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 96ZZZX4657Actuator · defectiveACTUATOR MAKES COMPUTER CLATTER INSIDE.Jul 11, 1996 · N312LF · Bolkms BK117A3SDR SWAA960648Yaw Damper · malfunctionedEN ROUTE, EXPERIENCED UNCOMMANDED YAW INPUT AFTER TAKEOFF. CREW CONTINUED AND LANDED WITHOUT INCIDENT AT OAK. REPLACED YAW DAMPER AND RUDDER PCU PER BOEING M/M.Jul 10, 1996 · N395SW · Boeing 7373H4SDR HEEA967569Tarsyn · malfunctionTARSYN WON'T SLAVE AND PRECESSES CONSTANTLY. TIME SINCE REPAIR 489:10.Jul 10, 1996 · N107X · Bell 412SDR HEEA967515Actuator · defectiveSPIRAL DISC SWITCH LEVER HAS EXCESSIVE PLAY.Jul 5, 1996 · N39PH · Beech 200CBEECHSDR CA960619004Resistor · burnt(CAN) RESISTOR OVERHEATED, LIKELY DUE TO HIGH CURRENT LOAD OR SHORT CIRCUIT. CIRCUIT BREAKERS TRIPPED AUTOMATICALLY, BUT NOT BEFORE SIGNIFICANT OVERHEATING OF THE MOTOR DRIVE RESISTOR HAD TAKEN PLACE.Jun 17, 1996 · Piper PA31SDR 9613179965Connector · looseAIRCRAFT EXPERIENCED EXCESSIVE YAW AFTER TAKEOFF. YAW DAMPER WAS CYCLED WITH NO HELP. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE RESEATED CANNON PLUG ON YAW DAMPER ACTUATOR, OPERATIONAL CHECK NORMAL.Jun 16, 1996 · N911RW · Doug DC931SDR 96UAL900418Coupler · failedSEVERAL UNCOMMANDED RUDDER MOVEMENTS, DESCENDED TO LOWER ALTITUDE. *S/D* YAW COUPLER WAS REPLACED. SHOP FOUND YAW COUPLER RATE GYRO FAULTY, CHECKS OK.Jun 6, 1996 · N305UA · Boeing 737322SDR HEEA967327Amplifier · defective#1 ROLL AFCS KICKING IN FLIGHT. SENT TO HELICOPTER SUPPORT, INC. FOR EXCHANGE.Jun 4, 1996 · N22342 · Skrsky S76ASDR 96ZZZX3034Computer · shortedMIA/TCB - FLT 381 - PILOT REPORT: ELECTRICAL SMOKE ENTERED CABIN ABOUT 5 MINUTES AFTER TAKEOFF. SUSPECT POSSIBLY BLOWER MOTOR. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPORT: TROUBLESHOOTING DISCLOSED YAW DAMP COMPUTER INTERNALLYJun 1, 1996 · N11ZR · Beech 1900CSDR CA960827101Card · corroded(CAN) DURING APPROACH WITH FLAPS AT 40, AIRCRAFT YAWED UNTIL YAW DAMPER TURNED OFF. AUTOPILOT WAS OFF, ALTITUDE 1200 AGL, WIND 10 MPH, TEMP 18C, REPLACED COUPLER. EXTENSIVE CORROSION ON ANODE CONNECTOR LUG FOR CR3 ON A1A1 CARD.May 25, 1996 · Boeing 737217SDR CA960604015Yaw Damper · intermittent(CAN) ON APPROACH WITH 40 UNITS OF FLAPS SELECTED AIRCRAFT HAD EXCESSIVE YAW TO THE RIGHT AND LEFT. AIRCRAFT STABILIZED WHEN YAW DAMPER SELECTED OFF. AUTOPILOT OFF/ALT 1200 AGL/WIND 10/TEMP 18 DEGREES. REPLACED.May 24, 1996 · Boeing 737217SDR CA960827102Card · corroded(CAN) TAKEOFF REJECTED DUE TO VIOLENT LATERAL MOVEMENT. YAW DAMPER REPLACED. VISUAL INSPECTION OF A1A1 YAW INTERLOCK CARD REVEALED EXTENSIVE CORROSION ON ANODE CONNECTOR LUG FOR CR3. REPLACED.May 12, 1996 · Boeing 737217SDR HEEA967172Vertical Gyro · defectiveKICK IN AFCS PITCH CHANNEL.May 8, 1996 · N1545X · Skrsky S76ASDR HEEA967150Control Unit · kicksKICKS INTERMITTENTLY..May 8, 1996 · N132AE · Bolkms BK117B2SDR 96ZZZX4187Rate Gyro · failedDURING CHECK, UPPER YAW DAMPENER FAILED SYSTEM NR 2 TEST ON FLIGHT GUIDANCE MANAGEMENT ASSESSMENT PANEL. TROUBLESHOT FOUND B-CHANNEL YAW RATE GYRO INOP. ALSO, FOUND RESISTANCE OF A AND B ON LVDT IS LOWER THAN NORMAL. REMOVED AND REPLACED RATE GYRO. REMOVEDMay 6, 1996 · N228NW · Doug DC1030SDR HEEA967090Amplifier Assy · faultyROLL CHANNEL WILLNOT ENGAGE WHEN AMP IS COLD OR HIGH HUMIDITY.May 2, 1996 · N8045T · Bell 214STSDR 96UAL900304Yaw Coupler · malfunctionDURING TEN DEGREE RIGHT TURN EXPERIENCED FULL YAW DAMPER DEFLECTION TO THE LEFT. AUTOPILOT WAS ON, RUDDER AND AILERON TRIM WERE SET AT ZERO. SIGNIFICANT AILERON REQUIRED TO KEEP AIRPLANE LEVEL UNTIL YAW DAMPER WAS TURNED OFF. *S/D* REPLACED YAW COUPLER. YMay 1, 1996 · N995UA · Boeing 737291SDR COMA9660073Yaw Damper · intermittentYAW DAMPER 2 WILL INTERMITTENTLY ENGAGE AND DISENGAGE. REPLACED NR 2 YAW DAMPER ACTUATOR.Apr 20, 1996 · N951CA · Cndair CL6002B19SDR 96ZZZM873Controller · overheatedIN CRUISE EXPERIENCED O-ZONE ODOR AND INTERMITTENT SMOKE FROM BEHIND INSTRUMENT PANEL WHEN AUTO-PILOT WAS ENGAGED. GROUND INSPECTION REVEALED AUTOPILOT CONTROLLER WAS SHORTED/OVERHEATED. REPLACED CONTROLLER AND AIRCRAFT RETURNED TO SERVICE.Apr 19, 1996 · N426FB · Doug DC8F54SDR HEEA967007Amplifier · defective#1 PITCH KICKING IN FLIGHT.Apr 17, 1996 · N22342 · Skrsky S76ASDR HEEA967006Transducer · defectiveCAUSED REPEATED YAW KICKING.Apr 17, 1996 · N132AE · Bolkms BK117B2SDR HEEA966983Amplr Assy · defectiveWILL NOT MONITOR TEST. WILL NOT MOVE ACTUATOR.Apr 10, 1996 · N8045T · Bell 214STSDR DLM11960834Autopilot · inoperativeBOTH A/P INOP, NO CURRENT FAULTS. ACFT RETURNED ATL. PERFORMED RTS ON BOTH FCC, ALL NORMAL.Apr 10, 1996 · N806DE · Doug MD11SDR 97ZZZX1619Servo Mount · malfunctionPILOT NOTED THAT ON APPROACHES WITH THE AUTOPILOT DISENGAGED, THE ELEVATOR CONTROLS WOULD CATCH WHEN SLIGHT ADJUSTMENTS WERE MADE. THE SMALL AMOUNT OF PRESSURE NEEDED TO BREAK IT LOOSE WOULD CAUSE THE AIRCRAFT TO PORPOISE A FEW TIMES. SUSPECT INTERNAL PROBLEApr 10, 1996 · N410BT · Braero BAE125800ASDR 96ZZZM810Control Panel · damagedWHILE EN ROUTE TO CUU FROM DFW, THE PILOT NOTICED A BURNING SMELL AND SAW SMOKE COMING FROM THE FLIGHT GUIDANCE CONTROL PANEL. HE TRIED TO DISCONNECT THE AUTOPILOT, HOWEVER, IT WOULD NOT DISENGAGE. WHILE THEY WERE LOOKING FOR THE CIRCUIT BREAKER IT POPPED BYApr 2, 1996 · N335LS · Dorner DO328100SDR 96ZZZX3186Servo Monitor · failedNR 1 AUTOPILOT FAILURE, 1E47. REMOVED AND REPLACED.Mar 25, 1996 · N317MC · Bolkms BK117C1SDR 96ZZZX3185Actuator · defectiveNR 1 AUTOPILOT FAILURE, 1E47. REMOVED AND REPLACED.Mar 25, 1996 · N317MC · Bolkms BK117C1SDR QXEA9600092Panel · smokingEN ROUTE, SMOKE WITH ASSOCIATED SMELL COMING FROM NOSE UP/ NOSE DOWN THUMB WHEEL ON FGC. AIRCRAFT DIVERTED TO EUG AND LANDED WITHOUT FURTHER PROBLEMS. FGC AND NR 1 IAC WERE REPLACED AND AUTOPILOT OPS CHECKED GOOD.Mar 3, 1996 · N332PH · Dorner DO328100SDR 96ZZZX2800Duplex Actuator · faultyPITCH CHANNEL DISENGAGEMENT AND PITCH C5 FAULT.Mar 2, 1996 · N92MD · Aerosp SA365N1SDR PLG3196E1Computer · failedFLT NR 4356 - ALB-BOS - AFTER TAKEOFF, FUMES AND SMOKE APPEARED IN THE CABIN AND COCKPIT. CREW DECLEARED AN EMERGENCY, DEPLOYED THE OXYGEN MASKS AND RETUREND TO ALB LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE YAW DAMP CIRCUIT BMar 1, 1996 · N7203C · Beech 1900CSDR 96ZZZX2801Duplex Actuator · failedFAILED INSULATION TEST LOW MEG CHECK.Feb 29, 1996 · N97MD · Aerosp SA365N1SDR HEEA966773Amplifier Assy · defectiveROLL NETWORK VOLTAGES ARE ERRATIC. TIME SINCE REPAIR 470:50.Feb 28, 1996 · N8045T · Bell 214STSDR HEEA966736Amplifier Assy · defectiveAMPLIFIER WILL NOT TEST OR ENGAGE.Feb 28, 1996 · N3897N · Bell 214STSDR CA960223016Auto Trim Sys · faulty(CAN) WHILE FLYING WITH AUTO PILOT ENGAGED, THE AUTO-TRIM SYSTEM (MISS-TRIM) LIGHT COMES ON AND THE SYSTEM IS UNABLE TO CORRECT THIS SITUATION THUS DISENGAGES THE AUTOPILOT AFTER A SHORT PERIOD OF TIME. CESSNA HAS BEEN MADE AWARE OF THE PROBLEM AND STATES THERFeb 15, 1996 · Cessna 560CESSNASDR CA960222021Control Cable · misinstalled(CAN)IN CRUISE,AT FL250,WITH AUTO PILOT ON, AIRCRAFT OSCILLATING ABOUT LATERAL AXIS,APPROX. 60 TO 80 FEET.INSPECTION FOUND NO TENSION ON THE AUTOPILOT SERVO CABLE WHICH SHOULD BE 15 TO 20 LBS.LH ELEVATOR CONTROL CABLE TENSION WITH SERVO DISCONNECTED WAS FOUND Feb 14, 1996 · Dhav DHC8311SDR CAL960283Yaw Damper · failedEWR - FLT 0485 - THE AIRCRAFT TAIL BEGAN TO KICK BACK AND FORTH IN-FLIGHT TO EWR. THERE WAS NO NOTICEABLE RUDDER PEDAL MOVEMENT. THE KICKING OCCURRED IN BOTH AUTOPILOT A AND B MODES. WHEN THE YAW DAMPER WAS TURNED OFF THE CONDITION WORSENED. THE AUTOPILOT Feb 13, 1996 · N59302 · Boeing 7373T0SDR CA960515006Turn And Slip · malfunction(CAN) AUTOPILOT DOES NOT MAINTAIN BANK ANGLES IN RIGHT TURN ONLY, ROLLS 45 DEGREES, PITCHES DOWN. SYSTEM TROUBLESHOT AND EVENTUALLY TURN AND SLIP INDICATORS REPLACED AND AIRCRAFT RETUNED TO SERVICE. ADDITIONAL SDR 960222011 WITH SAME TROUBLE ON ANOTHER AIRCRFeb 9, 1996 · Beech A100SDR 96ZZZM614Yaw Damp Servo · failedCIU - CREW DETECTED SMELL OF ELECTRICAL SMOKE THEN YAW DAMP CB POPPED. MAINTENANCE REPLACED YAW DAMP SERVO, SYSTEM CHECKED OK. (M)Feb 9, 1996 · N98GL · Beech 1900CSDR HEEA966657Control · defectiveCPL LIGHT WILL NOT COME ON WHEN CPL SWITCH IS PUSHED.Feb 6, 1996 · N108X · Bell 412SDR HEEA966655Tarsyn 333 · fail testFAILED FAST MCHRONIZATION RATE TEST #8.4 ON SST.Feb 6, 1996 · N3893P · Bell 412SDR HEEA966546Computer · defectiveWITH BOTH HELIPILOTS ENGAGED, IN A TURN A SLIGHT TAP IS FELT IN THE CYCLIC STICK.Jan 29, 1996 · N3893N · Bell 412SDR DLM88960220Switch · failedON FINAL APPROACH A/P WOULD NOT DISCONNECT WITH THE YOKE DISCONNECT SWITCHES OR THE ON/OFF SWITCH ON THE AUTO FLIGHT CONTROL PANEL. IT WAS NECESSARY TO PULL C/BS TO DISCONNECT A/P. REPLACED MODE CONTROL PANEL OPERATION NORMAL. ANALYSIS REVEALED THAT THE FGCJan 28, 1996 · N996DL · Doug MD88SDR 96ZZZX1240Actuator · failedSTL - FLT 503 - DURING CLIMB, UNCOMMANDED RUDDER MOVEMENT WAS DETECTED. REMOVED AND REPLACED YAW DAMPER ACTUATOR DUE TO INTERNAL FAILURE, MFG PN 2589445-933. OPERATIONAL CHECK NORMAL. CHECK C-12 - 1-11-95 - STL.Jan 26, 1996 · N410EA · Doug DC951SDR 96ZZZM208Actuator · failedSTL - DURING CLIMB, UNCOMMANDED RUDDER MOVEMENT WAS DETECTED. REMOVED AND REPLACED YAW DAMPER ACTUATOR DUE TO INTERNAL FAILURE, MFG P/N 2589445-933. OPERATIONAL CHECK NORMAL. (M)Jan 26, 1996 · N410EA · Doug DC951SDR 96ZZZX4241Switch · frozenON PRE-FLIGHT, FOUND AUTOPILOT DISCONNECT SWITCH FROZEN. THE SPRING LOADED PUSH BUTTON IS FIXED OR FROZEN SOLID. SUBMITTER STATED EVEN BEFORE IT FROZE, IT FELT CATCHY OR SCRATCHY WHEN BUTTON WAS DEPRESSED.Jan 22, 1996 · N4S · Beech B300SDR CA960320519Computer · inoperative(CAN)ON ENGAGING AUTO PILOT AFTER TAKEOFF, RED WARNING LIGHT AND "GEAR NOT DOWN" MESSAGE WITH A QUICK PITCH UP AND DOWN OF AIRCRAFT. AIRCRAFT RETURNED TO BASE. MAINTENANCE ACCOMPLISHED C.F.D.S. TEST OF A.F .S. AND DETERMINED F.A.C. #2 WAS AT FAULT. REPLACED F.Jan 20, 1996 · Airbus A320211SDR HEEA966489Actuator · defective#1 ROLL CHATTERS. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND TEST POINT E.4 OUT OF CALIBRATION.Jan 19, 1996 · N31219 · Skrsky S76ASDR 96ZZZX820Trim Monitor · failedON THREE SEPARATE OCCASIONS, AIRCRAFT HAS BEEN DEICED. ON ALL THREE OCCASIONS, THE AUTOPILOT QUIT SHORTLY AFTER TAKEOFF. INVESTIGATION REVEALED THE TRIM MONITOR BOX MOUNTED AT THE BASE OF VERTICAL FIN SPAR (AFT SIDE) WAS SATURATED WITH DEICING FLUID. KING RJan 17, 1996 · N92UG · Lear 31ASDR 96ZZZX2045Bridle Cable · pin slippageC/W CENTURY FLT SYSTEM SB CFS-95-01 DATED 10-11-95. BRIDLE CABLE INSPECTION FOUND PIN SLIPPAGE ON CABLE. REPLACED CABLE.Jan 12, 1996 · N5598J · Piper PA32260SDR 96ZZZX2044Bridle Cable · pin slippageC/W CENTURY FLT SYSTEM SB CFS-95-01 DATED 10-11-95. BRIDLE CABLE INSPECTION FOUND PIN SLIPPAGE ON CABLE. REPLACED CABLE.Jan 12, 1996 · N6589J · Piper PA28180
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