JASC 2215
Service difficulty reports · 267
Reports filed under 2215 · Autopilot Main Servo, 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 = '2215' 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 = '2215' 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 AT0600015Servo · malfunctionedAIRCRAFT A/P DISCONNECTED AT 13,000 FEET DURING DESCENT. AT THAT POINT HAD NO ROLL CONTROL. BOTH YOKES HELD FIRMLY BY ?. AFS OVERRIDE OFF, STILL NO ROLL CONTROL. AFTER 3-4 MINS CONTROLS RELEASED. AIRCRAFT OPERATED W/O A/P TO LANDING. FOUND -AILERON SERVO/SDR 2006FA0000234Servo · intermittentINVESTIGATED PILOT REPORT OF INTERMITTENT RUDDER BOOST FAILURE ALONG WITH SIMULATANEOUS AUTOPILOT AND YAW DAMPER DISEGAGEMENT. FOUND RUDDER SERVO INTERMITTENTLY FAILING. REPLACED RUDDER SERVO WITH OVERHAULED UNIT, RUDDER BOOST AND AUTOPILOT FUNCTIONAL TESTS SDR REXA200600019Actuator · bindingON APPROACH TO MSP, CLEARED FOR VISUAL APPROACH THE AUTO-PILOT WAS DISCONNECTED. UPON ATTEMPTING TO TURN IT WAS DISCOVERED THAT BOTH AILERON CONTROLS WHERE JAMMED. FOLLOWED QRH FOR JAMMED AILERON. ROLL DISCONNECT PULLED AND CLEARED JAM ON PILOTS CONTROL. DSDR SIM2006F00002Servo · malfunctionedAIRCRAFT REQUIRED EXCESSIVE TRIM IN FLIGHT. ALSO, HAD AILERON COMPARATOR AND AP MIS-TRIM. RETRIM WITH AP OFF NOT SUCCESSFUL. THEN GOT AP COMPARATOR. WITH AP DISCONNECTED AIRCRAFT BANKED 60 DEGREES RT. IT WAS BROUGHT BACK TO CENTER AND THEN BANKED 60 DEGRESDR AU510001575Servo · faultyRUDDER AUTOPILOT SERVO/YAW DAMPER FAULTY, OTHER CAUSE: FAILURE OF INTERNAL MECHANISM.SDR AU510001494Actuator · faultyAUTOPILOT PITCH ACTUATOR INCORRECT OPERATION. ACTUATOR HAD BEEN MODIFIED IAW HONEYWELL SB KSA372-M1 TO COMPLY WITH PILATUS SB 22-004 AND AD/PC12/39A1.SDR HEEA107320Actuator · inoperativeDURING CRUISE FLIGHT, THE AIRCRAFT STARTED FISH TAILING. RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE NR 1 AFCS YAW ACTUATOR.SDR AWXA200501458Actuator · malfunctionedPHX - FLIGHT CONTROL - FLT 266 - DURING CRUISE, CREW REPORTED THAT THE AIRPLANE FLEW AT 4 DEGREE LEFT BANK WITH THE FLIGHT CONTROL PAGE SHOWING LEFT AILERON UP, SLIGHT AMOUNT OF RIGHT RUDDER, AND RUDDER TRIM INDICATION SHOWING 0.0. CREW DISENGAGED AUTOPILOT, SDR CA050427004Servo · stickingAILERON CONTROL FELT JAMMED. AFTER ADDING PRESSURE TO AILERON CONTROL, JAM BROKE FREE AND SEEMED NORMAL, OCCURRED ON CAPT AND F/O SIDE. COULD NOT DUPLICATE BUT AS A PRECAUTION REPLACED AILERON SERVO AND SERVO MOUNT. SERVO MOUNT, P/N 822-0259-001, S/N 404SDR CA041108007Cable · frayed(CAN) AT INSPECTION THE AUTOPILOT ROLL SERVO BRIDLE CABLE WAS FOUND TO BE FRAYED WHERE IT RUNS OVER IT'S PULLEYS.SDR SWIA200413871Servo · malfunctionedELECTRIC TRIM DOES NOT FUNCTION ABOVE 180 KTS.REMOVED AND REPLACED ELECTRIC TRIM MOTOR, REFERENCE 22-10-05. OPERATIONAL CHECK GOOD.SDR SWIA200413790Servo · malfunctionedDURING FLIGHT RUDDER TRIM WILL DEFLECT THE BALL HALFWAY OUT OF CENTER UNCOMMANDED. REMOVED AND REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD IAW MM 22-11-00.SDR SWIA200413791Servo · weakELECTRIC TRIM WEAK ABOVE 180 KNOTS INDICATED AIRSPEED. REMOVED AND REPLACED ELECTRIC TRIM (ELEVATOR) SERVO IAW 27-32-00. OPERATIONAL CHECK GOOD.SDR SWIA200413660Servo · malfunctionedWITH THE RUDDER YAW ENGAGED DURING APPROACH, THERE WERE SEVERAL MODERATE VIBRATIONS FELT ON THE RUDDER PEDALS (BOTH SIDES). REMOVED AND REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD IAW MM 22-10-00.SDR SWIA200413636Servo · malfunctionedAUTOPILOT WANDERS IN PITCH AXIS EXCEEDING COMMAND BARS ABOVE AND THEN BELOW. REMOVED AND REPLACED ELEVATOR SERVO. AUTOPILOT OPERATIONAL CHECK GOOD IAW MM 22-11-00.SDR SWIA200413601Servo · malfunctionedAUTOPILOT DOESN'T CAPTURE ALTITUDES. REPLACED AUTOPILOT ELEVATOR SERVO PER MM 22-10-05. OPERATIONAL CHECK GOOD PER MM 22-11-00.SDR CA040714002Servo · inoperativeTHE FLIGHT CREW REPORTED A INTERMITTENT BINDING IN ROLL CONTROL ON APPROACH, ESPECIALLY TO THE RIGHT. MILD FORCE WAS REQUIRED TO OVERCOME, THE PILOT NOTED THAT IT DOES NOT APPEAR TO SIMPLY BE HEAVY AERODYNAMIC LOADING. THE MAINTENANCE AFTER TROUBLESHOOTING PSDR SWIA200413535Servo · wornRIGHT RUDDER PEDAL RUBBING AND GRINDING AND CATCHING ON SOMETHING DURING FLIGHT CONTROL CHECK. REMOVED AND REPLACED RUDDER AUTOPILOT SERVO AND SERVO CLUTCH IAW MM 22-10-05 AND 27-00-03. OPERATIONAL CHECK GOOD. P/N 622-5734-004, S/N OFF 7268.SDR SWIA200413515Servo · malfunctionedTRIM FAIL LIGHT ILLUMINATED TWICE ON CLIMBOUT. DISCONNECTED THE AUTOPILOT TO FIND HEAVY NOSE DOWN CONTROL PRESSURE ON FLIGHT CONTROLS. REMOVED AND REPLACED THE ELEVATOR TRIM SERVO IAW MM 27-32-00 AND REMOVED AND REPLACED NR 1 APC 65B. OPS CHECKS GOOD. APC SDR SWIA200413409Servo · malfunctionedCREW REPORTED ROUGH FEEL IN ELEVATOR CONTROL. REMOVED AND REPLACED ELEVATOR SERVO REF AMM 22-10-05. OPERATIONAL CHECK GOOD.SDR SWIA200413277Servo · malfunctionedCAPTAIN'S AUTOPILOT CONTINUOUS AURAL TRIM FAIL MESSAGE AND TRIM FAIL ON MAP, AND AP PANEL. REPLACED ELEVATOR TRIM SERVO SVO-65. CAPT'S AUTOPILOT OPS CK GOOD IAW MM 22-10-00.SDR SWIA200413256Servo · malfunctionedFEEL A BINDING WHEN MOVING AILERONS. REMOVED AND REPLACED AILERON SERVO WITH SERVICEABLE UNIT IAW EMB 120 MM CHAPTER 22-10-05. OPS CHECK GOOD.SDR CA040507002Servo · failedDURING CRUISE FLIGHT, AP TRIM IS RWD POSTED ON AND OFF EVERY FEW SECONDS. AUTO-PILOT DISCONNECTED. NOTICED THAT AILERON IS EXTREMELY HARD TO MOVE ALMOST BLOCKED. IN DESCENT WITHOUT AUTO-PILOT, WE NOTICED THAT THE ELEVATOR ALSO COULD NOT BE MOVED (FL310-300 /SDR AUS20040271Servo · faulty(AUS) AUTOPILOT ROLL SERVO FAULTY. INVESTIGATION FOUND THAT THE SCREWS HOLDING THE CLUTCH HAD LOOSENED ALLOWING THE CLUTCH TO REMAIN ENGAGED WHEN THE AUTOPILOT WAS DISENGAGED.SDR CA040507001Actuator · failedCAPT REPORTED THE PITCH CONTROL STICKING ( HARD POINT FEELING ) AFTER AP DISCONNECTION. CPT HAD TO PULL THE CONTROL COLUMN TO RECOVER THE FLIGHT CONTROL. PITCH SERVO ACTUATOR WAS REPLACED.SDR SWIA200413121Servo · faultyRATCHETING NOISE HEARD WITH SLIGHT NOTCH FEELING WHEN YOKE IS MOVED TO FULL AFT POSITION. MOVED YOKE THROUGH TRAVEL WITH A/P ON, SEEMED TO CLEAR PROBLEM. REPLACED AUTOPILOT ELEVATOR SERVO. OPS CHECK GOOD IAW MM 22-10-00.SDR SWIA200412986Servo · malfunctionedWHEN AUTOPILOT ENGAGED ON FIRST OFFICER'S SIDE, THE AIRCRAFT ABRUPTLY LEVELS OFF 300 FEET PRIOR TO SELECTED ALTITUDE. REPLACED ELEVATOR SERVO AS REQUIRED. SYSTEM OPS CHECKS GOOD IAW 22-10-00.SDR AUS20040137Servo · faulty(AUS) AUTOPILOT ROLL SERVO CAPSTAN FOUND IN PIECES ON AIRCRAFT FLOOR. SIX FASTENEING SCREWS FOUND IN CLOSE PROXIMITY TO THE SERVO MOUNT.SDR SWIA200412952Servo · malfunctionedFIRST FLIGHT RUDDER CHECK NOT SMOOTH WITH HYDRAULICS ON AND OFF. REMOVED AND REPLACED NR 1 RUDDER SERVO IAW MM 22-10-09. P/N: 622-5734-002, S/N ON: 10055, S/N OFF: 7980.SDR SWIA200412922Servo · failedAUTOPILOT JERKS LEFT AND RIGHT MAINLY IN TURNS AND MOST PRONOUNCED WHEN SELECTING AND DE-SELECTING TURBULENCE BUTTON. REMOVED AND REPLACED RIGHT AUTO PILOT SERVO IAW 22-11-21. OPS CHECK GOOD. P/N: 622-4404-101, S/N OFF: 122.SDR AUS20040200Servo · failed(AUS) ELEVATOR AUTOPILOT SERVO FAILED. LOSS OF AUTOPILOT CAUSED AIRCRAFT TO PITCH UP. RT ENGINE OVERTORQUED TO 134 PERCENT AND LT ENGINE OVERTORQUED TO 125 PERCENT. OVERTORQUE INSPECTION ON ENGINES AND PROPELLERS FOUND NO DAMAGE.SDR AUS20040040Servo · faulty(AUS) AUTOPILOT CAUSED AIRCRAFT TO PITCH UP ON APPROACH. INVESTIGATION FOUND ELEVATOR AUTOPILOT SERVO FAULTY. RT ENGINE OVERTORQUED TO 134 PERCENT AND LT ENGINE OVERTORQUED TO 125 PERCENT DURING RECOVERY FROM AUTOPILOT MALFUNCTION.SDR SWIA200412767Servo · malfunctionedAUTOPILOT FAILS INTERMITTENTLY ON CAPTAIN'S SIDE. WHEN THE AUTOPILOT ENGAGES, THE AIRCRAFT IS OUT OF PITCH TRIM. ADJUSTED ELEVATOR SERVO MOUNT BREAK AWAY TORQUE AND REPLACED ELEVATOR SERVO WITH A SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00.SDR 2004FA0000022Motor · failedMOTOR FAILED SPEED OF DISPLACEMENT. SLOW SPEED. (WO NR 33814)SDR SWIA200312684Servo · malfunctionedAUTOPILOT WILL NOT CAPTURE OR HOLD ALTITUDE USING EITHER LEFT OR RIGHT FLIGHT DIRECTOR. FLIGHT DIRECTORS APPEAR TO WORK, BUT AP WANDERS OFF. REPLACED ELEVATOR SERVO WITH SERVICEABLE UNIT. BOTH APS & CPS CHECKED GOOD IAW MM 22-11-00.SDR USAASB03211Servo · failedDURING FLIGHT, EN ROUTE, THE STABILIZER OUT OF TRIM LIGHT ILLUMINATED. THE AUTOPILOT WOULD NOT TRIM. FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT SERVO MOTOR. OPS CHECK AND BITE TEST NORMAL. (M)SDR SWIA200312583Servo · malfunctionedCONTROL COLUMN BINDING WHEN PERFORMING FLIGHT CONTROL CHECK. REMOVED AND REPLACED PRIMARY ELEVATOR SERVO REF EMB 120 MM 27-00-03. OPS CHECKS GOOD. P/N: 5734002, S/N OFF: 10584.SDR SWIA200312545Servo · malfunctionedRUDDER FEELS FIRM DURING TAXI. WITH RIGHT RUDDER PRESSURE, RUDDERS POP BACK INTO DIFFERENT POSITIONS. REMOVED AND REPLACED RUDDER SERVO MOTOR. REFERENCE EMB120 MM 22-10-05. OPERATIONAL CHECKS GOOD.SDR SWIA200312480Servo · malfunctionedRUDDER PEDALS JAMMED DURING TAKEOFF ROLL. TAKEOFF ABORTED. REMOVED AND REPLACED RUDDER SERVO WITH A SERVICEABLE UNIT. OPS CHECK GOOD.SDR SWIA200312449Servo · malfunctionedAUTOPILOT DISCONNECTED IN FLIGHT (F/O SIDE) WITH RED E AND AP LIGHTS ON AP PANEL. REMOVED AND REPLACED ELEVATOR SERVO IAW EMB MM 22-10-05. OPS CHECK GOOD.SDR SWIA200312385Servo · malfunctionedCAPTAIN SIDE AUTOPILOT INOP - WILL NOT MAINTAIN ALT OR PITCH IN CLIMB. REPLACED ELEVATOR AUTOPILOT SERVO. OPERATES NORMALLY PER MM 22-11-00.SDR SWIA200312346Servo · malfunctionedENGAGING EITHER YAW DAMPER CAUSES UNCOMMANDED RUDDER DEFLECTION. REMOVED AND REPLACED RUDDER SERVO MOTOR WITH NEW SERVO MOTOR IAW 22-10-09. OPS CHECK GOOD AT THIS TIME.SDR SWIA200312307Servo · malfunctionedWITH AUTOPILOT ENGAGED ON EITHER C/A OR F/O SIDE, AP MAKES UNCOMMANDED SLOW ROLL LEFT OR RIGHT. AUTOPILOT FAIL LIGHT ON MAP DOES NOT ILLUMINATE. REMOVED AND REPLACED THE AILERON AUTOPILOT SERVO IAW EMB120 MM 27-00-03. AUTOPILOT OPS CHECK GOOD IAW MM 22-10-0SDR SWIA200312304Servo · malfunctionedCAPT REPORTS A/P WILL NOT CAPTURE ALTITUDE AS GIVEN ON THE ALT ALERTER. REPLACED ELEVATOR SVO65 SERVO WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR SWIA200312274Servo · malfunctionedDURING FLIGHT CONTROL COLUMNS BEGIN TO OSCILLATE FOLLOWED BY AUTOPILOT FAIL ON MAP AND AP ON FCP. HAPPENED ON BOTH CAPT AND FO SIDE. REPLACED PITCH DATA RELAYS K0312 & K0256 (CAPT'S SIDE). REPLACED AILERON SERVO AND AP TRANSFER BOX. AP AND AP TRANSFER OPS SDR SWIA200312251Servo · ratchetingYOKE RATCHETS WHEN MOVED FORWARD AND AFT, REPLACED ELEVATOR SERVO MOTOR WITH SERVICEABLE UNIT IAW EMB MM 27-00-03. SYSTEM OPS CHECKS GOOD.SDR HEEA088441Actuator · inoperativeAFCS ACTUATOR WILL NOT WORK. INSPECTED BY ACCESSORY SHOP AND FOUND UNIT TO BE INOPERATIVE. SENT TO HELICOPTER SUPPORT, INC. FOR WARRANTY REPAIR.SDR HEEA088413Actuator · malfunctionedNR 1 YAW FULL DEFLECTION. TO BE SENT TO VENDOR FOR REPAIR.SDR HEEA088371Actuator · stuckAFCS ACTUATOR STUCK FULL DEFLECTION LEFT NR 1.SDR HEEA088419Stop · malfunctionedAFCS ACTUATOR STOP SHAFT WILL NOT CENTER. INSPECTED BY ACCESSORY SHOP AND FOUND THAT STOP SHAFT WOULD NOT CENTER BACK ON TEST. TO BE SENT TO VENDOR FOR REPAIR.
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