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 96ZZZX4657Actuator · defectiveACTUATOR MAKES COMPUTER CLATTER INSIDE.SDR 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.SDR HEEA967569Tarsyn · malfunctionTARSYN WON'T SLAVE AND PRECESSES CONSTANTLY. TIME SINCE REPAIR 489:10.SDR HEEA967515Actuator · defectiveSPIRAL DISC SWITCH LEVER HAS EXCESSIVE PLAY.SDR 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.SDR 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.SDR 96UAL900418Coupler · failedSEVERAL UNCOMMANDED RUDDER MOVEMENTS, DESCENDED TO LOWER ALTITUDE. *S/D* YAW COUPLER WAS REPLACED. SHOP FOUND YAW COUPLER RATE GYRO FAULTY, CHECKS OK.SDR HEEA967327Amplifier · defective#1 ROLL AFCS KICKING IN FLIGHT. SENT TO HELICOPTER SUPPORT, INC. FOR EXCHANGE.SDR 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 INTERNALLYSDR 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.SDR 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.SDR 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.SDR HEEA967172Vertical Gyro · defectiveKICK IN AFCS PITCH CHANNEL.SDR HEEA967150Control Unit · kicksKICKS INTERMITTENTLY..SDR 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. REMOVEDSDR HEEA967090Amplifier Assy · faultyROLL CHANNEL WILLNOT ENGAGE WHEN AMP IS COLD OR HIGH HUMIDITY.SDR 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. YSDR COMA9660073Yaw Damper · intermittentYAW DAMPER 2 WILL INTERMITTENTLY ENGAGE AND DISENGAGE. REPLACED NR 2 YAW DAMPER ACTUATOR.SDR 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.SDR HEEA967007Amplifier · defective#1 PITCH KICKING IN FLIGHT.SDR HEEA967006Transducer · defectiveCAUSED REPEATED YAW KICKING.SDR HEEA966983Amplr Assy · defectiveWILL NOT MONITOR TEST. WILL NOT MOVE ACTUATOR.SDR DLM11960834Autopilot · inoperativeBOTH A/P INOP, NO CURRENT FAULTS. ACFT RETURNED ATL. PERFORMED RTS ON BOTH FCC, ALL NORMAL.SDR 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 PROBLESDR 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 BYSDR 96ZZZX3186Servo Monitor · failedNR 1 AUTOPILOT FAILURE, 1E47. REMOVED AND REPLACED.SDR 96ZZZX3185Actuator · defectiveNR 1 AUTOPILOT FAILURE, 1E47. REMOVED AND REPLACED.SDR 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.SDR 96ZZZX2800Duplex Actuator · faultyPITCH CHANNEL DISENGAGEMENT AND PITCH C5 FAULT.SDR 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 BSDR 96ZZZX2801Duplex Actuator · failedFAILED INSULATION TEST LOW MEG CHECK.SDR HEEA966773Amplifier Assy · defectiveROLL NETWORK VOLTAGES ARE ERRATIC. TIME SINCE REPAIR 470:50.SDR HEEA966736Amplifier Assy · defectiveAMPLIFIER WILL NOT TEST OR ENGAGE.SDR 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 THERSDR 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 SDR 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 SDR 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 AIRCRSDR 96ZZZM614Yaw Damp Servo · failedCIU - CREW DETECTED SMELL OF ELECTRICAL SMOKE THEN YAW DAMP CB POPPED. MAINTENANCE REPLACED YAW DAMP SERVO, SYSTEM CHECKED OK. (M)SDR HEEA966657Control · defectiveCPL LIGHT WILL NOT COME ON WHEN CPL SWITCH IS PUSHED.SDR HEEA966655Tarsyn 333 · fail testFAILED FAST MCHRONIZATION RATE TEST #8.4 ON SST.SDR HEEA966546Computer · defectiveWITH BOTH HELIPILOTS ENGAGED, IN A TURN A SLIGHT TAP IS FELT IN THE CYCLIC STICK.SDR 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 FGCSDR 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.SDR 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)SDR 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.SDR 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.SDR HEEA966489Actuator · defective#1 ROLL CHATTERS. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND TEST POINT E.4 OUT OF CALIBRATION.SDR 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 RSDR 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.SDR 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.
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