JASC 2210

Service difficulty reports · 4,017

Reports filed under 2210 · Autopilot System, 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 jasc_code = '2210'
  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 ASAA1057199Circuit Breaker · trippedCAPTAIN EADI FD FLAG IN VIEW. FOUND AFCS "WARN / LIGHT BAT" C/B OUT. RESET SAME REF MM 20 60 01. PULLED & RESET "A" CHANNEL AFCS DC C/B. OPS CHECK "A" CHANNEL FCC GOOD. REF MM 22 11 33/401 DFCS BITE GP 35 PASS.Jan 4, 2010 · N559AS · Boeing 737890SDR CA100117007Autopilot Sys · malfunctioned(CAN) THE EVENT OCCURRED WHILE THE ACFT WAS FLYING WITH AUTO PILOT ON AND IN VERY TURBULENT CONDITION. AS A RESULT OF THE TURBULENT CONDITION THE PILOT CHANGED DIRECTION WITH AUTO PILOT STILL ON. A WARNING MESSAGE CAME ON INDICATING THE PILOT WAS ACTING AGAIDec 24, 2009SDR AALA20091223BOS01Yaw Damper · failedCREW REPORTED AIRCRAFT YAWING SIGNIFICANTLY. INHIBITED YAW DAMPER AND DE-PRESSURIZED RUDDER SYSTEM. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. REPLACED YAW DAMPER ACTUATOR.Dec 23, 2009 · N495AA · Doug DC982SDR CA091221007Selector · inaccurate(CAN) COMMENCING GPS OVERLAY FOR 09 IN YXE, CLEARED TO 3200 FT AND VECTORED THROUGH THE LOC, UPON REINTERCEPTION THE ALERTER CHIMED 1000 FT ABOVE ACKNOWLEDGED CHIME BY PUSHING IT IN, BUT WHEN PUSHED, IT RESET ITSELF TO 2000 FT, SO AT THAT POINT THE ACFT DID A Dec 17, 2009 · Beech B200SDR REXA200900133Yaw Damper · malfunctionedCONSTANT OSCILLATION WITH AUTO PILOT ON. REMOVED AND REPLACED LT AND RT YAW DAMPER IAW AMM 22-22-01 FOUND RUDDER POSITION TRANSMITTER TO BE MISS RIGGED. RE-RIGGED IAW AMM 27-21-0 5, OPS CHECK GOOD.Dec 13, 2009 · N8894A · Cndair CL6002B19SDR IPXA09557970Computer · inoperativeASA DISPLAY OF NO LAND 3 AT 10000'. NO ADDITIONAL EICAS MSG. ACCOMPLISHED MCDP LAST FLIGHT AND "NO LAND 3 AIL SRVO/FCC L" MSG. DEFERRED L FCC IAW MEL 22-10-1-1-2, DMP ACCOMPLISHED. R & R LT FCC IAW AMM 22-11-01-4. OPS CHECK NORMAL.Dec 3, 2009 · N462UP · Boeing 75724APFSDR IPXA09557971Control Panel · odorINSPECTION TYPE:N/A DURING FLIGHT, FAINT ELECTRICAL SMELL WITH LEFT & CENTER FLT DIRECTOR INOP, AUTO THROTTLE SYSTEM INOP. NO LAND 3 AND NO AUTO LAND ON ASA. NO EICAS MESSAGES PRESENT STATUS MSG APPEARED, WXR SYS. DURING GROUND TEST SUSPECT BAD MCP. REMOVEDec 3, 2009 · N462UP · Boeing 75724APFSDR CLCA113020091Computer · failedON TAKEOFF FROM SPIM, AIRCRAFT EXPERIENCE AUTO PILOT NR 2 WOULD NOT ENGAGE, WITH THE NR 1 AUTO PILOT ON DEFERRED MAINTENANCE. THE FLIGHT CREW ALSO REPORTED "ROLL SWS FAIL" DISPLAY. AIRCRAFT DUMPED FUEL AND RETURN TO SPIM WITHOUT FURTHER INCIDENT. REMOVED & Dec 1, 2009 · N985AR · Doug MD11FSDR ASAA0957094Position Sensor · out of adjustAUTOPILOTS DISENGAGED OVER FAF APPROX 1800FT MSL AIRCRAFT ON SPEED LIGHT TO MOD TURB (AUTOLAND EVAL ATTEMPT). FOUND FAULT CODE 22 11190 B SIDE. ADJUSTED AILERON POSITION SENSOR. AILERON RIG TEST GOOD. BITE TEST GROUP NR 46 AND LAND VERIFY TEST GOOD.Nov 30, 2009 · N517AS · Boeing 737890SDR A6WA200940761Pcu · malfunctionedRECEIVED AILERON TRIM CAUTION FLAG ON EVERY TURN INITIATED TO THE LT WITH AUTOPILOT ON IN CRUISE FLIGHT. DURING TURNS MADE TO THE LT ACFT ROLLS VIOLENTLY TO THE LT TO ABOUT 30 DEGREES. ACFT CONTROLS FEEL HEAVY IN FLIGHT. MAINT WORK CARD NR 8 FOR R & R OF THNov 19, 2009 · N470ZW · Cndair CL6002B19SDR FDEA200911173999Control Panel · failedON CLIMBOUT "STAB OUT OF TRIM LIGHT" LIGHT ON CONTINUOUSLY WITH AUTOPILOT ON. AUTOPILOT WOULD NOT TRIM OR HOLD ALTITUDE. RAN " STABILIZER OUT OF TRIM LIGHT REMAINING ILLUMINATED" CHECKLIST TWICE. AUTOPILOT WOULD NOT ENGAGE PROPERLY WITH A/P DISCONNECTED, ANov 17, 2009 · N257FE · Boeing 727233SDR ASAA0957016Unknown · malfunctionedON APPROACH TO 16L SEA AT APPROX 4000 FT AND 12 MILES AUTOPILOT "A" ENGAGED "APP" SELECTED. UPON CAPTURING G/S A/P PITCHED DOWN THEN UP FOLLOWED BY A/P DISCONNECT. DFCS LOGGED MSG 22 11368 G/S ANOMALY DETECTED. SYS TESTS GOOD REF FIM TASK 22 11 810 801. A/Nov 16, 2009 · N517AS · Boeing 737890SDR REXA200900123Autopilot Sys · malfunctionedAT 10,000 FT 100 FPM THRUST IDLE 250 KTS A/C ROLLED TO LEFT WITH AUTOPILOT ENGAGED A/P DISCONNECTED AND A/C STARTED ROLLING LEFT TO RIGHT AND YAWING LOSS OF CONTROL INCIDENT LASTED 30 SEC, NO MSG OR INDICATIONS. FELT LIKE A/C WAS STALLING.Nov 15, 2009 · N8932C · Cndair CL6002B19SDR A6WA200940755Actuator · malfunctionedUNCOMMANDED RUDDER DEFLECTION IN FLIGHT, YAW DAMPNER 1 DISENGAGED. NO FURTHER UNCOMMANDED MOVEMENTS. R & R LT YAW DAMPNER LINEAR ACTUATOR. RIGGING AND OPS TEST GOOD REF AMM 22-22-01.Nov 11, 2009 · N423AW · Cndair CL6002B19SDR HALA2009110400505Autothrottle Sys · malfunctionedETOPS SIGNIFICANT SYS - BTB- ABORTED TAKEOFF AT APPROX 75KTS DUE TO AUTO THROTTLE NOT ENGAGEING. ON TAXI BACK TO GATE, ENGAGED OK. PERFORMED MCDP TEST 2, 10,30 AND NO FAULTS NOTED. COMPLETED BRAKE CHECK, NR 1 AND 2 ENG TEST 3 AND PERFORMED THE ETOPS * ITEMSNov 4, 2009 · N585HA · Boeing 7673G5SDR HALA2009102500483Receiver · malfunctionedETOPS SIGNIFICANT SYSTEM - NO LAND 3 DISPLAYED ON ASA WITH APP MODE NOT SELECTED AND A/P OR F/D ENGAGED OR NOT ENGAGED. REMOVED AND REPLACED NR 2 MMR UNIT GROUND CHECK OK PER AMM 34-31-01 TEST 30 PASSED ACFT REMAINS IN LAND 3 STATUS.Oct 25, 2009 · N591HA · Boeing 76733ASDR ASAA0956788Autopilot Sys · malfunctionedAUTOLAND EVAL ATTEMPTED ON SEA 34L. A/P SEEMED TO PITCH DOWN A LITTLE TOO MUCH AT ABOUT 100' AGL SHOWING NO SIGNS OF CORRECTING. HGS GAVE "APP WARN" COUPLE OF SECONDS LATER. DISCONNECTED A/P AND LANDED MANUALLY. ATC SAID ILS 34L WAS OPERATING NORMALLY AND ILS Oct 9, 2009 · N560AS · Boeing 737890SDR ASAA0956775Unknown · malfunctionedWHEN "OFFSET" USED FOR LATERAL DEVIATIONS LNAV ENGAGED AIRCRAFT ASSUMES A 30 DEG ANGLE OF BANK TURN REGARDLESS OF ANGLE OF BANK SELECTED ON THE HEADING KNOB. FOUND FAULT CODE 22 11822 PERFORMED FIM 22 11 00 810 811. OPS TEST NORMAL.Oct 7, 2009 · N565AS · Boeing 737890SDR UALA2009100703148Control Panel · faultyMCDP SHOWS NO LAST FLT FAULTS. NO FAULTS TEST 30. PASSES TEST 04 THAT INCLUDES SELECTING THE HDG SEL SWITCH. REPLACED AFCS MODE CONTROL PANEL AND PERFORMED CAT III CHECK, OP CHECKED OKAY. ACFT OK FOR CAT III SVC.Oct 7, 2009 · N550UA · Boeing 757222SDR AALA20090929PHX01Circuit Breaker · faultyINFLIGHT SAN TO DFW. CREW REPORTED CLIMBING THROUGH FL260 THE AIRCRAFT YAWED AND THE AUTO PILOT AND AUTO THROTTLE KICKED OFF FOLLOWED BY YAW DAMP OFF AND MACH TRIM INOP INDICATION LIGHTS. ALTITUDE WINDOW WENT BLANK AND SPEED MACH FROZE ALONG WITH PITCH INDICSep 29, 2009 · N492AA · Doug DC982SDR 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 737890SDR ASAA0956648Unknown · malfunctionedIN DESCENT THRU 14000 WHILE IN VNAV/LNAV DESCENT AUTO WAS DOING NORMAL TRIMMING BUT MAKING A CLICK CLACK NOISE ON EACH ROTATION DISENGAGES TRIM WORKED SMOOTHLY NO NOISE, NORMAL AT 7000 RE-MESSAGE AUTOPILOT IT TRIMMED SMALL AMOUNTS USED BUT SAME CLICK CLACK NOISep 19, 2009 · N570AS · Boeing 737890SDR FDEA200909173326Control Panel · failedON CLIMB OUT ICT, CTR A/P FAILED. (HEAVY PITCH PULLS) RETURNED TO ICT C/W QRH. ORIGINAL PLAN DATE WAS ENTERED. RELEASED FOR SERVICE IAW MEL: 22-10-01-C CATEGORY: B EXPIRATION: 20SEP09 "MEL 22-10-01-C: ALL AUTOPILOTS INOP. - ACFT NOT C ATII - NO RVSM OSep 17, 2009 · N903FD · Boeing 7572B7SDR FDEA200909033255Computer · failedON DEPARTURE, ATS FAILED, BOTH AUTOPILOTS FAILES AND BOTH FLIGHT DIRECTORS FAILED AND WINDSHEAR DET FAIL LIGHT ILLUMINATED. UNABLE TO GET ANY OR ALL BACK. RETURNED TO DEPARTURE. MCDU SCRATCHED MESSAGE 'THRUST LIMIT MISMATCH' ALSO ILLUMINATED. PERFORMED BOTSep 3, 2009 · N587FE · Doug MD11FSDR CA090911001Limit Switch · failed(CAN) DURING THE DAILY FUNCTIONAL TEST OF THE SPEED TRIM LIMIT SWITCHES THE RETRACT LIMIT SWITCH FAILED TO STOP THE MOTOR. THIS SPEED TRIM ACTUATOR WAS IN SERVICE FOR 30 HOURS AFTER REPAIR FOR THE SAME FAILURE. (TC# 20090911001)Aug 26, 2009 · Boeing 1072SDR UHLA2009082400055Autopilot Sys · malfunctionedAT CRUISE FL370, THE AUTO PILOT FAILED WITH THE ASSOCIATED A/P FAIL CAUTION EICAS MESSAGE. ABOUT 3-4 SECONDS LATER THE SHAKER ANTICIPATED EICAS CAUTION APPEARED AND THE SHAKER BEGAN TO ENGAGE. ATC WAS NOTIFIED OF THE FAILURE, DESCENDED TO FL280. RAN QRH PROAug 24, 2009 · N864RW · Emb ERJ170100SESDR AALA20090813DFW01Gyro · inoperativeDFW - WHEN AIRCRAFT WAS MAKING A TURN OF FIFTEEN DEGREES THE CAPTAINS ATTITUDE INDICATOR FLUCTUATED WILDLY CAUSING THE AUTO PILOT AND AUTO THROTTLES TO DISENGAGE. RETURNED DFW WITHOUT INCIDENT. REMOVED AND REPLACED ALL THREE GYROS. SYSTEM GROUND CHECKED NORAug 12, 2009 · N467AA · Doug DC982SDR HNAA2009081000024Panel · malfunctionedPILOT REPORTED A BURNING SMELL IN COCKPIT, STATED THAT IT WAS POSSIBLY COMING FROM THE CAPT 802 PANEL. MAINTENANCE REMOVED AND REPLACED 802 ADVISORY PANEL, INSPECTED, AND DRIED OUT AREA. OPERATIONAL CHECK WAS GOOD IAW DASH-8 MM 22-10-09.Aug 9, 2009 · N333EN · Dhav DHC8102SDR 2009FA0000936Autopilot Sys · inoperativeUNIT WAS INITIALLY REMOVED FROM ACFT IN MARCH OF 2009 BECAUSE AUTOPILOT WOULD NOT OPERATE PROPERLY. TO VERIFY AUTOPILOT OUTPUTS FROM ATTITUDE GYRO WERE WORKING GYRO REMOVED FROM ACFT AND A BENCH TEST PERFORMED. BENCH TEST REVEALED THAT IT WOULD NOT ERECT AT Aug 7, 2009 · N8086Q · Piper PA34200TSDR CA090821003Altimeter · malfunctionedTHE CREW (FIRST OFFICER PILOT FLYING - PF) WAS ON THE RNP 16 APPROACH AND THROUGH 1000 FEET AGL THE PF DISENGAGED THE AUTOPILOT IN ORDER TO HAND FLY THE APPROACH. THE PF REPORTED EVERYTHING WAS NORMAL UNTIL APPROX 150 FEET AGL WHEN HE FELT THE THRUST LEVERS REAug 7, 2009 · Boeing 7377*SDR ASAA0956378Unknown · malfunctionedF/O FLIGHT DIRECTOR PITCH BAR DISAPPEARS INTERMITTENTLY DURING DESCENT. MACH TRIM FAIL LIGHT ILLUMINATES WITH MASTER CAUTION "RECALL" INTERMITTENTLY. PERFORMED TASK 22 11 00 740 801 DFCS OPERATIONAL TEST FLIGHT DIRECTOR GROUP 12 TEST AND DFCS OPERATIONAL TESAug 6, 2009 · N517AS · Boeing 737890SDR Y9PAN818WF709Relay · failedDURING CLIMB AFTER ENGAGING THE AUTOPILOT, THE CREW NOTICED THE A/P TRIM FAIL LIGHT ILLUMINATED ON THE MASTER CAUTION PANEL, THEN NOTICED THE AUTOPILOT ADVISORY THAT THE MACH TRIM HAD FAILED. THE CREW RETURNED TO HOME BASE (KHOU). DURING TROUBLESHOOTING FOUNJul 23, 2009 · N818WF · Israel ASTRASPXSDR CA090826005Retaining Clip · missingTURNBUCKLE CLIP WAS NOT ON TURN BUCKLE ALLOWING THE LOWER TURNBUCKLE TO UNSCREW AND SEPARATE FROM THE LWR CLEVIS INFLIGHT INDICATION WAS `PORPOSING O AUTOPILOT IN CRUISE`.Jul 15, 2009 · Cessna 425SDR IXXA090031OTransducer · defectiveDURING CRUISE, AN UNCOMMANDED RUDDER KICK WITH NO MOVEMENT OF PEDALS. THE CREW DIVERTED TO KDFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DEFERRED THE AUTOPILOT SYSTEM. MAINTENANCE IN KTOL REPLACED THE LINEAR POSITION TRANSDUCER. OPERATIONAL CHECK Jun 9, 2009 · N821BX · Doug DC871FSDR IPXA09556292Switch · inoperativeINSPECTION TYPE:N/A ATB - L NAV WOULD NOT ENGAGE - WHEN PRESSING L NAV SYSTEM LIGHTS ON PANEL WOULD SHORT OUT. V NAV WOULD NOT ENGAGE. FLT LEVEL CHANGE WOULD NOT ENGAGE. DEFERRED PER MEL 22-11-4-11. M402419 ASSIGNED. ***SDR FILED OPEN***Jun 9, 2009 · N412UP · Boeing 75724APFSDR 2009FA0000430Autopilot Sys · malfunctionedAUTOPILOT DISENGAGES INFLIGHT, AIRCRAFT ROLLS TO THE RT, AFTER RETRIMING AND ENGAGING ON THE COPILOTS SIDE THE AUTOPILOT DIS-ENGAGES AFTER SEVERAL MINS DEFERRED IAW MEL 22-1-1 CAT 'B' DUE DATE 05/24/09May 22, 2009 · N213QS · Amd FALCON2000SDR ASAA0955688Autopilot Sys · malfunctionedWHILE CAPTURING THE LOCALIZER HTE A AUTOPILOT DISENGAGED AND WOULD NOT RE ENGAGE. GROUNDED YES. "A" AUTOPILOT LOGGED INVALID MMR/ILS DATA LAST FLT. PERFORMED LRU TEST FOR MMR/ILS REF MM 34 31 42 TEST PASSED & DFCS CURRENT STATUS TEST PASSED REF MM 22 11 00 & HMay 18, 2009 · N517AS · Boeing 737890SDR UALA2009051801403Fcu · damagedFCU ALT SELECT SW BROKE OFF. ALT SEL STUCK AT 17K AND ALT CAPTURE ALERT HORN GOING OFF CONTINUOUSLY. REPLACED FCU, CHECKS GOOD.May 17, 2009 · N424UA · Airbus A320232SDR DXTA2009051303647Autopilot Sys · malfunctionedWITH AUTOPILOT ON IN CLIMB AN AMBER THEN RED BOXED "A" APPEARED ON THE PFD. WHEN THE AUTOPILOT WAS DISCONNECTED A LARGE ROLL RT FORCE WAS FELT. ADJUSTED LT WING AILERON DUE TO LT AILERON WAS 1 DEG UP. ADJUSTED TO STREAMLINE. TRAVELS AND TENSIONS CHECK GOOD. IMay 12, 2009 · N853QS · Cessna 560CESSNASDR QXEA2009050700316Roll Servo · bindingMSO - DURING CRUISE FLIGHT AT FL250, AIRCRAFT BEGAN MAKING SHALLOW S-TURNS. DURING TURNS "MISTRIM" MESSAGES APPEARED ON PFD INDICATING BOTH "TRIM R WING DOWN" AND "TRIM L WING DOWN". AFTER DISENGAGING AUTOPILOT, BOTH CAPT AND F/O NOTICED SIGNIFICANTLY HIGHERMay 3, 2009 · N405QX · Bombdr DHC8402SDR SWIA200921509Circuit Card · corrodedC-CHECK, CORROSION ON NR 1 HIRF CARD. REPLACED CARD.Apr 27, 2009 · N984CA · Cndair CL6002B19SDR ASAA0955245Autoland Sys · malfunctionedTRIED AUTOLAND 34L UNSAT (WENT BELOW G/P AND LEFT OF COURSE) MANUALLY DISCONNECTED. COULD NOT DUPLICATE. PERFORMED ILS OPS TEST REF MM 234 31 00 BOTH CHECK NORMAL. ALSO PERFORMED DFCS LAND VERIFY NR 49 CHECK LRU MMR/ILS NR 38 CK & CURRENT STATUS NR 20 CK REApr 22, 2009 · N577AS · Boeing 737890SDR HNAA2009041600121Panel · malfunctionedSMOKE, ELECTRICAL FIRE FROM UNDER GLARE SHIELD AFTER GROUND POWER APPLIED. REMOVED & REPLACED CAPTAIN'S AUTO PILOT DISENGAGE ANNUNCIATOR PANEL ASSEMBLY DUE TO A BURNT RESISTOR. INSPECT AREA IN THE VICINITY FOR OTHER DAMAGE NONE FOUND. OP'S CHECK GOOD. IN AApr 15, 2009 · N941HA · Dhav DHC8102SDR GLBA20090409ATransducer · malfunctionedAIR RETURN - PILOTS REPORTED A LIGHTNING STIKE ON THE NOSE WHICH RESULTED IN A RUNWAWAY RUDDER BOOST SITUATION IF THE RUDDER BOOST SWITCH WAS "ON". RUDDER BOOST ACTIVATES AND STAYED ACTIVATED. MAINTENANCE PLACED THE ISSUE ON MEL 22-2 CAT.C C/N 34624 AT THE TIMApr 9, 2009 · N245GL · Beech 1900DSDR VNAA2009040600002Control Panel · failedCREW REPORTED AUTOPILOT PORPOISES ON APPROACH +5 DEGREES UP -10 DOWN INTO CHO. CREW DIVERTED TO CRW AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FLIGHT CONTROL PANEL PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.Apr 2, 2009 · N216PS · Cndair CL6002B19SDR ASAA0954971Warning System · malfunctionedWHEN FLAPS RETRACTED TO UP FROM 1 DEG SPEED TRIM FAIL LIGHT ILLUMINATED WENT OUT AFTER FLAPS REACHED UP. DFGS BITE TESTS PASS ALL TEST PER FIM TASK 22 11 00 810 801. OPS NORMAL.Mar 29, 2009 · N519AS · Boeing 737890SDR HALA2009032500103Autoland Sys · malfunctionedETOPS SIGNIFICANT SYSTEM, AUTOLAND STATUS INDICATOR SHOWS "NO LAND 3" WILL NOT RESET. YELLOW G/S AND LOC WARNINGS SHOW ON CAPT ADI. LAST FLIGHT FAULT ON MCDP SHOWS LEFT ILS. FOUND LEFT MMR WILL NOT TEST CYCLED LEFT MMR C/B NOW LEFT MMR BITE TEST PASS. ALL Mar 25, 2009 · N588HA · Boeing 7673CBSDR SWIA200921112Computer · malfunctionedFLT 6265 - AUTOPILOT PITCH TRIM FOLLOWED BY STAB AND MACH TRIM MESSAGES. EXCESSIVE FORCE REQUIRED TO OVERRIDE NOSE HIGH ATTITUDE AND UNWANTED ROLL EXPERIENCED. REPLACED STAB TRIM MOTOR CONTROL, HORIZONTAL STABILIZER TRIM ACTUATOR AND HSTCU COMPUTER.Mar 5, 2009 · N962SW · Cndair CL6002B19SDR ASAA0954640Circuit Breaker · poppedFCC DC C/B POPPED. RESET C/B PER MM 20 60 01. PERFORMED DFCS BITE CHECK PER FIM TASK 22 41 00 810 801. NO CURRENT FAULTS NOTED. OPS NORMAL.Mar 5, 2009 · N587AS · Boeing 737890SDR CA090415002Autopilot Sys · malfunctioned(CAN) WHILE IN CRUISE, THE AUTO PILOT TRIM AURAL WARNING SOUNDED, AND THE A/P TRIM WARNING INDICATION ON THE CAWS ILLUMINATED. TRIM ADAPTER REPLACED AND ACFT RETURNED TO SERVICE. NO FURTHER PROBLEMS ENCOUNTERED.Mar 4, 2009 · Pilats PC1245
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