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 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)SDR 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 OFSDR 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.SDR 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.SDR 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.SDR 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.SDR HEEA088917Amplifier · inaccurateISOLATION AMPLIFIER CAUSES ADI TO TILT 30 DEGREES LEFT QUADRANT.SDR 374PA0003Coupler · failedYAW DAMPER OFF LIGHT ILLUMINATED (YAW DAMPER DC CIRCUIT BREAKER POPPED). REPLACED YAW DAMPER COUPLER PER MM 22-13-00. OPS CHECKS GOOD.SDR SWIA200312249Control Panel · faultyYD2 INOPERATIVE, CAME ON DURING TAXI OUT, WAS UNABLE TO RE-ENGAGE. INSTALLED SERVICEABLE YAW DAMPER CONTROL PANEL. OPS CHECK GOOD.SDR 251TR0004Pcu · malfunctionedYAW DAMPER WILL NOT COUPLE. REPLACED RUDDER PCU PER MM 27-21-91. OPS CHECKS OK PER MM 27-21-91.SDR 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.SDR 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 RECESDR 2003FA0000869Housing · crackedSERVO BODY, CRACK IN LOWER FLANGE AREA.SDR AUS20031071Capsule · misinstalled(AUS) AUTOPILOT ALTITUDE HOLD CAPSULE FITTED IN A DIFFERENT POSITION TO THAT STATED BY STC. PERSONNEL/MAINTENANCE ERROR. INCORRECT FIT.SDR HEEA088381Brake · malfunctionedFORE AND AFT CYCLIC STIFF AND RATCHETY.SDR 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 SAASDR 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.SDR 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. SDR HEEA088495Isolation Mount · damagedSEPERATION BETWEEN ELASTOMER AND CENTER PORTION OF MOUNT.SDR 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.SDR 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 SDR 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 PILSDR ALGA087940Amplifier · will not testNR 2 ELEVATOR WILL NOT TEST AND ALSO KICKS OFF.SDR HEEA087972Indicator · contaminatedCONDENSATION IN TOP INDICATOR. TO BE SENT TO VENDOR.SDR 250TR0020Coupler · failedYAW DAMPER INOPERATIVE. REPLACED YAW CAMPER COUPLER PER MM 22-12-01. OPS CHECKS NORMAL.SDR 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 SDR 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.SDR 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.SDR 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.SDR BAQA087577Module · faultyAT INSTALLATION FOUND UNIT TO BE FAULTY-CAUTION WARNING TRIM/ACTUATION. SAME PROBLEM WITH THIS UNIT BEFORE REPAIR. REPLACED WITH ORIGINAL UNIT.SDR GLBA2003085Transducer · malfunctionedRUDDER PEDALS STIFF WHEN POWER ADDED. REMOVED AND REPLACED RT RUDDER BOOST TRANSDUCER, OPS CK GOOD WITH DEAD WEIGHT TESTER.SDR 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 SDR 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. PERFORSDR 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)SDR 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 REPLACSDR 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 ADSDR HEEA086928Actuator · failedWOULD NOT AUTO TRIM WITH AFCS. SENT TO MFG FOR WARRANTY REPAIR.SDR 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.SDR 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.SDR HEEA086571Brake · stickingROLL MAG BRAKE STICKS IN LATERAL MODE. TO BE SENT TO VENDOR.SDR BAQA086475Control Head · malfunctionedRC-550, AFTER ENTERING FREQUENCY THEN TRYING TO TRANSMIT. ALL ENTERED INFORMATION IS DUMPED FROM SCREEN TO DEFAULT SETTINGS. 7/2/03SDR 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)SDR SWIA200312011Control Panel · malfunctionedBOTH AUTPILOTS TURN RIGHT, UNCOMMANDED, DO NOT FOLLOW COMMAND BARS. REPLACED APP-65. OPS CHECK GOOD IAW AMM 22-00-00.SDR 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.SDR 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.SDR 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 SSDR 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 CORRECTSDR CA030708002Indicator · failed(CAN) BEARINGS VERY NOISY AND ROUGH. BUT INSTRUMENT OPERATING NORMALLY.SDR 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.SDR 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.
Back to JASC 2210