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 ASAA2013070295441Fmc · false indicationDURING TAXI FOR TAKEOFF, RECEIVED AN FMC DISAGREE MESSAGE. ACFT GROUNDED. RAN FMC DISAGREE CHECKLIST IN QRH. MESSAGE CLEARED.SDR ASAA2013062695340Fmc · malfunctionedFMC DISAGREE LIGHT ON GROUND. ACFT GROUNDED. RAN CHECK LIST CLEARED MALFUNCTION.SDR ASAA2013061295089Unknown · unknownNR 2 FIRE SWITCH DID NOT ILLUMINATE ON OVERHEAT FIRE TEST. ACFT GROUNDED. INSPECTED AND PERFORMED ENGINE FIRE DETECTION OPS TEST, REF 26-11-00. NO FAULTS FOUND AFTER SEVERAL TIMES OF OPERATING SYS.SDR ASAA2013052594905Connector · inoperativeIMMEDIATELY FOLLOWING A NORMAL ENGINE START THE NR 2 FILTER BYPASS AMBER LIGHT ILLUMINATED AND ILLUMINATED. ALL ENGINE PARAMETERS NORMAL FOLLOWING ENGINE START. NR 2 ENGINE WAS SHUTDOWN NORMALLY 4 MINUTES AFTER IT WAS STARTED. ACFT GROUNDED. FOUND CONNECTOR SDR ASAA2013052194867Unknown · unknownSATCOM INOPERATIVE ON MCDU, THERE ISNT A MENU SELECTION FOR SATCOM. ACFT GROUNDED. COULD NOT GET SATCOM TO FAIL ON GROUND. SATCOM PROMPT ALWAYS PRESENT IN CDU AND SDU LIGHTS ALL GREEN WITH BOTTOM LIGHT BLINKING AS NORMAL. PERFORMED SATCOM NR 1 & NR 2 TEST SDR ASAA2013051394806Fmc · faultedLEFT FMC AND VTK CRUISE -ROLE ON CAPT FMS. NO OTHER INDICATIONS. VTK WENT AWAY WITHOUT ANY ABNORMAL PROCEDURE ACTION EXECUTED. ALL INDICATIONS NORMAL. POSITION SHIFT PAGE BEARING AND DISTANCE INFORMATION PRESENT LEFT FMC 0.0 DME. RT FMC DME 0.0. ACFT GROUSDR ASAA2013050294690Fmc · failedLEFT FMC FAIL. ACFT GROUNDED. ACCOMPLISHED FMC SYS. BITE IAW FIM TASK 34-61-801. NO FAULTS FOUND IAW FMC SYS. TEST IAW AMM 34-61-00-710-801. OPS CK GOOD ACFT OK FOR SERVICE.SDR ASAA2013040894428Fmc · failedRT NAV DISPLAY SHOWS MAP AND VTK ANNUNCIATION ON PREFLIGHT. R & R NR 2 FMC & PERFORMED SFTWR CONFIG CK & OPS CK ALL IAW AMM 34-61-02. OPS NORMAL. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2013032594260Warning Light · false activationON LANDING, LT PACK LIGHT ILLUMINATED. QRH PROCEDURE PERFORMED, LIGHT STAYED ON. EXTINGUISHED ON SHUTDOWN. ACCOMPLISHED PACK & ZONE TEMP CONTROLLER TEST IAW MM 21-61-00. NO FAULTS FOUND. NO LIGHT ON RECALL. NO HISTORY LAST 30 DAYS.SDR ASAA2013031594174Actuator · inoperativeON W/A FOUND LT RAM AIR DEFLECTOR DOOR NOT DEFLECTING. ACFT GROUNDED. RAN BITE CK OF ZONE TEMP CONTROLLER & FAULTED RAM AIR ACTUATOR & ACTUATOR WOULD NOT RETRACT TO PUSH DOOR OUT. R & R LT RAM AIR DOOR ACTUATOR, REF MM 21-51-21 ADJUSTMENT AND TEST GOOD.SDR ASAA2013022694116Seal · tornNR 1 ENGINE TREND DATA SHOWS A SUDDEN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES HARDWARE INSPECTION AND FAN LUBE REQUIRED. PERFORMED NR 1 ENG FAN BLADE LUBE IAW TC 78472002. DURING FAN BLADE INSPECTION FOUND PLATFORM SEAL POSITISDR ASAA2013021993946Connector · damagedWEATHER RADAR AURAL WARNING GO AROUND WINDSHEAR AHEAD VOLUME MUTED AND TOO QUIET. TEST VOLUME ALSO NOT THE SAME WITH SUBSEQUENT TEST PORTIONS ARE LOUDER THAN OTHERS, BUT NOT EVERY TIME. INTERMITTENT VOLUME CHANGES. FOUND WIRE MISPINNED ON CONNECTOR D189B (WESDR ASAA2013021693907Heat Exchanger · failedLEFT PACK LEAKING BETWEEN HEAT EXCHANGER AND PLENUM. REMOVED LT ACM IAW MM 21-51-04-000-802-002. REMOVED LT HEAT EXCHANGER/PLENUM ASSY IAW MM 21-51-03-000-805-002. REPLACED BOTH (2) PRIMARY AND SECONDARY HEAT EXCHANGERS ASSY IAW MM 21-51-03-400-804-002. RESDR ASAA2013020693878Power Supply · failedEMERGENCY LIGHTS POWER SUPPLY, M1676. R & R POWER SUPPLY AND TEST GOOD IAW AMM 33-51-06-960-806.SDR ASAA2013012993891Angle · corrodedMAIN CABIN LT CUSP INNER ANGLE IS CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 800-53EA-09778 AND REO-G15940, REV A.SDR ASAA2013012993887Seat Track · wornMAIN CABIN BS 520 LBL 24 SEAT TRACK UPPER CROWN IS WORN. CLEANED AREA IAW AMM 20-30-88 , BLEND AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 103, DETAIL A-A, CUT AND TRIMMED DAMAGE SECTION ON SEAT TRACK IAW SRM 53-00-52, FIG 202, LOCATED, DRILLED ASDR ASAA2013012993885Seat Track · wornMAIN CABIN BS 520, RBL 45 SEAT TRACK UPPER CROWN IS WORN. CLEANED AREA IAW 737NG 20-30-88, BLENDED SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 103, DETAIL A-A. CUT AND TRIMMED DAMAGE SEAT TRACK SECTION IAW SRM 53-00-52, FIG 202, PG 109. LOSDR ASAA2013012993883Seat Track · wornMAIN CABIN BS 520, LBL 45 SEAT TRACK UPPER CROWN IS WORN. CLEANED AREA IAW AMM 20-30-88, BLENDED SEAT TRACK AREA, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 103, DETAIL A-A, CUT & TRIMMED LOWER FLANGE OF SEAT TRACK IAW SRM 53-00-52, FIG 102, PG 109. FSDR ASAA2013012893896Door Frame · corrodedL1 DOOR FRAME CORRODED AT BS 303 AT CUSP AREA. REMOVED CORROSION, OUT OF LIMITS IAW SRM 53-00-07, DAMAGE 1, DETAIL C LIMITS, ACCOMPLISHED REPAIR IAW REO-G15946, REV A.SDR ASAA2013012893893Skin · crackedLEFT WING OTBD FLAP L/E VORTEX GENERATOR INBD OF NR 2 FLAP TRACK, SKIN IS CRACKED AROUND PERIMETER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW REO G15938, REV B AND EA CMPT-57EA-09791. PERFORMED HFEC OF CUTOUT IAW NTM 51-00-00 PG 6. NO CRACKS FOUNDSDR ASAA2013012893882Lock Fastener · chafedMAIN CABIN FLOOR, STA 967, 4 EA FLIGHT CONTROL CABLE FEED THROUGH TUBES LOWER LOCK FASTENERS CHAFED. R & R LOCK FASTENERS IAW SRM 51-40-02.SDR ASAA2013012893880Lock Fastener · chafedMAIN CABIN FLOORBEAM LOWER SIDE STA 947.5 HAS FOUR FLIGHT CONTROL CABLE FEED THROUGH TUBES LOWER LOCK FASTENER HEADS CHAFED. ACFT GROUNDED. R & R LOCK FASTENER IAW SRM 51-40-02 CABLES INSPECTED IAW AMM 20-20-31.SDR ASAA2013012793892Skin · corrodedEXTERNAL FUSELAGE SKIN SAFETY VALVE OUTLET CUTOUT CORRODED BS 970. REMOVED CORROSION EXTERNAL FUSELAGE SKIN SAFETY VALVE OUTLET CUTOUT IAW SRM 53-70-01. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01.SDR ASAA2013011693692Window · crackedF/O R2 WINDOW HAS .5" CRACK IN UPPER FORWARD CORNER OF OUTER PANE. REMOVED NR 2 RT SLIDING WINDOW. INSTALLED NEW R2 F/O SLIDING WINDOW REF MM TASK 56-12-11-400-801. OPS CHECKED GOOD AND LEAK CHECKED IAW 78256003, ACCOMPLISHED.SDR ASAA2013011593683Fmc · malfunctionedAPPROX 17.5 E OF OGG VOR. LT FMC FAILED, VTK FLAG APPEARRIED ON CAPTS INBD DU, LT FMC BLANKED AND ROLL QUIDANCE LOST FOR 45 SECONDS FMC RECOVERED ON ITS OWN, QRC FOLLOWED . OPERATED NORMALLY REMAINDER OF FLT. PERFORMED FIM 34-61, TASK 836, NR 1 FMC SHOWS NO SDR ASAA2013011393884Seat Track · wornMAIN CABIN BS 520, RBL 24, SEAT TRACK UPPER CROW IS WORN. CLEANED AREA IAW NG 20-30-88, BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 202. REPAIR 4. CUT AND TRIMMED DAMAGE SECTION OF SEAT TRACK IAW SRM 53-00-52, FIG 202, PG 109. LOCATED, DRSDR ASAA2013010293596Radio · malfunctionedAT APPROX 0300Z, NR 2 HF DISPLAYED NO COMM ON CDU AT 0500Z NR 2 HF AND NO RESPONSE. NR 2 HF INOPERATIVE TRANSMIT AND RECEIVE BOTH VOICE AND DATA. ACFT GROUNDED. PERFORMED HF COMMUNICATION SYS - OPS TEST OM BOTH NR 1 & NR 2 HF SYS, IAW AMM 23-11-00-710-801. SDR ASAA2012122993575Oil System · lowMAINTENANCE LIGHT ILLUMINATED ON APU CONTROL PANEL. ACCOMPLISHED APU BITE PROCEDURE IAW 49-60, TASK 801. FOUND FAULT CODE 49-91227. SERVICED APU OIL. MAINTENANCE LIGHT EXTINGUISHED. APU LEAK & OPS CHECKED GOOD. NO FAULTS DISPLAYED. OK FOR SERVICE.SDR ASAA2012121193442Fmc · failedDUAL FMC FAILURE. PERFORMED FIM 34-61 TASK 836, OPS CHECKED GOOD.SDR ASAA2012112993390Fmc · weakDEPARTED, APPROX 30 MINUTES INTO FLIGHT. LT NAV DISPLAY VTK BOTH FMC CDU WITH ACARS PROMPT. LOSS OF NAV DATA ON L NAV DISPLAY. RT NAV DISPLAY LT NAV INFORMATION REMIAINED. AUTOPILOT TO CWS/CWP. 20-30 SECONDS LATER LT FMC RETURNED TO NORMAL WITHOUT CREW INSDR ASAA2012111093278Fmc · malfunctionedDURING CRUISE, CAPTAIN RECEIVED AN VTK AND LOST FMC. F/O THEN LOST FMC. SELF CORRECTED WITHIN TWO MINUTES ON FINAL, FMC DISAGREE AND AND LANDING SPEEDS IN FMC NOT RIGHT. ALL PERFORMANCE DATA HAD DUMPED WITH BOXES SHOWING ON PERFORMANCE UNIT PAGE. DUAL FMC OSDR ASAA2012100293008Fmc · malfunctionedLEFT FMC INOPERATIVE. QRH FOLLOWED. DID NOT RECEIVE DUAL FMC OPS RESTORED MESSAGE. DUAL FMC OPS RESTORED. NO PREVIOUS HISTORY. OPS CHECKED NORMAL REF AMM 34-61-00. GROUND VERIFICATION CHECKED GOOD.SDR ASAA2012091992916Control Valve · failedIN CLIMB, RT DUCT PSI 38, LT DUCT PSI 15. IN CRUISE FL 380 N1 90 RT DUCT PSI 38, LT DUCT PSI 23. IN DESCENT RT DUCT PSI 30, LT DUCT PSI 28. PERFORMED BLEED AIR HEALTH CHECK USING PNEUMATIC KIT IAW TASK CARD NG-36WC-00001, FOUND PRECOOLER DEFECTIVE. REMOVEDSDR ASAA2012070592502Filter Element · dirtyAPU OIL FILTER INDICATOR SERVICING REQ. R & R APU OIL FILTER, RESET INDICATOR IAW AMM 49-91-13.SDR ASAA2012071992570Circuit Breaker · trippedFOUND WEATHER RADAR RT CIRCUIT BREAKER POPPED. ACFT GROUNDED. ACCOMPLISHED CIRCUIT BREAKER RESET PROCEDURE, NO DEFECTS NOTED REF MM 20-60-01-860-801. RADAR OPS CHECKED NORMAL. REF MM 34-43-020-710-802-001.SDR ASAA2012071192527Regulator · failedUNABLE TO CLOSE BLEED AIR WHEN THE NR 1 ENGINE IS THE AIR SOURCE. ACFT GROUNDED. VERIFIED THAT THE NR 1 ENGINE PRSOV IS CLOSED AND MOVES FREELY. VERIFIED THAT ELECTRICAL ON AND OFF COMMANDS AND GROUNDS CHECK OK. REF FIM 36-10-00-810-802 AND WIRING DIAGRAM 3SDR ASAA2012062192403Sensor · failedON CLIMB OUT AND AFTER LEVEL OFF AT FL370, AIR CONDITIONER DUCT PRESSURE MORE THAN 20 PSI, RT SHOWED 18 PSI, LT SHOWED 42 PSI. ACFT GROUNDED. COMPLETED T/C NG-36WC-00001. FOUND PRECOOLER CONTROL VALVE FAILING STEP 3.F.5. R & R PRECOOLER CONTROL VALVE REF ASDR ASAA2012062192401Keyboard · inoperativeCAPTAINS FMC BRIGHTNESS REOSTAT APPEARS INOP. VERIFIED, R & R CAPTAINS FMC CDU KEYBOARD REF MM 34-61-01-400-801-2, C/B OPEN & CLOSED, OPS NORMAL.SDR ASAA2012062292399Heater · malfunctionedLEFT WINDOW OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF. FOLLOWED QRH SHUT WINDOW HEAT OFF, WAITED 5 MINUTES, TURNED ON AND OVERHEAT LIGHT DID NOT ILLUMINATED. LT SIDE WINDOW WAS VERY HOT TO TOUCH AFTER OVERHEAT LIGHT CAME ON AND FOR 5-10 MINUTES AFTER, BUT TSDR ASAA12511596Sensor · failedAFTER ENGINE START THE FWD OVERHEAT RT CAME ON. ACFT GROUNDED. PERFORM BITE CHECK ON FWD RT (WHCU) FOUND WINDOW SENSOR FAULTY SWITCH TO ALTERNATE SENSOR OVERHEAT LIGHT IS OFF WINDOW HEAT IS WORKING OK FOR SERVICE.SDR ASAA12511442Intercostal · crackedINTERCOSTAL BS 312 TO 328 WL 201, LBL 40 CRACKED. R & R INTERCOSTAL.SDR ASAA12511429Antenna · failed"WX FAIL ANT" & "PWS FAIL" LIGHT DISPLAYED DURING PREFLIGHT ON RADAR. GROUNDED, YES. REPLACED WEATHER RADAR ANTENNA REF MM 34-43-11. OPS CHECKED NORMAL.SDR ASAA12511422Warning Light · false activationRADAR ON FOR APPROX 4 HRS GOT 'WX FAIL" & "PWS FAIL" AND RADAR FAILED. WENT TO TEST LATER BACK TO 'WX/ON" RADAR DISPLAY RETURNED TO NORMAL IN ALL MODES WARNING LIGHTS STAYED OFF. ACFT GROUNDED. WEATHER RADAR TESTED GOOD. PAINTS TARGETS NORMALLY.SDR ASAA12511361Radar · malfunctionedRECEIVED INTERMITTENT WEATHER RADAR FAIL WHEN USING WEATHER MODE. PERFORMED WEATHER RADAR TEST NUMEROUS TIMES AND OCCASIONALLY GOT RADAR TO FAIL AND PWS FAIL. PERFORMED OPERATIONAL TEST PER MM 34-43-00, ALL TEST PASS.SDR ASAA12511272Transceiver · faultyPWS FAIL COMES ON WHEN SWITCHED FROM GROUND POWER. UNABLE TO DUPLICATE FAILURE. REPLACED WEATHER RADAR R/T DUE TO HISTORY REF M/M 34 43 41. OPERATIONAL TEST NORMAL.SDR ASAA12511176Drive Unit · failedWEATHER RADAR FAILED ON GROUND WX FAIL FLAG IN VIEW. ACCOMP WXR SYSTEM OPS TEST, TEST PASSES EVERY TIME. DUE TO HISTORY REPLACED WXR ANTENNA DRIVE UNIT WITH SERVICABLE ONE. ACCOMP WXR SYSTEM OPS TEST, TEST PASS REF M/M 34 43 11 400 801 34 43 11 400 802 34 4SDR ASAA12510926Valve · faultyCABIN CONT ZONE TEMP INOP. PERFORMED FIM 21 62 00 810 833 NR 2 ZONE TEMP CONTROLLER FAULTED THE FLT DECK TRIM AIR VALVE. REPLACED PER SAME. OPS CK GOOD NO FAULTS ON CONTROLLER AFTER CHANGE.SDR ASAA11510866Apu · malfunctionedDUE TO APU EGT ABOVE THE THRESHOLD POWERPLANT ENGINEERING REQUEST THE APU BE REMOVED. REPLACED APU. OPS/LEAK CHECK OK. REF T/C 78349010.SDR ASAA11510838Tube · leakingNR 2 ENGINE SERVO FUEL HEATER LEAKING. REPLACED SERVO FUEL HEATER NR 2 ENG REF MM 73 11 07 400 801. LEAK CHECK GOOD.SDR ASAA11510811Engine · overspeedCLIMBING THROUGH APPROXIMATELY FL 260 PILOTS NOTICED NR 2 ENGINE SURGING IN N1 ACCOMPANIED BY YAW. ENGINE LIMIT/SURGE/STALL CHECKLIST COMPLETED. AS NR 2 THRUST LEVER WAS REDUCED ENGINE CONTINUED TO SURGE TO A LESSER EXTENT UNTIL 1/4 OF THE WAY TOWARDS IDLE W
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