JASC 2742
Service difficulty reports · 610
Reports filed under 2742 · Stabilizer Actuator, 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 = '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 CA001110011Actuator · failed(CAN) APPROXIMATELY 30 MINUTES AFTER TAKEOFF, STABILIZER TRIM MESSAGE ON ENGINE INDICATING CREW ALERT SYSTEM, NO CHANGE WITH AUTO PILOT ON/OFF. ATTEMPTED TO RESET MESSAGE DISAPPEARED MOMENTARILY, THEN FAULT REOCCURRED. AIRCRAFT RETURNED TO TORONTO. CHANGED SDR COMA0060821Actuator · failedSTAB TRIM IS INOP, WILL NOT TRIM NOSE DOWN. REPLACED THE HSTA.SDR CA001024043Actuator · failed(CAN) DURING TAKEOFF, STAB TRIM CAUTION MESSAGE ILLUMINATED. TAKEOFF ABORTED AT 100 KNOTS.RTO INSPECTION, HSTA AND MCU REPLACEMENT CARRIED OUT ON AIRCRAFT BEFORE RETURNING INTO SERVICE.SDR CA001024018Actuator · failed(CAN) WHEN OPERATING THE PILOT/CO-PILOT STAB TRIM SWITCHES, THE STAB TRIM CHANNEL NR 1 INOP MESSAGE APPEARS.REPLACED THE HSTA AND MCU. SERIAL NUMBERS NOT AVAILABLE AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.SDR 20001016SH016Screw · nickedSCREW ASSEMBLY BAD FROM STOCK. SCREW ASSEMBLY, S/N K320L, HAD TWO NICKS ON THREAD SURFACE. (X)SDR 20001016SH015Screw · corrodedSCREW ASSEMBLY BAD FROM STOCK. SCREW ASSEMBLY, S/N K138L, WAS FOUND CORRODED WHEN REMOVED FROM WRAPPING. (X)SDR DL72S001776Actuator · malfunctionedSTABILIZER JAMMED IN THE 3 DEGREE NOSE UP POSITION. OCCURRED DURING FLIGHT. A/C OFF LANDED IN CVG. MTC CHANGED ACTUATOR (P/N 274001078) (S/N 104-00AA) AND ACTUATOR (P/N 2774003971) (S/N 1278-00AA. ) A/C FERRY FLIGHT TO ATL FLT 9930 ON 9/14/00. MTC REPLACINSDR DL733001709Actuator · inoperativeELECTRIC STAB TRIM INOP BOTH MAIN AND AUTOPILOT. TRIM INITIALLY WORKED. PASSING 13,000 FEET TRIM QUIT WORKING. A/C AIR TURNBACK. REPLACED STAB TRIM ACTUATOR PER NR CARD NR 1 REF M/M.SDR 0003082769Actuator · failedDURING CLIMB THE HORIZONTAL STABILIZER JAMMED. FLIGHT CREW PERFORMED COM PROCEDURE AND WAS ABLE TO RELEASE STAB BRAKE. FLIGHT RETURNED TO MSP AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE PRIMARY STABILIZER TRIM ACTUATOR, AUTOPILOT TRIM SERVO, ANSDR AU000719Actuator · faulty(AUS) STABILISER TRIM ACTUATOR FAULTY.SDR COMA0060704Actuator · malfunctionedSTAB TRIM CAUTION MESSAGE. REPLACED THE HSTA.SDR CA000928021Roll Pin · displaced(CAN) ROLL PIN ON LEFT STABILIZER ACTUATOR SLID OUT AND GOT CAUGHT ON THE ACTUATOR HINGE ASSEMBLY. THIS PREVENTED THE STABILIZER TRIM FROM MOVING. THE TRIM ACTUATORS WERE REMOVED, THE PIN RE-INSTALLED, AND LOCKWIRED. SUGGEST LOCKWIRING PINS IN ALL ACTUATORS.SDR CA000919008Actuator · failed(CAN) PRIOR TO DEPARTURE, HORIZONTAL STABILIZER CHANNEL NR 2 WOULD NOT ENGAGE. FOUND MOTOR NR 2 FAULT. SENT A/C TO HANGAR, REPLACE HSTA AND MCU. DURING REPLACEMENT, FOUND RESTRICTED MOVEMENT OF STAB SURFACE. PIVOT PIN WAS BINDING. SENT AIRCRAFT TO MAINTENANCE SDR CA000810010Control Unit · failed(CAN) BRIT AIR HAVE REPORTED A STABILIZER PIVOT BUSHING SEIZED AND BOTH STAB TRIM CHANNELS INOPERATIVE. THE MAINTENANCE REPLACED THE MCU AND THE HSTA. ALSO ONE BUSHING, TWO BUSHINGS AND ONE FITTING WERE REPLACED.AIRCRAFT RETURNED TO SERVICE.SDR SCNA00086Actuator · crackedAFTER TAKEOFF FROM IAH, THE NUMBER THREE HYDRAULIC QUANTITY WAS LOST. THE CREW RETURNED TO POINT OF ORIGIN. THE HYDRAULIC FLUID WAS FOUND TO BE LEAKING FROM THE NUMBER TWO HYDRAULIC BAY. A HAIRLINE CRACK WAS FOUND ON THE RIGHT HORIZONTAL STABILIZER TRIM MOTSDR ASOA00087Actuator · inoperativeAPPROX 4 MINUTES INTO FLIGHT WITH AUTOPILOT ENGAGED, AP PITCH TRIM MESSAGE CAME ON. CREW FOLLOWED PROCEDURES, BUT MESSAGE RESUMED. THIS OCCURRED SEVERAL TIMES FOLLOWED BY A NOSE DOWN MESSAGE. CREW PERFORMED PRECAUTIONARY STEPS FOR SLIGHT TO MODERATE CONTROLSDR UPS00533473Actuator · inoperativeINSPECTION TYPE:N/A, HORIZ STAB WILL NOT TRIM NOSE DOWN. REPLACED RT SAM PER MM OPS NORMAL.SDR MASA00088Actuator · failedFLT 6003 - FAT-PHX - PILOT NOTICED NR 1 STAB TRIM WOULD NOT ENGAGE. MAINTENANCE TROUBLESHOT THE DISCREPANCY TO THE TRIM ACTUATOR AND THE MOTOR CONTROL UNIT. THE ACTUATOR AND THE MOTOR CONTROL UNIT WERE REPLACED. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED SDR JBXA0000191Actuator · intermittentNO MANUAL OR AUTOPILOT STABILZER TRIM AFTER T/O. NO ASSOCIATED CAUTIONS. MOMENTARY STAB CH 1 INOP STATUS MESSAGE, F/O HAD MOMENTARY TRIM. REMOVED AND REPLACED STAB TRIM ACTUATOR IAW AMM 27-42-01. OPS CHECK GOOD.SDR MASA00079Control Unit · failedFLT 6427 - PHX-ELP - PILOT REPORTED STAB TRIM CHANNEL NR 1 INOP. MAINTENANCE REPLACED THE HSTCU. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR MASA00078Actuator · inoperativeFLT 5760 - PHL-BHM - REPORTED STAB TRIM NR 2 WIN ENGAGE. MAINTENANCE REMOVED AND REPLACED ACTUATOR AND MOTOR CONT UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR CA000802007Control Unit · failed(CAN) DEPARTING MONTEREY, CA. CLIMBING OUT THRU FL200. EICAS ALERTED US OF AP PITCH TRIM MASTER CAUTION FOLLOWED BY AP PITCH TRIM NOSE DOWN MASTER CAUTION ANNUNCIATOR. WE FOLLOWED CFM PROCS&UPON DISCONNECTING AUTOPILOT HAD TO MAINTAIN ABOUT 2 IN OF NOSE DOWN SDR MASA00074Actuator · inoperativeMRY/PHX - FLT 6088 - DURING FLIGHT, HAD THE A/P TRIM AND A/P TRIM ANNUNCIATOR ILLUMINATE. THE STABILIZER WAS STUCK AT MINUS 5 DEGREES NOSE DOWN. A/P DISCONNECTED AND TRIM STILL STUCK AT MINUS 5 DEGREES. EMERGENCY DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENSDR JBXA0000187Actuator · failedTWENTY-FIVE MINUTES INTO FLIGHT, LEVEL CRIUSE A/P PITCH TRIM AMBER WARNING ILLUMINATED. UPON DISC A/P MANUAL TRIM WOULD NOT TRIM NOSE DOWN, ONLY NOSE UP DID NOT RE-ENGAGE. RETURNED TO RDU. INSPECTED AND FOUND HORIZONTAL STAB ACTUATOR BAD. REMOVED AND REPLASDR CA000712010Actuator · failed(CAN) A/C DEPARTED YEG AT 10:56 LOCAL TIME. ON INITAL CLIMB, PILOTS REALIZED PITCH TRIM NOT RESPONDING CORRECTLY. ATC INFORMED, AND REQUESTED TO RETURN TO YEG MADE. AT TIMES, BOTH PILOTS WERE REQUIRED TO MANHANDLE ELEVATOR CONTROL. A/C LANDED UNEVENTFULLY AT 1SDR JBXA0000184Actuator · malfunctionedRECEIVED AP PITCH TRIM MESSAGE IN FLIGHT. LEFT SIDE NO TRIM AVAILABLE, RIGHT SIDE NOSE DOWN ONLY. REMOVED AND REPLACED HORIZONTAL STABILIZER TRIM ACTUATOR IAW MM 27-42-01, OPS CHECK GOOD.SDR DL738001125Actuator · malfunctionedIN FLT DIVERT. AFTER REACHING CRUISE FL 350 THE STAB OUT OF TRIM LIGHT ILLU WITH B A/P ENGAGED. POM PROCEDURE FOUND ELEC TRIM INOP. UP AND DOWN STAB TRIM SW TO OVERRIDE, NO HELP. DISCUSSIONS WITH CHIEF PILOT AND ATL/MTC DIVERTED TO PHX. DURING DESCENT PASSDR CA000614014Actuator · contaminated(CAN) ON JUN 6/2000 MASTER FLT CAUTION LIGHT ILLUMINATED ALONG WITH BOTH UTILITY & FLT CNTL CHANNEL LIGHTS ON FLT CNTL PANEL AS REORTED BY CREW INBOUND ALT ELECTRIC SYS POPPED CCT BREAKER TWICE UPON ACTIVATION. CREW THEN PROCEEDED AS PER CHECK LIST WITH JAMMESDR CA000606010Switch · out of rig(CAN) PILOTS NOTICED OUTBOUND OF YXE. THAT THE HORIZONTAL STAB TRIM WHEEL WAS UNABLE TO BE ADJUSTED. THE CREW DECIDED TO RETURN AND AT THAT TIME THEY REALIZED THAT THE UTILITY AND FLIGHT CONTROL SYSTEM STAB CAUTION LIGHTS WERE ON - INDICATING NO HYDRAULIC POWSDR JBXA0000176Actuator · failedSTAB TRIM FAILED, BOTH PILOT AND CO-PILOTS. RECEIVED A/P PITCH (AMBER). A/P NO (AMBER). REMOVED AND REPLACED STAB TRIM ACTUATOR, OPS CHECK GOOD.SDR CA000519016Actuator · failed(CAN) WHILE TAXING TO RAMP PILOT MOVED STAB TRIM TO NOSE DOWN POSITION. CHANNEL 1 NOSE DOWN FAIL LIGHT CAME ON AND ACT WOULD NOT MOVE. MAINT CHANGED PITCH TRIM ACTUATOR AND RETURNED A/C TO SERVICE.SDR AT0000234Actuator · malfunctionedRUN AWAY TRIM - PRIMARY LONGITUDINAL AXIS 15 MIN FROM BOS. AUTOPILOT WAS ENGAGED. REMOVED AND REPLACED PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR, AND PRIMARY LONGITUDINAL TRIM CONTACTOR RELAY IAW DC9 MM 27-40, 27-40-04.SDR COMA0060385Actuator · malfunctionedTAKEOFF CONFIG WARNING WHEN POWER ADVANCED. REPLACED THE STAB TRIM ACTUATOR.SDR CA000501017Actuator · failed(CAN) ON DECENT, FOUND HORIZONTAL STAB NORMAL MODE U/S. SELECTED EMERGENCY STAB AND LANDED.FOUND STAB ACTUATOR NORMAL MODE MOTOR U/S.SDR F3LA00073Bolt · looseDEN - DURING C-7 CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER CENTER SECTION HINGE PIVOT BOLT ROTATING IN HOUSING. MAINTENANCE REPLACED LOCKING PLATE PER MM 27-41-31. (M)SDR 20000501SH020Spring · crackedSPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM CAUSING UNIT TO BIND AND JAM. IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE AND INCREASED SPRING COIL STRESSES. SPRINGS PN 69-77855-1 ARE TO BE REPLACED WITH PN 69-77855-2 SPRINGS ON ACTUATOR ASSEMBSDR USAASB00107Brake · failedFLL - FLT 2831 - ON APPROACH INTO FLL, CAPT REPORTED THE STABILIZER ELECTRIC TRIM JAMMED, THEN RELEASED, AT APPROX 1,500 FT AND WORKED NORMALLY. AT APPROX 1,000 FT, THE STABILIZER ELECTRIC AND MANUAL TRIM JAMMED. FLIGHT ATTENDANT IN REAR OF CABIN REPORTED HEASDR 20000501SH024Spring · crackedSPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM CAUSING THE UNIT TO BIND AND JAM. IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE, AND INCREASED SPRING COIL STRESSES. SPRINGS PN 69-77855-1 ARE TO BE REPLACED WITH PN 69-77855-2 SPRINGS ON ACTUATOR ASDR AT0000126Actuator · failedPRIMARY HORIZONTAL TRIM ACTUATOR MOTOR INOPERATIVE. CORRECTIVE ACTION: R/R PRIMARY TRIM MOTOR IAW MM 27-40.SDR 20000501SH040Spring · crackedSPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM. POSSIBLE CAUSE: IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE AND INCREASED SPRING COIL STRESSES. SPRINGS PN 69-77855-1 ARE TO BE REPLACED WITH PN 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIES MANUFACSDR 20000501SH039Spring · brokenSPRINGS PN 69-778551 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM. POSSIBLE CAUSE: IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE AND INCREASED SPRING COIL STRESSES. SPRINGS PN 69-77855-1 ARE TO BE REPLACED WITH PN 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIES MANUFACTUSDR USAASB00055Actuator · failedPHL - FLT 1063 - EN ROUTE FROM RIC TO BOS, THE STABILIZER ELECTRIC TRIM HAD FAILED. FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTEHR INCDIENT. NO EMEGENCY WAS DECLARED. MAINTENANCE PERFORMED FUNCTIONAL CHECK ON STABILIZER TRIM SYSTEM AND FOUND ALL FUNCTIONSDR CA000301038Actuator · malfunctioned(CAN) DURING CLIMB-OUT, FLIGHT CREW REPORTED AUTOPILOT WAS NOT PROPERLY TRIMMING THE A/C. THE CREW DISENGAGED THE AUTOPILOT AND MANUALLY TRIMMED STABILIZER NOSE DOWN UNTIL 4 UNITS WERE REACHED AND STOPPED UNCOMMANDED. EICAS DID NOT POST ANY MESSAGE RELATED TSDR JBXA0000149Actuator · failedPITCH TRIM INOP NOSE DOWN INTERMITENT NOSE UP WOULD NOT RUN PAST 4 STAB TRIM. REMOVED AND REPLACED HSTA IAW AMM 27-42-01. OPS CHECK GOOD.SDR 20000501SH038Spring · crackedSPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM. POSSIBLE CAUSE: IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE AND INCREASED SPRING COIL STRESSES. SPRINGS PN 69-77855-1 ARE TO BE REPLACED WITH PN 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIES MANUFACSDR 20000501SH041Spring · crackedSPRINGS PN 69-77855-2 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM. POSSIBLE CAUSE: IMPROPER HEAT-TREATING OR INCORRECT ALLOYS IN THE SPRINGS. REPLACED SPRINGS. (X)SDR 20000406SH052Bearing · damagedLUBRICANT IN ROLLER BEARING AT FORWARD END OF PITCH TRIM TUBE BECAME GUMMED UP AND HARDENED TO THE POINT THAT NEITHER ELECTRIC OR HAND WHEEL ACTUATION OF PITCH TRIM WAS POSSIBLE. MALFUNTION WAS CORRECTED BY REPLACING BEARING. THERE IS NO PROVISION FOR PERIODSDR 20000406SH007Spring · crackedSPRINGS, PN 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM. IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE AND INCREASED SPRING COIL STRESSES. SPRINGS, PN 69-77855-1, ARE TO BE REPLACED WITH PN 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIES MANUFACTURED PRIOR TSDR AU000203007Actuator · failed(AU) STABILIZER ACTUATOR FAILED.SDR CA000215008Bearing · stuck(CAN) MAIN TRIM ACTUATOR ERRATIC, STICKY
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