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 SWIA200210955Circuit Card · defectiveYAW DAMPER NR 2 INOP, WILL NOT ENGAGE IN FLIGHT. REMOVED AND REPLACED NR 2A FCC 4000 CARD. OPS CHECKS GOOD.Jun 18, 2002 · N587SW · Cndair CL6002B19SDR C2XA02CL133Autopilot Sys · malfunctionedCLE FLIGHT 4015 THE CREW REPORTED A AUTO PILOT FAIL MESSAGE AFTER FLIGHT INTO MODERATE TURBULENCE ASSOCIATED WITH BURNING SMELL IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED AND PERFORMED AUTO PILOT CHECKS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASJun 16, 2002 · N14514 · Emb EMB135LRSDR SWIA200210961Control Panel · malfunctionedWITH AUTOPILOT SELECTED TO EITHER SIDE AND AUTOPILOT ENGAGED, RECEIVED AN AURAL TRIM FAIL WITH ASSOCIATED MAP LIGHT ON AP PANEL, RED AP & E LIGHTS ILLUMINATED. REPLACED APP-65 WITH SERVICEABLE UNIT. OPS CHECK GOOD. RERACKED APC65. BOTH SIDES TESTED. OPS CJun 15, 2002 · N593SW · Emb EMB120RTSDR HEEA080099Sensor · malfunctionedYAW CHANNEL OF SCAS KICKS OFF LINE.Jun 14, 2002 · Bell 214STSDR GTIA020646Relay · corrodedFLT 632 - TPA - DURING CLIMBS/DESCENTS IN 'IAS' OR 'MACH' MODE, AP TRIM LIGHT ILLUMINATES. FOUND A/P TRIM RELAY CONTACTS CORRODED. REMOVED AND REPLACED RELAYS. OPS CHECKS GOOD IAW RTS 22-01-05. (M)Jun 12, 2002 · N801NK · Doug DC982SDR AUS20020659Display · faulty(AUS) ADVISORY DISPLAY FROZE. AIRCRAFT IS RAAF FALCON 900 A26-077.Jun 7, 2002 · Amd FALCON900SDR HEEA079713Tarsyn · malfunctionedTARSYN PITCH AND ROLL AXIS UNRELIABLE. REPLACED WITH SERVICEABLE PART.May 30, 2002 · N2149S · Bell 412SDR HEEA079359Rate Gyro · malfunctionedGYRO CAUSES THE T/R GYRO CIRCUIT BREAKER TO POP. SENT TO MASCO FOR INSPECTION AND REPAIR.May 30, 2002 · N5435V · Skrsky S76ASDR HEEA079358Actuator · inoperativeNR 1 YAW ACTUATOR NOT RESPONDING ON SYSTEM CHECK.May 30, 2002 · N911MJ · Skrsky S76ASDR HEEA079357Knob · crackedKNOB CRACKED, SLIPS.May 30, 2002 · N760PH · Skrsky S76ASDR HEEA079356Actuator · damagedAFCS ACTUATOR CHATTERS.May 30, 2002 · N760PH · Skrsky S76ASDR HEEA079355Actuator · failedFAILED TEST ON BRAKE OUT BOX CHATTERS DURING OPERATION.May 30, 2002 · N505PH · Skrsky S76CSDR HEEA079354Actuator · intermittentNR 2 PITCH CHANNEL KICKING INTERMITTENTLY IN FLIGHT.May 30, 2002 · N911MJ · Skrsky S76ASDR ZW0A0205603Accelerometer · malfunctionedAFTER TAKEOFF YAW DAMPER OFF LT-YAW KICKS LT-RT UNSKD LANDING AFTER UNCOMMANDED RUDDER INPUT. REMOVED AND REPLACED ACCELEROMETER PER MM 22-19-01 PG 201. ACCOMPLISHED RTS PER MM 22-01-05 PG 201.May 29, 2002 · N929TW · Doug DC982SDR GTIA020530Sensor · failedLGA - FLT 874 - CIRCUIT BREAKER C17 WILL NOT RESET AUTO PILOT INOPERATIVE, WINDSHEAR INOPERATIVE, MACH TRIM INOPERATIVE, MACH TRIM INOPERATIVE DFGS NR 1 AND NR 2. PERFORMED RTS CHECK ON NR 1 AND NR 2 FAILED RT SPOILER POSITION SENSOR REPLACED RT SPOILER POSITMay 27, 2002 · N824NK · Doug DC983SDR SABA020063Damper · failedAIRCRAFT 801 ON FLIGHT 5099 FROM CLT TO PGV. DURING CRUISE THE RIGHT AND LEFT YAW DAMP FAILED. AIRCRAFT RETURNED TO THE FIELD AT CLT WITH NO OTHER PROBLEMS. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE YAW DAMP ACTUATOR. A TEST FLIGHT WMay 27, 2002 · N801WP · Dhav DHC8103SDR HEEA079194Amplifier · malfunctionedAUTOFLIGHT AMPLIFIER MALFUNCTIONED, ELEVATOR WOULD NOT STAY ON LINE.May 24, 2002 · Bell 214STSDR R7M016235185Module · inoperativeAUTO PILOT MODULE INOPERATIVE. YELLOW DIAGONAL SPLASH MARKS ON PFD AND AP2. CIRCUIT BREAKER POPPED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.May 22, 2002 · N101HN · Urocop EC135P1SDR C2XA02IA104Autopilot Sys · malfunctionedIAH- DURING TAKEOFF ROLL THE CREW NOTED THAT THE AFCS FAIL INDICATION ILLUMINATED. THE CREW ABORTED TAKEOFF, FLIGHT 3758. THE CREW PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED AND THE CREW RECEIVED CLEARANCE FOR TAKEOFF. NO DISCREPANCIES NOTED.May 11, 2002 · N14828 · Aerosp ATR42320SDR SWIA200210859Computer · faultyON TAKEOFF ROLL, AUTOPILOT AND TRIM FAIL LIGHTS ILLUMINATED. AP SELECTED TO FO. ABORTED TAKEOFF. REMOVED AND REPLACED AP COMPUTER NR 2. GROUND TESTED OK PER MM 22-10-00.May 6, 2002 · N268UE · Emb EMB120ERSDR N249TR0005Autopilot SysCapt. Flt director during App. while on "B" channel turns itself off. Bite test OK.May 5, 2002 · N249TR · Boeing 7372K5SDR N249TR0004Autopilot SysCapt. Flt director during App. while on "B" channel turns itself off. Bite test OK.May 5, 2002 · N249TR · Boeing 7372K5SDR 249TR0004Autopilot SysAuto pilot in B mode shakes aircraft while engaged. Bite ck OK.May 5, 2002 · N249TR · Boeing 7372K5SDR 0126417Control Panel · malfunctionedAFTER TAKEOFF FROM CAE TO CVG, CREW NOTICE ELECTRICAL SMELL COMING FROM THE GP300 AUTO PILOT PANEL. AN EMERGENCY WAS DECLARED WITH ATC; FLIGHT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE May 3, 2002 · N417FJ · Dorner DO328300SDR HEEA078749Amplifier · failedACTUATOR ROLL DROPS OFF DURING FLIGHT.May 1, 2002 · Bell 214STSDR UIEA02014Computer · faultyAIT TURNBACK, DURING CLIMB-OUT FROM JFK EN ROUTE TO MIA LOWER RUDDER DEFLECTION 5 DEGREES LEFT TO 3 DEGREES RIGHT CONTINUOUSLY. RETURNED TO JFK. DEFLECTIONS CONTINUED DURING DESCENT AND APPROACH. MAINTENANCE USED PITOT STATIC TEST EQUIPMENT TO FIND FAULT. Apr 29, 2002 · N508MC · Boeing 747230BSDR SWIA200210801Damper · faultyYAW DAMPER NR 1 WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER IAW 22-22-00. OPS CHECKS GOOD.Apr 21, 2002 · N496SW · Cndair CL6002B19SDR HEED089115Actuator · malfunctionedAFCS ACTUATOR FEEDBACK IN CYCLIC KICKS. REPLACE UNIT.Apr 18, 2002 · N476X · Skrsky S76CSDR GTIA020292Autopilot Sys · malfunctionedAEX - AUTOPILOT TURNS A/C RIGHT WITH TURN KNOB CENTERED AUTOPILOT OVER TRIMS AIRCRAFT DURING TURNS RESULTING IN LARGE OUT OF TRIM CORRECTIONS. (M)Apr 17, 2002 · N130NK · Doug DC9SDR XNOA01045Damper · inoperativeNR 2 YAW DAMPER WILL NOT ENGAGE AFTER START UP. TRANSFERRED TO DMI 2268 IAW ENA MEL 22-21-01. CAT "C" PLACARDS INSTALLED.Apr 16, 2002 · N224KW · Airbus A300B4203SDR GTIA0200448Bracket · corrodedFTW - YAW DAMPER ACTUATOR ATTACHED BRACKET CORRODED. REMOVED RUDDER YAW DAMPER ACTUATOR MOUNT BRACKET. INSTALLED NEW YAW DAMPER ACTUATOR MOUNT BRACKET. (M)Apr 13, 2002 · N820NK · Doug DC982SDR HEEA078592Amplifier · intermittentNR 1 ELEVATOR SYSTEM WILL ONLY STAY ON LINE FROM 15 MINUTES TO ONE HOUR 30 MINUTES. CAN RE-ENGAGE SYSTEM AND WILL WORK FOR ABOUT ANOTHER HOUR BEFORE KICKING OFF LINE.Apr 8, 2002 · Bell 214STSDR SABA020048Controller · failedAircraft 883 on flight 5078 from OAJ to CLT. During cruise flight the autopilot and both yaw-damp became inoperative. Flight continued to CLT with no other problems and no emergency declared. Maintenance removed and replaced the flight guidance controller. Apr 8, 2002 · N882CC · Dhav DHC8103SDR R7MR34634Module · inoperativeAPM2000 AUTO PILOT MODULE - UNIT INOPERATIVE. FAILURE WITH YELLOW BARS ON PFD SHOWN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.Apr 7, 2002 · N101HN · Urocop EC135P1SDR SABA020045Dampener · malfunctionedAIRCRAFT 801 ON FLIGHT 5097 FROM CLT TO PGV. AFTER TAKEOFF THE RIGHT CHANNEL OF THE YAW DAMP SYSTEM FAILED. THE YAW DAMP SYSTEM FAILED TO TRANSFER FROM THE RIGHT CHANNEL TO THE LEFT CHANNEL. THE AIRCRAFT RETURNED TO CLT AND LANDED WITH NO OTHER PROBLEMS. NApr 3, 2002 · N801WP · Dhav DHC8103SDR SWIA200210768Autopilot Sys · malfunctionedJUST AFTER ROTATION, TRIPLE CHIME AUTOPILOT WITH ASSOCIATED AUTOPILOT FAIL RED MAP INDICATION AND TRIPLE CHIME TRIM FAIL WITH ASSOCIATED TRIM FAIL MAP LIGHT. RAN QRH, RETURNED TO PSP. COMMAND BARS ON CAPTAIN'S SIDE STUCK 15 DEGREES DOWN AND 30 DEGREES RIGHT.Mar 31, 2002 · N218SW · Emb EMB120ERSDR 375PA0003Autopilot Sys · malfunctionedAUTOPILOT WOULD NOT INTERCEPT LOC AND ATTEMPTED TO CORRECT IN WRONG DIRECTION.Mar 23, 2002 · N375PA · Boeing 7373Y0SDR GTIA020242Controller · faultyACY - FLT 8012 - A/P WILL NOT STAY ENGAGED. REMOVED AND REPLACED AUTOMATIC PILOT CONTROLLER. OPERATIONAL CHECK NORMAL IAW DC9 MM 22-10-2. (M)Mar 22, 2002 · N12536 · Doug DC932SDR 372PA0007Autopilot Sys · malfunctionedVNAV FAILED REPEATEDLY, AFTER T/O, CLIMB AND CRUISE. DEFAULTED TO TOGA, SPEED, AND PATH IS ABANDONED.Mar 21, 2002 · N372PA · Boeing 737306SDR SWIA200210742Actuator · malfunctionedAT AIRSPEEDS ABOVE 290 KIAS THERE IS A VIBRATION IN THE RUDDER PEDALS. ALSO NOTICED A VIBRATION 2 MINUTES AFTER SHUTDOWN ON THE GROUND. REPLACED NR 1 YAW DAMPER ACTUATOR IAW MM 22-22-01. OPS CHECKS GOOD.Mar 20, 2002 · N594SW · Cndair CL6002B19SDR 372PA0006Autopilot Sys · malfunctionedAUTOPILOT & FD ON INTERSECTION OF LOC, AP TURNED OPPOSITE DIRECTION. CAPT WAS MASTER. CAPT'S INDICATIONS WERE WRONG. F/O INDICATIONS WERE CORRECT. OP'S CHECK OK.Mar 15, 2002 · N372PA · Boeing 737306SDR 372PA0005Autopilot SysV-Nav Disconnect in descent. A/T @ A/T limit. Aircraft abandoned path descent. Op's Ck's OKMar 15, 2002 · N372PA · Boeing 737306SDR COMA0260191Damper · faultyFLIGHT 9468 YAW DAMPER NR 1 INOP MESSAGE. REPLACED YAW DAMPER NR 1.Mar 14, 2002 · N455CA · Cndair CL6002B19SDR 372PA0004Autopilot SysVNAV Disconnects in flight without command. Will not re-engage. All nav data lost. "Verify IRS position" message appears. CND.Mar 14, 2002 · N372PA · Boeing 737306SDR HEEA078256Amplifier · will not testWILL NOT MONITOR TEST AND YAW DISENGAGE LIGHT TOO DIM.Mar 13, 2002 · Bell 214STSDR HEED089125Ahrs · inoperativeAHRS INOPERATIVE. OFF AND ON. REPLACED UNIT.Mar 8, 2002 · N478X · Skrsky S76CSDR HEEA078172Actuator · will not testOPPOSITE ELEVATOR SYSTEM WOULD NOT MONITOR TEST.Mar 7, 2002 · Bell 214STSDR HEEA078171Actuator · malfunctionedELEVATOR ACTUATOR OCCASSIONALLY KICKS OFF LINE ON TAKE OFF AND LANDING.Mar 7, 2002 · Bell 214STSDR 372PA0003Autopilot SysV-nav disconnects in flight uncommanded will not engage.Mar 7, 2002 · N372PA · Boeing 737306SDR GTIA020140Control Panel · faultyFLL - FLT 461 - A/P WOULD NOT ENGAGE IN FLIGHT (1 OR 2). REMOVED AND REPLACED GUIDANCE CONTROL PANEL. PERFORMED RTS ON BOTH DFGS COMPUTERS. BOTH SYSTEM. OPS CHECK GOOD IAW MD80 MM 22-01-05. (M)Mar 1, 2002 · N805NK · Doug DC981
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