JASC 2742
Service difficulty reports · 610
Reports filed under 2742 · Stabilizer Actuator, newest first.
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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 = '2742' 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 = '2742' 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 CA030324008Actuator · seized(CAN) FLIGHT CREW HAD A AUTOPILOT DISCONNECT IN CRUISE FLIGHT THEY SHUT DOWN AUTOPILOT SYSTEM AND CONTINUED FLIGHT HOME. MAINTENANCE TESTED AUTOPILOT SYSTEM AFTER RESETTING C/B AND SYSTEM WORKED AS PER M/M.THEY THEN CARRIED OUT THE TEST ON THE HORIZONTAL STAB SDR SWIA200311786Actuator · malfunctionedSTAB TRIM CH 1 WILL NOT STAY ENGAGED. REMOVED AND REPLACED STAB TRIM ACTUATOR IAW MM 27-42-01. REMOVED AND REPLACED STAB TRIM MCU IAW MM 27-42-05. OPS CHECK GOOD. STAB TRIM ACTUATOR P/N: 8396-3, S/N OFF: 816.SDR SWIA200311674Control Unit · malfunctionedSTAB TRIM CHANNEL 1 INOP MESSAGE. REMOVED AND REPLACED HSTA AND MOTOR CONTROL UNIT IAW RII 27-415. OPS CHECK GOOD AT THIS TIME. HSTA PN OFF: 8396-3 SN OFF: 728.SDR CA030103020Connector · burned(CAN) DURING OVERNIGHT CHECK IN THE HANGER, AVIONICS FOUND THE A/P STAB TRIM MOTOR C/B WAS POPPED. TRIED A RESET BUT NO JOY AND C/B FELT ODD. TURNED A/C POWER OFF AND C/B WOULD NOT RESET. C/B REPLACED. C/B RESET BUT POPPED A FRACTION OF A SECOND LATER. AVIONSDR HALA0200673Trim Motor · failedFLT 240 - HNL - PRIMARY TRIM FAILURE, NO ALERT. ON CLIMB-OUT AND RETURN TO HNL, TRIM STARTED WORKING AGAIN ON SHORT FINAL APPROACH. TRIED USING PRIMARY TRIM SEVERAL TIMES IN FLIGHT. RAN F/O, CAPTAIN CONTROL, DID NOT WORK. REMOVED AND REPLACED HORIZONTAL STSDR AALA20021603Actuator · faultyORD - FLT 1891 - BOS-ORD, STAB TRIM FAILED WHEN AUTO PILOT WAS DISCONNECTED DURING DESCENT. TRIM BEGAN TO RUN AWAY ON SHORT FINAL. TURNED OFF BOTH TRIM MOTORS. LANDED ORD WITHOUT INCIDENT. AFTER LANDING TURNED TRIM MOTORS BACK ON AND WAS UNABLE TO TURN TRISDR 00059Control Box · inoperativeAIRCRAFT DEPARTED AND AFTER INTERMIDIATE LEVEL OFF, NORMAL PITCH TRIM WAS FOUND TO BE NOT WORKING. AIRCRAFT RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE USING EMERGENCY TRIM. REMOVED AND REPLACED TRIM SPEED CONTROL BOX, OPS CHECK GOOD. RETURN AIRCRAFT TSDR SWIA200211381Control Unit · malfunctionedSTAB CH 1 WILL NOT ENGAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-42-01. REMOVED AND REPLACED HORIZONTAL STAB TRIM MOTOR CONTROL UNIT IAW 27-42-05. OPS CHECK GOOD IAW MM 27-40-00 & 27-41-00. PN OFF 8369-3 SN OFSDR SWIA200211359Control Unit · malfunctionedSTAB TRIM CH1 STATUS MESSAGE INTERMITTENTLY ON. ABLE TO RESET 1ST 2 TIMES, 3RD TIME TOOK SEVERAL TRIES TO RESET. REMOVED AND REPLACED MCU, HSTA AND HSTCU IAW 27-42-01 AND 27-42-05. SYSTEMS OPS CHECK GOOD IAW 27-41-00.SDR SWIA200211353Control Unit · malfunctionedSTAB TRIM CHANNEL 1 STATUS MESSAGE. COULD NOT ENGAGE STAB TRIM CHANNEL 1. MOTOR 1 FAILURE ON HSTCU ON GROUND TEST. REPLACED HSTA ACTUATOR IAW 27-40-00 AND REPLACED MOTOR CONTROL UNIT IAW 27-42-05. OPS CHECK GOOD.SDR AUS20021242Actuator · faulty(AUS) STABILIZER TRIM FAILED TO OPERATE DUE TO A FAULTY ACTUATOR.SDR SWIA200211360Control Unit · malfunctionedSTAB CH 1 INOP. STATUS MESSAGE WILL NOT ENGAGE AFTER NUMEROUS ATTEMPTS. REPLACED CH 1 WIRING HARNESS FROM THE MOTOR CONTROL UNIT TO THE AFT PRESSURE BULKHEAD. REPLACED THE HSTA 1 3-PHASE C/B, REPLACED THE HSTCU, MOTOR CONTROL UNIT AND THE STAB TRIM ACTUATORSDR SWIA200211326Actuator · failedSTAB TRIM CHANNEL NR 2 WILL NOT ENGAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-42-01 AND 27-42-05. OPS CHECK GOOD.SDR SWIA200211310Actuator · failedSTAB AND MACH TRIM DISENGAGED AT THE GATE WITH A CAUTION MESSAGE. REENGAGED SYSTEM AND STAB CHANNEL 2 WOULD NOT REENGAGE. REPLACED HORIZONTAL STAB ACTUATOR AND MOTOR CONTROL UNIT IAW 27-42-01. OPS CHECKED GOOD.SDR RAIA00210277Control Unit · failed5324-RIC- UPON DESCENT INTO PIT PITCH TRIM 1&2 FAILED. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT, OPS CK OK.SDR CA021101001Pin · sheared(CAN) UPON INSPECTION OF THE HORIZONTAL STAB TRIM ACTUATOR, P/N 600-92301-963, PER THE TIME LIMITS/MAINTENANCE CHECKS, 600 HOUR INSPECTION, IT WAS FOUND THAT PIN 21207-1440 WAS FOUND SHEARED. THE SHEAR OCCURRED ON THE THREADED PORTION OF THE PIN.SDR SWIA200211262Actuator · failedSTAB CH 1 INOP. WOULD NOT RESET.REMOVED AND REPLACED STAB HSTA ACTUATOR IAW CRJ MM 27-42-01. OPS CHECK GOOD. ALSO REMOVED AND REPLACED STAB MOTOR CONTROL UNIT IAW CRJ MM 27-42-05. OPS CHECKS GOOD.SDR CA020923005Actuator · inoperative(CAN) FLIGHT CREW REPORTED AUTOPILOT DISCONNECTED IN FLIGHT AND TRIM INDICATOR WOULD MOVE FULL DEFLECTION WHEN PITCH TRIM OPERATED. SUSPECT INTERNAL FAULT WITH ACTUATOR. ACTUATOR REPLACED.SDR CA020923004Actuator · failed(CAN) FLIGHT CREW REPORTED AUTOPILOT FAILED IN FLIGHT, CREW SUSPECTED PITCH TRIM ACTUATOR DUE TO AN 'OUT OF TRIM' CONDITION WHEN AUTOPILOT FAILS. REMOVED ACTUATOR AND NOTICED THAT THE SHAFT SEAL WAS DIRTY AND WORN, SUSPECT THAT MOISTURE WAS ENTERING ACTUATOR ASDR SWIA200211210Actuator · failedSTAB CHANNEL NR 1 INOP. REMOVED & REPLACED STAB TRIM ACTUATOR & MOTOR CONTROL UNIT IAW 27-40-00, 27-42-01, 27-42-05. OPS CHECKS GOOD.SDR SWIA200211123Control Unit · malfunctionedSTAB TRIM CH 2 WILL NOT ENGAGE. REPLACED HSTA AND MOTOR CONTROL UNIT. STAB TRIM OPS CHECKS GOOD.SDR C2XA02IA169Actuator · faultyCrew reported pitch trim failure during cruise. The aircraft returned to IAH and landed without incident. Maintenance removed and replaced the horizontal stabilizer actuator. The aircraft was operationally checked, test flown satisfactorily, and returned to seSDR C2XA02IA168Control Unit · failedCrew reported a pitch trim fail indication inflight. The aircraft returned to IAH without further incident. A reset of the system was performed along with an operational check of the stab trim. The aircraft was returned to service. The problem reocurred and reSDR 02FDEA00538Actuator · damagedTHS ACTUATOR LWR CLAW STOP RUBBER BUFFER BETWEEN INNER & OUTER RACE SHOWS AXIAL MIGRATION OF 5 MM. THS ACTUATOR SCREW THREAD HAS SCRATCH MARK ON UPPER FACE 27.5 CM ABOVE LWR CLAW STOP. REMOVED AND REPLACED ACTUATOR PER AMM 27-44-11-4.SDR WIB2002F00006Actuator · failedSTAB ACTUATOR BAD FROM STOCK. DAMAGED ANOTHER COMPONENT. NOT THE FIRST TIME. PITCH TRIM WOULD FAIL IN PRIMARY MODE AFTER OVERHAULED UNIT WAS INSTALLED.SDR SWIA200211080Actuator · malfunctionedRECEIVED STAB TRIM CH 1 MESSAGE IN FLIGHT. REMOVED AND REPLACED HSTA IAW 27-42-01 AND REMOVED AND REPLACED MOTOR CONTROL UNIT IAW 27-47-00.SDR SWIA200211068Actuator · failedSTAB CH 2 INOP STATUS MESSAGE IN FLIGHT, WOULD NOT RE-ENGAGE. REMOVED AND REPLACED THE HSTA AND MOTOR CONTROL UNIT WITH SERVICEABLE HSTA AND MOTOR CONTROL UNIT. OPS AND FUNCTION CHECK GOOD IAW CRJ MM 27-40-00, 27-42-00 & 27-42-05.SDR F3LA200200197Actuator · malfunctionedFLIGHT CREW REPORTED MOMENTARY PITCH TRIM RUNAWAY ON CLIMBOUT AT FL260. NOSE DOWN FOR APPROXIMATELY 2 SECONDS. BACK PRESSURE WAS APPLIED TO COUNTER TRIM AND NOSE UP ELECTRIC TRIM WAS SELECTED AND TRIM STOPPED. AUTO PILOT WAS OFF. REPLACED STABILIZER TRIM ASDR SWAA021499Motor · failedAIR TURNBACK, INFLIGHT FAILURE OF BOTH NORM AND AUTOPILOT ELECTRIC PITCH TRIM. REMOVED AND REPLACED STAB TRIM MOTOR PER MM.SDR SWIA200211002Actuator · failedAT THE GATE, STAB TRIM CH 2 WILL NOT ENGAGE. REMOVED AND REPLACED HST ACTUATOR AND MCU IAW 27-41-00. ALL OPS CHECKS GOOD.SDR SWIA200210998Actuator · failedNR 2 STAB TRIM CHANNEL WILL NOT ENGAGE. REMOVED AND REPLACED HSTA. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW 27-42-05. PERFORMED OPS CHECK. OPS CHECK GOOD.SDR SWIA200210966Control Unit · malfunctionedSTABILIZER TRIM CHANNEL 1 POPPED THE CIRCUIT BREAKER. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW 27-41-00. OPS CHECK GOOD.SDR CA020726010Actuator · failed(CAN) MACH AND STAB TRIM MESSAGE ON CLIMB, PROCEDED WITH STAB TRIM 1 INOPERATIVE, FAULT DISAPEARED, AUTOPILOT ENGAGED, FLT CREW DISENGAGED A/P AT 10,000 FT, FOR MANUAL LANDING, EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REPLACED HORIZONTAL STAB TRIM ACSDR HKG2002F00000Actuator · failedSECOND IN COMMAND IN RT SCAT REPORTED TO CAPTAIN THAT THE PITCH TRIM WOULD NOT TRIM NOSE DOWN. PILOT IN CHARGE ATTEMPTED TRYING AUX TRIM SWITCH WITH SAME RESULTS. PITCH TRIM WAS TRANSFERRED TO THE NR 1 POSITION, PILOT IN CHARGE REPORTED THAT THERE WAS STILL SDR SWIA200210931Control Unit · malfunctionedSTAB TRIM CH2 WILL NOT ENGAGE. REPLACED HORIZONTAL STAB ACTUATOR IAW 27-42-01 AND REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT IAW 27-42-05. OPS CHECK GOOD IAW MM. OK FOR CAT II OPERATIONS.SDR SWIA200210883Actuator · malfunctionedSTAB CH 1 & 2 AND MACH TRIM FAILED SHORTLY AFTER TAKEOFF. RAN QRH, RESET AND IT FAILED AGAIN. WAS ABLE TO GET ALL TO WORK WHILE FLYING TO BURN OFF GAS. RETURNED TO BOI. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW 27-42-05. REMOVED AND REPLACED HSTA IAW 2SDR GTIA020431Motor · malfunctionedACY - PRIMARY TRIM HESITATES NOSE UP DIRECTION OCCURS USING BOTH CAPTAINS OR F/O'S YOKE SWITCHES AND USING SUIT CASE HANDLES. REMOVED AND REPLACED PRIMARY TRIM MOTOR. OPERATIONAL CHECKS GOOD. (M)SDR QXEA0200628Actuator · leakingPDX - EN ROUTE FROM YEG TO SEA, THE UTILITY AND FLIGHT CONTROL HYDRAULIC QUANTITY DROPPED TO ZERO. AIRCRAFT DIVERTED TO PDX. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE HORIZONTAL STABILIZER ACTUATOR LEAKING FLUID AND REPLACED SAME. OPERATIONAL CHECK ASDR RFTOJackscrew · wornJACKSCREW REMOVED FROM A DC10-10,N910SF, THIS PART TO OUR KNOWLEDGE HAS 69567 HOURS, 25480 LANDINGS AND WAS INSTALLED IN PRODUCTION 1971. WE SENT THE UNIT IN FOR INSPECTION AND OVERHAUL AS NECESSARY TO THE PART MANUFACTURE AS THERE IS NOT A CURRENT INSPECTION/SDR P2EA2002M021Actuator · malfunctionedON FINAL APPROACH INTO LAX BOTH PRIMARY AND ALTERNATE STAB TRIM FAILED TO WORK. AFTER THREE MINUTES BOTH RESUMED WORKING. REMOVED AND REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR IAW MM 27-40-01.SDR GTIA020268Actuator · failedLGA - PREFLIGHT, FOUND PRIMARY STAB TRIM WOULD NOT OPERATE NORMALLY FROM THE SUITCASE HANDLES, MOTOR THERMALLY CUTS OUT AFTER ONLY SHORT USAGE 5-10 SECONDS FROM YOLK SWITCHES. FOUND 'B' PHASE C/B BAD REMOVED AND REPLACED 'B' PHASE C/B, OPS CHECK NORMAL PER A/SDR 2002FA0000533Bushing · looseDURING A SCHEDULED CORROSION INSPECTION THE RIGHT ELEVATOR WAS REMOVED. UPON REMOVAL THE BUSHING IN THE END OF THE ACTUATOR WAS FOUND TO BE LOOSE ON THE SHAFT. WITH THIS BUSHING NOT INSTALLED THE POSSIBILITY OF TAB FLUTTER OR NOT ALLOWING THE TAB ITS FULL MOSDR CA020328007Switch · failed(CAN) STABILIZER TRIM AND MACH TRIM TRIPPED OFF IN FLIGHT, WOULD NOT RE-ENGAGE. REPLACED CAPTAINS STAB TRIM DISCONNECT SWITCH, FUNCTIONAL TEST CARRIED OUT. AIRCRAFT FOUND SERVICEABLE.SDR CA020328002Fitting · failed(CAN) PLAY AT TRIMMABLE HORIZONTAL STABILIZER (THS) REAR ATTACH FITTINGS. THS REAR ATTTACH FITTINGS HAVE PLAY BETWEEN BUSHINGS AND THS LT AND RT AFT ATTACH FITTING BORES.SDR HEED089126Actuator · stuckLINEAR ACTUATOR STICKING. REPLACED UNIT.SDR SWIA200210698Actuator · failedDURING INITIAL POWER UP IN FAT, STAB TRIM CH2 WOULD NOT ENGAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MCU IAW CRJ MM 27-42-01. OPS CHECK GOOD. AIRCRAFT OK FOR RETURN TO CAT II SERVICE.SDR MEX2002054Motor · failedFLT 420 - MEX-MID - CABIN CREW REPORTED PRIMARY LONGITUDINAL TRIM O/S, AIRCRAFT WAS REPAIRED IN THE HANGAR FACILITIES. PRIMARY TRIM WAS REPLACED AND TESTS WERE PERFORMED IAW M/M 27-40-01. (M)SDR AWXA200200187Fitting · wornYWG - MAJOR REPAIR - "C" - DURING C-02 INSPECTION CENTER JOINT FITTINGS FOR THE TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WERE FOUND WORN BEYOND DRAWING LIMITATIONS. L/H DIMENSIONS RANGE FROM 2.4746' TO 2.4751", R/H SIDE DIMENSIONS RANGE FROM 2.6007" TO 2.6009"SDR CA020509014Actuator · failed(CAN) DURING CLIMB OUT PITCH TRIM CAUTION LIGHT ILLUMINATED, AUTO TRIM FAIL MESSAGE ON PFD & TRIM INDICATOR FULLY NOSE UP. FAULTS LOGGED IN CDS: 67,E7,63,E3,ED,EE. SPEED APPROX 185 KTS. FLT OPERATED MANUALLY. UNEVENTFUL APPROACH & LANDING. TROUBLESHOOTING REVESDR C2XA02CL025Actuator · inoperativeCLE FLIGHT#3230 THE CREW REPORTED BOTH CAPTAINS AND FIRST OFFICER'S PITCH TRIM DID NOT WORK.MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STABILIZER ACTUATOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.
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