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 97ZZZM231Auto-Pilot · malfunctionedFLT 174 - DTW - AUTO-PILOT PORPOISES IN ALL FLIGHT MODES. CREW DISCONTINUED USE OF AUTO-PILOT. DEFERRED PITCH ACCESS COMPUTER IAW MEL 22-1 CATEGORY C, CONTROL NR 00127. (M)Jan 26, 1997 · N947ML · Doug DC932SDR 97UAL900073Coupler · malfunctionedIRREGULAR YAW INPUT. THIS WAS A LONG TERM CHRONIC PROBLEM DURING WHICH A TOTAL OF 7 YAW DAMPER COUPLERS WERE REPLACED. OF THESE, 5 HAD PROBLEMS WITH THE RATE GYROS. THE AIRCRAFT HAS FLOWN 60 DAYS WITHOUT A YAW DAMPER SYSTEM ANOMALLY.Jan 26, 1997 · N322UA · Boeing 737322SDR 97ZZZX877Actuator Sleeve · wornTHE ELONGATED HOLE WHERE THE CAM SEGMENT IS INSERTED INTO THE YAW DAMPER PISTON IS BEING RUBBED AND WORN BY THE CAM SEGMENT.Jan 15, 1997 · Boeing 737201SDR HEEA978885Tarsyn · precessesTARSYN PRECESSES EXCESSIVELY.Jan 14, 1997 · N22608 · Bell 412SDR HEEA978876Tarsyn · defective#1 AFCS KICKS OCCASIONALLY.Jan 14, 1997 · N3893N · Bell 412SDR 97UAL900018Coupler · malfunctionedAIRCRAFT HAS SLIGHT ROCKING MOTION WHEN CLIMBING THROUGH FL270. *S/D* DUPLICATE DISCREPANCY. SEE MRR REPORT NR 97UAL900073.Jan 7, 1997 · N322UA · Boeing 737322SDR 9700229302Sensor Wire · failedON DEPARTURE, AUTOPILOTS 1 AND 2 FAILED, FLIGHT DIRECTOR 1 AND 2 FAILED, AND AUTO THROTTLES FAILED, UNABLE TO RECONNECT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRING TO THE LEFT ELEVATOR POSITION SENSOR, OPERAITONAL CHECK OJan 7, 1997 · N302RC · Doug DC982SDR 97UAL900009Coupler · malfunctionedYAW DAMPER PROBLEM. *S/D* DUPLICATE DISCREPANCY. SEE MRR REPORT NR 97UAL900073.Jan 3, 1997 · N322UA · Boeing 737322SDR 97UAL900031Coupler · malfunctionedAT 14,000 FT, 230 KNOTS, THE YAW DAMPER ENGAGED. *S/D* DUPLICATE DISCREPANCY. SEE MRR REPORT NR 97UAL900073.Jan 1, 1997 · N322UA · Boeing 737322SDR 97ZZZM225Auto Pilot · malfunctionedACY - FLT 256 - DURING CLIMB CONFIGURATION THE AUTO PILOT DIS-ENGAGED EXPERIENCED A VERY BRISK PITCH DOWN CONDITION. MAINTENANCE COULD NOT DUPLICATE MALFUNCTION. RAN FULL SYSTEM SELF TEST, FOR HALF HOUR OPERATIONAL CHECKS GOOD IAW DC-9 MM, CHAPTER 22-10-01. Dec 28, 1996 · N942ML · Doug DC932SDR 96UAL900962Yaw Damper · malfunctionedTUNING NR 1 HF CAUSES RIGHT YAW DAMPER INOP, ACCOMPANIED WITH EICAS MESSAGE.Dec 23, 1996 · N587UA · Boeing 757222SDR DLM88962692Panel · shortedAFTER LIGHT CHECK ON PREFLIGHT, F/O TRP PANEL UPPER RIGHT CORNER BEGAN TO SMOKE WITH ACRID ELECTRICAL ODOR. SECURED ALL ELECTRICS, REPLACED TRP PANEL, ALL CHECKS NORMAL.Dec 14, 1996 · N979DL · Doug MD88SDR HEEA968724Tarsyn · intermittentREPORTED #1 AFCS KICKS INTERMITTENTLY ON ROLL CHANNEL. TIME SINCE REPAIR 149:15.Dec 13, 1996 · N3893N · Bell 412SDR DHL96708007Yaw Damper · malfunctionedAT FL 310 AND MACH .80, RECEIVED SUDDEN UNCOMMANDED RUDDER INPUTS FROM LOWER YAW DAMPER. WHEN YAW DAMPER SWITCH TURNED OFF, THE UNCOMMANDED RUDDER INPUTS CEASED. CLEANED LOWER YAW DAMPER CONNECTOR AND RERACKED COUPLER, CYCLED RUDDER TO FULL TRAVEL LEFT AND Dec 9, 1996 · N708DH · Boeing 72725SDR CA970130003Amplifier · failed(CAN) AUTO PILOT CAME OFF LINE AND COCKPIT FILLED WITH SMOKE. TROUBLESHOOTING OF PROBLEM REVEALED AUTO PILOT AMP WAS DEFECTIVE. AMP REMOVED AND SYSTEM DEACTIVATED, ALSO WIRING IN THE AREA WAS INSPECTED NO OTHER FAULT FOUND.Nov 19, 1996 · Cvac 340CVACSDR HEEA968448Control · defectiveATT. LIGHT INOPERATIVE ONLY WHEN #2 HP IS ENGAGED. TIME SINCE REPAIR 701:20.Nov 6, 1996 · N22347 · Bell 412SDR COMA9610310Auto Pilot · malfunctionedDURING AUTO PILOT TEST THE ELEVATOR TRIM RUNS WILD. AUTO PILOT SYSTEM PLACED ON DEFERRED MAINTENANCE LIST.Oct 25, 1996 · N1110J · Emb EMB120RTSDR 97ZZZX16Shuttle Valve · failedINTERNAL VALVE FAILED IN THE PRECISE FLIGHT SUSIII SHUTTLE VALVE. A RIVET HEAD MIGRATED DOWNSTREAM TO THE ENGINE DRIVEN VACUUM PUMP. THE VACUUM PUMP SUBSEQUENTLY FAILED DUE TO FOREIGN OBJECT INJESTION. SUBMITTER STATED CHECK SYSTEM VISUALLY ON AN ANNUAL BASOct 25, 1996 · N1043X · Piper PA28R200SDR 96UAL900834Coupler · corrodedAT FL310 GOT A YAW DAMPER KICK THAT STARTED A OSCILLATION THAT KEPT GETTING STRONGER. AIRCRAFT FELT LIKE IT WANTED TO ROLL TO THE LEFT. TURNED YAW DAMPER OFF, STILL HAD SOME OSCILLATION, RECOVERED WITH AILERON CONTROL. AIRCRAFT NORMAL REST OF DESCENT. *S/DOct 23, 1996 · N9054U · Boeing 737222SDR HEEA968360Module Assy · failedNO PITCH COMMANDS FROM AUTOPILOT THUMBWHEEL STEP #22 OF AFCS CHECK.Oct 14, 1996 · N3208H · Bell 212SDR HEEA968290Tarsyn · defectiveDG PRECESSES EXCESSIVELY.Oct 14, 1996 · N27805 · Bell 212SDR HEEA968274Gyro · defective#2 ROLL KICKS.Oct 14, 1996 · N911MJ · Skrsky S76ASDR HEEA968273Gyro · defectiveVG KICKS IN ROLL.Oct 14, 1996 · N1547D · Skrsky S76ASDR HEEA968245Actuator · defectiveACTUATOR INTERMITTENTLY MOVES FROM RIGHT TO LEFT. TIME SINCE REPAIR 905:40.Oct 11, 1996 · N1546K · Skrsky S76ASDR HEEA968235Amplifier Assy · defectiveALT HOLD LIGHT TOO DIM ENGAGE LIGHT.Oct 11, 1996 · N3897N · Bell 214STSDR HEEA968232Alt Controller · defectiveALT HOLD UNRELIABLE.Oct 11, 1996 · N3897N · Bell 214STSDR HEEA968231Amplifier Assy · failedALT HOLD INOPERATIVE.Oct 11, 1996 · Bell 214STSDR HEEA968215Amplifier Assy · malfunctionALT HOLD WILL NOT ENGAGE.Oct 10, 1996 · N3897N · Bell 214STSDR HEEA968076Tarsyn Gyro · precessesCOPILOTS GYRO COMPASS PRECESSES. TIME SINCE REPAIR 839:15.Oct 3, 1996 · N3893P · Bell 412SDR HEEA968022Afcs · failedALTITUDE HOLD LIGHT INOPERATIVE.Oct 3, 1996 · N8045T · Bell 214STSDR HEEA968015Control Panel · failedROLL CHANNEL NOT SHOWING RESPONSE OR INDICATOR PANEL.Oct 3, 1996 · N911MJ · Skrsky S76ASDR 96UAL900762Yaw Coupler · intermittentYAW DAMPER ABRUPTLY MOVES RUDDER OCCASIONALLY FOR NO APPARENT REASON. *S/D* YAW COUPLER WAS INTERMITTENT. REPLACED YAW DAMPER COUPLER, CHECKED OK.Sep 30, 1996 · N9007U · Boeing 737222SDR DL76L962172Yaw Damper · failedLT HYD QUANTITY DECREASED TO .039, EDP DEPRESSURIZED AND ACMP OFF AND QUANTITY CONTINUED TO DECREASE. FOUND YAW DAMP MODULE LEAKING. REPLACED RT YAW DAMP MODULE.Sep 23, 1996 · N172DN · Boeing 767332SDR 96UAL900719Servo Stop · failedAUTOPILOT CAUSES SHARP UNCOMMANDED TURNS. REPLACED AILERON SERVO AND STOP MECHANISM.Sep 21, 1996 · N7945U · Boeing 727222SDR COMA9660145Yaw Damper · failedTHE NR 1 YAW DAMPER FAILED. REPLACED THE NR 1 YAW DAMPER.Sep 18, 1996 · N912CA · Cndair CL6002B19SDR 9619943220Flt Contl Unit · malfunctionedIMMEDIATELY AFTER LEVEL OFF AT CRUISE FL350, LOST NR 1 AUTO-PILOT. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RESET NR 1 FLIGHT MANAGEMENT AND GUIDANCE COMPUTER WITH NO HELP. LATER, LOST THE FLIGHT CONTROL UNIT. AIRCRAFT DIVERTED TO MIA AND LANDED WITSep 14, 1996 · N320US · Airbus A320211SDR 96UAL900695Coupler · malfunctionedCREW REPORTS UNCOMMANDED YAW DAMPER KICK ON TAKEOFF AT V-1. *S/D* AIRCRAFT SYSTEMS WERE TESTED AND FUEL LOAD CHECKED. COULD NOT FIND ANYTHING THAT FAILED. YAW DAMPER COUPLER WAS REPLACED PRECAUTIONARY. SHOP COULD NOT FIND ANYTHING WRONG.Sep 13, 1996 · N9063U · Boeing 737222SDR CALA9601260Computer · malfunctionedTHE AIRCRAFT HAD A 12 DEGREE UNCOMMANDED ROLL TO THE LEFT WITH AUTOPILOT-B ENGAGED WHILE ON APPROACH. THE FIRST OFFICER DISCONNECTED B-AUTOPILOT AND THERE WERE NO FURTHER PROBLEMS. THE FLIGHT CONTROL COMPUTER WAS REPLACED AS A PRECAUTIONARY MEASURE. A LAND Sep 3, 1996 · N14336 · Boeing 7373T0SDR DHL96804011Yaw Damper · malfunctionedAFTER TAKEOFF, RUDDER BEGAN EXTREME OSCILLATION. AFTER YAW DAMPER DISENGAGED, OSCILATION STOPPED. DEFERRED PER MEL.Aug 25, 1996 · N804DH · Doug DC873FSDR CALA9601211Ap Accy Unit · inoperativeUPON SELECTING THE APP MODE AIRCRAFT LOST ALL FLIGHT DIRECTION, NR 1 AIRSPEED BUG, YAW DAMPER, BOOST PUMPS, BUT NO BUSS OFF LIGHT ILLUMINATED. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT ACCESSORY UNIT AND THE Aug 23, 1996 · N14341 · Boeing 7373T0SDR AWXA960371Yaw Dmpr Module · malfunctionedPHX - FLT 2610 - UNCOMMANED RUDDER ON CLIMB-OUT, RUDDER KICKED TWICE, ONCE UPON TURNBACK. APPROX 1 HOUR LATER LATER, RUDDER KICKED ONCE AT 500 FEET FROM TOUCHDOWN. CHECKED YAW DAMPER PER FIM 22-21-00, PAGE 101. NO FAULTS NOTED. CHECKED THE YAW DAMPER MODULAug 21, 1996 · N914AW · Boeing 757225SDR 96ZZZM1325Yaw Dmpr Module · malfunctionedPHX - FLT 2610 - UNCOMMANED RUDDER ON CLIMB-OUT, RUDDER KICKED TWICE, ONCE UPON TURNBACK. APPROX 1 HOUR LATER LATER, RUDDER KICKED ONCE AT 500 FEET FROM TOUCHDOWN. CHECKED YAW DAMPER PER FIM 22-21-00, PAGE 101. NO FAULTS NOTED. CHECKED THE YAW DAMPER MODULAug 21, 1996 · N914AW · Boeing 757225SDR AWXA960397Yaw Dmp Coupler · malfunctionedPHX - FLT 2450 - DURING TAKEOFF ROLL, EXPERIENCED TWO SEVERE SIDE JOLTS ABOUT 4-5 SECONDS APART. PER QUALITY CONTROL ALERT BULLETIN NR 95-15 PERFORMED RUDDER PCU LEAK CHECK IAW A8M27001, NO DEFECTS NOTED. PER MX CONTROL CHANGED YAW DAMPNER COUPLER IAW 22-11-Aug 19, 1996 · N138AW · Boeing 7372E3SDR COMA9660133Yaw Damper · inoperativeYAW DAMPER NR 1 INOP MESSAGE ON EICAS DURING TAXI. REPLACED THE NR 1 YAW DAMPER.Aug 17, 1996 · N956CA · Cndair CL6002B19SDR USAASB96155Autopilot Sys · malfunctionedPIT - FL 1595 - ON CLIMB-OUT, THE FLT EXPERIENCED AN UNCOMMANDED ROLL TO THE LT. FLT WAS CLEARED TO 6,000 FT AND ENCOUNTERED A BUFFET AT ABOUT 4,500 FT, WHILE CLIMBING STRAIGHT AHEAD AT 230 KTS INDICATED. A/C BEGAN ROLLING SLOWLY LT WITH A CHANNEL AUTOPILOT Aug 14, 1996 · N300AU · Boeing 737301SDR C2XA96BT007Controller · failedBTV - FLT 3689 - DURING CLIMB-OUT, AUTOPILOT KICKED OFF AND RECEIVED STICK SHAKER AND OVERSPEED WARNING. COULD NOT TRIM TO LEFT AND ACFT TRIMMED BY ITSELF TO THE RT. COULD NOT RE-TRIM TO LT WITH ONE-HALF AILERON TRIM TO RT. ACFT RETURNED TO BTV AND LANDED UAug 6, 1996 · N86842 · Aerosp ATR42320SDR CALA9601134Coupler · inoperativeTHE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL OF 30 DEGREES LEFT AT 7,000 FEET AND 210 KNOTS. THE AUTOPILOT WAS DISCONNECTED AND LEVEL FLIGHT WAS REGAINED. WHEN THE AUTOPILOT WAS RECONNECTED THE AIRCRAFT FLEW NORMALLY. THE FLIGHT WAS CONTINUED WITHOUT FURTHERAug 2, 1996 · N59630 · Boeing 737524SDR 96ZZZX4872Actuator · failedUNIT FAILED AFTER 161.1 HOURS. SPAS IS INTERMITTENT TO TEST, LIGHT COMES ON AS SOON AS SWITCH IS PUT IN TEST POSITION.Jul 29, 1996SDR CA960802001Control · plate shorted(CAN) A/P SYSTEM CONTROL BOX HAD BACK PLATE LIGHTING SHORT.Jul 24, 1996 · Boeing 72725SDR AU961033Autopilot · faulty(AUS) AUTOPILOT SUSPECT FAULTY - GROUND CHECK COULD FIND NO FAULTS - DEFECT NOT CONFIRMEDJul 14, 1996 · Beech 200BEECH
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