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.
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
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 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)SDR 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.SDR 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.SDR HEEA978885Tarsyn · precessesTARSYN PRECESSES EXCESSIVELY.SDR HEEA978876Tarsyn · defective#1 AFCS KICKS OCCASIONALLY.SDR 97UAL900018Coupler · malfunctionedAIRCRAFT HAS SLIGHT ROCKING MOTION WHEN CLIMBING THROUGH FL270. *S/D* DUPLICATE DISCREPANCY. SEE MRR REPORT NR 97UAL900073.SDR 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 OSDR 97UAL900009Coupler · malfunctionedYAW DAMPER PROBLEM. *S/D* DUPLICATE DISCREPANCY. SEE MRR REPORT NR 97UAL900073.SDR 97UAL900031Coupler · malfunctionedAT 14,000 FT, 230 KNOTS, THE YAW DAMPER ENGAGED. *S/D* DUPLICATE DISCREPANCY. SEE MRR REPORT NR 97UAL900073.SDR 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. SDR 96UAL900962Yaw Damper · malfunctionedTUNING NR 1 HF CAUSES RIGHT YAW DAMPER INOP, ACCOMPANIED WITH EICAS MESSAGE.SDR 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.SDR HEEA968724Tarsyn · intermittentREPORTED #1 AFCS KICKS INTERMITTENTLY ON ROLL CHANNEL. TIME SINCE REPAIR 149:15.SDR 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 SDR 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.SDR HEEA968448Control · defectiveATT. LIGHT INOPERATIVE ONLY WHEN #2 HP IS ENGAGED. TIME SINCE REPAIR 701:20.SDR COMA9610310Auto Pilot · malfunctionedDURING AUTO PILOT TEST THE ELEVATOR TRIM RUNS WILD. AUTO PILOT SYSTEM PLACED ON DEFERRED MAINTENANCE LIST.SDR 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 BASSDR 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/DSDR HEEA968360Module Assy · failedNO PITCH COMMANDS FROM AUTOPILOT THUMBWHEEL STEP #22 OF AFCS CHECK.SDR HEEA968290Tarsyn · defectiveDG PRECESSES EXCESSIVELY.SDR HEEA968274Gyro · defective#2 ROLL KICKS.SDR HEEA968273Gyro · defectiveVG KICKS IN ROLL.SDR HEEA968245Actuator · defectiveACTUATOR INTERMITTENTLY MOVES FROM RIGHT TO LEFT. TIME SINCE REPAIR 905:40.SDR HEEA968235Amplifier Assy · defectiveALT HOLD LIGHT TOO DIM ENGAGE LIGHT.SDR HEEA968232Alt Controller · defectiveALT HOLD UNRELIABLE.SDR HEEA968231Amplifier Assy · failedALT HOLD INOPERATIVE.SDR HEEA968215Amplifier Assy · malfunctionALT HOLD WILL NOT ENGAGE.SDR HEEA968076Tarsyn Gyro · precessesCOPILOTS GYRO COMPASS PRECESSES. TIME SINCE REPAIR 839:15.SDR HEEA968022Afcs · failedALTITUDE HOLD LIGHT INOPERATIVE.SDR HEEA968015Control Panel · failedROLL CHANNEL NOT SHOWING RESPONSE OR INDICATOR PANEL.SDR 96UAL900762Yaw Coupler · intermittentYAW DAMPER ABRUPTLY MOVES RUDDER OCCASIONALLY FOR NO APPARENT REASON. *S/D* YAW COUPLER WAS INTERMITTENT. REPLACED YAW DAMPER COUPLER, CHECKED OK.SDR 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.SDR 96UAL900719Servo Stop · failedAUTOPILOT CAUSES SHARP UNCOMMANDED TURNS. REPLACED AILERON SERVO AND STOP MECHANISM.SDR COMA9660145Yaw Damper · failedTHE NR 1 YAW DAMPER FAILED. REPLACED THE NR 1 YAW DAMPER.SDR 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 WITSDR 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.SDR 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 SDR DHL96804011Yaw Damper · malfunctionedAFTER TAKEOFF, RUDDER BEGAN EXTREME OSCILLATION. AFTER YAW DAMPER DISENGAGED, OSCILATION STOPPED. DEFERRED PER MEL.SDR 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 SDR 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 MODULSDR 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 MODULSDR 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-SDR COMA9660133Yaw Damper · inoperativeYAW DAMPER NR 1 INOP MESSAGE ON EICAS DURING TAXI. REPLACED THE NR 1 YAW DAMPER.SDR 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 SDR 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 USDR 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 FURTHERSDR 96ZZZX4872Actuator · failedUNIT FAILED AFTER 161.1 HOURS. SPAS IS INTERMITTENT TO TEST, LIGHT COMES ON AS SOON AS SWITCH IS PUT IN TEST POSITION.SDR CA960802001Control · plate shorted(CAN) A/P SYSTEM CONTROL BOX HAD BACK PLATE LIGHTING SHORT.SDR AU961033Autopilot · faulty(AUS) AUTOPILOT SUSPECT FAULTY - GROUND CHECK COULD FIND NO FAULTS - DEFECT NOT CONFIRMED
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