N566AS

Service difficulty reports · 575

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 = 'N566AS' 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 ASAA11510153Antenna · malfunctionedPWS FAULT ON CA / FO ND'S. UNABLE TO DUPLICATE DUE TO HISTORY REPLACED WEATHER RADAR ANTENNA REF MM 34 43 11. WXR SYSTEM OPERATIONAL TEST PASSED.Jul 21, 2011 · N566AS · Boeing 737890 · Weather Radar SystemSDR ASAA11510133Transceiver · faultyWXR FAIL AND PWS FAIL FLAGS DISPLAYED ON BOTH NAV DISPLAYS. CONFIRMED PROBLEM. REPLACED WXR R/T REF MM 34 43 41. OPS NORMAL REF MM 34 43 00. ETOPS GND VERIFICATION SUCCESFUL.Jul 18, 2011 · N566AS · Boeing 737890 · Weather Radar SystemSDR ASAA11510017Battery · defectiveMAIN AIRCRAFT BATTERY INDICATED NR 2 AMPS 27 28 VOLTS FOR ENTERING FLIGHT (2 + 20 HRS). AUX BATT INDICATED 0 AMPS 27 VOLTS AND ALL OTHER ELECTRIC SYSTEMS ARE INDICATING NORMAL. REPLACED BOTH BATTERIES PER MM 24 31 11. INSTALLATION TEST GOOD PER MM 24 31 11.Jul 6, 2011 · N566AS · Boeing 737890 · Battery/Charger SystemSDR ASAA1159906Sensor · failedAPU AIR SHUT OFF WITH SWITCH IN THE ON POSITION NO OTHER INDICATIONS OF ABNORMAL AIR SYSTEM. RAN APU W/ FULL LOAD ON ELEC & AIR BOTH PACKS ON. APU BLEED SW. OPS NORMAL W/ GOOD INDICATIONS. TSR ISSUED. REPLACED APU TOTAL PRESSURE SENSOR PER AMM 49 52 32 OPS Jun 20, 2011 · N566AS · Boeing 737890 · APU Bleed Air SystemSDR ASAA1159893Bleed Air Sys · malfunctionedAFTER SHUTDOWN ATTEMPTED TO APPLY AIR CONDITIONING WITH APU INITIALLY. APU BLEED AIR SWITCH APPEARED NOT TO WORK. NO AIR WITH APU BLEED SWITCH ON. PERFORMED CURRENT STATES BITE NO FAULTS NOTED AND A FAULT HISTORY BITE NO FAULTS FOUND AND A MAINTENANCE HISTOJun 19, 2011 · N566AS · Boeing 737890 · APU Bleed Air SystemSDR ASAA1159889Bleed Air Sys · malfunctionedSTARTED APU IN SAN ELEC OK NO AIR PRESSURE WHEN APU BLEED OPEN. PERFORMED BITE TEST ON APU REF MM 49 61 00, NO FAULTS FOUND. RESTARTED APU AND APU BLEED WORKS NORMAL REF MM 49 11 00. NO HISTORY FOR 30 DAYS, GROUND VERIFICATION SATISFACTORY OK FOR SERVICE.Jun 17, 2011 · N566AS · Boeing 737890 · APU Bleed Air SystemSDR ASAA1159868Unknown · malfunctionedPWS FAIL LIGHT ILLUMINATED. RESET WEATHER RADAR C/B IAW B737NG AMM 20 60 05. SYSTEM CHECKS GOOD IAW B737NG FIM 34 43 00 810 815.Jun 13, 2011 · N566AS · Boeing 737890 · Weather Radar SystemSDR ASAA1159696Sensor · malfunctionedON CLIMBOUT APU FAULT LIGHT & MASTER CAUTION ILLUMINATED FOLLOWED QRH CONTACTED MX CONTROL & DISPATCH AGREED AFTER 5 MIN RESTART APU IF FAULT LIGHT GOES OUT. AFTER FAULT LIGHT WENT OUT RESTARTED APU, APU STARTED NORMALLY & WAS AVAILABLE. FOUND MAINT MSG 49-5May 28, 2011 · N566AS · Boeing 737890 · APU Bleed Air SystemSDR ASAA1159689Unknown · malfunctionedAFTER DE-ICE CONFIGURED TO START AND HAVE NO APU AIR. TESTED APU PER AMM 49 11 00 710 801. NO FAULTS FOUND. APU AIR SUPPLY OPERATES NORMAL. THERE IS NO MAINTENANCE HISTORY WITHIN PAST 30 DAYS.May 25, 2011 · N566AS · Boeing 737890 · APU Bleed Air SystemSDR ASAA1159649Connector · looseDURING ETOPS PDC FOUND NR 1 ENG DRIVEN HYDRAULIC PUMP DEPRESSURIZATION SOLENOID CONNECTOR LOOSE. REMOVED CONNECTOR, CLEANED & RESECURED. FUNCTIONAL CHECK GOOD.May 15, 2011 · N566AS · Boeing 737890 · Hydraulic Power System WiringSDR ASAA1159494Switch · inoperativeWHILE PERFORMING WORK CARD T/C 7827300 FOUND MESSAGE NUMBER 73 20312. THE START SWITCH SIGNAL AND AIRINC DATA BUS DISAGREE SHORT TIME FAULT NR 2 ENGINE. PERFORMED FIM 73 24 00 810 813 AND REMOVED AND REPLACED ENGINE START SWITCH AND TEST GOOD IAW AMM 80 11 0Apr 17, 2011 · N566AS · Boeing 737890 · Engine CrankingSDR ASAA1159413Battery · defectiveAUX BATTERY READING 2 AMPS DRAW. PERFORMED AUX BATTERY CHARGER OPERATIONAL TEST PER M/M 24 31 31 710 801 TESTS WITHIN LIMITS. AUX BATTERY STILL 27 VOLTS 2 AMP CHARGE. REPLACED AUX BATTERY REF M/M 24 31 11 TEST NORMAL. AFTER APPROX 20 MINUTES AUX BATTRY REApr 10, 2011 · N566AS · Boeing 737890 · Glide Slope SystemSDR ASAA1159063Panel · damagedMCP IAS/MACH WINDOW BACKGROUND HAS CHIPS ALLOWING BACKLIGHTING TO SHINE THROUGH SMALL CHIPS DOES NOT INTERFERE WITH OPERATION. DUPLICATED DEFECT. REPLACED DFCS MCP REF MM 22 11 34, OPS CHECK NML. ALSO ACCOMP DFCS LRU MCP #32 TEST LAND VERIFY NR 49 TEST AND Feb 21, 2011 · N566AS · Boeing 737890 · Autopilot ComputerSDR ASAA1158988Unknown · malfunctionedON PRACTICE AUTOLAND INTO FAI THE AUTOLAND FUNCTION WAS OUT OF LIMITS TO THE LEFT OF CENTER LINE UPON TOUCHDOWN. HUD APPEARED NORMAL. COULD NOT DUPLICATE. ACCOMP FIM:22 11/825 LAND VERIFY TEST CK NML NO FAULTS & PRECAUTIONARY PERFORMED ILS SYSTEM TEST REF MFeb 7, 2011 · N566AS · Boeing 737890 · Autopilot SystemSDR ASAA1158964Regulator · faultyFL 320 N1'S 84.9 PERCENT LEFT DUCT PRESSURE 42 PSI R DUCT PRESS 20 PSI. PACK AUTO NORMAL PRESSURE. PERFORMED ENG BLEED AIR HEALTH CHECK ON NR 2 ENG REF AMM 36 11 00. FOUND PRECOOLER CONT VALVE "KISS" SEAL LEAKING. REMOVED AND REPLACED KISS SEAL REF AMM 36 1Feb 2, 2011 · N566AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1158791Unknown · malfunctionedZONE TEMP CONTROL CABIN LIGHT ILLUMINATES ON RECALL. EXTINGUISHES UPON MASTER CAUTION LIGHT PUSHED. TROUBLESHOT PER FIM TASK 21 62 00 810 848. BITE 21 62 00 810 801 VERIFICATION SHOWS NO CURRENT FAULTS. VERIFIED PACK OPERATION ALL ZONE TEMP LIGHTS REMAIN EJan 15, 2011 · N566AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1158743Autoland Sys · malfunctionedAUTOLAND UNSUCCESSFUL AIRCRAFT LINED UP ON APPROACH LIGHTS & RUNWAY CENTERLINE. DURING THE LAST 20FT IT STARTED TO DRIFTING LEFT WITHOUT CORRECTING TO RUNWAY CENTERLINE TOUCHED DOWN ON LEFT HALF OF RUNWAY & DRIFT CONTINUED. CAPT INTERVENED TO RETURN AIRCRAFJan 9, 2011 · N566AS · Boeing 737890 · Autopilot SystemSDR ASAA1058262Tape · looseLOOSE ANTISKATE FOIL FOUND ON AFT GATE OF OUT FLOW VALVE. REMOVED LOOSE ANTISKATE FOIL FROM OUT FLOW VALVE IAW EA 2130 01028 REV B. MAY CONTINUE IN REVENUE SERVICE WITH NO TIME LIMITATION. SEAMC CONTACTED.Sep 11, 2010 · N566AS · Boeing 737890 · Pressure Regulator/Outflow ValveSDR ASAA1058251Wire Harness · defectiveON TAXI IN 1 FUEL "FILTER BYPASS" LIGHT ILLUMINATED. FOUND PRESS SW CONN NOT FULLY SEATED SELF LOCKING MECH JAMMED AND RECESSED PIN 3. REPLACED J 8 HARNESS ON NR 1 ENG EEC OPS CHECK GOOD PER MM 73 21 00 700. PERFORMED ACTUATORS TEST OPS NORMAL REF MM 71 00 Sep 4, 2010 · N566AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA1058217Unknown · malfunctionedFOUND LONG TERM FAULT 73-31071 "THE FUEL FILTER SIGNALS DISAGREE" WHILE ACCOMPLISHING FMC CDU INTERROGATION ON NR 1 ENGINE. PERFORMED T/C 78273000 NO FAULTS FOUND. OPS NORMAL.Aug 20, 2010 · N566AS · Boeing 737890 · Engine Fuel Indicating SystemSDR ASAA1058118Warning System · malfunctionedAFTER APU START THE BLUE APU "MAINT" LIGHT WAS ILLUMINATED. ACCOMPLISHED TASK 49 11 00 APU OPERATIONAL TEST NO FAULTS FOUND, OPS CHECK NORMAL. NO MESSAGES ON CURRENT STATUS OF BITE TEST.Jul 31, 2010 · N566AS · Boeing 737890 · APU Indicating SystemSDR ASAA1058053Keypad · intermittentF/O SIDE FMC/CDU HAS INTERMITTENT PROBLEM WITH LINE SELECT KEY 2L. WHEN PUSHED THE KEY DOES NOT ALWAYS WORK. VERIFIED FAULT. REPLACED F/O MCDU. SYS TESTS GOOD REF TASK 34 61 01 400 802.Jul 11, 2010 · N566AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1057997Warning System · malfunctionedON PREFLIGHT FOUND "ELEC" LIGHT ON OVERHEAD PANEL. PERFORMED FIM TASK 24 31 00 ELEC LIGHT BIT PROCEDURE FOUND TO BE INTERMITTENT FAULTS CLEARED FAULTS ACCOMPLISHED BIT CHECK NO CURRENT FAULTS NOTED GROUND VERIFICATION SUCCESSFUL.Jun 20, 2010 · N566AS · Boeing 737890 · DC Indicating SystemSDR ASAA1057928Unknown · malfunctionedLEFT FMC FAILURE SHORTLY AFTER LEVEL OFF AT FL390. VTK AND MAP CAUTION FLAGS ON CAPTAINS MAIN NAVIGATION DISPLAY PANEL. FOLLOWED QRH PROCEDURE PLACING THE FMC SWITCH ON THE OVERHEAD PANEL TO BOTH FMC'S ON RIGHT. VTK AND MAP FLAGS EXTINGUISHED AND NORMAL OPSJun 14, 2010 · N566AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1057861Anti-Ice System · malfunctionedON DESCENT INTO OGG RIGHT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURE OVERHEAT LIGHT EXTINGUISHED AND REMAINED OUT. ACFT GROUNDED. PERFORMED WINDOW HEAT CONTROL UNIT TEST PER AMM 30 41 11 710 801. NO DEFECTS NOTED SYSTEM OPS NORMALMay 23, 2010 · N566AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA1057849Filter · brokenFWD PAX CABIN TEMP SENSOR GRILL IS BROKEN. REMOVED & REPLACED FWD PAX CABIN TEMP SENSOR GRILL REF MM 21 61 06 400 801. GROUND VERIFICATION IS COMPLETE.May 21, 2010 · N566AS · Boeing 737890 · Cabin Temperature SensorSDR ASAA1057824Eec · faultyNO EGT RISE AFTER START LEVER RAISED TO IDLE. GROUNDED YES. REPLACED NR 1 EEC REF AMM 73 21 60. OPS NORMAL.May 16, 2010 · N566AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA1057754Control Valve · faultyON RECALL AFTER ENGINE START THE AIR COND LIGHT ILLUMINATED ALONG WITH THE PACK LIGHT FOR THE RIGHT AC SYSTEM. COMPLIED WITH QRH CHECKLIST, LIGHTS EXTINGUISHED. FOUND RT ZONE TEMP CONTROLLER WITH RT PACK TCV FAULT. REMOVED AND REPLACED TCV RT PACK, OPS CHECApr 25, 2010 · N566AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1057753Exciter · faultyNR 1 ENG FAILED TO LIGHT OFF AFTER FUEL LEVER BROUGHT TO IDLE. ALL N1 N2 AND OIL PRESSURE INDICATIONS WERE NORMAL. INITIAL FUEL FLOW OF 1500LBS THEN DROPPED BACK TO 500LBS THEN 0 WITH NO LIGHT OFF. IGNITION SWITCH WAS ON RIGHT. ACCOMPLISHED FIM TASK 74 21 Apr 24, 2010 · N566AS · Boeing 737890 · ExciterSDR ASAA1057616Unknown · malfunctionedWHILE STARTING ENGINE NR 1 NO FUEL FLOWS OBSERVED AFTER START. LEVER RAISED FROM IDLE N2 HUNG BETWEEN 33 35 DURING 2 ATTEMPTS. TESTED (AUDIBLE TEST) OF NR 1 ENG RT 810 IGNITION SYS REF 74 21 00 810 807 F10 AND AMM 74 00 00 750 801 FOO. OPS CHECK GOOD. NO FMar 26, 2010 · N566AS · Boeing 737890 · Ignition SystemSDR ASAA1057605Controller · faultyRIGHT PACK LIGHT ILLUMINATES WITH RECALL RESETS WITH MASTER CAUTION. TSR ISSUED. REPLACED THE AACU REF MM 21 51 02, OPS CHECK NORMAL. REPLACED THE NR 2 PACK ZONE TEMP CONTROLLER. ACCOMPLISHED BITE OF NR 2 TEMP CONTROLLER REF MM 21 51 00, NO FAULTS. REPLACMar 24, 2010 · N566AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1057555Autoland Sys · malfunctionedAPP SURVEY AUTO LAND UNSUCCESSFUL. PERFORMED AUTO LAND VERIFY TEST PER MM 22 03 10/101. ALL TESTS PASSED. A/C REMAINS CAT IIIA AUTO LAND QUALIFIED.Mar 20, 2010 · N566AS · Boeing 737890 · Autopilot SystemSDR ASAA1057544Spring · bindingON THE LANDING CHECK MASTER RECALL RIGHT PACK ILLUMINATED WENT OUT ON PRESS TO RESET. WAS ABLE TO REPEAT STICKING/BINDING DURING DEFLECTOR DOOR OPERATION. FOUND THE DOOR CLOSING SPRING BINDING ON THE DEFLECTOR DOOR ACTUATING SHAFT. RE-ASSEMBLED THE DEFLECTOMar 12, 2010 · N566AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1057514Actuator · out of adjustRIGHT PACK TRIP LIGHT COMES ON DURING RECALL ONLY EXTINGUISHERS WITH MASTER CAUTION RESET. PERFORMED PACK/ZONE TEMP CONTROL BITE TEST FOUND ACT FAULT LIGHT. CHECKED AND FOUND DEFLECTOR DOOR OUT OF ADJUSTMENT. ADJUSTED DEFLECTOR DOOR REF AMM 21-51-22. PERFOMar 10, 2010 · N566AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1057492Controller · intermittentRIGHT PACK LIGHT ILLUMINATES ON RECALL RESETS WHEN MASTER CAUTION IS RESET. PERFORMED PACK /ZONE TEMP CONTROLLER BITE TEST PER M/M 21 61 00 ON NR 2 CONTROLLER CONFIRMED FAULT FOUND INTERMITTENT FAULT ON RAM AIR ACTUATOR REPLACED SAME PER M/M 21 51 21. STILL Mar 5, 2010 · N566AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1057491Control Valve · malfunctionedRT PACK LIGHT ILLUMINATES ON MASTER RECALL. RESETS WITH MASTER CAUTION RESET. ACCOMPLISHED REV S/P 21 5C BY RE-ACTIVATED RAM AIR MODULATION SYSTEM PER MM 21 00 00/901. PERFORMED BITE ON NR 2 ZONE TEMP CONTROLLER AND FOUND THIS PACK TCV FAULTY. REPLACED RIGMar 4, 2010 · N566AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1057388Fmc · failedFMC FAULT. "CHECK FMC TO FMC" MESSAGE. RIGHT FMC WOULD NOT UPDATE POSITION. LENGTH OF DIVERSION 28 MINUTES. DUPLICATED FAULT RT FMC COMP WOULD NOT ACCEPT ANY S/W LOADS. REPLACED RT FMC REF MM 34 61 02, OPS CHECK NORMAL AND ALL S/W CHECK OK.Feb 15, 2010 · N566AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1057364Unknown · malfunctionedWHILE PERFORMING T/C 78273000 ENG FMC CDU FAULTS FOUND FAULT CODE 77 20872 THE TOP LEFT EGT SIGNAL (T495S4) IS OUT OF RANGE LONG TERM FAULT FOR NR 2 ENGINE ESN895406. ON DEFERRAL.Feb 9, 2010 · N566AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA1057360Unknown · malfunctionedWHILE PERFORMING T/C 78273000 ENG FMC CDU FAULTS FOUND FAULT CODE 77 20872 THE TOP LEFT EGT SIGNAL (T495S4) IS OUT OF RANGE LONG TERM FAULT FOR NR 2 ENGINE. ON DEFERRAL.Feb 9, 2010 · N566AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA0957163Support Angle · crackedOUTBOARD AFT RAM AIR INLET SUPPORT ANGLE IS CRACKED. REMOVED FABRICATED AND INSTALLED NEW ANGLE.Dec 23, 2009 · N566AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA0957164Skin · dentedRIGHT WING NR 7 SPOILER LOWER SKIN SURFACE HAS SEVERAL DENTED AREAS.Dec 23, 2009 · N566AS · Boeing 737890 · SpoilersSDR ASAA0956869Indicator · activatedFOUND APU OIL FILTER DELTA P INDICATOR EXTENDED. REMOVED AND REPLACED APU OIL FILTER AND PERFORMED OIL FILTER INDICATOR SERVICING PER AMM 49 91 13. PERFORMED APU RUN-UP PER AMM 49 11 00, NO LEAKS NOTED AND DPI STAYED DEPRESSED.Oct 27, 2009 · N566AS · Boeing 737890 · APU Oil SystemSDR ASAA0956810Wire · damagedRT FWD WINDOW OVERHEAT LIGHT ILLUMINATED WITH ASSOCIATED WARNINGS. CB WINDOW CONTROL POPPED. AIRCRAFT WAS FL 40.0 2 HOURS AND 20 MINUTES INTO FLIGHT. PERFORMED FIM TASK 30 41 TASK 813. FOUND BAD CRIMP ON TERMINAL AT C/B 394 ON LOAD SIDE. REPLACED C/B AND Oct 14, 2009 · N566AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA0956809Terminal · looseRIGHT FWD WINDOW OVERHEAT LIGHT ILLUMINATED. C/B P6 12 B8 POPPED. FOUND RT FRONT WINDOW HEAT PWR C/B OUT. R1 TEMP CONTROLLER SHOWS BUS POWER FAULT. FOUND UPPER I/B GND TERM AT R1 WINDOW LOOSE. SECURED SAME. RESET C/B. OPS CHECK WINDOW HEAT (R1) GOOD. BOct 14, 2009 · N566AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA0956793Outflow Valve · failedSHORTLY AFTER TAKEOFF AUTOFAIL LIGHT ON OVERHEAD PRESSURIZATION CONTROL PANEL ILLUMINATED. CHECKLIST ACCOMPLISHED AND OPERATED IN ALTN MODE. CB FOR AUTO CONTROLLER 2 IS POPPED GROUNDED YES. CONFIRMED FAULT. NR 2 AUTO MODE MOTOR ON OUTFLOW VALVE OPS C/B REFOct 12, 2009 · N566AS · Boeing 737890 · Pressure Regulator/Outflow ValveSDR ASAA0956711Stator · out of toleranceNR 2 ENGINE SHOWS FMC CDU SHORT TIME FAULT CODE 73-21272 "THE ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE". PLT DEFERRED MAINT. REPLACED STATOR ALTERNATOR AND ROTOR ALTERNATOR REF MM 73-21-08-000-801-F00. REQ TESTS 13-3A ACCOMPLISHED INSTALLATION OFSep 28, 2009 · N566AS · Boeing 737890 · AC Generation SystemSDR ASAA0956696Unknown · malfunctionedREF TC 78273000 NR 2 ENGINE SHOWS FMC CDU SHORT TIME FAULT CODE 73 21272 "THE ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE". REF FIM TASK 73 27 00 810 804 FOO REPAIR CONFIRMATION SHOWS NO FAULTS. MAINT HISTORY ON FMC CDU SHOWS ONLY ON ORIGINAL LEG. NSep 23, 2009 · N566AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA0956655Warning System · malfunctioned"INFO ONLY" ON TAXI OUT FMC DISAGREE ANNUNCIATED ON BOTH INBOARD DU'S. QRH PROCEDURE ACCOMPLISHED AND BOTH FMC'S NORMAL FOR DEPARTURE. PILOTS ACCOMPLISHED QRH PROCEDURE BOTH FMC'S NORMAL FOR DEPARTURE. INFO NOTED.Sep 22, 2009 · N566AS · Boeing 737890 · Central WarningSDR ASAA0956649Unknown · malfunctionedDESCENT BELOW 10K IN VNAV PATH F/O'S TARGET BUG PROGRAMMED TO 240 KIAS (CORRECT) CAPT'S TARGET BUG DROPPED TO APPROX 205 KIAS BUGS AGREED IN LVL CNG & V/S MODES. PERFORMED AUTOPILOT FLT FAULT REVIEW NO FAILURES LOGGED. ADRU BITE CHECKS NORMAL. SMC HAVE LOGGSep 19, 2009 · N566AS · Boeing 737890 · Autopilot SystemSDR ASAA0956581Hf Comm · malfunctionedNR 2 HF RADIO INOP. VERIFIED NR 2 HF SHOWED FAIL ON CONTROL HEAD. NO HISTORY PERFORMED NR 2 HF BITE WITH NO FAULTS. VERIFIED COMMUNICATIONS WITH SFO ARINC REF 23 11 0, NO CURRENT FAULTS NOTED.Sep 9, 2009 · N566AS · Boeing 737890 · HF Communications System
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