JASC 2216
Service difficulty reports · 128
Reports filed under 2216 · Autopilot Trim 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 = '2216' 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 = '2216' 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 6CBA2025121625001Adapter · faultyDURING A ROUTINE FLIGHT FROM KPSM TO KBTV, THE CREW EXPERIENCED DURING CLIMB THE YAW DAMP WOULD NOT ENGAGE. ON THE THIRD ATTEMPT TO ENGAGE THE YAW DAMP, AP FAIL CAS MESSAGE FOLLOWED 2 SECONDS LATER BY A RED TRIM RUNAWAY CAS. AN EMERGENCY WAS DECLARED AND THE SDR 3WTR20221013Bolt · corrodedWHILE COMPLYING WITH EMBRAER SB 505-22-0004 R3, THE SUBJECT CLUTCH RETAINING BOLT WAS FOUND TO BE SEVERELY CORRODED. THE PURPOSE OF THE SERVICE BULLETIN IS TO INSPECT AND REPLACE THIS BOLT BUT THE CORROSION FOUND ON THIS BOLT WAS THROUGH APPROXIMATELY 50% OF TSDR 9JLA2022071938701Trim System · failedTHE FLIGHT CREW REPORTED THE PITCH TRIM DID NOT WORK WITH AUTO-PILOT ELECTRIC PITCH TRIM ON BOTH THE LEFT AND RIGHT SIDE BELOW 200KTS ON DESCENT. OPERATIONS WERE CONTINUED UNDER MEL 27-31-01. THE BASE MAINTENANCE TEAM DETERMINED THE ELEVATOR ELECTRIC TRIM MOTOSDR UIEA2022070700729None · none4 UN-COMMANDED LEFT YAW EVENTS WHILE IN CRUISE. EICAS YAW DAMPER UPPER AND YAW DAMPER UPPER STS MSG(<P>PLACED UPPER YAW DAMPER ON MEL 22-21-01.</P>)SDR CALA2021041600480Trim Motor · failedSPEED TRIM FAIL BOTH CHANNELS UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN REPLACED RELAY R384 REF WDM 22-13-11 AND IPCSDR 2018FA0000068Servo Drive · brokenWHEN DESCENDING THROUGH 20,000 FEET, PLANE PITCHED UP ABRUPTLY AND STARTED BUFFETING. SHUT DOWN THE ENGINE AND FEATHERED THE PROPELLER. THE BUFFETING CONTINUED. MADE AN ENGINE-OFF EMERGENCY LANDING. DURING INSPECTION, THE ELEVATOR SERVO TRIM ARM HAD BROKEN SDR FDEA201708182263Warning Light · false activationSTAB OUT OF TRIM LIGHT ILLUMINATED AT 10,000 FT. PERFORMED A LEAK AND OPS CHECK THE STAB MOTOR AND BRAKES. LEAK AND OPS CHECKED GOOD IAW AMM 27-43-01-2. NO DEFECTS NOTED. PERFORMED AN OPS CHECK OF THE STAB DRIVE GEARBOX IAW AMM 27-44-03-2. SDR 1DFR20160127001Servo · misriggedAUTOPILOT ELEVATOR TRIM SERVO MOTOR REPLACED AFTER INSPECTION FOUND 1 CABLE GUIDE BROKEN OFF. REPLACEMENT SERVO MOTOR INSTALLED AND DURING OPS CHECK, FOUND SERVO MOTOR TO RUN OPPOSITE OF DESIGN. REMOVED SERVO MOTOR AND BENCH CHECKED TO VERIFY BY APPLYING VOLSDR 2016FA0000027Servo · out of rigAUTOPILOT ELEVATOR TRIM SERVO MOTOR REPLACED AFTER INSPECTION FOUND 1 CABLE GUIDE BROKEN OFF. REPLACEMENT SERVOMOTOR INSTALLED AND DURING OPS CHECK, FOUND SERVOMOTOR TO RUN OPPOSITE OF DESIGN. REMOVED SERVO MOTOR AND BENCH CHECKED TO VERIFY BY APPLYING VOLTASDR CA140602016Cable · frayed(CAN) TRIM CABLE FOUND FRAYED DURING SCHEDULED MAINTENANCE.SDR CA140602015Cable · frayed(CAN) CABLE FOUND FRAYED DURING SCHEDULED MAINTENANCE.SDR CA140317003Actuator · failed(CAN) UNCOMMANDED YAW IN FLIGHT. QRH FOR UNCOMMANDED YAW MOTION COMPLETED. EMERGENCY DECLARED. OSCILLATIONS SEEMED TO INTENSIFY AS SPEED APPROACHED V REF. INTENSIFIED AS SPEED REDUCED. MAINTENANCE REPLACED BOTH ACTUATORS.SDR CA140523005Actuator · malfunctioned(CAN) THE PILOT SELECTING THE AFCS TRIM SWITCH ON THE CYCLIC STICK, AFT AND THEN RELEASING, THE PITCH TRIM ACTUATOR CONTINUED TO OPERATE, ATHOUGH THE SWITCH HAD RETURNED TO THE NUETRAL POSITION. A CONDITION KNOW AS "TRIM RUNAWAY". PILOT TOOK APPROPRIATE ACTIONSDR CALA2013112093099Trim Switch · faultyUPPER MESSAGE "AUTO FLT RUD TRIM 2 FAULT" DISPLAYED. IAW ORD-TECH SUPPORT REPLACED FAC NR 1 & FAC NR 2 FROM ACFT 4712 IAW MM22-66-34. REPLACED RUDDER TRIM RESET SWITCH 8CC IAW MM22-62-12. ACCOMPLISHED OPERATIONAL TEST OF THE AFS IAW MM22-96-00 & LAND CAT IISDR CALA2013112093127Relay · failedAUTO FLT RUDDER TRIM 1 FAULT. REPLACED THE RELAY 7CC IAW FIM 22-62-00, SYSTEM CHECKED OK. CAT III TESTED OK IAW MM 22-9 7-00, AIRCRAFT IS FULL AUTO LAND CAPABLE.SDR ALGA2013021129626Actuator · faultyWHILE HOVERING BEFORE TAKEOFF, TRIM ACTUATOR FAIL LIGHT ILLUMINATED ON CAUTION AND ADVISORY DISPLAY. TAKEOFF ABORTED.SDR CA120612009Magnetic Brake · no test(CAN) AS PART OF A DAILY MAINTENANCE INSPECTION THE FORCE TRIM RELEASE OF THE YAW MAGNETIC BRAKE ASSY WAS TESTED. THE MECHANIC WAS ABLE TO DETECT THAT THE BRAKE ASSY WAS NOT RELEASING ON APPLICATION OF THE FORCE TRIM SWITCH. THE UNIT WAS REMOVED AND A SERVICESDR CA120608011Connector · disconnected(CAN) WHILE IN CONFINED SPACE, FORCE TRIM OFF, PILOT FELT PEDALS BIND AND COULD NOT INPUT MORE TAIL ROTOR CONTROL. IT THEN BROKE LOOSE AND NORMAL FEEL WAS ESTABLISHED. MAINTENANCE WAS ABLE TO DUPLICATE THE SNAG IN THE HANGER. MAGNETIC BRAKE FOR THE TAIL CONTSDR CA120515003Cable · damaged(CAN) DURING ROUTINE SCHEDULED MAINTENANCE A DEFECT AILERON CONTROL CABLE WAS FOUND. THE DEFECTIVE CABLE CONNECTS THE AILERON AUTOPILOT SERVO WITH THE RT REAR QUADRANT. THE CABLE HAD SOME DAMAGE, TORN WIRE STRINGS. THE AILERON SERVO AND THE SERVO MOUNT WERE SDR CA120515004Cable · damaged(CAN) PILOT REPORTED DURING FLIGHT CONTROL CHECK HARD TO REACH FULL LT AILERON DEFLECTION, CHECK MAINTENANCE ACTIONS: FOUND CONTROL CABLE OF THE AILERON SERVO BROKEN ALSO FOUND SIGNS OF CORROSION AT THE CONTROL CABLE OF THE SERVO. AILERON SERVO MOUNT REMOVEDSDR CA120203009Servo · malfunctioned(CAN) DURING DESCENT, THE AP SEEMED TO BE HAVING PROBLEMS STAYING ON COURSE, THE AUTOPILOT WAS DISCONNECTED AND ROLL CONTROL APPEARED TO BE SOMEWHAT, JAMMED, BUT COULD STILL CONTROL ACFT WITH AVAILABLE ROLL CONTROL. IT WAS JUST A REALLY, STIFF, CONDITION THSDR CA120111011Actuator · failed(CAN) DURING A TRAINING FLIGHT AND FOLLOWING TAKEOFF THE RUDDER TRIM MOVED TO THE FULL LT TRIM POSITITION UNCOMANDED. THE AIRCRAFT RETURNED AND CONDUCTED AN OUT OF TRIM LANDING. TROUBLESHOOTING LATER THE FAULT WAS DUPLICATED ON THE GROUND. FOLLOWING THE AUTOPSDR BSYA2011019Servo · faultyWHILE EN ROUTE FROM CLT TO LCK PILOT SMELLED SMOKE COMING FROM AFT COMPARTMENT, DIVERTED INTO LNP. MAINTENANCE FOUND THAT THE PITCH SERVO CAUSING THE SMOKE, PULLED AND TYRAPED CIRCUIT BREAKER FOR PITCH SERVO, MEL'D AUTO-PILOT AND FLEW IT BACK TO MAINTENANCE BSDR CA101206011Actuator · leakingEN ROUTE AT FL380, THE FLIGHT EXPERIENCED A GREEN HYD FAILURE. THE QRH WAS FOLLOWED AND THE FLIGHT CONTINUED TO DESTINATION AND CARRIED OUT AN UNEVENTFUL LANDING. THE CREW USED DIFFERENTIAL BRAKING TO EXIT TO TAXIWAY. ERS DID RESPOND BUT AN EMERGENCY WAS NSDR 2010FA0000089Trim System · malfunctionedCLIMBING ON DEPARTURE FROM PSP WITH AUTOPILOT ENGAGED, AUTOPILOT WAS DISCONNECTED MANUALLY BECAUSE IT WAS GOING TO GO THROUGH THE LEVEL OFF ALTITUDE, THE TRIM WHEEL CONTINUED TO TRIM NOSE UP UNTIL IT WAS HELD AND FORCED TO STOP. RED TRIM LIGHT AND MACH TRIM FSDR RU3A1003Servo · malfunctionedDURING CLIMBOUT AFTER 1000 MSL, PILOT WENT TO ENGAGE AUTOPILOT. HDG AND ALT SEL SELECTED FOR PHASE OF FLIGHT. AIRCRAFT MADE IMMEDIATE 30 DEGREE LEFT THEN 30 DEGREE RIGHT ROLL FOLLOWED BY AUTOPILOT DISCONNECT AND ILLUMINATION OF RED WARNING LIGHTS AND TONE OFSDR FDEA200911274207Actuator · failedIN CRUISE FLIGHT AT FL310, MACH .84, THE AUTOPILOT WAS PULSING BACK AND FORTH WITH A CORRESPONDING ACFT PITCHING MOVEMENT. DECIDED TO TRY SERVO B, UPON DISCONNECTING AUTOPILOT, DISCOVERED ACFT WAS OUT-OF-TRIM NOSE UP. COULD NOT TRIM THE ACFT NOSE DOWN WITHSDR QMLA2009102709036Servo · intermittentDURING CRUISE FLIGHT FROM SGF TO SUS AT 19000FT, THE AUTOPILOT MADE A SHARP UNCOMMAND PITCH UP. THE PILOT DISCONNECTED THE A/P AND CONTINUED THE FLIGHT WITH A NORMAL APPROACH AND LANDING.SDR PCSA2009072001Servo · malfunctionedIN FLIGHT FROM SAP TO MIA "NOSE DOWN RUNAWAY TRIM" AND "JAM STABILIZER AFTER RUNAWAY TRIM". MAINTENANCE FOUND THE STABILIZER TRIM WHEEL MOVING IN THE SAME DIRECTION AT ALL TIMES REGARDLESS OF THE POSITION OF THE STABILIZER CRUISE TRIM SWITCH. THE AUTOPILOT SSDR 2009FA0000218Bracket · brokenDURING A 100 HR/ ANNUAL INSP THE AUTOPILOT PITCH TRIM SERVO BRACKET WAS FOUND TO HAVE BROKEN FREE FROM THE 90 DEGREE SUPPORT BRACKET THAT IT ATTACHES TO. THIS BRACKET IS A FACTORY INSTALLED PART FOR THE AUTOPILOT SYS AND IS RIVETED TO THE EXISTING AIRFRAME. SDR CA081024006Ground Wire · open(CAN) ON LANDING, A WHITE CAS MESSAGE (SECONDARY TRIM FAULT) APPEARED. SYS TROUBLESHOT AND FOUND AN OPEN GROUND WIRE AT RBA0664N-22 AT SPLICESP322. SPLICE REPAIRED AND FUNCTION CHECKED SERVICEABLE.SDR SWIA200819286Servo · roughFLT 6653 - CONTROL YOKE FEELS LIKE THE AILERONS ARE STICKING. REPLACED AILERON SERVO IAW CRJ MM 23-11-21. OPS CHECK GOOD, P/N: 622-4404-101, S/N OFF: 1RTYY.SDR 243DR1Servo · misinstalledWHILE UNDERGOING A SCHEDULED INSPECTION, MECHANIC FOUND ELEVATOR TRIM SYS WAS MISRIGGED. TRAVEL LIMITS WERE NOT CORRECT AND WERE ACTUALLY RIGGED OPPOSITE WITH REGARDS TO MAX TRAVEL UP/DOWN. TRAVEL LIMITS IN MM NR D2070-3-13 FIGURE 1-1 WERE MISINTERPRETED, MFG SDR HNAA0700145Servo · malfunctionedAFTER TAKEOFF THE ELEVATOR WAS SLOW TO MOVE. PITCH WAS VERY SLOW AS WELL. THE CREW DECLARED AN EMERGENCY AND RETURNED TO LGA. THE FLIGHT LANDED AND TAXIED WITHOUT INCIDENT. REMOVED AND REPLACED ELEVATOR SERVO, EVALUATION FLIGHT CHECK SATISFACTORY.SDR 2007FA0000494Cable · frayedWE HAVE FOUND THE ELEVATOR CABLE AT THIS SERVO P/N 4006719-904 SHOWING EXCESSIVE WEAR ON AIRCRAFT UNDERGOING PHASE 1-4 AND ALSO PHASE 5 INSPECTIONS. THE CABLE WAS FOUND WHERE IT PASSES THROUGH AT FS. 428.50 AND IS DIFFICULT TO SEE. THIS CABLE HAD APROX. 3 STRASDR SWIA200718096Actuator · malfunctionedAUTOPILOT TRIM LWD CAUTION INTERMITTENT WITH ASSOCIATED "A" FLAG ON BOTH PFD'S. REPLACED AILERON SERVO IAW AMM 22-11-21.SDR SWIA200617444Servo · malfunctionedAUTO PILOT KICKS OFF WITH FLAPS 20 DEGREES WHEN A TURN IS INITIATED. REPLACED ELEVATOR SERVO IAW MM 22-11-24. OPERATIONAL CHECKS GOOD.SDR MASA200602443Servo · malfunctionedASH 7333 IAD. CAPTAIN REPORTED AT MACH .72 AIRCRAFT ALTITUDE OSCILLATES +/- 200 FPM AND AT .77 MACH RH ELEVATOR POSITION INDICATOR ON MFD CONTROL PAGE APPEARS TO SHOW SMALL HIGHT FREQUENCY DISPLACEMENT. MAINTENANCE REMOVED AND REPLACED ELEVATOR SERVO.SDR SWIA200617269Servo · malfunctionedAUTO PILOT DISENGAGES UPON APPLICATION OF FLAPS 8 DURING ARRIVALS AND IN LIGHT TURBULENCE OR PITCH CHANGES. REPLACED ELEVATOR SERVO. OPERATIONAL CHECKS GOOD IAW 22-16-00.SDR SWIA200616640Actuator · malfunctionedRADICAL PITCH CHANGES TAKE PLACE WHEN DOING COUPLED ILS. REPLACED ELEVATOR SERVO ACTUATOR IAW 22-11-24. OPERATIONAL CHECK GOOD.SDR SWIA200616659Servo · malfunctionedTRIM LIGHT ON CAPT AUTOPILOT FCP ILLUM IN FLIGHT WHEN AUTOPILOT SELECTED ON CAPT SIDE WITH A RED TRIM FAIL LIGHT AND AURAL WARNING. REPLACED PITCH TRIM SERVO, OPERATIONAL CHECK GOOD IAW EMB 120 22-10-00.SDR SWIA200616649Actuator · malfunctionedAP TRIM IS LWD CAUTION MESSAGE IN FLIGHT. REPLACED ELEVATOR SERVO ACTUATOR IAW MM 22-11-24. OPERATIONAL CHECK NORMAL.SDR SWIA200616623Servo · malfunctionedFLIGHT DIRECTOR WILL NOT FOLLOW COMMAND BARS (+10 TO -5 DEG DISCREP INFLIGHT). REPLACED ELEVATOR PRIMARY SERVO IAW 22-10-05. OPERATIONAL CHECK GOOD.SDR SWIA200616601Servo · malfunctionedPILOT REPORTS AUTOPILOT DISENGAGING ON APPROACHES. REPLACED ELEVATOR AUTOPILOT SERVO IAW MM 22-11-24. OPERATIONAL TEST GOOD IAW MM 22-11-24-710-801.SDR SWIA200616577Servo · malfunctionedTRIM LIGHT ON AUTOPILOT ENGAGE PANEL ILLUM INFLIGHT. REPLACED RUDDER SERVO IAW 22-00-00. OPERATIONAL CHECK GOOD.SDR SWIA200616546Servo · malfunctionedDURING CRUISE FLIGHT AT 11,000 A/P AND YAW DAMP ENGAGED. AIRCRAFT UNCOMMAND RT YAW. REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD IAW EMB MM 22-10-05. P/N: 622-5734-002, S/N ON: 5155, S/N OFF: 8045.SDR SWIA200616570Servo · malfunctionedON PREFLIGHT OF FLIGHT CONTROLS. NOTICED RESISTANCE IN AILERON CIRCUIT. REPLACED AILERON SERVO IAW MM 22-10-05, OPERATIONAL CHECK GOOD.SDR SWIA200616524Servo · malfunctionedRUDDER CLICKS AND WON'T MOVE SMOOTHLY THROUGH NORMAL TRAVEL. REPLACED RUDDER AP/YAW SERVO IAW EMB 120 MM 22-10-05. OPERATIONAL CHECK GOOD.SDR SWIA200616453Servo · malfunctionedWITH AUTOPILOT ENGAGED RUDDER TRIM GETS STICK WHEN TRIMING LEFT OR NOSE RIGHT RUDDER TRIM. REPLACED RUDDER SERVO IAW MM 22-10-05. OPERATIONAL TESTS GOOD, PN 622-5734-002, SN ON 1G7X SN OFF 8027.SDR SWIA200616308Servo · malfunctionedINFLIGHT WITH AUTOPILOT ON CAPT SIDE ACFT WOULD MOMENTARILY PITCH UP THEN QUICKLY BACK DOWN TO ORIGINAL FLIGHT ATTITUDE. REPLACED ELEVATOR SERVO AND ATTITUDE AND HEADING COMPUTER 1. OPERATIONAL CHECK IAW 22-10-00 GOOD. PN 622-6190-204 SN OFF 2738 PN 622-5
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