUND RT ENG START VALVE C/B OPEN P6 2 ROW C COL 4. OPENED/CLOSED NR 2 ENG INBOARD FAN COWL FOR GVI NO SYSTEM DEACTIVATED. INSPECTED CIRCUIT WDM 80 11 11 FOR NR 2 ENG START VALVE C/B. FOUND NORMAL RESET NR 2 ENG START VALVE C/B. NO PRIOR WRITE UPS REF MM 2Aug 20, 2009 · N570AS · Boeing 737890 · Engine CrankingSDR ASAA0956428Ignition Sys · malfunctionedNO START ENG NR 1. ACCOMPLISHED ABORT, START QRC. FOUND NR 1 IGNITION LT AND RT OUT. INSPECTED CIRCUIT WDM 74 11 11 FOUND NORMAL, RESET NR 1 ENGINE IGNITION LEFT + RIGHT C/B ON P18 2 A 1 + A 3 REF MM 20 60 01. NR 1 ENG COWL OPENED \ CLOSED FOR GVI NO SYSTEAug 20, 2009 · N570AS · Boeing 737890 · Ignition Power SupplySDR ASAA0956426Unknown · malfunctionedAPU BITE INOP SHOWS ON CDU. RESET APU SYS POWER. MSG CLEAR, NO CURRENT FAULTS, VERIFICATION GOOD REF FIM 49 65 00, NOTIFIED SEAMC.Aug 20, 2009 · N570AS · Boeing 737890 · APU ControlsSDR ASAA0956375Fire Loop · faultyAPU DET INOP LIGHT ILLUMINATED INFLIGHT APU WAS OFF. DUPLICATED DEFECT FIRE DETECTION MODULE FAULTED APU TAILPIPE LOOP REPLACED IAW MM 26 15 01, GROUND VERIFICATION TESTS PASS.Aug 4, 2009 · N570AS · Boeing 737890 · Fire DetectionSDR ASAA0956337Wire Harness · defectiveR2 WINDOW OVERHEAT LIGHT REMAINS ON AFTER COOL DOWN PERIOD. REPLACED R2 SLIDER WINDOW HEAT POWER CORD AS REQUIRED. R2 WINDOW HEAT OPS CHECK NORMAL REF MM 30 41 00.Jul 28, 2009 · N570AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA0956002Eec · faultyFOUND FAULT NR 73 21271, THE ALTERNATOR VOLTAGE INPUT TO EEC IS OUT OF RANGE, ENG NR1, WHILE PERFORMING T/C 78273000 ESN894536 GROUNDED YES. IAW FIM 73 27 TASK 804. REMOVED AND REPLACED NR 1ENG EEC IAW MM 73 21 60, OPS TESTS GOOD.Jun 21, 2009 · N570AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA0954998Paint · missingNR 1 ENG SPINNER CONE PAINT GONE. REMOVED & REPLACED FRONT SPINNER CONE REF MM 72 21 01.Mar 30, 2009 · N570AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA0954969Fmc · malfunctionedFMC DISAGREE LIGHT ON GROUND. PERFORMED FMC DISAGREE CHECK IN QRH. RESET CIRCUIT BREAKERS, OPS NORMAL.Mar 27, 2009 · N570AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0954827Bleed Air Sys · malfunctionedUPON APU START AND SELECTION OF APU BLEED AIR ONLY RECEIVED 2 PSI ON DUCT PRESSURE GAUGE (OUTSIDE AIR TEMP 32 DEG AND SNOWING). ACCOMPLISHED FIM TASK 49 55 00 810 804 INITIAL EVALUATION CHECKED NORMAL. ACCOMPLISHED APU BITE PROCEDURE PER 49 60 TASK 801, NO FMar 15, 2009 · N570AS · Boeing 737890 · APU Bleed Air SystemSDR ASAA0954523Warning System · activatedFMC DISAGREE WARNING ANNUNCIATED. CHECK LIST PERFORMED ON GROUND. C/B P18 2 A6 AND P6 D16 PULLED AND RESET IAW CHECK LIST. CHECK LIST COMPLETE, OPS NORMAL.Feb 24, 2009 · N570AS · Boeing 737890 · Central WarningSDR ASAA0954522Fmc · malfunctionedFMC DISAGREE MESSAGE DURING TAXI OUT AT HNL. ACCOMPLISHED QRH, RESTORE PROCEDURE RESET FMC C/BS, OPS CHECK NORMAL.Feb 24, 2009 · N570AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0954194Battery · dischargedFOUND ACFT GROUND POWER DISCONNECTED. MAIN DC AND AUX DC BATTERIES DRAINED. TR UNIT ANNUNCIATOR ILLUM. ON OVERHEAD PANEL TR3 SHOWS 0 VOLTS. BAT BUS SEC 1 CIRCUIT BREAKER POPPED. 28V DC TR3 DC IND CIRCUIT BREAKER POPPED. GROUNDED YES. R&R AND TESTED MAIN AJan 10, 2009 · N570AS · Boeing 737890 · Battery/Charger SystemSDR ASAA0954193Sensor · dirtyFA S REPORT CABIN TEMP IMBALANCE VERY COLD IN BACK. ROW 6 12 ARE GOOD (OR SLIGHTLY WARM) FORWARD OF ROW 6 IS COOL GROUNDED YES. CLEANED CABIN SENSORS FOR REF AMM 21 61 06 100 801. CABIN TEMP IS NOW EVENLY MAINTAINED. SEAMC NOTIFIED. ETOPS SIGNIFICANT SYS. Jan 8, 2009 · N570AS · Boeing 737890 · Cabin Temperature SensorSDR ASAA0954132Housing · damagedAPU LUBE FILTER HOUSING DAMAGED, GROUNDED, YES. REMOVED AND REPLACED APU LUBE FILTER HOUSING AND LUBE FILTER INDICATOR IAW MM 49-91-13 AND 49-91-12 SEAM, NOTIFIED FOR PARTS VERIFICATION.Jan 3, 2009 · N570AS · Boeing 737890 · APU Oil SystemSDR ASAA0954131Starter Gen · malfunctionedAPU FAULT LITE ILLUMINATED. GROUNDED YES. REMOVED AND INSTALLED A NEW APU STARTER GENERATOR IAW AMM 49-41-21 00 801 APU MAINT MSG 49 41012 NO APU ROTATION. DURING STARTER GENERATOR INSTALLATION TEST APU STARTED BUT AUTOSHUT DOWN AFTER 1 MIN FAULT LIGHT ILLUMINJan 2, 2009 · N570AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA0854010Circuit Breaker · poppedNR 1 ENG FAILED TO START AFTER LEVER RAISED TO IDLE N1 4.5 EGT22 N2 30 PERCENT FUEL FLOWS .50. GROUNDED YES. ENG NR 1 SHOWS MAINTENANCE MESSAGE 74 30981 RT IGNITION OUT OF RANGE. FOUND ENG NR 1 RT C/B OUT. CHECKED BEHIND P18 2 PANEL FOR CONTAMINATION OR DDec 8, 2008 · N570AS · Boeing 737890 · Ignition Harness (Distribution)SDR ASAA0854009Wire · chafedMAIN FIRE WARNING INOP. GROUNDED YES. FOUND WIRE CHAFED AT REMOTE APU CONTROL PANEL & FIRE PROTECTION MASTER WARNING & CONTROL C/B POPPED. REPLACED REMOTE APU CONTROL PANEL REF MM 26 22 03 000 801. MAIN FIRE WARNING OPS NORMAL REF MM 26 15 00 & MM 26 11 00Dec 8, 2008 · N570AS · Boeing 737890 · Fire Protection System WiringSDR ASAA0853763Filter · dirtyFOUND ON WALKAROUND NR 1 ENG DPI INDICATOR POPPED OUT. REPLACED SCAVENGE FILTER CHANGE PER FIM 21 11 00 810 803, RAN NR 1 ENG 5 MIN, NO OIL LEAKS AND DPI INDICATOR OK. CONFIRM FILTER SCAVENGE CHECK PER FIM 24 11 41 200. 801.Nov 10, 2008 · N570AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0853687Controller · malfunctionedON RECALL CONT CABIN ZONE TEMP LIGHT ILLUMINATES, LIGHT EXTINGUISHES WITH MC RESET. COULD NOT DUPLICATE. ACCOMPLISHED FIM 21 62 00 810 842. NO FAULTS. FAULT WAS INTERMITTENT. ACCOMPLISHED BITE TEST AND NO FAULT FOUND. NO HISTORY 90 DAYS.Nov 2, 2008 · N570AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0853659Vent · leakingNR 1 IDG HAS A HISTORY OF FREQUENT OIL SERVICING. FOUND NR 1 IDG LEAKING FROM SERVICE PORT AND VENT RELIEF BUTTON. REMOVED AND REPLACED FILL PORT AND VENT RELIEF PER CMM 24 11 85, LEAK CHECK OK CLEARED TSR.Oct 20, 2008 · N570AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0853634Control Valve · faultyUPON DEPARTURE FROM HNL AIRFLOW FROM GASPERS WAS EXCESSIVELY HIGH NOISE LEVEL WAS 120 DBT AND TEMPERATURE IN CABIN WAS VERY COLD. AFTER APPROX 5 MIN AIRFLOW DB LEVEL AND TEMPERATURE RETURNED TO NORMAL. SUSPECT THAT A 9TH STAGE BLEED VALVE STUCK OPEN. NO OTHOct 19, 2008 · N570AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA0853590Fmc · malfunctionedFMC DISAGREE LIGHT PROCEDURE FOLLOWED, 11.2 QRH INFO NOTED. ACCOMPLISHED FIM TASK 34 61 00 810 801 FOR GROUND VERIFICATION OF ETOPS AC TESTS OK.Oct 13, 2008 · N570AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0853533Filter · cloggedCABIN TEMPERATURE CONTROL WAS VERY ERRATIC IN AUTO CABIN TEMP WOULD RANGE FROM VERY HOT TO VERY COLD WITH EXTREMELY SMALL MOVEMENTS OF TEMP CONTROLS. ALSO LARGE DIFFERENCES (TEMP) BETWEEN FWD & AFT SELECTIONS OF MAIN CABIN. NO PERMANENT FRC FOUND (FAULT REPOSep 26, 2008 · N570AS · Boeing 737890 · Cabin Temperature SensorSDR ASAA0853517Transceiver · failedHF RADIO NR 1 INOP VERIFIED MALFUNCTION BITE CHECK PER MM 23 11 00 SHOW TRANCEIVER NR 1 FAILURE. REMOVED AND REPLACED NR 1 HF TRANCEIVER. OPERATIONAL TEST GOOD PER MM 23 11 21, SYSTEM CHECKS GOOD.Sep 19, 2008 · N570AS · Boeing 737890 · HF Communications SystemSDR ASAA0853513Controller · malfunctionedZONE TEMP LIGHT ILLUMINATED ON RECALL CHECK LIST COMPLETED WILL NOT RESET ACCOMPLISHED ZONE TEMP CONTROLLER BITE COCKPIT TRIM VALVE FAULT ON STANDBY CONTROLLER. VERIFY & RETEST OK REF 21 61 00 PG 501. NO FURTHER DISCREPANCIES NOTED. GROUND VERIFICATION TESTSep 15, 2008 · N570AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0853430Control Panel · malfunctionedTHE "PWS FAIL" "WXR FAIL" AMBER ANNUNCIATOR ON BOTH NAV DISPLAYS DURING COCKPIT SET UP WITH WXR SELECTED ON EFIS CONTROL PNL. PROBLEM VERIFIED 'PWS FAIL' C W FIM 344-010-00-34-43 TASK 810 WXR SYSTEM OPS TEST AMM TASK 34-43-00-710-802 001, ALL CHECKS NORMAL AFAug 29, 2008 · N570AS · Boeing 737890 · Weather Radar SystemSDR ASAA0853322Indicator · failedNR 1 REFUELING INDICATOR AT WING PANEL INOP, FLT DECK INDICATIONS NML. COULD NOT DUPLICATE ACCOMP. FQIS BITE NO FAULTS ACCOMP. GRD TEST, TEST PASS REF. FIM 28-41 TASK 801. REMOVED WING REFUEL PANEL. ACCOMP GVI OF WIRES FOR NR 1 TANK IND AND OHMED SAME WIRES NOAug 8, 2008 · N570AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA0853264Transceiver · failedPWS FLAGS IN VIEW AS WELL AS WX RADAR RT 'FAIL' DISPLAYED. VERIFIED FAULT. REMOVED & REPLACED WETHER RADAR TRANCIEVER IAW MM 34-43-41. ALSO REMOVED & REPLACED RADAR ANTENNA MOUNT IAW MM 34-43-11. OPS TESTED IAW MM 34-43-00-710-802-001. TESTS OK. ACCOMP GVI FOAug 1, 2008 · N570AS · Boeing 737890 · Weather Radar SystemSDR ASAA0853257Drive Unit · failedPWS FAILED AFTER ENGINE START. REPLACED WXR ANT DRIVE UNIT WITH SERVICABLE ONE. VERIFIED PN. OPS TEST PASS REF MM 34-43-11-000-802.Aug 1, 2008 · N570AS · Boeing 737890 · Weather Radar SystemSDR ASAA0853249Transceiver · failed"PWS FAIL" ILLUMINATED ON NAV DISPLAY ON TAXI IN. DUPLICATED FAULT ALONG W WXR FAIL FALG. ALSO FOUND UNKNOWN FLUID, COFFEE, SODA ON TOP & ON TRAY OF WXR R/T. CLEANED FLUID FROM TRAY & AREA. REPLACED WXR RT REF MM:34 43 41.Jul 30, 2008 · N570AS · Boeing 737890 · Weather Radar SystemSDR ASAA0853212Start Valve · failedON STARTING ENGINE NR 1, WHEN START SWITCH PUT TO GROUND THERE WAS NO START VALVE LIGHT ILLUMINATION AND NO N2 ROTATION BUT THE EGT GAUGE DID ILLUMINATE. DID NOT SEE A DUCT PRESSURE RISE ON THE DUCT PRESSURE GAUGE. REMOVED AND REPLACED NR 1 ENGINE START VALVEJul 20, 2008 · N570AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA0853169Inlet Bullet · erodedNR 1 ENGINE FWD SPINNER (CONE) HAS EXCESSIVE ERROSION OF BLACK AND WHITE COATING. REMOVED AND REPLACED SPINNER (CONE) PER TC 78472002.Jul 1, 2008 · N570AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA0853091Filter · dirtyRT ENG OIL FILTER POP OUT INDICATOR EXTENDED. DRAINED ENG OIL AND AGB PER 737 AMM 12 13 11. REMOVED AND REPLACED RT ENGINE OIL SUPPLY FILTER PER MM 79 21 00 802 FOO. OPS AND LEAK CHECK GOOD, POP OUT INDICATOR CKS GOOD. NO CONTAMINATION IN FILTER.Jun 25, 2008 · N570AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0853090Filter · dirtyLT ENG OIL FILTER POP OUT INDICATOR EXTENDED. REMOVED AND REPLACED LT ENG OIL SUPPLY FILTER PER MM79 21 03 000 802 F00. OPS AND LK CK GOOD. POP OUT IND CKS GOOD.Jun 25, 2008 · N570AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0853016Oil System · lowNR ONE ENGINE OIL AT 13 QTS TOP OF DESCENT. NR TWO ENGINE OIL AT 14 QTS TOP OF DESCENT VERIFIED NR 1 AND NR 2 ENG OIL SERVICED TO 16 AND 17 QTS RESPECTIVELY. TOPPED OFF BOTH ENG OILS TO FULL. NR 1 ENG OIL ADDED 2.5 QTS, NR 2 ENG OIL ADDED 2.5 QTS, APU OIL AMay 30, 2008 · N570AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0852981Probe · dirtyNR 1 ENGINE EGT HOT DAY MARGIN HAS NOT RECOVERED TO EXPECTED LEVELS AFTER LAST COMPRESSOR WASH. ALL OTHER PARAMETERS ARE NORMAL. COMPLETED T C 78273000, NO FAULTS LOGGED. PRE CLEAN T49.5 S1 S4 106 61 67 128. AFTER CLEANED 62 32 35 78. DURING ENG RUN AFTMay 26, 2008 · N570AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA0852978Compressor · dirtyGE REMOTE DIAGNOSTICS NR 2 ENGINE TREND DATA CONTINUES TO SHOW A GREATER THAN NORMAL EGT MARGIN LOSS. ACCOMPLISH NR 2 ENGINE SINGLE ENGINE COMPRESSOR CLEANING IAW AMM SUPPLEMEMT 72-00-00 P710. ACCOMPLISHED COMPRESSOR WASH ON NR 2 ENG REF MM SUPP 72-00-00 PGMay 16, 2008 · N570AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA0852930Filter Element · dirtyTO MAINTAIN A COMFORTABLE TEMPERATURE IN THE AFT CABIN THE AFT CABIN TEMP KNOB HAS TO BE TURNED FARTHER CLOCKWISE THAN USUAL TO AROUND 3 O'CLOCK. THIS PRODUCES APPROX 20C DUCT TEMP. THE OTHER KNOBS WERE IN THE USUAL POSITION: CONTROL CAB 11:00 AND FWD CAB 1May 8, 2008 · N570AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0852873Computer · faultySPEED TRIM FAIL AND MACH TRIM FAIL LIGHTS CAME ON DURING RECALL CHECK AFTER ENGINE START. F/O'S FD FLAG ALSO CAME ON. VERIFIED FAULT. FCC "B" COMPUTER INOP. REPLACED FCC "B" COMPUTER. PERFORMED LRU TEST FOR FCC & LAND VERIFY TEST. HGS SENSOR TEST FOR FCCMay 3, 2008 · N570AS · Boeing 737890 · Autopilot ComputerSDR ASAA0852754Coupler · faultyUNABLE TO TUNE OR TRANSMIT ON NR 2 HF. REPLACED NR 2 HF COUPLER. GROUND VERIFICATION TEST PASSED.Mar 23, 2008 · N570AS · Boeing 737890 · HF Communications SystemSDR ASAA0852709Filter · dirtyWHILE CHECKING APU OIL FOR PRE DEPARTURE CHECK FOUND RED OIL FILTER CLOGGING INDICATOR PROTRUDING FROM FILTER BOWL. PERFORMED BITE CHECK OF CDU NO CURRENT FAULTS. REPLACED APU LUBE OIL FILTER. FILTER CHECK GOOD. OIL FILTER INDICATOR CHECK GOOD. MAG DRAIN Mar 14, 2008 · N570AS · Boeing 737890 · APU Oil SystemSDR ASAA0852708Transceiver · faultyHF 2 DOES NOT TRANSMIT. NR 2 HF DOES NOT TRANSMIT ON 10 MEGS BUT VOICE HEARD ON 13 MEGS. REPLACED NR 2 HF TRANSCEIVER. OP CHECKS GOOD.Mar 13, 2008 · N570AS · Boeing 737890 · HF Communications SystemSDR ASAA0852684Engine · oil consumptionNR 1 ENGINE OIL CONSUMPTION IS AT 0.8QTS HR OUT OF LIMITS FOR ETOPS OIL CONSUMPTION. ENGINE OIL CONSUMPTION RATE HAS RETURNED TO NORMAL.Feb 26, 2008 · N570AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA0852533Oil Filter · cloggedDURING TASKCARD 78349013, FOUND APU OIL FILTER DELTA P INDICATOR EXTENDED. REPLACED OIL FILTER. RESET INDICATOR. INSPECTED FILTER AND MAG PLUG. OP AND LEAK CHECKS GOOD.Feb 1, 2008 · N570AS · Boeing 737890 · APU Oil SystemSDR ASAA0852506Modulating Valve · faultyTHE "ZONE TEMP" LIGHT ILLUMINATED ON RECALL EXTINGUISHED ON MASTER CAUTION RESET. REPLACED TRIM AIR MOD VALVE IAW 21 61 21. OPS NORMAL, NO LIGHTS ON RECALL.Jan 28, 2008 · N570AS · Boeing 737890 · Cabin Temperature ControllerSDR ASAA0852461Cabin Pressure · malfunctionedTHE "AUTO FAIL" AMBER LIGHT ON PRESSURIZATION PANEL ILLUMINATED DURING PRE-FLIGHT. PERFORMED FIM 21 31 TASK 801. SYSTEM RESET, NO FAULTS NOTED. NO HISTORY. OP CHECKS GOOD.Jan 10, 2008 · N570AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA0752350Start Valve · unknownNO N2 ROTATION. START SWITCH WAS ENGAGED FOR NR 1 ENGINE. OPENED COWL CHECKED CONNECTORS ON START VALVE AND CONDITION OF STARTER. FOUND ALL SECURE. RAN ENGINE OPS NORMAL. OK FOR SERVICE.Dec 4, 2007 · N570AS · Boeing 737890 · Engine Start Valves/Controls
Back to N570AS