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.

SDR ASAA2016101618366Warning Light · false activationLEFT A/C PACK LIGHT ILLUMINATED. EXTINGUISHES WITH MASTER CAUTION RECALL. ACFT GROUNDED. VERIFIED THE LT PACK LIGHT FAULT LIGHT, RESET AFTER MASTER CAUTION, IAW FIM 21-62 TASK 801, PERFORMED PACK TEMP CONTROL BITE PROCEDURE, THIS PACK TCV LIGHT FLAGGED. AFTOct 16, 2016 · N569AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016100518220Control Valve · faultedRIGHT PACK LIGHT ILLUMINATED ON RECALLS. RESETS WITH MASTER CAUTION RESET. ACFT GROUNDED. BITE CHECK OF THE NR 2 ZONE TEMP CONTROLLER, FOUND PREVIOUS FLT AND CURRENT FAULT 'THIS PACK TCV.' REPLACED RT PACK TCV IAW AMM 21-51-10-000-801 AND -400-801. OPS AND Oct 5, 2016 · N569AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016100218183Warning Light · false activationRIGHT PACK LIGHT ILLUMINATES ON RECALL, RESETS WITH MASTER CAUTION. ACFT GROUNDED. ACCOMPLISHED PACK/ZONE TEMPERATURE CONTROL BITE. CLEARED FAULTS, OPS CHECK GOOD. GROUND VERIFICATION SUCCESSFUL, REF B737-800 AMM 21-61-00.Oct 2, 2016 · N569AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016082317784Satcom · malfunctionedSATCOM LOCKUP. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE IAW QRH. SATCOM OPS RESTORED NORMAL.Aug 23, 2016 · N569AS · Boeing 737890 · HF Communications SystemSDR ASAA2016080817648Engine · faultedDURING ACCOMPLISHMENT OF T/C 78273000, NR 1 ENGINE HAS FAULT MSG 75-20391, VSV POSITION SIGNAL IS OUT OF RANGE. LONG TERM FAULT. ACFT GROUNDED. INTERROGATED THE FMC CDU FOR ENGINE FAULTS REF T/C 78273000 AND FOUND MESSAGE 75-20391, NO LONGER ACTIVE LAST 10Aug 8, 2016 · N569AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2016080817646Engine · faultedDURING ACCOMPLISHMENT OF T/C 78273000, NR 1 ENGINE HAS FAULT MESSAGE 73-20341, FMV POSITION SIGNAL IS OUT OF RANGE. SHORT TERM FAULT. ACFT GROUNDED. ACCOMPLISHED INITIAL EVALUATION, REF FIM 73-25-00-810-803-F00, STEP E 1-3. NO DEFECTS NOTED. SUSPECT INTERMAug 8, 2016 · N569AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2016080217589Unknown · unknownA/T'S WILL NOT STAY ENGAGED AUTOMATICALLY DISCONNECTS. FAULT CODE 223130-00. ACFT GROUNDED. PERFORMED A/T BITE TEST IAW FIM 22-31, TASK 801 AND A/T OPERATIONAL TEST IAW AMM 22-31-00, ALL OPS NORMAL: CURRENT STATUS, NO FAULTS AND INTERACTIVE SERVO MOTOR TEST,Aug 2, 2016 · N569AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016070717303Autopilot Sys · malfunctionedDURING CRUISE, IN SMOOTH AIR AT FL 340. THE "CMD A" AUTOPILOT DISENGAGED. IT WAS IMMEDIATELY RE-ENGAGED AND WORKED NORMALLY UNTIL IT DISENGAGED AGAIN DESCENDING THROUGH FL 300 AT 280 KTS. IT WAS RE-ENGAGED NORMALLY. WE FLEW THE REMAINDER OF THE FLIGHT ON THJul 7, 2016 · N569AS · Boeing 737890 · Autopilot SystemSDR ASAA2016060616963Transceiver · failedPWS FAIL, ON THE GROUND. ACFT GROUNDED. WXR WOULD NOT GO INTO BITE WITH WXR FAIL MESSAGE ON DU'S. REPLACED WXR TRANSCEIVER, REF MM 34-43-41. LEFT PITOT ADM WAS NOT DISCONNECTED. OPS NORMAL, REF MM 34-43-00.Jun 6, 2016 · N569AS · Boeing 737890 · Weather Radar SystemSDR ASAA2016060216936Servo · failedAUTOTHROTTLE SWITCH WILL NOT STAY ENGAGED. ACFT GROUNDED. CONFIRMED FAULT, A/T ASM-2, FAILS SERVO MOTOR TEST MSG 22-31795, ASM-2 10 DEG RATE FAULT. A/T FLIGHT FAULT REVIEW ALSO SHOW MSG 22-31688, ASM-2 FAULTS. R & R NR 2 A/T SERVO MOTOR REF AMM, TASK 22-31-Jun 2, 2016 · N569AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016051516782Warning Light · false activationTHE MAINTENANCE LIGHT ON APU ILLUMINATED AFTER STARTING THE APU DURING TAXI IN. ACFT GROUNDED. DID BITE CHECK OF APU IAW 49-60, TASK 801, GOT MESSAGE 49-11019, ACCOMPLISHED FIM TASK 49-10, TASK 801, DID 2 RESTARTS, NO MAINT LIGHT OR DEFECTS NOTED, RE DID BMay 15, 2016 · N569AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2016041316389Gust Lock · damagedR1 DOOR WILL NOT RELEASE TO ALLOW CLOSURE. IAW MEL 52-7D CONTACTED MAINTENANCE. ACFT GROUNDED, REF LP 11625772, R1 DOOR GUST LOCK PIN MISSING. R1 DOOR LEVER ON MEL 52-7D. MANUALLY RELEASED LEVER. OPS CHECK NORMAL. R & R R1 RELEASE BUTTON ASSY. OPS CHECK GApr 13, 2016 · N569AS · Boeing 737890 · Service DoorsSDR ASAA2016040516247Warning Light · false activationLEFT PACK LIGHT ILLUMINATES, BON ON MASTER CAUTION RECALL CANCELS WHEN MASTER CAUTION LIGHT PRESSED TO RESET. ACFT GROUNDED. RAN SYS TEST IAW AMM 21-61-00, SYS OPS CHECKS GOOD.Apr 5, 2016 · N569AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016031915991Warning Light · false activationLEFT PACK ILLUMINATED ON RECALL, EXTINGUISHED ON RESET. ACFT GROUNDED. PERFORMED BITE CHECK OF NR 1 CONTROLLER. FAULT SHOWS RAM AIR ACTUATOR. FAULT RESET AND BITE TEST NORMAL REF AMM 21-61-00.Mar 19, 2016 · N569AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016021515460Apu · contaminatedAT ROTATION DURING A BLEEDS OFF TAKEOFF ACFT FILLED UP WITH SMOKE IN CABIN AND COCKPIT. DISSIPATED AFTER ABOUT 5 MINUTES. WE DEICED WITH TYPE 1 AND TYPE 4 AT DCA PRIOR TO TAKEOFF. HEAVY WEIGHT LANDING AT IAD, 167.OK, 400 FPM. LANDING WAS SMOOTH AND UNEVENTFeb 15, 2016 · N569AS · Boeing 737890 · APU Core EngineSDR ASAA2016020815342Indicator · no testNR 1 FUEL QTY FAILS SYS TEST IAW AMM TASK 28-41-00-730-801. ACFT GROUNDED.Feb 8, 2016 · N569AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016020815329Probe · failedFUEL QTY INDICATION PROBLEMS FOR NR 2 RT TANK. ACFT GROUNDED. R & R NR 2 TANK COMPENSATOR PROBE AND TANK UNITS F8R, F7R, F6R, AND F1R REF AMM 28-41-21. REPLACED NR 2 TANK UNITS F5R, F4R,F3R, F2R IAW AMM 28-41-21/401. REPLACED NR 2 TANK UNITS F12R, F11R, F10Feb 8, 2016 · N569AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016020415300Satcom · malfunctionedSAT SELECTION MISSING ON THE MCDU MENU PAGE AND NO SATCOM PAGES AVAILABLE. ACFT GROUNDED. ACCOMPLISHED SATCOM LOCKUP RESET PROCEDURE IAW QRH. SAT DISPLAYS RETURNED TO NORMAL.Feb 4, 2016 · N569AS · Boeing 737890 · Communications SystemSDR ASAA2016020115233Indicator · out of toleranceFUELERS STOPPED FUELING WHEN FUEL TANK INDICATORS EXCEEDED TOLERANCES. ACFT GROUNDED. REF FIM 28-41, TASK 801. PERFORMED FQIS BITE. REACCOMPLISHED BITE TEST AND BITE TEST PASSED. REF AMM 28-41-00-720-801, PERFORMED FUEL QTY COMPARISON CHECK, COMPARISON CHECFeb 1, 2016 · N569AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016012114958Satcom · no indicationMISSING SAT SELECTION ON THE MCDU MENU PAGE AND NO SATCOM PAGES AVAILABLE. ACFT GROUNDED. PERFORMED QRH SATCOM LOCK UP PROCEDURE. NORMAL SATCOM DISPLAY RETURNED.Jan 21, 2016 · N569AS · Boeing 737890 · Communications SystemSDR ASAA2016012114956Servo · faultedAUTOTHROTTLE INOPERATIVE. ACFT GROUNDED. 16 ASM -2 FAULTS LAST FLIGHT MESSAGE 22-31688. REPLACED NR 2 AUTOTHROTTLE SERVO REF AMM. 22-31-91. INSTALLATION TEST NORMAL. AUTOTHROTTLE OPS TEST REF AMM 22-31-00/501. NO FAULTS. ACFT REMAINS CATIIIA AUTOLAND ANJan 21, 2016 · N569AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016010714681Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.Jan 7, 2016 · N569AS · Boeing 737490 · Communications SystemSDR ASAA2016010314627Warning Light · false activationELECTRIC LIGHT ILLUMINATED AFTER TRANSFER TO APU POWER. ACFT GROUNDED. PERFORMED P5-13, PANEL BITE CK. SHOWED AUXILIARY BATTERY CHARGER FAULT. RESET PANEL AND FAULTS CLEARED REF FIM 24-31, TASK 801.Jan 3, 2016 · N569AS · Boeing 737490 · Central WarningSDR ASAA2016010114616Fuel Nozzle · failedWHILE ACCOMP T/C 78273000 RECORDED FAULT CODE 73-31371 UPPER EGT SECTORS READING HIGH NR 1 ENGINE ECONOMIC FAULT. ACFT GROUNDED. R & R NR 1 ENGINE UPPER 11 FUEL NOZZLES IAW POWERPLANT-73CMPT-07267-2. PERFORMED REPAIR CONFIRMATION IAW FIM 73-11, TASK 801. NOJan 1, 2016 · N569AS · Boeing 737490 · Engine Fuel DistributionSDR ASAA2015121814324Fmc · malfunctionedDURING PREFLIGHT FMCS WENT INTO DATA LOADER PROTOCOL MAINTENANCE PAGE. ACFT GROUNDED. POWERED DOWN ACFT. VERIFIED POSITION OF DATA LOADER SELECTOR SWITCHES. NO DEFECTS NOTED. FMCS OPS NORMAL.Dec 18, 2015 · N569AS · Boeing 737490 · Flight Management Computing Hardware SystemSDR ASAA2015112413988Regulator · failedNR 2 ENGINE HIGH STAGE REGULATOR TESTS BAD ON HEALTH CHECK. ACFT GROUNDED. R & R NR 2 ENGINE HIGH STAGE REGULATOR IAW AMM 36-11-07. OPS/LEAK CHECK GOOD.Nov 24, 2015 · N569AS · Boeing 737490 · Pneumatic Distribution SystemSDR ASAA2015112413987Shutoff Valve · failedNR 2 ENGINE PRSOV STICKS IN THE CLOSED POSITION. ACFT GROUNDED. R & R NR 2 ENGINE PRSOV IAW AMM 36-11-04. OPS/LEAK CHECKS GOOD.Nov 24, 2015 · N569AS · Boeing 737490 · Pneumatic Distribution SystemSDR ASAA2015112413986Bleed Air Sys · malfunctionedBLEED TRIP OFF, RT SIDE, JUST AFTER TOP OF DESCENT. RAN QRH, FIXED PROBLEM. ACFT GROUNDED. PERFORMED CROSSOVER CHECK IAW AMM 36-11-00-710-801 AND FIM TASK 36-10, TASK 801, BLEED TRIP OFF LIGHT ON. OPS CHECK NORMAL.Nov 24, 2015 · N569AS · Boeing 737490 · Pneumatic Distribution SystemSDR ASAA2015110413641Acm · damagedLEFT ACM DAMAGED, DISCOVRED DURING PACK FLOW CONTROL VALVE CHANGE. ACFT GROUNDED. R & R LT ACM IAW AMM TASK 21-51-04-400-802-002 THROUGH STEP 31H, 7, I, 39071. COMPLETED STEPS I, J. LT ACM. OPS CK GOOD.Nov 4, 2015 · N569AS · Boeing 737490 · Cabin Cooling SystemSDR ASAA2015100613345Fuel Nozzle · faultedNR 2 ENGINE LOGGED ECONOMIC FAULT 73-31372. ACFT GROUNDED. REPLACED UPPER 11 FUEL NOZZLES MONITORED IN THE UPPER SEGMENT, REF T/C PWRPL-73CMPT-07267-2.Oct 6, 2015 · N569AS · Boeing 737490 · Fuel Injector NozzleSDR ASAA2015092513210Warning Light · false activationWITH ENGINES SHUTDOWN AT GATE,M NR 2 ENGINE VALVE CLOSED LIGHT REMAINS BRIGHT BLUE NOT DIM BLUE WHICH IS A NORMAL INDICATION. ACFT GROUNDED.Sep 25, 2015 · N569AS · Boeing 737890 · Central WarningSDR ASAA2015092213173Blade · wornNR 1 ENGINE FAN BLADE PLATFORM SEALS MISSING OVER 42", EXCEEDS MM 72-21-02 ALLOWABLE LIMITS OF 39.37. ACFT GROUNDED. REPLACED ALL 24 PLATFORMS ON NR 1 ENGINE REF TASK CARD NR 78472002.Sep 22, 2015 · N569AS · Boeing 737490 · Turbine Engine Air Inlet SectionSDR ASAA2015092213172Spinner · wornNR 1 ENGINE SPINNER CONE WHITE PAINT WORN IN SEVERAL SPOTS. ACFT GROUNDED. R & R NR 1 ENGINE SPINNER CONE REF MM 72-21-01.Sep 22, 2015 · N569AS · Boeing 737490 · Turbine Engine Air Inlet SectionSDR ASAA2015090312922Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. RESET, NORMAL OPS, PERFORMED SAT SYS, TEST REF 23-15-00. SYS CKS NORMAL.Sep 3, 2015 · N569AS · Boeing 737490 · Communications SystemSDR ASAA2015081312896Warning Light · malfunctionedNR 1 ENGINE VALVE CLOSED LIGHT IS DIM AND DOES NOT GO OUT WHEN CUTOFF LEVER IS RAISED. ACFT GROUNDED.Aug 13, 2015 · N569AS · Boeing 737890 · Engine Indicating SystemSDR ASAA2015080712790Hmu · faultedENGINEERING REQUESTS NR 2 ENGINE HMU REPLACEMENT FOR CONTINUING HPT ACCV FAULTS. ACFT GROUNDED. REPLACED NR 2 ENGINE HMU IAW TASK CARDS N8473000, N8473001. NO RECENT OR FAULT HISTORY NOTED PRIOR TO HMU INSTALLATION TESTS.Aug 7, 2015 · N569AS · Boeing 737490 · Fuel Controlling SystemSDR ASAA2015080712767Light · inoperativeMODE CONTROL PANEL DISENGAGE LIGHTS INOPERATIVE. ACFT GROUNDED. REPLACED MCP IAW AMM 22-11-34-000-801. ACCOMPLISHED OPS CHECKS TO AMM 22-11-34-740-801 AND ADDITIONAL TESTS BITE GROUP NR 32, NR 49. DFCS LRU INTERFACE TEST FOR MCP, LAND VERIFY TEST AND HOUSIAug 7, 2015 · N569AS · Boeing 737490 · Instrument PanelSDR ASAA2015080512744Gcu · failedWITH APU RUNNING, NO VOLTS OR FREQUENCIES, APU WILL NOT GO ONLINE. ACFT GROUNDED. REMOVED AND RE-INSTALLED APU GCU IAW MM 24-21-81-400-801. FOUND S16 BAD, R & R APU REMOTE CONTROL PANEL IAW MM 26-22-03-400-801. ACCOMPLISHED APU FIRE EXTINGUISHING BOTTLE SQAug 5, 2015 · N569AS · Boeing 737490 · AC Generator-AlternatorSDR ASAA2015080312704Generator · malfunctionedAFTER LANDING APU STARTED NORMALLY BUT APU GEN SHOWED NO VOLTS, NO FREQ'S WITH BLUE APU OFF, BUS LIGHT ILLUMINATED. ALL C/B'S CHECKED IN. APU GENERATOR WOULD NOT SWITCH ON & TAKE POWER. ACFT ACCEPTED GROUND POWER OK. ACFT GROUNDED. ACCOMPLISHED APU OPS TESAug 3, 2015 · N569AS · Boeing 737490 · AC Generator-AlternatorSDR ASAA2015073112662Fmc · malfunctionedSINGLE FMC FAIL, CAPTAIN SIDE. ACFT GROUNDED. ACCOMPLISHED FMC BITE, IAW FIM 34-61, TASK 801. NO FAULTS. GROUND VERIFICATION ACCOMPLISHED.Jul 31, 2015 · N569AS · Boeing 737490 · Flight Management Computing Hardware SystemSDR ASAA2015073112653Warning Message · false activationDATA LINK FULL MESSAGE, ACFT GROUNDED. RESOLVED IAW QRH.Jul 31, 2015 · N569AS · Boeing 737490 · Flight Management Computing Hardware SystemSDR ASAA2015072812620Warning Light · false activationSTARTED APU, HAD BLUE LIGHT "APU GEN OFF BUSS" LIGHT UP BUT NO VOLTS OR FREQUENCIES. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT. STARTED APU, BLUE GENERATOR OFF BUSS LIGHT ON WITH GOOD VOLTS AND FREQUENCIES. GROUND VERIFICATION TEST PASSED IAW MM 24-21-00. Jul 28, 2015 · N569AS · Boeing 737490 · AC Generation SystemSDR ASAA2015070712352Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. PULLED AND RESET C/B'S PROBLEM RESOLVED.Jul 7, 2015 · N569AS · Boeing 737490 · Flight Management Computing Hardware SystemSDR ASAA2015062112172Regulator · malfunctionedIN CLIMB, THRU FL 300, LT DUCT PRESSURE 20 PSI, RT 47 PSI IN CRUSE AT FL 350, LT 22 PSI, RT 31 PSI BOTH PACKS IN AUTO AND ANTI-ICE OFF. ACFT GROUNDED. PERFORMED T/C NG-36WC-00001 "ENGINE BLEED AIR SYS HEALTH CHECK" ON NR 1 ENGINE. PRE-COOLER CONTROL VALVE FJun 21, 2015 · N569AS · Boeing 737490 · Pneumatic Distribution SystemSDR ASAA2015061912124Wire Harness · faultedWHILE ACCOMPLISHING TC 78273000, FOUND THE FOLLOWING MAINTAINCE MESSAGES: MSG 75-10362 HPTACC POSITION SIGNAL OUT OF RANGE FOR THE NR 2 ENGINE, MSG 75-30412 HPTACC POSITION SIGNALS DISAGREE, ACFT GROUNDED. ACCOMPLISHED EEC BITE TEST RECENT FAULT ON NR 2 ENGINJun 19, 2015 · N569AS · Boeing 737490 · Engine Indicating System WiringSDR ASAA2015061212075Valve · intermittentRIGHT "SPAR VALVE CLOSED" LIGHT ILLUMINATED BRIGHT BLUE IN FLIGHT. ACFT GROUNDED. PERFORMED FIM TASK 28-22, TASK 810, RT SPAR VALVE INTERMITTENT. REPLACED RT SPAR VALVE IAW MM 28-22-11, OPS CHECKED GOOD.Jun 12, 2015 · N569AS · Boeing 737490 · Aircraft Fuel Distribution SystemSDR ASAA2015061012055Autothrottle Sys · malfunctionedAUTOTHROTTLES WILL NOT REMAIN ENGAGED. ACFT GROUNDED. FFR LOGGED ASM-2, 22-31688. ACCOMPLISHED FIM 22-32, TASK 819. COULD NOT DUPLICATE MALFUNCTION. AUTOTHROTTLES OP CK NORMAL IAW REFERENCED FIM & MM 22-31-00. CAT STATUS REMAINS AUTOLAND & HGS QUALIFIED. SCJun 10, 2015 · N569AS · Boeing 737490 · Auto Throttle SystemSDR ASAA2015053111926Engine · faultedDURING ACCOMPLISHMENT OF T/C 78273000, FOUND NR 2 ENGINE SN 894-475, MAINTENANCE MSG 75-20802 T25 SIGNALS DISAGREE, SHORT TERM FAULT. MUST BE CORRECTED WITHIN 50 FLIGHT HOURS. ACFT GROUNDED. REF FIM TASK 75-33 TASK 805, EEC BITE TEST GOOD, VERIFIED FAULT MSMay 31, 2015 · N569AS · Boeing 737490 · Engine (Turbine/Turboprop)SDR ASAA2015041611391Actuator · failedDURING ACTUATOR TEST OF NR 2 ENGINE FAULT CODE 75-10392 IS PRESENT, VSV POSITION SIGNAL OUT OF RANGE CHANNEL A. ACFT GROUNDED. FIM 75-31, TASK 803, FDN BAD CONNECTOR ON "A" VSV ACTUATOR. REMOVED RT VSV ACTUATOR REF AMM 75-31-01-000-802, INSTALLED RT VSV AApr 16, 2015 · N569AS · Boeing 737890 · Compressor Bleed ControlSDR ASAA2015041611367Probe · damagedNR 2 ENGINE HAS HISTORY OF HPTACCV ECONOMIC FAULT MESSAGES 75-30412, 75-20412, 75-10362, 75-10412. PREVIOUS MAINTENANCE EEC AND HPTACCV HAVE BEEN REPLACED AND FAULTS CONTINUE. TECH SERVICE REQUESTS FOLLOW-UP. ACFT GROUNDED. REPLACED J9 & J10 HARNESS REF MM Apr 16, 2015 · N569AS · Boeing 737490 · Fuel Controlling System
Back to N569AS