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.

SDR CA011227004Hose · ruptured(CAN) ON DESCENT INTO YQM,FLIGHT CREW EXPERIANCED HYD SYSTEM "B" FLUID QTY DECREASING. UPON ARRIVAL, MAINTENANCE FOUND SYTEM "B" PUMP NR 2 HYDRAULIC HOSE ASSY IN SERVICE BAY FAILED, HOSE ASSY REPLACED, HYDRAULIC SYSTEM COMPONENTS INSPECTED, AND FOUND B SYDec 26, 2001 · Boeing 727227SDR SWIA200110470Control Unit · failedSTAB TRIM AND MACH TRIM DISCONNECT WHEN RUNNING TRIM UP AND DOWN. (CAT II). REMOVED AND REPLACED STAB TRIM ACTUATOR. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW WITH 27-42-01 AND 27-42-05. OPS CHECKS GOOD. STAB TRIM UNIT P/N 8391-3, S/N OFF 254.Dec 24, 2001 · N589SW · Cndair CL6002B19SDR CA020103009Computer · failed(CAN) STAB TRIM / MACH TRIM WILL NOT STAY ENGAGED. REMOVED AND REPLACED THE HORIZONTAL STABILIZER COMPUTER.Dec 16, 2001 · Cndair CL6002B19SDR C2XA01TY191Actuator · failedTYS DURING A SCHEDULED INSPECTION THE HORIZONTAL STABILIZER ACTUATOR FAILED A FUNCTIONAL CHECK. THE ACTUATOR INNER PISTON HAS PLAY AND NONE WAS ALLOWED IAW CONTINENTAL EXPRESS TASK CARD 27-40-02-220-001-A00. MAINTENANCE REMOVED AND REPLACED THE ACTUATOR IAWDec 11, 2001 · N27512 · Emb EMB135ERSDR CA020104014Control Unit · failed(CAN) STAB TRIM FAILED BOTH CHANNELS ON APPROACH INTO BOSTON. EMERGENCY LANDING DECLARED BY FLIGHT CREW. HORIZONTAL STAB CONTROL UNIT (HSTCU, MOTORS CONTROL UNIT (MCU) AND HORIZONTAL STAB ACTUATOR (HSTA)REPLACED. SYSTEM TESTED AS PER AMM. CONSIDERED SERVICEABLDec 6, 2001 · Cndair CL6002B19SDR GTIA011145Motor · failedFLT 779 - LGA - PRIMARY STABILIZER TRIM STALLED, AND EXPERIENCED THERMAL SHUTDOWN TWICE ON CLIMB-OUT, AND ONCE IN LEVEL CRUISE. REMOVED AND REPLACED HORIZONTAL STAB PRIMARY LONGITUDINAL TRIM ACTUATOR MOTOR. OPS CHECK NORMAL IAW MM 27-40-01. (M)Nov 27, 2001 · N812NK · Doug DC982SDR UG82001F00011Seal · damagedHORIZONTAL STABILIZER TRIM ACTUATOR TEFLON SEAL ON JACKSCREW DAMAGED AND PROTRUDING. FOUND DURING SCHEDULED LUBRICATION CALL OUT. REPLACED WITH SERVICEABLE UNIT.(K)Nov 20, 2001 · N5115 · Cessna 750SDR AUS20011396Actuator · faulty(AUS) STABILISER ACTUATOR SUSPECT FAULTY.Nov 16, 2001 · Fokker F28MK4000SDR AUS20011395Actuator · failed(AUS) STABILISER ACTUATOR FAILED.Nov 13, 2001 · Fokker F28MK4000SDR C2XA01CL228Actuator · failedMSN FLIGHT#3110 THE CREW REPORTED THE HORIZONTAL STABILIZER PITCH TRIM FAILED AFTER TAKEOFF.THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE HORIZONTAL STABILIZER PITCH TRIM ACTUATOR AND THE HORIZONTAL STABILIZER CONTNov 12, 2001 · N16502 · Emb EMB135ERSDR UPS01837269Fastener · corrodedINSPECTION TYPE:N/A SEVERAL FASTENERS CORRODED IN COMPARTMENT 60 HORZ STABILIZER ACTUATING MECHANISM AREA ITEM SUBMITTED BY FOG TEAM. REMOVED AND REPLACED FASTENERS. CLEANED CORROSION FROM MARKET BOTLS APPROX 120 EA HUCK FASTENERS EXTENDING THROUGH LIGHTENINNov 9, 2001 · N779UP · Doug DC871FSDR JGV2001F00014Actuator · damagedFOUND SCREW ASSEMBLY SEIZED AROUND MID RANGE OF TRAVEL AND UNABLE TO MOVE. DISASSEMBLED AND FOUND THE NUT SEIZED ON THE SCREW IN AN AREA WHERE FIVE INDEXED THREADS WERE GALLED AT THE TOP END OF THE NUT. THE GREASE ON THE NUT AND SCREW WAS ADEQUATE. THE PHYSNov 2, 2001 · N73GP · Lear 55LEARSDR CA030416004Actuator · failed(CAN) FROM TSB A01A0112, FOLLOWING TAKE OFF OF A FLOAT EQUIPPED DHC 3T, THE CONTROL COLUMN PITCHED VIOLENTLY FORWARD AND BACK BEFORE RETURNING TO A NEUTRAL POSITION. THE AIRCRAFT THEN PITCHED DOWN AND CONTACTED THE WATER IN A NOSE DOWN, WINGS LEVEL ATTITUDE. Nov 1, 2001 · Dhav DHC3SDR SWIA200110279Actuator · failedSTAB TRIM AND MACH TRIM MESSAGE AFTER TAKEOFF. RE-ENGAGED BOTH SYSTEMS. BOTH SYSTEMS FAILED AGAIN. RETURNED TO SLC. REMOVED AND REPLACED HSTA WITH A SERVICEABLE UNIT IAW AMM 27-42-01. ALSO REMOVED AND REPLACED MCU WITH A SERVICEABLE UNIT IAW AMM 27-42-05.Oct 27, 2001 · N594SW · Cndair CL6002B19SDR 0103699920Motor · leakingON CLIMBOUT, THE PRIMARY TRIM CONTROL AND BOTH YOKE SWITCHES WERE INOPERATIVE. CREW RESET THE CIRCUIT BREAKERS AND CHECKED THE CUTOUT WITH NO HELP. ALTERNATE TRIM VIA AUTOPILOT DID OPERATE NORMALLY. FLIGHT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE FOUNOct 22, 2001 · N942N · Doug DC932SDR CA010924006Actuator · failed(CAN) ON DEPARTURE YYZ ATTEMPTED FORWARD HORIZONTAL STAB TRIM USING CONTROL WHEEL SWITCHES. NO FORWARD TRIM AVAILABLE, FULL AFT TRIM OK. AUTO PILOT SEEMED ABLE TO TRIM FORWARD. STABILIZER TRIM MAIN ACTUATOR REPLACED AS PER AIRCRFT MAINTENANCE MANUAL 27-41-71. Sep 9, 2001 · Boeing 7372T7SDR GTIA012055Drive Unit · wornFOUND HORIZONTAL STABILIZER DRIVE ACME DRIVE AND NUT WEAR OUT OF LIMITS. REMOVED ACME SCREW ASSY FROM LONGITUDE ACTUATOR. INSTALLED ACME SCREW AND NUT ASSY IAW MD80 MM 27-40-01. (M)Aug 30, 2001 · N814NK · Doug DC983SDR CA010831009Actuator · slipped(CAN) DURING A TRAINING FLIGHT, THE PITCH TRIM FAILED TO MOVE WHEN SELECTED BY EITHER PILOTS OR CO-PILOTS CONTROL FOR APPROXIMATELY 2 MINUTES DURING THE FLIGHT. ONCE PITCH TRIM CONTROL WAS RESTORED, THE AIRCRAFT LANDED WITHOUT INCIDENT. A SUBSEQUENT INSPECTIOAug 27, 2001 · Swrngn SA226TCSDR SWAA012115Actuator · inoperativeAIR TURNBACK, STAB TRIM MOTOR INOP. REMOVED AND REPLACED STAB TRIM ACTUATOR PER MM.Jul 26, 2001 · N739GB · Boeing 7377H4SDR 2001UALA01343Actuator · failedCREW REPORTS A GRINDING NOISE HEAR WHEN CRUISE TRIM ENGAGED. MANUAL TRIM WAS JAMMED IN THE NOSE UP POSITION. AIRCRAFT RETURNED TO DEN. REPLACED THE MAIN STAB TRIM ACTUATOR, CRUISE STAB TRIM ACTUATOR AND STAB BRAKE ASSY. SYSTEM OPERATIONS CHECK NORMAL.Jul 4, 2001 · N7277U · Boeing 727222SDR AUS20010781Actuator · leaking(AUS) STABILIZER ACTUATOR LEAKING. LOSS OF HYDRAULIC FLUID.Jun 26, 2001 · Fokker F28MK4000SDR CA010703011Actuator · noisy(CAN) PITCH TRIM ACTUATOR FAILED ROUTINE FUNCTION CHECK. PRIMARY MOTOR SOUNDS ROUGH WHEN ACTUATED.Jun 25, 2001 · Pilats PC1245SDR CA010629035Actuator · failed(CAN) IN CRUISE THE CREW NOTICED THAT THE STAB TRIM WAS INOPERATIVE IN NOSE DOWN MODE. FURTHER TROUBLE SHOOTING AFTER LANDING CONFIRMED THE ACTUATOR FAILED INTERNALLY. LOUD GRATING NOISE WHEN TRIMED IN THE NOSE DOWN DIRECTION. ACTUATOR REPLACED AND AIRCRAFT REJun 5, 2001 · Pilats PC1245SDR DHL2001741010Actuator · intermittentMAIN ELECTRIC TRIM WILL NOT TRIM NOSE UP FOR CAPT OF P/N CRUISE TRIM WORKS NORMAL. PROBLEM IS INTERMITTENT. REMOVED AND REPLACED MAIN ELECTRIC TRIM STAB ACTUATOR. OPS CHK'D GOOD ALL WORK DONE IAW MM 27-40-31.May 26, 2001 · N741DH · Boeing 7272Q9SDR DHL2001805010Actuator · failedCONTROL WHEELS TRIM SWITCHES INOP. REMOVED AND REPLACED LT ROTARY ACT PER DC-8 MM 27-41-10.May 18, 2001 · N805DH · Doug DC873FSDR DHL2001805009Actuator · failedCONTROL WHEELS TRIM SWITCHES INOPERATIVE. REMOVED AND REPLACED LEFT LONG TRIM ACTUATOR. OP CHECKS GOOD PER M/M.May 18, 2001 · N805DH · Doug DC873FSDR ABXA010221Actuator · seizedTHE CREW REPORTED THE STABILIZER HYDRAULIC SYSTEM TO BE INOPERATIVE. THE LEFT SUITCASE HANDLE WAS JAMMED FULL FORWARD. MAINTENANCE INSPECTED AND REPLACED THE LEFT LONGITUDINAL TRIM ACTUATOR IAW DC8 MM.May 8, 2001 · N819AX · Doug DC863SDR QXEA0100764Fitting · corrodedYYC - HORIZONTAL STAB DRIVE FITTING HAS SOME FRETTING OF THE RIGHT-HAND AFT LUGS, INBOARD SIDE. REPAIRED IAW HORIZON AIR EA 4-55-290 AND FOKKER FAX TS06.54293.Apr 27, 2001 · N486US · Fokker F28MK4000SDR 0101511233Case · splitDURING CLIMBOUT OF LGW, NR 3 HYDRAULIC SYSTEM ELEVATOR OFF LIGHT ILLUMINATED. FOLLOWED COM PROCEDURES AND RETURNED TO LGW LANDING WITHOUT INCIDENT. FOUND RIGHT STABILIZER DRIVE MOTOR CASE SPLIT. REPLACED MOTOR AND FILTERS AND SERVICED NR 3 HYDRAULIC SYSTEM.Apr 22, 2001 · N233NW · Doug DC1030SDR C2XA01TY084Fitting · gougedTYS DURING A SCHEDULED INSPECTION THE RIGHT HORIZONTAL ACTUATOR SUPPORT FITTING WAS FOUND GOUGED. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1340/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Apr 22, 2001 · N16502 · Emb EMB135ERSDR CALA0100317Actuator · wornINSPECTION FOUND HORIZONTAL STABILIZER ACTUATOR GIMBAL WORN BEYOND LIMITS. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 27-41-10.Apr 9, 2001 · N58101 · Boeing 757224SDR SWIA972517Actuator · malfunctionedAUTOPILOT PITCH TRIM MESSAGE ILLUMINATED WHILE DESCENDING TO FL 270. AFTER FOLLOWING QRH PROCEDURE MESSAGE EXTINGUISHED. RETURNED TO SLC. AUTOPILOT PITCH TRIM SYSTEM OPS CHECKS GOOD. REPLACED THE STABILIZER TRIM ACTUATOR AND MOTOR CONTROL UNIT.Apr 6, 2001 · N413SW · Cndair CL6002B19SDR SIMA200108602Actuator · failedORD - FLT 4433 - CREW REPORTED AFTER TAKEOFF PRIMARY TRIM CONTROL TO BE INOPERATIVE, FOLLOWED LATER BY AUTO TRIM FAIL. BACKUP TRIM FUNCTIONED NORMALLY. REMOVED AND REPLACED PITCH TRIM ACTUATOR IAW AMM. OPS CHECK GOOD. (M)Mar 27, 2001 · N718AE · Emb EMB135ERSDR 2001UALA00370Actuator · corrodedHORIZONTAL STABILIZER TRIM ACTUATOR PRIMARY BRAKE FAILURE INSIDE UNIT. FOUND EXTREME CORROSION INSIDE AND OUTSIDE OF UNIT. BREAKDOWN OF GREASE DUE TO EXCESSIVE WATER INSIDE UNIT. REPLACED ACTUATOR.Mar 25, 2001 · N507UA · Boeing 757222SDR COMA0160304Actuator · malfunctionedSTABILIZER TRIM WILL NOT REMAIN ENGAGED. REPLACED THE HSTA.Mar 8, 2001 · N967CA · Cndair CL6002B19SDR 20010503CW007Actuator · inoperativePILOT SELECTED 10 DEGREES FLAPS, FLAPS MOVED TO THE SETTING BUT HORIZONTAL STABILIZER DID NOT AGREEE WITH FLAP SETTING. PILOT SELECTED FULL FLAPS DOWN SETTING BUT FLAPS WOULD NOT MOVE. MAINTENANCE CREW FOUND THAT A/C HORZ STAB ACTUATOR WAS INOPERATIVE. ON RFeb 28, 2001 · N440CP · Gulstm GIVSDR SWIA972387Actuator · inoperativeSTAB TRIM WILL NOT OPERATE (PILOT OR COPILOTS) USING STAB TRIM CH-2. REMOVED AND REPLACED MOTOR CONTROL UNIT. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR, REF MM 27-42-61, 27-42-05. OPS CHECK GOOD ON BOTH CHANNELS. MEETS CAT II STANDARDS. CONTROL Feb 21, 2001 · N411SW · Cndair CL6002B19SDR 20010406CW005Plate · crackedMOUNTING LUGS CRACKED AND BROKEN ON THE PLATE. PROBABLE CAUSE, FATIGUE, OVERSTRESSED.Feb 20, 2001 · Boeing 747*SDR COMA0160245Actuator · malfunctionedSTAB TRIM, MACH TRIM DISENGAGED. REPLACED THE HSTA.Feb 15, 2001 · N918CA · Cndair CL6002B19SDR COMA0160159Actuator · malfunctionedCONFIG STAB AND CONFIG TRIM WARNING. REPLACED THE HSTA.Jan 24, 2001 · N785CA · Cndair CL6002B19SDR COMA0160029Actuator · malfunctionedSTABILIZER TRIM CHANNEL 2 DISENGAGED. REPLACED THE HSTA.Dec 29, 2000 · N956CA · Cndair CL6002B19SDR MWEA001318Actuator · failedACTUATOR PRIMARY TRIM INOPERATIVE. -- OPS CHECK OF PRIMARY TRIM SYSTEM, ALL FUNCTIONS NORMAL.Dec 27, 2000 · N215ME · Doug DC932SDR 20010223CW004Actuator · failedNORMAL PITCH SYSTEM INOPERATIVE. AC WAS ON RAMP ALL NIGHT. DISCREPANCY FOUND BEFORE DEPARTURE. COLD AND DAMP WEATHER CONTRIBUTED TO ACTUATOR NOT WORKING. DURING REMOVAL AND INSTALLATION OF AN O/H ACTUATOR IN HANGER SYSTEM WORKED OK. NOTED: GREASE PLUGGINDec 22, 2000 · N62ND · Israel 1124SDR CA010126014Control Unit · failed(CAN) HORIZONTAL STAB LOCKED UP. PILOTS COULD MOVE NOSE DOWN BUT NOT BACK TO NOSE UP WITH TRIM WHEEL. HOWEVER, STAB WORKED NORMAL ELECT.LY. MAINT CNTL ADVISED CREW TO CYCLE STAB SWITCHES&RESET HYDRAULIC CNTL PANE L - UNSUCCESSFUL RESULTS. A/C RETURNED&LANDED WDec 20, 2000 · Fokker F28MK1000SDR 20010125CW013Spring · brokenSPRINGS ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM, CAUSING THE UNIT TO BIND AND JAM.PROBABLE CAUSE/IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE AND INCREASED SPRING COIL STRESSES.Dec 18, 2000 · Boeing 737SDR CA001229018Actuator · failed(CAN) DURING TAKEOFF, THE STAB TRIM CHANNEL 1 DISCONNECTED IN FLIGHT. AIRCRAFT RETURNED NORMALLY TO THE AIRPORT.MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB TRIM ACTUATOR.Dec 11, 2000 · Cndair CL6002B19SDR CA001129027Actuator · failed(CAN) BOTH STABILIZRER TRIM CHANNELS FAILED, BOTH WENT BACK TO NORMAL, THEN REOCCURRED ON LANDING. ATTEMPTED TO RESET, MESSAGE DISAPPEARED MOMENTARILY, THEN FAULT REOCCURRED. HISTORY FAULT.STABILIZER MOTOR CONTROL UNIT (P/N 7062-3) AND HORIZONTAL STABILIZER TRNov 6, 2000 · Cndair CL6002B19SDR CA001205016Actuator · failed(CAN) PRIMARY HORIZONTAL STABILIZER TRIM FAILED CREW ADVISORY SYSTEM WARNING. SECONDARY TRIM SERVICEABLE. REPLACED HORIZONTAL TRIM ACTUATOR.Oct 28, 2000 · Lear 45LEARSDR AU001215Actuator · faulty(AUS) HORIZONTAL STABILISER TRIM MOTOR FAULTY.Oct 27, 2000 · Boeing 737476SDR CA001218010Bearing · separated(CAN) RT LOWER ROD END ON PITCH TRIM ACTUATOR FOUND SEPARATED FROM RACE ALLOWING RACE TO CONTACT RT INBOARD FLANGE OF FORWARD HORIZONTAL STAB SUPPORT. THIS CAUSED WEAR ON THE FORWARD NORIZONTAL STAB FORWARD SUPPORT RENDERING IT UNSERVICEABLE. FORWARD HORIZONTAOct 26, 2000 · Beech 100BEECH
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