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 CA081122004Actuator · loose(CAN) AV670-23105-003 (LT) AND -004 (RT) DURING ROUTINE MX ON THE HORIZONTAL STAB TRIM ACTUATOR (HSTA), LOOSE BOLTS (ITEMS 24 AND 35) WERE FOUND IN THE UPPER BOLT LOCATIONS OF THE RT AND LT HSTA UPPER ATTACHMENT FITTING ASSY ITEM 33).SDR VNAA2008111700003Bolt · looseDURING ROUTINE MAINTENANCE ON THE HORIZONTAL STABILIZER TRIM ACTUATOR (HSTA), LOOSE BOLTS WERE FOUND IN THE UPPER BOLT LOCATIONS OF THE UPPER HSTA FITTING ASSEMBLIES (LT AND RT). THE BOLTS WERE RETORQUED TO THE PROPER SPECIFICATION. CHECKS WERE PERFORMED ANDSDR VNAA2008111700002Bolt · looseDURING ROUTINE MAINTENANCE ON THE HORIZONTAL STABILIZER TRIM ACTUATOR (HSTA), LOOSE BOLTS WERE FOUND IN THE UPPER BOLT LOCATIONS OF THE UPPER HSTA FITTING ASSEMBLIES (LT AND RT). THE BOLTS WERE RETORQUED TO THE PROPER SPECIFICATION. CHECKS WERE PERFORMED ANDSDR L19A2008102400050Adapter · brokenTHE HELICOPTER WAS IN CRUISE FLIGHT AND THE VSCS ADAPTER BROKE IN TWO. THIS CAUSED THE A CONTROL PROBLEM WITH THE HELICOPTER UNTIL IT SLOWED BELOW 100 KTS. THE AIRCRAFT CAME BACK TO THE AIRPORT AND LANDED WITH NO PROBLEMS. THERE IS NOW A NEW AD ON THIS MATTESDR ABXA200810160252Jackscrew · damagedHORIZONTAL STAB BALL SCREW INSPECTION FAILED IAW J/C 27-030-01. REPLACED HORIZONTAL STABILIZER ACTUATOR. STAB TRIM ACTUATOR ASSY SENT OUT ON R/O 501586374 TO REPAIR VENDOR DELTA AIRLINES INC. REASON FOR REMOVAL STATED AS JACKSCREW PITTED. UNIT WAS EXCHANGESDR UG82008F00002Actuator · malfunctionedINCIDENT OCCURRED AFTER DEPARTURE FROM DTW AND DURING CLIMBOUT AT 11000 FT WITH AUTOPILOT ENGAGED IN SMOOTH AIR, CONTROL WHEEL JOLTED FWD BRIEFLY AND "UNCOMMANDED STAB" AMBER ICAS MESSAGE ILLUMINATED. NO FURTHER UNCOMMANDED INPUTS TO STAB OCCURRED. AIRCREW COMSDR 2008FA0000557Control Rod · brokenEXPERIENCED EXCESSIVE LT PEDAL (2-3 INCHES) DURING CRUISE FLIGHT AT 70 TO 80 PERCENT TRANSMISSION TORQUE. DURING POST FLIGHT FOUND THAT THE LT VERTICAL STABILIZER MOVED FREELY. FURTHER INSPECTION REVEALED THAT THE LT VERTICAL STABILIZER CONTROL SYSTEM (VSCS)SDR CA080625008Actuator · malfunctioned(CAN) DURING A FLIGHT, PILOT REPORTED A PITCH TRIM CHANNEL NR1 INOP LIGHT ON. TROUBLESHOOT THE TRIM SYS AND FOUND NR1 TRIM ACTUATOR BRAKE COIL OPEN. HORIZ STAB TRIM ACTUATOR (P/N 600-92301-67/21207-008 S/N Y2003) WAS REPLACED WITH A REPAIRED UNIT WITH TSN 868SDR CA080609004Actuator · unresponsive(CAN) SHORTLY AFTER DEPARTING, AND ACCELERATING THROUGH 200KTS, THE PITCH TRIM STOPPED RESPONDING. TRIM SONALERT WAS SOUNDING WHENEVER THE TRIM SWITCH WAS USED, HOWEVER THE TRIM GAUGE WAS NOT MOVING AND THE ACFT CERTAINLY WAS NOT TRIMMING. THIS WAS ATTEMPTED OSDR C2XA08ON117Actuator · inoperativeFLT 223 - SAT - FLIGHT CREW REPORTED MAIN PITCH TRIM FAIL INFLIGHT. MX PERSONNEL REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR OPERATIONALLY CHECKED SATISFACTORY, AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.SDR C2XA08SH057Attach Bracket · damagedSHV - DURING C-CHECK LT HORIZONTAL STABILIZER ACTUATOR ATTACHMENT POINT O/B LUG O/B HAT BUSHING HOLE IS ELONGATED. MX REMOVED AND REPLACED LT UPPER HORIZONTAL STAB ACTUATOR ATTACHMENT BRACKET IAW EMB 145 SRM 51-40-04 (DRILLING), 51-20-01 (SEALING), SRM 51-40-SDR C2XA08CL043Actuator · faultyCLE FLIGHT 2898 THE CREW REPORTED A YAW TRIM RUNAWAY IN FLIGHT. QRH WAS FOLLOWED AND FOUND BOTH SYSTEMS TO BE INOPERATIVE. EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE YAW TRIM SWITCH AND ACSDR AALA200800543Actuator · inoperativeMIA INFLIGHT T592/10MAR - BOTH CAPTAIN AND FIRST OFFICERS STABILIZER TRIM INOPERATIVE. RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED HORIZONTAL STABILIZER TRIM ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR ASAA0752158Actuator · inoperativeSTABILIZER OUT OF TRIM LIGHT ILLUMINATED DURING ACCELERATION. APPEARS AUTO PILOT NOSE DOWN TRIM IS INOP. REPLACED STABILIZER TRIM MOTOR.SDR SWIA200719154Actuator · crackedBASE OF STABILIZER ACTUATOR IS CRACKED, FOUND AT C-CHECK. REPLACED STAB ACTUATOR PER CRJ200 MM CH 27-42-01-400-801, OPS CHECK GOOD.SDR ABXA070266Actuator · failedDURING MAINTENANCE, REF JOB CARD 12-003-C1, STABILIZER TRIM BALL NUT UPPER SEAL APPEARED TO HAVE FAILED - STEP (23) (B) NOTE 2 (BEAVER UNIT). REMOVED AND REPLACED TRIM BALL SCREW ACTUATOR IAW B767 MM 27-41-10.SDR CA070720005Actuator · malfunctioned(CAN) AFTER FLAP RETRACTION, FLIGHT CREW DISCOVERED THAT THEY HAD NO CONTROL OF PITCH TRIM USING PRIMARY OR SECONDARY CIRCUITS. AFTER DISCUSSION WITH MAINTENANCE, FLIGHT CONTINUED TO MAINTENANCE BASE WHERE MAINTENANCE REPLACED TRIM ACTUATOR. (TC NR 20070720005SDR FDKA200706282Actuator · malfunctionedFDM 9964 MCO-FLL (1005 PHX LCL). PITCH TRIM MAIN INOP MESSAGE. MX REMOVED AND REPLACED HSA.SDR EBVR200700000Motor · failedFAILED NORMAL MOTOR TRAVEL TIME CHECKS. SUSPECT NORMAL MOTOR BRAKE WAS PREVIOUSLY ASSEMBLED INCORRECTLY CAUSING DAMAGE TO MOTOR.SDR CA070503009Actuator · inoperative(CAN) THE SECONDARY ELECTRIC MOTOR, WHICH ACTUATES THE PITCH TRIM ACTUATOR IN RESPONSE TO AUTO PILOT COMMANDS WAS NOT OPERATIVE. THIS RENDERED THE AUTOPILOT SYSTEM U/S. THE ACTUATOR WAS REPLACED AND THE SYSTEM WAS CHECKED AIRWORTHY. THE O/H INTERVAL ON THESE ASDR COMA0770023Control Unit · faultyFLIGHT 5280 - STAB CH2 STATUS MESSAGE DISPLAYED ON AND OFF CONTINUOUSLY DURING CLIMB, CRUISE, LANDING AND TAXI. TRIM IN MOTION ORAL ON CONTINUOUSLY. ELECTRICAL SMELL IN AFT CABIN. LANDED DEN WITHOUT INCIDENT. REPLACED STAB ACTUATOR MCU. NO FURTHER DEFECTSSDR COMA0770022Motor · faultyFLIGHT 5280 - STAB CH2 STATUS MESSAGE DISPLAYED ON AND OFF CONTINUOUSLY DURING CLIMB, CRUISE, LANDING AND TAXI. TRIM IN MOTION ORAL ON CONTINUOUSLY. ELECTRICAL SMELL IN AFT CABIN. LANDED DEN WITHOUT INCIDENT. REPLACED NR 2 STAB ACTUATOR MOTOR. NO FURTHER SDR FDKA200703122Actuator · defectiveFDM 5968 CAK-ATL. PITCH TRIM MAIN CAUTION. MX REMOVED AND REPLACED PITCH TRIM ACTUATOR.SDR FDKA200702092Actuator · malfunctionedFDM 6004 LEX-ATL (1831 PHX LCL). AUTOPILOT FAILED IN FLIGHT ON CLIMBOUT. MX REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR.SDR CALA0700072Trim Motor · failedTHE ELECTRIC STAB TRIM FAILED WHILE ON APPROACH TO CLE. THE QRH WAS CONSULTED, AN EMERGENCY WAS DECLARED, AND MANUAL ADJUSTMENT OF TRIM WAS USED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ELECTRIC STAB TRIM MOTOR IAW MM 27-4SDR CA070503001Actuator · unserviceable(CAN) SHORTLY AFTER DEPARTURE, RUNWAY 27L, AT APPROXIMATELY 3000 FEET, THE AC ROLLED TO 45 DEGREES, AND PITCHED UP > 18 DEGREES. THE CREW RECOVERED THE AIRCRAFT AT AN ALTITUDE OF 4500 FEET. POST INCIDENT INVESTIGATION FOUND NO ANOMALIES WITH THE AILERON CONTSDR 2007UALA00125Actuator · faultyRTFL DUE TO LOSS OF LEFT ELAC. REPLACED TRIM ABLE HORIZONTAL STABILIZER ACTUATOR. SYSTEM OPS CHECKS OK.SDR 2007FA0000065Actuator · seized(REF NR: PT202781) AIRCRAFT ARRIVED WITH PITCH TRIM ACTUATOR SEIZED IN FULL NOSE UP POSITION. ACTUATOR IS DRIVEN BY TRIM CABLE LOOPED OVER ACTUATOR PULLEY WITH NO MEANS OF PREVENTING CABLE FROM SLIPPING ON THE PULLEY. IT IS POSSIBLE TO RUN TRIM TO FULL TRAVESDR MASA200602604Actuator · malfunctionedASH 2624 STL. AIRCRAFT HAD AN PITCH FEEL CAUTION MESSAGE. MX REMOVED AND REPLACED NR 2 PITCH FEEL ACTUATOR.SDR DL757091676Actuator · unknownHORIZONTAL STABILIZER TRIM ACTUATOR REPLACEMENT IAW 06-086621-03. C/W 06-086621-03.SDR 06FDEA02986Case · crackedALERT HYD 3 FAIL DURING CRUISE HYD 1 AND HYD 2 GOOD, USED ALTERNATE GEAR EXTENSION. TOWED TO PARKING. HYD 3 RIGHT EDP DISPLAYED AMBER TEMPERATURE "T". REMOVED AND REPLACED BOTH NR 3 ENGINE DRIVEN HYDRAULIC PUMPS. FOUND NR 2 HORIZONTAL STAB TRIM MOTOR CASSDR WRLA2006016Motor · leakingWOA8198/01 BGR/BGR AIR TURNBACK. ABOUT 10 MINS AFTER DEPT, HYD 3 OFF ALERT DISPLAYED (FLUID LOSS). RETURNED TO BGR WHEN SLATS WERE EXTENDED, HYD 3 FAIL ALERT DISPLAYED 0 FLUID. FOUND NR 1 STAB TRIM MOTOR LEAKING. REMOVED AND REPLACED STAB TRIM MOTOR. LEAK ANDSDR AMTA200600427Actuator · unserviceableON CLIMB OUT PASSING 4500 FT 250 KIAS, CAPT AND OF ELECTRIC TRIM DID NOT RESPOND. ALL STAB TRIM SWITCH IN NORMAL. STAB TRIM WHEEL WORKS NORMAL. PERFORMED FIM, NO FAULTS NOTED ALL OPS NORMAL. REMOVED AND REPLACED STAB TRIM MOTOR FOR PRECAUTIONARY REASON IAWSDR MASA200601561Motor · faultyASH 6302 TUS - STAB CH 2 W/NOT ENGAGE. MX REPLACED THE STAB MOTOR.SDR MASA200601564Actuator · failedASH 6332 PHX - STAB CHANEL 1 WILL NOT ENGAGE. MAINTENANCE REMOVED AND REPLACED HSTA AND MCU.SDR 0601213216Actuator · malfunctionedLOST BOTH AUTOPILOTS ON DESCENT, ECAM MESSAGE FLT STABILIZER JAM ANNUNCIATED, MANUAL TRIM OK. UNEVENTFUL NORMAL LANDING IN DIRECT LAW. INSPECTED PITCH TRIM CONTROL WHEEL, INSPECTED AND LUBED CABLES, CHECKED FOR FREEDOM OF MOVEMENT. PRECAUTIONARY REPLACEMENTSDR 06FDEA2240Attach Fitting · crackedTHS ACTUATOR UPPER EMPENNAGE ATTACH FITTING CRACKED IN VERT RADIUS FR 86 FR 87 REF N00371. REMOVED AND REPLACED FITTING IAW A310-200 SRM 51-72-10.SDR C2XA06IA092Actuator · failedIAH - FLIGHT 2173, THE CREW REPORTED THE NUMBER TWO PITCH TRIM RUNAWAY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER ACTUATOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT SDR CL6054052740Actuator · failedCREW REPORTED THAT HORIZONTAL STAB TRIM INDICATION WAS BOUNCING BETWEEN TWO DEGREES AND CREW WAS UNABLE TO TRIM NOSE-DOWN BELOW 1.2 DEGREES. T/S FOUND FAULTY HSTA.SDR 2006FA0000485Jackscrew · strippedMAINTENANCE PERSONNEL WERE ADVISED BY THE PILOT THE HORIZONTAL STABILIZER TRIM QUIT WORKING. INSPECTION FOUND THE BARREL SIDE OF THE TRIM SCREW JACK HAD STRIPPED OUT. THE SYSTEM INCLUDES 2 TRIM SCREW JACKS THE OTHER TRIM SCREW JACK TOOK ALL OF THE LOAD AND JSDR 2006F00016Shaft · fodFOREIGN OBJECT DAMAGE TO BALLSCREW ASSY SPA DURING OVERHAUL. SPA ON MARCH 21, 2006 AND DUPLICATED IN THIS REPORT AS REQUIRED FOR THIS REPAIR STATION. PROBLEM AS STATED IN REPORT: "THE MAJOR COMPONENTS ARE BEYOND ECONOMIC REPAIR (SCRAP). THE DAMAGE WAS CAUSSDR SWIA200616254Actuator · malfunctionedSTAB CHANNEL 1 INOP. REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW CRJ MM 27-42-01 AND 27-42-05, PN ON 8396-3 OFF 868 PN ON 7067-3 SN OFF 138.SDR SWIA200616246Actuator · malfunctionedSTAB CH1 INOP STATUS MESSAGE. REPLACED MCU AND TRIM ACTUATOR WITH SERVICEABLE UNITS PER CRJ MM 27-42-01. OPERATIONAL CHECK GOOD. PN 1 ON/OFF 8396-3 SN 1 OFF 796, PN 2 ON/OFF 7062-3 SN 2 OFF 1009.SDR AU510002164Motor · failedSTABILIZER TRIM MOTOR FAILED. CIRCUIT BREAKER TRIPPED.SDR CA051114001Actuator · unknown(CAN) DURING CLIMB, PITCH TRIM CAUTION LIGHT, AUTO TRIM FAIL MESSAGE ILLUMINATED. PITCH TRIM INDICATOR SHOWED FULL NOSE UP POSITION. FLIGHT CREW ELECTED TO RETURN TO DEPARTURE AIRPORT. MAINTENANCE: FCECU PRESENT FAULTS FOUND 63, 67, E3, AND E7. RESET FCECU SDR CA051114006Adapter · failed(CAN) RED (PITCH TRIM) ANNUNCIATOR WOULD ILLUMINATE INTERMITTENTLY WHEN DESCENT COMMANDED. THIS WOULD SOMETIMES OCCUR AS THE AUTO PILOT WOULD ATTEMPT TO TRIM. AUTO PILOT WOULD NOT DISENGAGE. PITCH TRIM ADAPTER REPLACED 31.4 HRS PREVIOUS DUE TO A DIFFERENT DEFESDR AU510001468Actuator · failed(AUS) STABILISER ELECTRIC TRIM ACTUATOR FAILED. CAUSED BY WORN AND STICKING CLUTCH. (OTHER CAUSE: STICKING CLUTCH PLATES ) (CASA# 510001468)SDR 2005FA0001492Bearing · corrodedTAILPLANE ACTUATOR EXCEEDED SCREW/CASING END PLAY LIMIT OF 0.25 MM AS LISTED IN MM. DISASSEMBLED UNIT AND FOUND PRESENCE OF WATER CONTAMINATION AND INTERNAL BALL BEARINGS RUSTED. DATE DISCOVERED 17 AUG 2005. UNIT SHOULD BE CHECKED INTERNALLY FOR CONDITION OSDR CA051101004Actuator · unknown(CAN) UNMODIFIED LOWER CLAW STOP FITTED WHICH IS NOT IN COMPLIANCE WITH DGAC AD NR. F2002-414R3 REF. TRW SB 47172-27-03 PARAGRAPH D (4). UNIT WAS REPAIRED AND SCREW SHAFT ASSY WAS REPLACED BY RETRO-FITTED ONE ON WHICH THE CLAW HAD NOT BEEN TO THE LATEST STANDASDR SWIA200515302Actuator · malfunctioned"STAB CH 2" STAB TRIM WILL NOT ENGAGE. REPLACED BOTH HSTCA AND HSTMC IAW AMM 27-40-00, 27-42-01, AND 27-42-05. OPERATIONAL CHECK GOOD, PN 7062-3, SN/OFF 799.
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