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 ASAA2020092433223Autothrottle Sys · malfunctionedAUTO THROTTLE WILL NOT ARM. GROUNDED-YES. AUTHROTTLE OPS NORMAL, REF B737-800 FIM 22-31 TASK 801.SDR ASAA2020092133207Autoland Sys · malfunctionedAUTOLAND FAIL-AIRCRAFT NOSEWHEEL TOUCHED DOWN HALFWAY BETWEEN LEFT RUNWAY EDGE AND CENTERLINE AND CONTINUED TO TRACK LEFT UNTIL I DISENGAGED AUTO PILOT. AIRPORT REPORTED CALM WINDS AND RUNWAY WAS PROTECTED FOR CAT III OPS. GROUNDED-YES. PERFORMED LAND VERIFSDR ASAA2020091833196Connector · meltedNR 1 ENG NO START AFTER 2 ATTEMPTS ON RT IGNITION. GOOD ROTATION, GOOD FF, NO IGNITION. GROUNDED-YES. PERFORMED IGNITION SYSTEM TEST, PER B737-800 AMM 74-00-00. RIGHT IGNITER BITE TEST SHOWS FAULT 74-30981, RT EXCITOR IS OUT OF RANGE. REMOVED & REPLACED NSDR ASAA2020091403165Valve · intermittentNR 2 COWL ANTI ICE FAIL REQUIRED MULTIPLE ATTEMPTS TO OPEN. GROUNDED - YES. REPLACED NR 2 ENG TAI VALVE, IAW B737-800 AMM 30-21-11/401. NO LEAKS NOTED W/NR 2 ENG IDLE RUN. OPS NORMAL AT THIS TIME.SDR ASAA2020090633154Fire Loop · inoperativeAPU DET INOP LIGHT AND APU BOTTLE DISCHARGE LIGHT ON OVHT FIRE TEST & NR 1 ENGINE FIRE HANDLE NOT ILLUMINATING, 'A' LOOP WORKING, 'B' LOOP INOP. GROUNDED - YES. WORKED ON ETOPS CRITICAL SYSTEM. REPLACED MW0325 HARNESS, REF B737-800 AMM 26-11-02, CLEARS MEL SDR ASAA2020090181121Lamp · inoperativeEMERGENCY EXIT SIGN AT ROW 17 A/C LEFT DOES NOT ILLUMINATE. GROUNDED - YES. RELAMPED EMERGENCY EXIT SIGN AT ROW 17 A/C LEFT. OPS CHECK GOOD, AIRCRAFT OK FOR SERVICE.SDR ASAA2020081753030Heat Exchanger · brokenOIL FUEL HEAT EXCHANGER ON NR 2 ENGINE HELICOILS BROKEN FUEL IN. GROUNDED - YES. REMOVED NR 2 ENGINE MAIN OIL/FUEL HEAT EXCHANGER, REF B737-800 AMM 79-21-02-000-801-F00. INSTALLED SERVICEABLE MAIN OIL/FUEL HEAT EXCHANGER, REF BOEING B737-800 AMM 79-21-02-40SDR ASAA2020081733029Attach Bracket · damagedNR 2 ENG INLET AND FAN BLADE DETAILED INSPECTION. FOUND GOUGES ON DRAIN PLATE, AFT SIDE OF ASSY DRIVE GEAR BOX AT THE MAIN FUEL PUMP ATTACHMENT. GROUNDED - YES. REMOVED HIGH METAL FROM INBOARD EDGE OF DRAIN PLATE GOUGE, REF B737-900 AMM 70-10-07-800-801-F00SDR ASAA2020071632915Bleed Valve · stuckDURING DESCENT THROUGH 350, #1 ENGINE FAIL, EGT SPIKE, SHUTDOWN. SUCCESSFUL XBLEED RESTART, VIBRATION WHEN THRUST ADDED FOR APPROACH. GROUNDED - YES. PER TSR 705027, ACCOMPLISHED #1 ENGINE 5TH STAGE CHECK VALVE INSPECTION PER B737-800 AMM 36-11-02/601. FOUND SDR ASAA2020070832877Battery Pack · dischargedRT OVER WING EMERGENCY LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED RT POWER SUPPLY BATTERY PACK IAW AMM 33-51-06. CHARGED BATTERY PACKS IAW AMM 33-51-06-610-802.SDR ASAA2020070832876Battery Pack · dischargedFOUND EMERGENCY CABIN LIGHTS AT SEAT 7 FED THRU SEATS 10 FED TO BE INOP. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK EMERGENCY LIGHTING IAW AMM 33-51-06. OPS CHECK GOOD AT THIS TIME. NO DEFECTS FOUND.SDR ASAA2020070762875Battery Pack · dischargedLEFT FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. GROUNDED - YES. REMOVED AND REPLACED THE LT POWER SUPPLY BATTERY PACK IAW AMM 33-51-06. CHARGED BATTERY PACKS IAW AMM 33-51-06-610-802. SYSTEM CHECKED GOOD.SDR ASAA2020041332637Warning System · false activationAFTER LANDING NUMBER 2 ENGINE CONTROL LIGHT ILLUMINATED. GROUNDED - YES. ACCOMPLISHED B737-800 FIM TASK 73-00-801 AND ACT TEST PER B737-800 AMM 71-00-00-700-807-F00 TEST 12 AIRCRAFT OK FOR SERVICE.SDR ASAA2020041332630Modulating Valve · faultyPACK LIGHT ILLUMINATED ON RECALL, EXTINGUISHES WITH MASTER CAUTION RESET. GROUNDED - YES. REMOVED AND REPLACED TRIM MODULATOR VALVE LEAK AND OPS NORMAL PER B737-800 AMM 21-51-10.SDR ASAA2020040932627Idg · failed#2 GENERATOR WOULD NOT COME ON LINE. GROUNDED - YES. REMOVED AND REPLACED #2 ENG IDG LEAK AND OPS CK NORMAL. REF B737-800 AMM 24-11-11. GROUND VERIFICATION SUCCESSFUL. REF AMM 24-11-00-700-803.SDR ASAA2020040332595Warning System · false activationLEFT PACK LIGHT ILLUMINATED AFTER ENGINE START ON RAMP. LIGHT EXTINGUISHES WITH CLEARING MASTER CAUTION. GROUNDED - YES. PERFORMED B737-800 FIM 21-53 TASK 803, NO FAULTS NOTED AT THIS TIME. THIS CLEARS MEL 21-32B.SDR ASAA2020040632620Valve · failedGE DIAGNOSTICS REPORTS THE #2 ENGINE TREND DATA SHOWS A SUDDEN SHIFT IN DEGT, D CORE AND DFFHPTACCV IS MOST LIKELY CAUSE OF SHIFT(#PRI: 2) ETOPS SIGNIFICANT SYSTEM CNR ISSUED. GROUNDED - YES. REPLACED HPTACCV ON THE #2 ENGING. REF B737-800 AMM 75-21-01 ACTUATOSDR ASAA2020032432526Wire Harness · faulty#2 ENGINE HAS REPORTS OF CONTROL LIGHT ILLUMINATING. WITH FAULT CODE 75-20582, 7520572, 75-20532. GROUNDED - YES. REMOVED AND REPLACED ENG #2 FAN WIRE HARNESS J6 IAW B737-800 AMM 73-21-06. ACCOMPLISHED EEC TEST AMM 73-21-00 FAULTS NO LONGER EXISTS.SDR ASAA2020031732446Unknown · malfunctionedRIGHT ENGINE CONTROL LIGHT ON DURING TAXI. GROUNDED - YES. PERFORMED B737-800 FIM 73-06 TASK 801 EEC BITE SHOW FAULTS. POSITION SIGNALS DISAGREE AND FAULT CODE 75-20572 LPTACC DEMAND AND SIGNAL DISAGREE. PERFORMED ACTUATORS TASK 71-00-00 ONLY FAULT CODE 75-20SDR ASAA2020010631783Knob · looseFO SIDE RADAR GAIN KNOB LOOSE. GROUNDED - YES. F/O SIDE RADAR GAIN KNOB RESECURED. OK TO PROCEED IAW B737-800 AMM 34-43-91.SDR ASAA2020011331838Control Valve · defectiveINFORMATION ONLY - AT FL370 RIGHT DUCT 43PSI LEFT DUCT 22PSI. THIS OCCURRED 4HRS 30 MIN INTO FLIGHT. GROUNDED - YES. PERFORMED NR 1 ENG BLEED AIR SYSTEM HEALTH CHECK PER T/C NG-36WC-00001. FOUND PRECOOLER CONTROL VALVE TO BE DEFECTIVE. REMOVED AND REPLACED PRESDR ASAA20191231735Wire Harness · brokenNR 1 ENGINE B LOOP DID NOT ILLUMINATE ON TEST PRIOR TO FLIGHT. GROUNDED - YES. HIGH RESISTANCE ON THE B LOOP FROM M279 BOX. RESISTANCE FLUCTUATES DURING SHAKE DOWN CORE MW0326, FOUND THE TERMINAL BROKE AT RT CORE DUE TO CORROSION. REPLACED MW0326 B LOOP CORSDR ASAA20191231736Sensor · failedPER INBOUND ACARS PILOT REPORT (FLT 816): AT FL350 R DUCT PRESS 40 PSI LEFT DUCT PRESS 20 PSI. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 36-10 TASK 804 STEPS F 32 & 33 (REMOVED AND REPLACED 450 F THERMOSTAT & PRECOOLER CONTROL VALVE SENSOR ON #1 ENGINE).SDR ASAA201912231677Fire Detector · out of limitsDURING TEST, THE NR 1 ENGINE FIRE HANDLE AND ENG 1 OVERHEAT DOES NOT ILLUMINATE. GROUNDED - YES. FOUND THE NR 1 ENG AFT RIGHT DETECTOR 2 "B" OUT OF LIMITS PER TASK 26-10 TASK 810. REMOVED AND REPLACED AFT RIGHT DETECTOR 2"B" IAW AMM 26-11-01. ACCOMPLISHED ENSDR ASAA2019121101566Regulator · failedON TAXI OUT R DUCT PRESS READ 0, NO RESPONSE WITH POWER CHANGES. GROUNDED - YES. REMOVED AND REPLACED BLEED AIR REGULATOR REF B737-800 AMM 36-11-03-000-801/-400-801. REMOVED AND REPLACED PRECOOLER CONTROL VALVE REF AMM 36-12-02-000-801/400-801. INSTALLATION TESDR ASAA2019112503427Pump · failedLEFT (#1) AFT FUEL PUMP LOW PRESS LIGHT ILLUMINATED. GROUNDED - YES. REMOVED AND REPLACED #1 LH AFT FUEL BOOST PUMP REF B737-800 AMM 28-22-41. OPS AND LEAK CHECK GOOD.SDR ASAA2019111971371Sliding Window · overheatedCOPILOT #2 WINDOW CRACKED WITH WINDOW OVHT LIGHT. GROUNDED - YES. REMOVED RH OPENABLE WINDOW AND INSTALLED SERVICEABLE WINDOW ASSY REF B737-800 AMM 56-12-11-000/400-801. CHANGED WHCU, REF AMM 30-41-11, OPS NORMAL.SDR ASAA2019091130664Control Valve · failedRIGHT PACK LIGHT ILLUMINATES DURING RECALL AND EXTINGUISHES DURING MASTER CAUTION RESET. GROUNDED - YES. REMOVED & REPLACED TCV2 REF AMM 21-51-10, RT PACK/ZONE TEMP CONTROLLER BITE TEST & LK TEST NML REF AMM 21-61-00-700-806-002. PULLED & RESET 3 TOTAL C/BS. TSDR ASAA2019082653489Lens · brokenFOUND R/H AFT WING EXIT EMERGENCY LIGHT LENS BROKEN. GROUNDED - YES. REPLACED LIGHT LENS, OPS CK NML REF AMM 33-51-00-710-801.SDR ASAA2019071730090Warning System · false activationUPON MASTER CAUTION RECALL RT PACK LIGHT ILLUMINATES AND EXTINGUISHES WITH MASTER CAUTION RESET. GROUNDED - YES. ACCOMPLISHED FIM 21-62 TASK 801 TEMP CONTROLLER BITE. FOUND RT TEMP CONTROL VALVE LOGGED FAULT. ACCOMPLISHED VERIFY TEST, NO FAULTS FOUND. RESET FASDR ASAA2019071330044Control Panel · defectiveWX RADAR FAILED, "WXR FAIL CONT STAB". GROUNDED - YES. REMOVED & REPLACED WXR CONTROL PANEL REF AMM 34-43-91. PULLED & RESET 1 TOTAL C/B. ACCOMPLISHED WXR SYSTEM BITE PROCEDURE REF FIM 34-43 TASK 801 & WXR SYSTEM OPERATIONAL TEST REF AMM 34-43-00-710-802-001, SDR ASAA2019071230043Warning System · false activationFO'S WXR DISPLAY BLANK. FAULT CODE: 344 090 32 WXR STAB FLAG FOLLOWED BY A WXR FAIL FLAG UPON ACTIVATION. GROUNDED - YES. PERFORM FIM 34-43 TASK 801. WXR BITE SHOWS NO FAULT AND OPERATED NORMAL. OK FOR SERVICE.SDR ASAA2019071230042Unknown · malfunctionedWEATHER RADAR ON BOTH SIDES DISPLAY WXR FAIL & CONT STAB 3 HOURS INTO FLIGHT. GROUNDED - YES. PERFORMED WEATHER RADAR SYSTEM TEST REF AMM 34-43-00-730-802-001 NO FAULTS FOUND. TECH SERVICE CONTACTED DUE TO ONE EARLIER EPISODE.SDR ASAA2019062199780Window · crackedON CLIMBOUT THROUGH FL 280 L1 WINDSCREEN CRACKED SIMUTANOUSLY WITH OVERHEAT LIGHT. COMPLIED WITH BOTH CHECKLISTS. GROUNDED - YES. REMOVED AND REPLACED THE L1 WINDOW IN FLIGHT DECK PER B737-800 AMM 56-11-11-400-801 TESTED WINDOW HEAT SYSTEM PER AMM 30-41-00-710SDR ASAA201906139658Warning Light · false activationRH PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL. RESETS ON MASTER CAUTION PUSH TO RESET. GROUNDED - YES. RESET SYSTEM AND RAN PACKS FOR 10 MINUTES, AFTER RUNNING PACKS THE ETOPS GROUND FUNCTIONAL CHECK GOOD IAW B737-800 AMM 21-61-00-700-806-002.SDR ASAA2019061399636Autopilot Sys · malfunctionedCREW REPORTS A/C PITCHED DOWN DURING FLARE. THEY DISCONNECTED A/P & MANUALLY LANDED NORMAL. GROUNDED - YES. ACCOMPLISHED DFCS BITE LIBRARY TEST REF AMM 22-11-00-740-806, DFCS LAND VERIFY (GP 49) TEST REF AMM 22-11-00, HGS SYSTEM TEST REF SMM 34-36-00, OPS CK SDR ASAA2019050829266Warning System · false activationNR 1 ENG COWL VALVE OPEN LIGHT ON BRIGHT. GROUNDED - YES. ACCOMPLISHED ENG COWL TAI VALVE TEST REF AMM 30-21-11. RAN NR 1 ENG VERIFIED COWL LIGHT & TAI INDICATION ON PFD NORMAL. GROUND VERIFICATION SUCCESSFUL NR 1 ENG COWL LT NOT ILLUMINATED IN OFF POSITION.SDR ASAA2019050429246Warning System · false activationAFTER PUSHBACK AND ENG START BOTH ENG CONTROL LIGHTS CAME ON. GROUNDED - YES. CREW REPORTED ON POWER TRANSFER, A/C POWER WAS LOST MOMENTARILY, EEC BITE 12 NR 2 SHOWED FAULT 73-31351 AND 73-31352 RAN FIM TASK 73-22 TASK 808 MESSAGE DOES NOT SHOW, RAN EEC BITE RSDR ASAA2019050129203Nut Plate · corrodedREF T/C 78472000 NR 2 ENG INLET AND FAN BLADES DETAILED INSP FOUND 25 EA NUTPLATES ON O/B SIDE OF FAN FRAME FROM 1 O'CLOCK TO 6 O'CLOCK POS BEHIND OIL TANK, ALF, WITH 1 NUTPLATE BEHIND HMU HAVE CORROSION UNDER NUTPLATES. GROUNDED - YES. REMOVED AND REPLACED ENSDR ASAA2019041862934Heat Exchanger · leakingREF T/C #78472000 #2 ENGINE INLET AND FAN BLADES - DETAILED INSPECTION FOUND FUEL OIL HEAT EXCHANGER IS LEAKING FUEL FROM IT'S BASE. GROUNDED - YES. REMOVED #2 ENG MAIN FUEL HEAT EXCHANGER REF B737-800 AMM 79-21-02-000-801-F00. INSTALLED SERVICEABLE MAIN OIL FSDR ASAA2019041869032Duct · gougedREF TC 78472000 #2 ENGINE INLET AND FAN BLADES - DETAILED INSPECTION FOUND FWD SECTION OF TAI VALVE DUCTING GOUGED FROM TURNBUCKLE. LWR O/B SIDE. GROUNDED - YES. REMOVED AND REPLACED #2 ENG TAI DUCT REF CFM 56-7 PBUM 71-00-02 FIG 27-1/33-1. LEAK CHECK GOOD.SDR ASAA2019041769015Mount · gougedREF T/C #78472000 #2 ENG INLET AND FAN BLADES - DETAILED INSPT. FOUND START VALVE LWR DUCT MOUNT GOUGED FROM TURNBUCKLE FWD SIDE. GROUNDED - YES. REMOVED AND REPLACED START VALVE LOWER DUCT. REF CFM56-7 P/P BUILDUP MANUAL 71-00-02.SDR ASAA2019022658354Idg · failedENGINE #1 DRIVE ILLUMINATED IN CRUISE. GROUNDED - YES. REMOVED AND REPLACED IDG AIR/OIL COOLER REF B737-800 AMM 24-11-21. REMOVED AND REPLACED #1 IDG REF AMM 24-11-11. LEAK CHECK AND OPS CHECK GOOD.SDR ASAA2019022518309Satcom · lockedSATCOM LOCK-UP. GROUNDED - YES. ACCOMPLISHED RESET PROCEDURE PER ASA 737NG QRH. COMPLETED SUCESSFULY.SDR ASAA201902228280Anti-Ice Valve · intermittentLEFT TAI AMBER LT ON ENGINE DISPLAY CAME ON ITER MD ON CLIMB ENG ANTI ICE SWITCH WAS OFF AND COWL BLUE STATUS LIGHTS WERE EXTINGUISHED TAI AMBER LIGHT WENT OUT AT 9 C ON TAT NOTE APU CONTINUES OPS WITH BLEED SWITCH OFF. GROUNDED - YES. REMOVED AND REPLACED #1 SDR ASAA2019022088233Autothrottle Sys · malfunctionedAUTO THROTTLES WILL NOT ENGAGE. GROUNDED - YES. UNABLE TO DUP/VERIFY DISCREP. A/T FFR SHOWED ASM 2 FAULT LOGGED ON FLT 6. PERFORMED B737-800 FIM 22-31 TASK 801 CURRENT STATUS TEST GOOD NUMEROUS TIMES. PERFORMED FIM 22-31 TASK 824, A/T INTERACTIVE SERVO TEST GOSDR ASAA2019021428214Engine · making metalWHILE ACCOMPLISHING T/C 78472040 FOUND MAGNETIC PARTICLES IN AGB/TGB SCAVENGE MCD ON NR 1 ENGINE. GROUNDED - YES. INSPECTED STARTER MAGNETIC PLUG ON NR 1 ENG FOUND NO MATERIAL ON MAGNETIC PLUG REF AMM 79-00-00-240-001-F00. REMOVED AND REPLACED NR 1 ENGINE REF SDR ASAA201902048015Terminal · brokenENGINE #2 FAILS OVHT/FIRE TEST. GROUNDED - YES. ALTERNATE DEACTIVATION PROCEDURE USED PER CH5 TABLE 3 ITEM 8. ACCOMPLISHED FIM 26-10 TASKS 801 & 805. FOUND RIGHT CORE DETECTOR HARNESS TERMINAL LUG AT M1760 A/1 BROKEN. RE-TERMINATED CONNECTION. ALTERNATE DEACTISDR ASAA2019011927872Processing Unit · failedREF L/P 12046316 FQIS FAULTED PROCESSOR DURING BITE. PROCESSOR FAULT MSG 28-41002 ALSO LOGGED INFLIGHT FLIGHT FAULTS LEG #4. GROUNDED - YES. REMOVED DISCREPANT FUEL PROCESSOR UNIT AND REPLACED WITH SERVICEABLE UNIT. ALL TEST PASS. REF AMM 28-41-81, 28-41-00.SDR ASAA2019011227802Apu · leakingWET SOCK SMELL IN CABIN AND FLT DECK ON CLIMB & DESCENT 5000 FT MSL. APU ON FOR TAKEOFF/ NO BLEED/ APU OFF FOR LANDING. GROUNDED - YES. REMOVED AND REPLACED APU REF T/C 78349010 AND AMM 49-11-00-000-803. OPS CHECK GOOD. ACCOMPLISHED AMM TASK 21-00-01-100-801,O
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