JASC 2210

Service difficulty reports · 4,019

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 730PA0003Damper · malfunctionedYAW DAMPER WILL NOT ENGAGE. PERFORMED YAW DAMPER SYSTEM BITE TEST. ALL FAULTS CLEARED. NO CURRENT FAULTS PRESENT.May 3, 2003 · N730PA · Boeing 7373L9SDR ABXA030140Computer · malfunctionedAUTOPILOT PITCHED UP AND DOWN 1500 FT./MIN., THEN MADE AN UNCOMMANDED 30 DEGREES RIGHT TURN. AUTOPILOT CHECKED GOOD ON GROUND. REMOVED AND REPLACED PITCH AXIS COMPUTER AS PRECAUTION. PITCH COMPUTER CHECKED GOOD IAW DC-9 MM 22-13-01.May 2, 2003 · N948AX · Doug DC931SDR SWIA200311954Actuator · malfunctionedNR 1 YAW DAMPER WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW LINEAR ACTUATOR WITH A SERVICEABLE UNIT IAW MM 22-22-01. PERFORMED OPS CHECK IAW MM 22-22-01.Apr 28, 2003 · N426SW · Cndair CL6002B19SDR DXTA200300018Motor · lack of lubeCLIMBING THROUGH 35,000 FT YOKE JERKED ABRUPTLY, AUTOPILOT WAS DISCONNECTED AND AIRCRAFT NEED NOSE DOWN TRIM. FIFTEEN SECONDS LATER WITH AUTOPILOT OFF SECOND JERK OCCURRED IN YOKE.Apr 28, 2003 · N610QS · Cessna 560XLSDR 249TR0018Circuit Breaker · trippedNO AUTO PILOT TRIM. FOUND AUTO PILOT TRIM CIRCUIT BREAKER POPPED. RESET BREAKER. OPS CHECKED OK PER MM 22-11-01.Apr 26, 2003 · N249TR · Boeing 7372K5SDR MDAS092019Switch · failedON APRIL 16, EXPERIENCED ABORTED TAKEOFF DUE TO FCC INTERMITTENT FAULT. TO/GA DIDN'T SHOW AND FD DISAPPEARED FROM BOTH MONITORS AFTER PUSHED THE AUTO-THROTTLE TO/GA SWITCHES DURING TAKEOFF. THE CREW FOLLOWED QRH AND DECIDED TO ABORT TAKEOFF. IAW AMM 22-11-00, Apr 16, 2003 · Boeing 737800*SDR HE66085919Module · defectiveAFTER INSTALLING THIS MODULE WE WERE HAVING TRIM ACTUATOR FAILURES AND AUTO PILOT WOULD NOT PASS BIT. REINSTALLED OLD MODULE.Apr 7, 2003 · N135CR · Urocop EC135T1SDR BAQA085912Module · failedGIVING P/R SAS LIGHT AND ACTUATION W/A CORRESPONDING (P) ON PFD. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT.Apr 4, 2003 · N533ME · Urocop EC135T1SDR NACA20030082Coupler · oscillatesRIGHT ON TAKE-OFF, UPPER YAW DAMPER OSCILATE AUTO PILOT DISENGAGE, LIGHT STAYED ON, WIND SHEAR CAUTION LIGHT STAYS ON. REPLACED UPPER YAW DAMPER COUPLER AND TESTED GOOD.Apr 3, 2003 · N930FT · Boeing 727100SDR ABXA030128Servo Valve · malfunctionedUNCOMMANDED YAW IN FLIGHT. AUTOPILOT ON. REPLACED RUDDER POWER PACK TRANSFER VALVE IAW DC-8 MM 27-21-6.Apr 1, 2003 · N828AX · Doug DC863FSDR ABXA030129Computer · defectiveRUDDER UNCOMMANDED LT INPUT AT 3,000 FT, 200 KTS, AND 23 DEGREES FLAPS. AUTOPILOT OFF, YAW DAMPER ON. COULD NOT DUPLICATE PROBLEM. REPLACED YAW DAMPER COMPUTER. OPS CHECKED GOOD IAW DC-8 MM 22-10-00.Apr 1, 2003 · N828AX · Doug DC863FSDR BAQA085891Computer · inoperativeYAW CSAS WILL NOT COME ON LINE.Apr 1, 2003 · N213AE · Bolkms BK117B1SDR SWIA200311864Computer · malfunctionedON TAKEOFF ROLL AT 90 KTS (INTERMITTENTLY) AND LANDING ROLL TRIM FAIL ILLUMINATION ON MAP AND MASTER CAUTION SYSTEM. REMOVED FIRST OFFICER'S AUTOPILOT COMPUTER AND INSTALLED A SERVICEABLE UNIT. OPS CHECK GOOD.Mar 30, 2003 · N268UE · Emb EMB120ERSDR 2003UALA00348Damper · leakingLANDED UNDER AMBER ALERT DUE TO A GREEN HYDRAULIC SYSTEM INDICATION AND LOSS OF QUANTITY. YAW DAMPER NR 1 WAS FOUND LEAKING. UNIT WAS REPLACED.Mar 28, 2003 · N422UA · Airbus A320232SDR COMA0360168Clutch · out of toleranceFLIGHT 5847 A/P TRIM CAUTION MESSAGE - AILERONS FELT NOTICABLE STIFF. COULD NOT DUPLICATE DISCREPANCY, FOUND THE AUTO PILOT SERVO SLIP-CLUTCH OUT OF TOLERANCE, ADJUSTED SLIP CLUTCH TO PROPER VALVE.Mar 25, 2003 · N915CA · Cndair CL6002B19SDR SWIA200311855Circuit Card · failedON DESCENT TO FINAL APPROACH RECEIVED AN AP PITCH TRIM CAUTION MESSAGE. RAN QRH, HEAVY NOSE DOWN WHEN DISCONNECTED. REENGAGED, AP MESSAGE WENT AWAY AFTER RE-TRIMMING. MESSAGE CAME BACK ON SHORT FINAL. REINITIALIZED FCC CARD NR 1 AND FCC CARD NR 2. OPS CHEMar 24, 2003 · N905SW · Cndair CL6002B19SDR SWIA200311851Relay · malfunctionedAFTER TAKEOFF WITH AUTOPILOT SELECTED TO CAPTAIN'S SIDE, TRIM FAIL ILLUMINATED ON MAP MOMENTARILY, BUT THEN EXTINGUISHED. AUTOPILOT WAS ENGAGED; ON DESCENT PLANE PITCHED DOWN AND LIGHT CAME ON AGAIN. REPLACED TRIM PROXIMITY RELAY K0393. BOTH AUTOPILOT FLIGHMar 23, 2003 · N234SW · Emb EMB120ERSDR SWIA200311850Computer · malfunctionedAUTOPILOT AND CAPTAIN'S FLIGHT DIRECTOR PITCHES UP AND DOWN 300 FT PRIOR TO LEVEL OFF. REPLACED AUTOPILOT COMPUTER APC-65B WITH SERVICEABLE UNIT. TESTED AND OPS CHECK GOOD.Mar 22, 2003 · N234SW · Emb EMB120ERSDR DLM88030259Probe · failedIN FLT CREW REPORTED AUTOPILOT PROBLEM, HAD BOTH DFGCS NOT RESPONDING TO ANY FLT GUIDANCE PANEL IMPUTS AND MSG OF FAIL 26 ON FMAS. THEN REPORTED A LITTLE BURNING ODOR AND DECIDED TO DIVERT TO BHM. REPLACED TOTAL AIR TEMP PROBE. PERFORMED DUCT BURNOUT FOR ODMar 20, 2003 · N947DL · Doug MD88SDR C7WA200200041Control Panel · shortedWHEN ENGAGING AUTOPILOT, CRUISE STABILIZER TRIMS TO THE FULL NOSE DOWN POSITION. WITH AUTOPILOT DISCONNECTED, AFTER LEVEL OFF AT FL350, AN ELECTRICAL OVERHEAT ODOR STARTED TO FILL THE COCKPIT. CHECKLIST PERFORMED, ODOR STOPPED. REMOVED AND REPLACED RIGHT ELMar 14, 2003 · N128NA · Boeing 7272J7SDR ABXA030116Computer · defectiveIN CRUISE FLIGHT, FL350, MACH .770, AUTOPILOT ON. RUDDER GAVE UNCOMMANDED INPUT TO LEFT SIDE ON TWO OCCASIONS. RETURNED TO CENTER BY ITSELF, YAW DAMPER ON. REPLACED YAW AXIS COMPUTER. SYSTEM OPS CHECKED GOOD IAW DC-8 MM 22-10-00.Mar 12, 2003 · N822AX · Doug DC863SDR U30A200300008Computer · faultyDURING CRUISE ON FLT 0441 CUN-CLE, NR 2 FMGC WILL NOT RESET AND AUTOPILOT NR 2 WOULD NOT ENGAGE AS A RESULT. DEFERRED PER MEL 22-10-01. ON MARCH 11, 2003, REPLACED NR 2 FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC) IAW AMM 22-83-34-400-001. TESTED AFS OK. PERMar 10, 2003 · N262AV · Airbus A320214SDR DL757030215Video Display · burnedF/A REPORTED SMELL IN CABIN AND ORANGE GLOW COMING FROM VIDEO CONTROLLER UNIT. FOUND VIDEO ON LIGHT ARCED AND SHORTED. REPLACED VIDEO ON LIGHT.Mar 4, 2003 · N647DL · Boeing 757232SDR 249TR0013Limit SwitchBoth A & B auto pilots disengage after flaps reach #1 positon during approach. Will not re-engage until selected beyond flaps 5 positon. Replaced flaps up limit switch 5245(?) per MM 27-51-291 ops chk normal per MM 22-11-01.Mar 3, 2003 · N249TR · Boeing 7372K5SDR BAQA084838Control Unit · inoperativeYAW CSAS WILL NOT COME ON LINE. REPLACED WITH SERVICEABLE UNIT.Feb 27, 2003 · N213AE · Bolkms BK117B1SDR SWIA200311823Computer · malfunctionedWINDSHEAR FAIL STATUS MESSAGE ILLUMINATES DURING FLIGHT. MESSAGE WENT CLEAR AFTER LANDING. FAULT HISTORY SHOWED FCC CARD FAULTS. REMOVED AND REPLACED FCC 4000 IN IAPS CARD CAGE IAW MM 22-12-14. PERFORMED OPS CHECK IAW MM 22-11-00. OPS CHECK GOOD.Feb 27, 2003 · N449SW · Cndair CL6002B19SDR HEEA084912Amplifier · malfunctionedSCAS WILL AMPLIFIER NOT HOLD PITCH CHANNEL.Feb 25, 2003 · Bell 412SDR MEX2003041Accelerometer · inoperativeAIRCRAFT RETURNED FROM FLIGHT, AFTER TAKEOFF FLIGHT GUIDANCE COMPUTER WENT OFF. ON BOTH COMPUTERS THERE WERE NO AUTO PILOT AND ATS, PITOT HEAT OFF LIGHT TURN ON AND YAW DAMPER FAILURE LIGHT TURN ON. RESPECT TO PITOT STALL HEATER OFF LIGHT ON, IT WAS DETERMINFeb 22, 2003 · N1075T · Doug DC987SDR SWIA200311806Control Panel · inoperativeNR 1 YAW DAMPER WILL NOT ENGAGE. FERRIED TO SLC. REMOVED AND REPLACED FLIGHT CONTROL PANEL. PERFORMED OPS CHECK OF YAW DAMPERS. OPS CHECKS GOOD.Feb 19, 2003 · N591SW · Cndair CL6002B19SDR SWIA200311785Computer · malfunctionedAUTOPILOT FAIL AND TRIM FAIL LIGHT ON MAP CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED NR 2 APC-65B WITH SERVICEABLE UNIT. RAN THROUGH TESTS. OPS CHECK GOOD.Feb 15, 2003 · N294SW · Emb EMB120ERSDR HEEA084482Tarsyn · malfunctionedTARSYN COMPASS FLAG WON'T PULL UNTIL 10 MINUTES AFTER INVERTERS PUT ON. TO BE SENT TO VENDOR FOR REPAIR.Feb 14, 2003 · N2149S · Bell 412SDR IXXA0300014OComputer · failedAFTER DEPARTURE FROM MCO DURING CLIMBOUT DESTINED FOR TOL AIRCRAFT EXPERIENCED YAW ABNOMALY. CREW ELECTED TO RETURN TO MCO. AFTER UNEVENTFUL LANDING IN MCO MAINTINANCE INSPECTED SYSTEM AND TRANSFERRED THE YAW DAMPNER TO MEL. ALL WORK COMPLETED PER APPLICABLFeb 11, 2003 · N827BX · Doug DC871FSDR B652003F00000Autopilot Sys · malfunctionedWHILE ON A IFR TRAINING FLIGHT AIRCRAFT EXPERIENCED UN-COMMANDED ROLL AND PITCH MOVEMENTS WITH NO CAUTION LIGHTS OR MESSAGES. AUTOPILOTS DISENGAGED (REVISION TO FLIGHT MANUAL). NOTE: MAINTENANCE DID NOT FIND A CAUSE FOR THE UNCOMMANDED MOVEMENTS.Feb 10, 2003 · N135CR · Urocop EC135T1SDR PA03003Controller · failedAUTOTHROTTLE 2 NUMEROUS INTERMITTENT FAILURES. FOUND NO FAILURES REPORTED IN MDUA FAULT HISTORY. OPERATIONALLY CHECKED AUTOTHROTTLE SYSTEM CHANNELS 1 AND 2 IAW CMP CODE 223005 SEVERAL TIMES WITH NO FAILURES NOTED. AIRCRAFT WAS RETURNED TO SERVICE.Feb 6, 2003 · N920DC · Gulstm GULFSTREAMGVSDR PA03004Controller · malfunctionedABNORMAL AUTOTHROTTLE DISENGAGMENT OCCURRED AFTER TAKEOFF. PERFORMED AUTOTHROTTLE OPERATIONAL CHECK IAW MM. NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.Feb 6, 2003 · N910DC · Gulstm GULFSTREAMGVSDR ABXA030055Control Panel · defectiveAIRCRAFT SHOOK VIOLENTLY WHEN AUTO PILOT TURNED ON. TURNED OFF AND TRIED AGAIN. SAME RESULTS. TURNED OFF AUTO PILOT, NOTICED NO YOKE MOVEMENT. REMOVED AND REPLACED AUTO PILOT CONTROLLER. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 22-10-00-5.Jan 30, 2003 · N908AX · Doug DC931SDR 159PL0026Computer · malfunctionedROLL CHANNEL AUTO PILOT WILL NOT ENGAGE. REMOVED AND REPLACED ROLL CHANNEL COMPUTER PER MM 22-11-161.Jan 27, 2003 · N159PL · Boeing 737242SDR 219PA0006Autopilot SysElevator channel of auto pilot will not stay engaged. Re-racked A/P pitch control channel unit. Ops chks good IAW MM 22-10-10.Jan 27, 2003 · N219PA · Boeing 737222SDR GTIA030018Actuator · failedDTW - FOUND FLT 639 - AIR RETURN TO DTW, DUE TO INFLIGHT FLIGHT CONTROL PROBLEM. AIRCRAFT BEGAN AN INCREASING DUTCH ROLL CONDITION AND REQUIRED 5 UNITS OF RIGHT RUDDER TRIM AN 3 UNITS OF RIGHT WING DOWN TRIM TO MAINTAIN STRAIGHT AND LEVEL. AIRCRAFT WAS NOT SJan 26, 2003 · N815NK · Doug DC983SDR BAQA084019Actuator · malfunctionedERROR CODE NR 1 ON AUTO-PILOT TEST. REPLACED WITH SERVICEABLE UNIT.Jan 22, 2003 · N915ME · Aerosp AS365N2SDR 2003FA0000033Servo · chafedTHE SECONDARY YAW SERVO CABLE KEEPER WAS RUBBING THE PRIMARY YAW SERVO CABLE ON THE RT SIDE CAUSING EXCESSIVE WEAR ON BOTH COMPONENTS.Jan 14, 2003 · N520SC · Lear 55LEARSDR 249TR0012ComputerF/O's ADI & HSI will not self test in VOR or ILS. Removed & replaced FCCB computer. Ops checknormal per MM 34-31-0 and 22-11-01. Ops check good.Jan 13, 2003 · N249TR · Boeing 7372K5SDR AC2A092340Gyro · malfunctionedIN CRUISE FLIGHT WITH NR 1 AUTOPILOT ENGAGED THE AIRCRAFT EXPERIENCED AN UNCOMMANDED RIGHT HAND DESCENDING TURN. VERTICAL GYRO REPLACED.Jan 6, 2003 · N430CT · Bell 430SDR SWIA200311682Dampener · malfunctionedON PUSHBACK YD NR 2 STATUS MESSAGE CAME ON. RESET YAW DAMPER NR 2, MESSAGE REOCCURRED. REPLACED NR 2 YAW DAMPER IAW 22-22-01. OPS CHECK OK.Jan 5, 2003 · N412SW · Cndair CL6002B19SDR SWIA200311688Module · malfunctionedAT FL310 AND .74 MACH, EXPERIENCED RUDDER FLUTTER. ADDED RIGHT RUDDER TRIM, AIRCRAFT WAS THEN OUT OF TRIM BUT FLUTTER WENT AWAY. REPLACED BOTH LIGHTNING WIRE PROTECTION MODULES IAW 22-12-0B. OPS CHECK GOOD. P/N 2: 822-0332-401, S/N OFF: 216.Jan 4, 2003 · N589SW · Cndair CL6002B19SDR MEX2003001Computer · failedATL-MEX - FLT 601 - AIRCRAFT RETURNED TO GATE DUR TO DFGC NR 1 FAILURE, AFTER ENGINES STARTED, DFGS NR 1 WAS NOT WORKING PROPERLY. COMPUTER NR 1 WAS REPLACED IAW MM 22-01-01, AND SWITCHES WERE RE-ESTABLISHED, TESTS OK. (M)Jan 3, 2003 · N861LF · Doug MD83SDR ERAA082936Actuator · wornUNIT INOPERATIVE. ARMATURE AND BRUSHES WERE BOTH WORN, REQUIRING OVERHAUL. REPLACED MOTOR, CLUTCH WASHER, POTENTIOMETERS, SEAL, PACKING, GROMMETS, GROUND STRAP, AND BEARING. CALIBRATED FOR OPTIMUM PERFORMANCE. REPAIRED AS REQUIRED.Jan 3, 2003 · N578EH · Skrsky S76ASDR 159PL0024SolenoidElev. channel auto pilot disengaged during flight. Elev. "B" PCU solenoid Inop. MEL Elev channel per MEL 22-1, Control No. 12-31-001, Class B.Dec 31, 2002 · N159PL · Boeing 737242SDR 249TR0011SwitchA/P & F/D mode indicates TO/GA prior to take-off without input from crew & IAS changes to 165 knots on its own. Cleaned #2 throttle TO/GA switch, performed AP/FD bite test per MM 22-11-01.System tests normal.Dec 24, 2002 · N249TR · Boeing 7372K5SDR SWIA200211608Actuator · malfunctionedYAW DAMPER NR 1 INOP (STATUS MESSAGE), WOULD NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER ACTUATOR IAW CRJ MM 22-22-01. OPS CHECK GOOD.Dec 21, 2002 · N403SW · Cndair CL6002B19
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