N564AS
Service difficulty reports · 539
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 = 'N564AS' 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 = 'N564AS' 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 ASAA2018070325281Case · corrodedNR 2 ENGINE INLET AND FAN BLADE - DETAILED INSPECTION : FOUND 15 NUTPLATES WITH POSSIBLE CORROSION ON O/B SIDE OF ENGINE FAN CASE BETWEEN B6- B8 FLANGES (M) ENGINE 893738. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE REF SHOP W/O 419621.SDR ASAA2018061865066Fmc · malfunctionedRIGHT FMC FAILED INFLIGHT, ERROR MESSAGE FOR FMCS, SINGLE FMC OPERATION. ACFT GROUNDED. ACCOMPLISHED FIM 34-61, TASK 836. NO DEFECTS NOTED. NORMAL FMC OPS. DEFECT CLEARED.SDR ASAA2018060624893Actuator · leakingA TRANSIT CHECK REVEALED LIQUID LEAKING FROM APU DRAIN MAST. ACFT GROUNDED. REPLACED APU IGV ACTUATOR IAW AMM 49-52-12-000-801, & 49-52-12-400-801. OPS, LEAK, AND BITE CHECKED GOOD.SDR ASAA2018060424885Actuator · failedRIGHT PACK LIGHT ILLUMINATED DURING RECALL. EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. RIGHT PACK PRIMARY TEMP CONTROL SYSTEM INOPERATIVE. CONFIRMED FAULT, NR 2 PACK - ZONE TEMP CONTROLLER BITE TESTED IAW AMM 21-61-00-700-806-002 SHOWS A HARDSDR ASAA2018053192857Display · malfunctionedDURING FLIGHT, INFORMATION ON LESS PAGE DISAPPEARED. BOTH FMC SCREENS DID NOT GO BLANK BUT LINES 1, 2, 3, 4, DISAPPEARED. NO LESS INFO WAS DEPICTED MEANWHILE BOTH ND'S DISPLAYED CURRENT INFO IE MAGENTA LINE, ACTIVE WAYPOINT, DATA ETC IN AN ATTEMPT TO RESTORESDR ASAA2018052974814Warning Message · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL, GOES OUT WITH PUSH TO RESET. ACFT GROUNDED. RESET TEMP VALVE FAULT. ACCOMPLISHED A PACK - ZONE TEMP CONTROL BITE TEST IAW AMM 21-61-00. NO CURRENT FAULTS NOTED. NO HISTORY 30 DAYS.SDR ASAA201805214696Hf Comm · malfunctionedNR 1 HF RADIO DISPLAYS FAILED FLAGS. ACFT GROUNDED. POWER CYCLED SYSTEM. PERFORMED RADIO CHECK, CHECKED GOOD. AIRCRAFT OK FOR SERVICE.SDR ASAA2018041324250Acoustic Panel · damagedNR 2 ENGINE FAN ACOUSTICAL PANEL FASTENERS LOOSE AND WORN, A.L.F., 9 - 10 O'CLOCK FWD UPPER LOCATION AND 10 - 11 O'CLOCK FWD MIDDLE LOCATION. ACFT GROUNDED. REMOVED AND REPLACED 2 WORN FASTENERS; ONE AT 9 - 10 O'CLOCK FWD UPPER LOCATION & ONE AT 10 - 11 O'CLSDR ASAA2018041324249Acoustic Panel · damagedNR 2 ENGINE FAN ACOUSTICAL PANEL AT 7 - 8 O`CLOCK POSITIONS, FWD MIDDLE FASTENERS THROUGH PANEL. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE FAN ACOUSTICAL PANEL IAW AMM 72-23-02.SDR ASAA2018032824057Mount · brokenR/H HEAT EXCHANGER DIFFUSER/PLENUM DUCT ASSY IS BROKEN OFF ITS MOUNT BRACKETS. ACFT GROUNDED. REMOVED AND REPLACED THE RT HEAT EXCHANGER DIFFUSER, PLENUM DUCT ASSY, LEAK AND OPS CHECKED NORMAL IAW AMM 21-51-03.SDR ASAA2018022023608Acoustic Panel · damagedNR 1 ENG INLET AND FAN BLADES-DETAILED INSP. FOUND NR 1 FAN ACOUSTICAL PANEL HAS 1 EACH FASTENER THAT HAS WORN THRU THE PANEL, MIDDLE I/B SIDE. GROUNDED - YES. REMOVED AND REPLACED NR 1 FAN ACOUSTICAL PANEL REF AMM 72-23-07-401.SDR ASAA2018021723584Control Valve · faultedON RECALL, NR 2 PACK LIGHT ILLUMINATED ON MASTER CAUTION, PUSHED TO RESET, LIGHT EXTIGUISHED. GROUNDED - YES. RELEASED PER MEL 21-32B RT HAND PACK PRIMARY TEMP CONTROL IS INOP. PERFORMED B737-800 FIM 21-62 TASK 801 FOUND RIGHT PACK TCV ILLUMINATED. REMOVED SDR ASAA2018020523417Blade · damagedNR 2 ENG (SN 893738) FAN BLADE 6, 21, AND 22 CU-NI DAMAGED BEYOND CONTACT AREA X AND NOT PERMITTED PER AMM 72-21-02-801-F00. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG (SN 893738) FAN BLADE 6, 21, AND 22 AND THEIR MATCHING PAIR PER AMM 72-21-02-802-F00.SDR ASAA2017122723027Stator Vane · leakingRIGHT ENGINE FUEL LEAK, RT VSV DRAIN. ACFT GROUNDED. REMOVED & REPLACED THE RT VSV ACTUATOR ON RT ENGINE IAW AMM 75-31-01-000-802, & AMM 75-31-00-400-802. COMPLETED A RT VSV ACTUATOR LEAK TEST IAW AMM 75-31-00-790-801, STEPS 7E, & F. COMPLETED A NR 2 ENGISDR ASAA2017122223003Pitot Tube · failedFIRST OFFICER`S PITOT LIGHT ILLUMINATED. ACFT GROUNDED. RESET THE CIRCUIT BREAKER AND TESTED, PITOT HEAT STAYS ON AND PITOT PROBE IS COLD. OPENED THE CIRCUIT BREAKER AND COLLARED IAW SP2 WDM 30-31-12, REMOVED AND REPLACED THE FIRST OFFICER'S PITOT PROBE IASDR ASAA2017121522923Control Valve · faultedRT PACK LIGHT ILLUMINATES ON RECALL EXTINGUISHES ON RESET. ACFT GROUNDED. PERFORMED BITE OF THE NR 2 TEMP CONTROLLER, FOUND THE RT PACK TCV FAULTING IAW FIM 21-62 TASK 801. REMOVED AND REPLACED RT PACK TCV IAW AMM 21-51-10, ACCOMPLISHED BITE IAW AMM 21-61-00SDR ASAA2017120122745Unknown · unknownLEFT SIDE WINDOW OVERHEAT GROUNDED - YES. POSSIBLE OVERHEAT LIGHT SHOWING. PERFORMED B737-800 FIM 30-41 TASK 801, BITE TEST. BIT VERIFY, BIT TEST OK (GREEN LIGHT) CAME ON . NO HISTORY IN 30 DAYS. OPS NORMAL.SDR ASAA2017113022742Control Valve · failedRIGHT PACK LIGHT ILLUMINATES AFTER MASTER CAUTION RECALL. GROUNDED - YES. CONFIRMED RT PACK TEMP CONTROL VALVE INOP. REPLACED RT PACK TEMP CONTROL VALVE PER B737-800 AMM 21-51-10-400-801. OPERATED PACK PER AMM 21-00-00-800-803. PERFORMED BITE CHECK PER AMM 21-SDR ASAA2017112022646Indicator · failedNR 1 FUEL QUANTITY INDICATOR ON WING REFUEL PANEL INOPERATIVE. FLIGHT DECK APPEARS NORMAL. ACFT GROUNDED. REPLACED THE FUEL QUANTITY INDICATOR, IAW AMM 28-41-61-000-801. OPS CHECKED NORMAL IAW AMM 28-41-61-400-801.SDR ASAA2017111822615Fire Bottle · shortedON PRE-FLIGHT CARGO DISCH LIGHT ON. GROUNDED - YES. ATTEMPTED TO APPLY MEL 26-19I, MEL MTX PROCEDURE DOES NOT PASS. DISCONNECTED THE NR 1 CARGO FIRE BOTTLE PRESSURE SWITCH CPD12792, DISCHARGE LIGHT EXTINGUISHES. FOUND PIN NR 3 IN THE FIRE BOTTLE SHORTED DIRECTSDR ASAA2017111522600Hf Comm · false indicationHF 2 DISPLAY INDICATED FAILED. ACFT GROUNDED. ACCOMPLISHED FIM 23-11, TASK 803. HF FAIL MESSAGE NO LONGER PRESENT. GROUND VERIFICATION SUCCESSFUL. OK FOR SERVICE.SDR ASAA2017101022174Idg · failedNR 1 GENERATOR AT FL 360, DRIVE LIGHT DID NOT ILLUMINATE. TRIED TO RESET THE GENERATOR IAW QRH BUT DID NOT COME BACK ONLINE. APU STARTED AND POWERED LEFT TRANSFER BUSS FOR REMAINDER OF FLIGHT. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 IDG IAW AMM 24-11-11.SDR ASAA2017081921659Warning Light · false activationMASTER CAUTION ILLUMINATED BRIEFLY AT 1500 AGL. AT ABOUT 700 WE NOTICED ONE AUTOPILOT HAD DISENGAGED WITH NO AURAL WARNING. AUTOPILOT B. GROUNDED - YES. ACCOMPLISHED DFCS BITE IAW FIM TASK 22-11-00-810-801. NO CURRENT FAULTS IN CH A OR B. LEGS 01/02 ON CH A SHSDR ASAA2017081521651Anti-Ice Valve · failedAMBER TAI IS INDICATED ON THE NR 1 ENGINE UPPER DISPLAY, N1 WHEN NR 1 ENGINE ANTI-ICE SWITCH IS TURNED ON. ENGINE BLUE LIGHT COWL VALVE OPEN INDICATES BRIGHT THEN DIM WHEN ANTI-ICE SWITCH IS TURNED ON. ACFT GROUNDED. PERFORMED NR 1 ENGINE COWL TAI VALVE TESSDR ASAA2017070821313Transceiver · failedAIRBORNE, HF1 ACTIVE AND STBY WINDOWS SHOWED FAIL WORKED NORMALY THROUGHT FLIGHT. ACFT GROUNDED. R & R HF 1 TRANSCEIVER IAW AMM 23-11-21.SDR ASAA2017070621307Circuit Breaker · trippedON WALK-AROUND, FOUND WEATHER RADAR CIRCUIT BREAKER TRIPPED (P6-1 D13). ACFT GROUNDED. CHECKED RADAR R/T FOR SECURITY, RESET WEATHER CIRCUIT BREAKER & CHECKED COOLING FAN OPERATION & FOR OBSTRUCTION. NO DEFECT NOTED. OPS NORMAL IAW AMM 34-43-00-710-802-001. SDR ASAA2017062421179Shim · wornWHILE ACCOMPLISHING TASK CARD 78472002, FOUND 24 FAN BLADE SHIMS WORN ON THE NR 2 ENGINE. ACFT GROUNDED. REMOVED AND REPLACED THE FAN BLADE SHIMS.SDR ASAA2017062221155Control Valve · failedRIGHT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL, EXTINGUISHED WHEN RESET. ACFT GROUNDED. RT PACK TCV FAILED BITE TEST IAW AMM 21-61-00-700-806-002 ON NR 2 CONTROLLER. REMOVED AND REPLACED THE RT PACK TCV IAW AMM 21-51-10. LEAK CHECKED AND GROUND VSDR ASAA2017062121153Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED ON RECALL. RESET WITH MASTER CAUTION. ACFT GROUNDED. WHEN TESTED WITH MASTER CAUTION RECALL, PACK LIGHT DID NOT ILLUMINATE. BITE CHECKED ZONE TEMP CONTROLLER SHOWS NO FAULTS. SYSTEM OPS NORMAL IAW AMM 21-61-00.SDR ASAA2017061921122Controller · faultedCABIN ZONE TEMP ILLUMINATED ON RECALL, EXTINGUISHED ON RESET. ACFT GROUNDED. INITIAL INSPECTION FOUND THE NR 2 TEMP CONTROLLER WITH FLIGHT DECK TRIM VALVE RED FAULT LIGHT ON. PERFORMED AMM TASK 21-61-00-700-806-002. RESET AFTER SUCCESSFUL VERIFY TEST. FLISDR ASAA2017060420936Warning Light · false activationAFTER PUSHBACK, THE RIGHT PACK ILLUMINATED ON RECALL. RESET WITH MASTER CAUTION RESET. ACFT GROUNDED. OPS NORMAL IAW AMM 21-61-00.SDR ASAA2017052920906Hmu · failedNR 2 ENGINE VALVE CLOSED LIGHT REMAINS BRIGHT. ACFT GROUNDED. REMOVED & REPLACED THE NR 2 ENGINE HMU IAW TASK CARDS N8473000 & N8473001. TESTED THE NR 2 ENGINE IAW AMM 71-00-00-800-811-F00 TABLE 502. GROUND VERIFICATION REPAIR CONFIRMATION SUCCESSFUL IAW FSDR ASAA2017052920926Water Heater · failedONE HOUR INTO CRUISE AT FL 320, F/A REPORTED FUMES IN BOTH AFT LAVATORIES. OVER TIME FUMES INCREASED IN INTENSITY AND F/A REPORTED EYE IRRITATION AND HEADACHES. ACFT GROUNDED. ACCOMPLISHED CABIN ODOR TROUBLESHOOTING IAW AMM 05-51 TASK 814 CONDITIONAL INSPECSDR ASAA2017052920918Lubrication Unit · leakingREPORT OF THE NR 2 ENGINE LEAKING OIL FROM TAIL PIPE. ACFT GROUNDED. REMOVED AND REINSTALLED SERVICEABLE LUBRICATION UNIT IAW AMM TASK 79-21-01-000-801-F00, AND TASK 79-21-01-400-801-F00. ACCOMPLISHED LUBE UNIT INSTALL TEST IAW AMM 71-00-00-800-811-F00, TEST SDR ASAA2017032420259Control Panel · intermittentMODE CONTROL PANEL BACKGROUND LIGHTING ON CAPTAIN'S SIDE INTERMITTENT. GROUNDED - YES. REPLACED MODE CONTROL PANEL, REF AMM 22-11-34-000-801 AND 22-11-34-400-801. TESTED, REF AMM 22-11-34-740-801. TESTS OK. PERFORMED REQUIRED LWMP TESTS, REF AMM 22-00-01 LWMP SDR ASAA2017031720191Warning Message · false activationRIGHT PACK LIGHT ILLUMINATED ON RECALL. YELLOW MASTER CAUTION LIGHT EXTINGUISHED WHEN RESET IS PRESSED. ACFT GROUNDED. NR 2 ZONE CONT LOGGED A TCV FAULT, FAULT CLEARED & TESTED NORMAL IAW AMM 21-61-00. RAN PACK, SYSTEM OPS NORMAL.SDR ASAA2017020119638Case · crackedNR 1 ENGINE FAN INLET CASE HAS CRACK AT B1 FLANGE 11:30 O'CLOCK AFT LOOKING FWD AT FIRE DETECTOR BRACKET. ACFT GROUNDED. COMPLETED REWORK OF FAN CASE REF TASK CARD SBCFM56-7B ASA 36205.SDR ASAA2017012019630Regulator · failedDURING CLIMB FROM FL 360 TO 370 A DUCT PRESSURE SHOWED 23 PSI DIFFERENCE. LEFT DUCT 27 PSI, RIGHT DUCT 50 PSI. AT CRUISE FL 370 DUCT PRESSURE SHOWED 7 PSI DIFFERENCE, LEFT DUCT 35 PSI, RIGHT DUCT 42 PSI. ACFT GROUNDED. PRECOOLER CONTROL VALVE FAILED HEALTHSDR ASAA2017011119322Pump · failedTHE NR 1 AFT BOOST PUMP LIGHT ILLUMINATED WITH SWITCH ON. ACFT GROUNDED. FOUND THE CIRCUIT BREAKER CLOSED, BUT CFI OPEN WITH WHITE BAND SHOWING. RESET THE GFI, LIGHT EXTINGUISHED THEN REILLUMINATED. WHITE BAND IS SHOWING ON GFI. AFTER GFI RESET , LOW PRESSSDR ASAA2016122319150Fmc · malfunctionedFMC DISAGREE INFO ONLY COMPLIED WITH QRH MESSAGE NO LONGER DISPLAYED. ACFT GROUNDED. PERFORMED FIM 34-61 TASK 838. RESET FMCS CHECKED DATA LINK FOR VHF AND SATCOM DATA LINK TEST OK. NO DEFECTS NOTED IAW FIM 34-61 TASK 838.SDR ASAA2016121319027Start Valve · failedNR 2 ENGINE HAD NO ROTATION DURING START. STARTER VALVE FAILED. ACFT GROUNDED. REMOVED & REPLACED THE NR 2 STARTER VALVE IAW AMM 80-11-03-000-801-F00 & 80-11-03-400-801-F00. OPS CHECKED GOOD.SDR ASAA2016120919013Probe · out of toleranceNR 1 ENGINE ECONOMIC MESSAGE 77-20871 "THE TOP LEFT EGT SIGNAL (T495S4) IS OUT OF RANGE." GROUNDED - YES. ACCOMPLISHED EEC BITE - FAULT PRESENT ALL FLIGHT LEGS. REMOVED & REPLACED T49.5 S4 PROBE. OPS GOOD, REF AMM 77-21-01/401.SDR ASAA2016120818984Valve · failedNR 2 ENGINE AMBER TAI ANNUNCIATOR ILLUMINATED AT CRUISE. NO CHANGE IN N1, EGT, OR N2. DURING DECENT, THE TAI OPERATED NORMAL. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE TAI VALVE IAW AMM TASK 30-21-11-000-801 PAGES 1-5, AND AMM TASK 30-21-11-400-801SDR ASAA2016120218916Transceiver · failedRADAR HAS BEEN GIVING FALSE RETURNS AT FL390, 10 AND 2 OCLOCK POSITION AT ABOUT 5 MILES CONSISTENTLY COMES AND GOES. ACFT GROUNDED. REMOVED AND REPLACED THE RADAR TRANSCEIVER IAW AMM 34-43-41. OPS CHECKED GOOD.SDR ASAA2016112419266Wire Harness · faultedFOUND FAULT CODE 77-20871 THE TOP LEFT EGT SIGNAL (T495S4) IS OUT OF RANGE FOR NR 1 ENGINE. ECONOMIC FAULT. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE CJ10 HARNESS IAW AMM 73-21-06-400-803-F00 & FADEC SYSTEM TESTED GOOD IAW AMM 73-21-00-700-F00.SDR ASAA2016112319207Compensator · out of toleranceENGINEERING REQUEST CHECK NR 2 (RIGHT) FUEL TANK UNIT AND COMPENSATOR VALUES. GROUNDED - YES. REF T/C NG-28FCD-18090-1, REMOVED AND REPLACED TANK 2 F8, F9 AND F10 TANK PROBES, REF AMM 28-41-21-400-801. REMOVED AND REPLACED TANK NR 2 F1 AND F15, REF AMM 28-41-2SDR ASAA2016112318809Hf Comm · malfunctionedNR 1 HF FAIL ILLUMINATED IN BOTH FREQUENCY WINDOWS. ACFT GROUNDED. FOUND FAIL MESSAGE CAPTAINS RADIO TUNING PANEL. PERFORMED FIM 23-12 TASK 815. RESET POWER ON RADIO TUNING PANEL AND HF SYSTEM FAULT CLEARED. PERFORMED GROUND VERIFICATION CHECK, GROUND VERIFISDR ASAA2016102518474Actuator · failedRIGHT AC PACK LIGHT ILLUMINATES ON RECALL, EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. REMOVED AND REPLACED RAM AIR DOOR ACTUATOR ASSY, OPS CHECKED GOOD, IAW AMM 21-51-21.SDR ASAA2016102318464Warning Light · false activationDURING RECALL, RT PACK LIGHT ILLUMINATED. LIGHT EXTINGUISHED WHEN MASTER CAUTION RESET. ACFT GROUNDED. THE NR 2 ZONE CONT LOGGED 'RAM AIR ACT' FAULT, FAULT CLEARED & CHECKED NORMAL IAW AMM 21-61-00, GROUND VERIFICATION SUCCESSFUL.SDR ASAA2016101218411Floor Support · crackedFWD CAROG FLOOR SUPPORT BS 500E - 500F IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, DWG 143A7502 REV - , SRM 51-40-05, AND SRM 51-40-02.
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