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 AALA20030886Actuator · defectiveEN ROUTE JFK-MIA, AIRCRAFT HAD OSCILLATIONS THAT WERE LATERAL IN MOTION. CREW DECLARED AN EMERGENCY AND AIRCRAFT RETURNED TO JFK WITHOUT FURTHER INCIDENT. REPLACED YAW DAMPNER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Aug 21, 2003 · N41063 · Airbus A300B4605RSDR QXEA200301008Autopilot Sys · malfunctionedON DESCENT RECEIVED AN AURAL TRIM IN MOTION WARNING FOLLOWED BY STAB CHANNEL 2 INOPERATIVE WHITE MESSAGE AND AUTOPILOT PITCH TRIM CAUTION MESSAGE. FOLLOWED CHECKLIST AND DISENGAGED AUTIOPILOT. RE-TRIMMED THE AIRCRAFT MANUALLY. PERFORMED FIM OPERATIONAL TEST OFAug 20, 2003 · N609QX · Cndair CL6002C10SDR SWIA200312296Switch · defectiveAUTOPILOT WILL NOT TEST. AMBER 'R' ON PEDISTAL PANEL. REPLACED FIRST OFFICER'S AP DISCONNECT SWITCH AS REQUIRED. SYSTEM OPS CHECK GOOD IAW 22-10-00.Aug 19, 2003 · N579SW · Emb EMB120ERSDR CA031106011Actuator · failed(CAN) DURING TAKE OFF ROLL YAW DAMPER-DISENGAGED. TAKEOFF ABORTED AND TCC CONTACTED. THE PROBLEM WAS LOCALIZED TO THE YAW DAMPER ACTUATOR WHICH WAS REPLACED. THE FAULT WAS LATER CONFIRMED TO BETHE LINEAR POTENTIOMETER AT THE SHOP.Aug 18, 2003 · Bombdr DHC8400SDR 375PA0019Coupler · inoperativeYAW DAMPER INOPERATIVE. RELEASED ON MEL 22-3-1. 8/16/2003: REPLACED YAW DAMPER COUPLER IAW MM22-12-32 PG.401 AND ACCOMPLISHED OPS. TEST, SELF TEST, SERVO TEST AND RUDDER PRESSURE REDUCER TEST. ALL OK.Aug 16, 2003 · N375PA · Boeing 73739ASDR CA030819001Servo · malfunctioned(CAN) DURING TAKE-OFF ROLL, OUT OF EXETER AND A COUPLE OF TIMES IN FLT, CREW REPORTED RUDDER KICKED, FOLLOWED BY A BANK OF 10 DEGREES. THE YAW AUTOPILOT ACTUATOR WAS REPLACED AND THE SYSTEM WAS CONFIRMED SERVICEABLE AFTER A VERIFICATION FLT.Aug 13, 2003 · Airbus A310300SDR HEEA088917Amplifier · inaccurateISOLATION AMPLIFIER CAUSES ADI TO TILT 30 DEGREES LEFT QUADRANT.Aug 12, 2003 · N3893P · Bell 412SDR 374PA0003Coupler · failedYAW DAMPER OFF LIGHT ILLUMINATED (YAW DAMPER DC CIRCUIT BREAKER POPPED). REPLACED YAW DAMPER COUPLER PER MM 22-13-00. OPS CHECKS GOOD.Aug 9, 2003 · N374PA · Boeing 73736MSDR SWIA200312249Control Panel · faultyYD2 INOPERATIVE, CAME ON DURING TAXI OUT, WAS UNABLE TO RE-ENGAGE. INSTALLED SERVICEABLE YAW DAMPER CONTROL PANEL. OPS CHECK GOOD.Aug 8, 2003 · N916SW · Cndair CL6002B19SDR 251TR0004Pcu · malfunctionedYAW DAMPER WILL NOT COUPLE. REPLACED RUDDER PCU PER MM 27-21-91. OPS CHECKS OK PER MM 27-21-91.Aug 6, 2003 · N251TR · Boeing 737228SDR 250TR0022Gyro · malfunctionedB CHANNEL AUTO PILOT JERKS EXCESSIVELY IN RIGHT AND LEFT TURNS. PLACED B CHANNEL AUTO PILOT ON MEL 22-1. 8/15/2003: REPLACED NR 1 AND 3 VERTICAL GYROS PER MM34-22-1. AUTO PILOT BITE TEST NORMAL PER MM22-11-01.Aug 3, 2003 · N250TR · Boeing 7372K5SDR SWIA200312227Pin · backed outAUTOPILOT DISCONNECTED IN FLIGHT WITH 'AUTOPILOT FAIL' ON MAP AND 'AP' ON AUTOPILOT CONTROL PANEL. WHEN AP DISCONNECTED, A/C FELT OUT OF TRIM IN ROLL. DISCONNECT OCCURED WITH FO FLYING. MEL 22-11-1A. FOUND PIN 12 AT J2 OF NR 2 AUTO PILOT COMPUTER RACK RECEAug 3, 2003 · N268UE · Emb EMB120ERSDR 2003FA0000869Housing · crackedSERVO BODY, CRACK IN LOWER FLANGE AREA.Jul 30, 2003 · N1540 · Gulstm GULFSTREAMGVSDR AUS20031071Capsule · misinstalled(AUS) AUTOPILOT ALTITUDE HOLD CAPSULE FITTED IN A DIFFERENT POSITION TO THAT STATED BY STC. PERSONNEL/MAINTENANCE ERROR. INCORRECT FIT.Jul 29, 2003 · Cessna U206GSDR HEEA088381Brake · malfunctionedFORE AND AFT CYCLIC STIFF AND RATCHETY.Jul 24, 2003 · N911MJ · Skrsky S76ASDR MALA030345Autopilot Sys · malfunctionedINFLIGHT ON FLIGHT NR 3114, AT 15000 FT AN ELEV MISTRIM NOTICED, DISCONNECTED AUTOPILOT TO RETRIM AND FOUND MAIN ELEVATOR PITCH TRIM HAD FAILED, STANDBY WORKS NORMALLY. AIR RETURN TO MSP. MAINTENANCE COMPLETED OPERATIONAL TEST OF ELEVATOR TRIM SYSTEM PER SAAJul 23, 2003SDR 234TR0003Sensor · malfunctionedAUTO-PILOT A&B NEUTRAL SHIFT SENSOR OUT OF TOLERANCE PER ELEVATOR RIGGING BITE TEST. REMOVED, REPLACED, AND ADJUSTED NEUTRAL SHIFT SENSOR. OPS. CHECKS GOOD PER MM 22-11-122.Jul 15, 2003 · N234TR · Boeing 737228SDR 03FDEA01091Controller · failedCWF CLOSER DURING CATIII APPROACH WITH A NORMAL GLIDE SLOPE AND SINK RATE A RAPID COUNTDOWN (50,40,30,ECT) OCCURED AND THE AIRCRAFT FLARED EARLY FOLLOWED BY A PUSHOVER AND SUBSEQUENT FIRM LANDING. REMOVED AND REPLACED TCC IAW AMM 22-36-34-4 AND RADIO ALT. Jul 11, 2003 · N670FE · Airbus A300B4605RSDR HEEA088495Isolation Mount · damagedSEPERATION BETWEEN ELASTOMER AND CENTER PORTION OF MOUNT.Jul 10, 2003 · N911RC · Bell 230SDR SWIA200312174Actuator · malfunctionedINTERMITTENT UNCOMMANDED RIGHT RUDDER INPUTS IN CLIMB, CRUISE, WITH OR WITHOUT AP ON. MUST HOLD + 5 DEGREES RIGHT RUDDER FOR COORDINATED FLIGHT. REMOVED AND REPLACED NR 1 YAW DAMPER ACTUATOR IAW CL600 MM 22-22-01. OPS CHECK GOOD.Jul 5, 2003 · N591SW · Cndair CL6002B19SDR KPVA200331Relay · failedDURING CLIMB-OUT, 'AFTER T/O' CHECKLIST, WHEN AUTO-FEATHER DESELECTED ARM LIGHT REMAINED ILLUMINATED. COMPLETED A NORMAL APPOACH AND LANDING, TAXIED TO TERMINAL. MAINTENANCE T/S SYSTEM BY SWAPPING THE NR 1 AND NR 2 TSCU'S, DID NOT SOLVE PROBLEM REPLACED THE Jul 3, 2003 · N808WP · Dhav DHC8103SDR BAQ2003F00002Roll Servo · inoperativeREMOVED AND REPLACED SERVO WITH AN OVERHAULED SERVO. UPON GROUND RUN AND LEAK CHECK, PILOT STATED: ON START, AIRCRAFT CYCLIC WENT FULL LEFT. COULD NOT GET CENTERED. PILOT SHUT DOWN AIRCRAFT BEFORE POSSIBLE ROLL-OVER. REMOVED AND INSPECTED SERVO. FOUND PILJul 2, 2003 · N915ME · Aerosp AS365N2SDR ALGA087940Amplifier · will not testNR 2 ELEVATOR WILL NOT TEST AND ALSO KICKS OFF.Jun 29, 2003 · N390AL · Bell 214STSDR HEEA087972Indicator · contaminatedCONDENSATION IN TOP INDICATOR. TO BE SENT TO VENDOR.Jun 28, 2003 · N505PH · Skrsky S76CSDR 250TR0020Coupler · failedYAW DAMPER INOPERATIVE. REPLACED YAW CAMPER COUPLER PER MM 22-12-01. OPS CHECKS NORMAL.Jun 27, 2003 · N250TR · Boeing 7372K5SDR N382004F00000Computer · inoperativeAUTOPILOT SYSTEM, WHEN AUTOPILOT SELECTED TO ALTITUDE PRESET, A/C DID NOT CAPTURE SELECTED ALTITUDE. FMS HEADING IN ONE DIRECTION AC DID NOT CAPTURE HEADING AS SELECTED. ON APPROACH TO RDG, PILOT WAS UNABLE TO SELECT APP NR ON AUTOPILOT CONTROLLER. REMOVED Jun 26, 2003 · N192FG · Gulstm G1159ASDR 373PA0016Computer · malfunctionedWHEN AUTO PILOT -B- ENGAGED, HDG SELECT ONLY GIVES 10 DEGREES OF BANK. PLACED ON MEL 22-15-8. 6/28/2003: RAN AUTO PILOT BITE TEST IAW MM 22-11-00. OPS CHECKS NORMAL AT THIS TIME. SWAPPED FCC'S AS A PRECAUTION.Jun 26, 2003 · N373PA · Boeing 7373Y0SDR 252TR0005Coupler · inoperativeAUTO PILOT AT 315 KTS TRIM ROLLS BACK AND FORTH 3 TURNS EACH DIRECTION. REPLACED MACH TRIM COUPLER IAW MM 22-21-0. OPS TEST NORMAL.Jun 23, 2003 · N252TR · Boeing 737228SDR AUS20030669Handle · transposed(AUS) AIRCRAFT PITCH AND ROLL DISCONNECT HANDLES TRANSPOSED. THE ROLL DISCONNECT HANDLE WAS IN THE PITCH DISCONNECT HANDLE POSITION AND THE PITCH DISCONNECT HANDLE WAS IN THE ROLL HANDLE POSITION.Jun 18, 2003 · Dhav DHC8102SDR BAQA087577Module · faultyAT INSTALLATION FOUND UNIT TO BE FAULTY-CAUTION WARNING TRIM/ACTUATION. SAME PROBLEM WITH THIS UNIT BEFORE REPAIR. REPLACED WITH ORIGINAL UNIT.Jun 18, 2003 · N911TS · Urocop EC135P1SDR GLBA2003085Transducer · malfunctionedRUDDER PEDALS STIFF WHEN POWER ADDED. REMOVED AND REPLACED RT RUDDER BOOST TRANSDUCER, OPS CK GOOD WITH DEAD WEIGHT TESTER.Jun 17, 2003 · N208GL · Beech 1900DSDR USAABB03093Control Panel · failedPHL - FLT 98 - AT FL330, WITH CENTER COMMAND SELECTED, THE AUTOPILOT DISCONNECTED WITH THE ASSOCIATED LIGHTS AND WARNING. A STRONG ACRID SMELL WAS NOTED COMING FROM THE MODE CONTROL PANEL (MCP). THE AUTOPILOT WAS SWITCHED. FLIGHT RETURNED TO PHL AND LANDED Jun 15, 2003 · N650US · Boeing 767201SDR 375PA0016Connector · dirtyVARIOUS ANOMALOUS (SIC) INDICATIONS FROM FMA/MCP. A/T ANN RAPIDLY CHANGES MODES, SPURIOUS ALTITUDES APPEAR. IN ALT HOLD A/C CLIMBS & DESCENDS +/- 300 FT. VS MODE CYCLES, ALT HOLD CYCLES. CLEANED AND CHECKED EFIS RT AND CLEANED CONNECTOR TO THE FMA. PERFORJun 14, 2003 · N375PA · Boeing 737317SDR AALA20030633Actuator · malfunctionedWHEN YAW DAMP NR 1 IS ENGAGED, RUDDER MOVES RAPIDLY TO THE LT AND REMAINS IN THAT POSITION UNTIL ITS DISARM/DISENGAGED. REPLACED YAW DAMP NR 1 ACTUATOR AND LEAK, OPERATIONAL CHECKED GOOD. (M)Jun 3, 2003 · N14065 · Airbus A300B4605RSDR WRLA200312Control Panel · inoperativeAUTOPILOTS 1 AND 2 FAILED TO ENGATE RETURNED TO LAX, THE AIRCRAFT RETURNED TO THE DEPARTING STATION LAX FOR REPAIR. ALIGNED INU'S PRESSURIZED HYDRAULICS, YAW UPPER AND LOWER YAW ON, FD'S ON FLAGS IN VIEW PERFORMED TEST TO SYSTEM. OPERATIONAL CHECKED OK REPLACJun 3, 2003 · N541SA · Doug DC10SDR CA030606002Clamp · jammed(CAN) AUTO PILOT BRIDLE CABLE CLAMP (PITCH) JAMS AGAINST EACH OTHER AT OR NEAR FULL UP (NOSE UP) CONTROL MOVEMENT. THIS IS A RECURRING PROBLEM. THIS HAS ALSO HAPPENED YEARS AGO WITH OLD EDO-AIR (ALTIMATIC III A/P). THESE CLAMPS ARE NEWER STYLE (MANDITORY BY ADMay 29, 2003 · Piper PA31SDR HEEA086928Actuator · failedWOULD NOT AUTO TRIM WITH AFCS. SENT TO MFG FOR WARRANTY REPAIR.May 29, 2003 · Bell 412SDR ABXA030182Computer · defectiveAUTOPILOT ROLLED INTO A 30 DEGREES LEFT BANK UNCOMMANDED. REPLACED THE ROLL AXIS COMPUTER. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 22-10-00.May 28, 2003 · N948AX · Doug DC931SDR SWIA200312020Computer · malfunctionedTHE CAPTAIN'S FLIGHT DIRECTOR INOP WITH AN INTERMITTENT COMPUTER FLAG INDICATION ON THE ADI, FOLLOWED BY TRIM AND AP INDICATIONS ON THE FCP. REPLACED NR 1 AUTOPILOT COMPUTER FLIGHT DIRECTOR. OPS CHECK NORMAL.May 23, 2003 · N291SW · Emb EMB120ERSDR HEEA086571Brake · stickingROLL MAG BRAKE STICKS IN LATERAL MODE. TO BE SENT TO VENDOR.May 22, 2003 · N761PH · Skrsky S76ASDR BAQA086475Control Head · malfunctionedRC-550, AFTER ENTERING FREQUENCY THEN TRYING TO TRANSMIT. ALL ENTERED INFORMATION IS DUMPED FROM SCREEN TO DEFAULT SETTINGS. 7/2/03May 21, 2003 · N533ME · Urocop EC135T1SDR A6WA200340074Actuator · malfunctionedYAW DAMPER NR 2 WILL NOT STAY ENGAGED WHEN MOVING AIRCRAFT. YAW DAMP INOPERATIVE STATUS MESSAGE. REMOVED AND REPLACED NR 2 YAW DAMPER ACTUATOR. CHECKS OK. (M)May 20, 2003 · N410AW · Cndair CL6002B19SDR SWIA200312011Control Panel · malfunctionedBOTH AUTPILOTS TURN RIGHT, UNCOMMANDED, DO NOT FOLLOW COMMAND BARS. REPLACED APP-65. OPS CHECK GOOD IAW AMM 22-00-00.May 19, 2003 · N197SW · Emb EMB120ERSDR 372PA0028Computer · malfunctionedALTITUDE ALERT HORN DOES NOT WORK. COMPLETED OPERATIONAL CHECKS PER MM 22-11-01 AND PERFORMED BITE CHECK USING FMC DFCS. NO DEFECTS NOTED.May 11, 2003 · N372PA · Boeing 737306SDR SWIA200311972Actuator · malfunctionedBEFORE PUSH BACK, NR 1 YD INOP STATUS MESSAGE CAME ON. REPLACED NR 1 YAW DAMPER ACTUATOR WITH SERVICEABLE UNIT IAW MM 22-22-01. OPS CHECK GOOD.May 10, 2003 · N442SW · Cndair CL6002B19SDR SWIA200311970Computer · malfunctionedAT CRUISE, AIRCRAFT BEGAN YAW SERIES LEFT AND RIGHT WITH AUTHORITY. AFTER SEVERAL SECONDS, YD2 INOP STATUS MESSAGE APPEARED AND AIRCRAFT RETURNED TO NORMAL FLIGHT. AT CRUISE, AUTOPILOT ON, AND YD2 OFF, AIRCRAFT BEGAN YAW SERIES LEFT AND RIGHT AFTER SEVERAL SMay 8, 2003 · N939SW · Cndair CL6002B19SDR FCPR20030010Autopilot Sys · malfunctionedPILOT REPORTED THAT WHILE FLYING IN IMC CONDITIONS WITH AUTO PILOT ENGAGED IN HEADING MODE, HE COMMANDED A COURSE CHANGE AND THE AUTOPILOT PERFORMED A TURN IN THE OPPOSITE DIRECTION. CONDUCTED AT P-STATIC TEST AND FOUND SEVERAL STATIC WICKS NOT BONDED CORRECTMay 6, 2003 · N700PX · Socata TBM700SDR CA030708002Indicator · failed(CAN) BEARINGS VERY NOISY AND ROUGH. BUT INSTRUMENT OPERATING NORMALLY.May 5, 2003 · Cessna 441SDR MEX2003154Valve · failedDURING COCKPIT CHECK THE CAPTIAN FOUND PROBLEMS WITH (AUTO LAND) BUTTON AND LEFT PRESSURE REGULATOR VALVE. THE BUTTON WAS DEFERRED BY MEL CATEGORY C AD THE VALVE WAS REPLACED IAW MM.May 3, 2003 · N491SH · Doug MD83SDR 801DM0009Servo · malfunctionedNO LAND 3 AILERON SERVO FCCR MESSAGE ON MCDP. REMOVED AND INSTALLED SERVICEABLE AILERON LATERAL CONTROL SERVO. ADJUSTMENT, TEST, LEAK AND OPS CHECK GOOD IAW MM 22-13-03.May 3, 2003 · N801DM · Boeing 757200
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