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 SWIA200515304Actuator · malfunctionedSTAB TRIM CHANNEL 2 STATUS MESSAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MCU IAW CRJ 200 MM 27-42-01. OPERATIONAL CHECK GOOD, PN 7062-3, SN/OFF 851.SDR SWIA200515220Control Unit · malfunctionedSTAB CH 1 INOP STATUS MSG AT FL390. REPLACED HORIZONTAL STAB MOTOR CONTROL UNIT IAW 27-42-07, OPERATIONAL CHECK GOOD.SDR ASMF200507001Motor · failedCAPTAIN REPORTED PRIMARY STAB TRIM STICKS OCCASIONALLY. COMPENSATION MECHANISM OF HORIZONTAL STABILIZER CHECKED IAW MM 27-40-0, BEING CORRECT. DURING TESTS, PRIMARY MOTOR OF STABILIZER FAILED. REPLACED IAW MM 27-40-01. TESTED CORRECT.SDR SWIA200515232Actuator · malfunctionedON DESCENT, GOT STAB TRIM CHANNEL 1 INOP STATUS MESSAGE. REPLACED HORIZONTAL STAB TRIM CONTROL ACTUATOR IAW AMM 27-42-01. OPERATIONAL CHECK IAW AMM 27-40-00.SDR SWIA200515147Actuator · malfunctionedAP PITCH TRIM MESSAGE DISPLAYED NUMEROUS TIMES DURING FLIGHT. REPLACED HSTA AND MCU IAW CRJ MM 27-42-01 AND 27-42-05. OPS CHECK GOOD, PN: 7062-3 SN OFF: 1296.SDR CA050407004Actuator · failed(CAN) INTERMITTENT FAILURE. AIRCRAFT DID NOT ARRIVE AT THE STATED POSITION. THE AUTOPILOT COMPENSATOR INDICATED FUNCTIONED NORMALLY, BUT THERE WAS NO MOVEMENT FROM THE HORIZONTAL STABILIZER WHICH CAUSED AN AUTO DISCONNECT OF THE AUTOPILOT SYSTEM. THE TWO MOTSDR CA050215002Ballscrew · corroded(CAN) INSP OF HORIZONTAL STABILIZER SCREWJACK DURING M01 CHECK REVEALED EVIDENCE OF INTERNAL CORROSION AS A RESULT OF DISCOLORATION IN LUBRICANT. TEARDOWN AND SHOP ANALYSIS REQUESTED WITH RESULTS TO BE FORWARDED TO AWC/YUL. NOTE: SDR ISSUED AGAINST (GDSP) REFSDR CA050214006Ballscrew · corroded(CAN) FAULT: WHILE CARRYING OUT AN INSPECTION. FOUND RUSTY COLORED LUBRICANT AND REDDISH STAINING ON THE STAB. JACKSCREW GIMBAL. A PURGING OF THE LUBRICANT FROM THE GIMBAL ASSY WAS CARRIED OUT. THE RUST COLORING WAS CONFIRMED TO BE DUE TO IRON IN THE GREASSDR AWXA200500037Actuator · failedON ARRIVAL, RECEIVED ECAM MESSAGE "F/CTL STABILIZER JAM. MX TROUBLESHOT IAW TSM 27-40-00-810-807, BITE TEST INDICATED "THS ACTR POS ERROR 9CE OF ELAC2", PERFORMED VISUAL INSPECTION OF MECHANICAL LATCHED INDICATOR, INDICATOR WAS NOT EXTENDED. TSM RECOMMENDS REPSDR 623456Actuator · failedAFTER LANDING, SELECTED FLAPS TO UP BUT DID NOT MOVE. FLAP / STAB FAIL MESSAGE, FLAP / STAB IND INOP MESSAGE.SDR W9YA200400001Actuator · inoperativeDURING A 14 CFR 91 REPOSITIONING FLIGHT, THE HORIZONTAL STABILIZER PITCH TRIM ACTUATOR FAILED IN THE MAIN AND STAND-BY MODES DURING CRUISE FLIGHT. THE PILOT REPORTED DIFFICULTY MAINTAINING LEVEL FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONSDR CA041006006Actuator · corroded(CAN) INSPECTION OF HORIZONTAL STABILIZER SCREWJACK DURING M01CHECK REVEALED EVIDENCE OF INTERNAL CORROSION AS A RESULT OF DISCOLORATION IN LUBRICANT.SDR CA041124010Actuator · failed(CAN) DURING DECENT INBOUND TO BASE, THE PITCH TRIM CAUTION LIGHT CAME ON, QRH PERFORMED AND IT BECAME APPARENT THAT WE HAD A FAILURE OF THE PITCH TRIM. ATC NOTIFIED AND THE APPROACH PLANNED WITH HIGH SPEED FOR AS LONG AS POSSIBLE. DURING SPEED REDUCTION STICSDR CA041124002Actuator · malfunctionedDURING TAKEOFF RUN AT A SPEED BETWEEN 100 AND 120 KIAS, GOT 'ELEVATOR FEEL' FAULT LIGHT ON. TAKEOFF ABORTED, PASSENGERS DEBRIEFED, AND RETURNED TO GATE. THE CENTRAL DIAGNOSTIC SYSTEM (CDS) WAS INTERROGATED AND FCECU FAULT CODES EA AND E9 WERE FOUND LOGGED INSDR CA040920001Actuator · corroded(CAN) WATER INGRESS INTO GEAR BOX CAUSED EXTENSIVE CORROSION, INVESTIGATION ON GOING WITH MFG (STAB TRIM ACTUATOR).SDR AUS20040498Actuator · faulty(AUS) HORIZONTAL STABILIZER TRIM ACTUATOR FAULTY.SDR 0423JKWActuator · inoperativeCREW REPORTED (PRIMARY TRIM FAULT) WHITE EICAS MESSAGE, WHICH CHANGED TO (PRIMARY AND SECONDARY TRIM FAIL EICAS) AMBER MESSAGE ON APPROACH TO LANDING. HORIZONTAL STAB SYSTEM LOCKED OUT ALL MOVEMENT FOR REMAINDER OF THE FLIGHT. CREW RESET SYSTEM POST LANDING,SDR CA040401006Actuator · failed(CAN) AUTO-PILOT TEST FAILED. ALTERNATE TRIM WAS SELECTED AND TESTED AND FOUND TO BE INTERMITTENT. PITCH TRIM ACTUATOR WAS REPLACED. NO FURTHER ACTION REQUIRED. PITCHTRIM FAILED TO MAKE OVERHAUL LIFE.SDR 3M57931704Resolver · inaccurateFLAP STAB MISCOMPARE CAS MESSAGE. STAB ACTUATOR HAS BAD RESOLVER.SDR COMA0460184Control Unit · malfunctionedFLIGHT 5492 STAB TRIM FAIL MESSAGE. REPLACED THE HSTCU.SDR CA040309004Motor · jammed(CAN) 2 HRS INTO FLT (STAB OUT OF TRIM) LIGHT ILLUMIN. NON-NORMAL CKLIST WAS COMPLETED, ELEC TRIM REMAINED INOP,TRIM CHANGES ACCOMPLISHED MANUALLY. MAINT CTRL WAS CONSULTED AND CB 6B AND 610 WERE PULLED AND RESET. (STAB OUT OF TRIM) LIGHT CONTINUED INTERMITTSDR QXEA200400172Motor · failedTUS - FLIGHT 2571 - IN FLIGHT, THE STAB CHANNEL INOP STATUS MESSAGE APPEARED WITH RUNAWAY TRIM CLACKER. MAINTENANCE INTERROGATED THE MAINTENANCE DIAGNOSTICS COMPUTER AND FOUND THE H-STAB RESOLVER FAILED. THE HSTA MOTOR WAS THEN REPLACED, OPERATIONAL CHECKS WSDR DHL2004873001Trim Motor · malfunctionedAFTER ROTATION AIRCRAFT RAPIDLY PITCHED UP TO 20 DEG ACTUATING THE STICK SHAKER. CREW PUSHED FULL UP ON CONTROL WHEEL TO FORWARD STOP. F/O ACTIVATED TRIM FROM 5.3 TO ZERO. RETURNED TO NORMAL CLIMB ATTITUDE. TRIM WAS 10 TO 2 DEG FOR CRUISE, 4.0 FOR APPROACHSDR AUS20040012Actuator · faulty(AUS) YAW DAMPER LINEAR ACTUATOR FAULTY.SDR SWIA200312732Actuator · malfunctionedSTAB TRIM CH 2 FAILS FFOD CHECK. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL PER TASK CARD RII 27-415. OPS CHECK GOOD. P/N 7062-3, S/N ON 786, S/N OFF 1184.SDR QXEA200301574Actuator · failedPDX - FLIGHT 2310 - ON APPROACH TO PDX, CREW RECEIVED A PITCH TRIM CAUTION. TRIM INDICATOR WENT TO FULL NOSE UP AND AUTO TRIM MESSAGES APPEARED ON BOTH PFD'S. NO TRIM WAS AVAILABLE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE PITCH TRIM ACTUATOR. OSDR AUS20031159Actuator · incorrect(AUS) INCORRECT GREASE USED ON TRIM ABLE HORIZONTAL STABILIZER ACTUATOR (THSA). AEROSHELL 22 USED INSTEAD OF CORRECT AEROSHELL 33. USE OF INCORRECT GREASE MAKES AIRCRAFT NON COMPLIANT WITH AD/330/7.UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR.SDR DJFA200300005Actuator · jammedAT 20,000 FT THE ELEVATOR TRIM DOWN ANNUNCIATOR ILLUMINATED. THE PILOTS DISCONNECTED THE AUTOPILOT, THE AIRCRAFT PITCHED DOWN AND WAS UNABLE TO MAINTAIN LEVEL FLIGHT. PILOTS DECLARED AN EMERGENCY AND LANDED WITH NO FURTHER PROBLEMS.SDR CA031120004Actuator · inoperative(CAN) DURING LEVEL FLIGHT, THE CREW ATTEMPTED TO INITIATE A SLOW DESCENT USING HORIZONTAL STAB PITCH TRIM AND NOTICED IT WAS INOPERATIVE. THEY TRIED TO USE THE SECONDARY (ALTERNATE) TRIM FUNCTION AND NOTICED IT WAS ALSO INOPERATIVE. THEY PERFORMED APPROPRIATE SDR AKG2003F00002Actuator · wornTHE THREADS IN THE ACTUATOR NUT ARE WORN AND ALLOWING THE NUT TO MOVE ON THE JACK SCREW AND BECOME JAMMED WHEN IT CONTACTS THE STOP ON EITHER END OF TRAVEL NOSE UP OR NOSE DOWN. PART LOCATION IS BETWEEN THE PILOT AND COPILOT SEATS UNDER THE FLOOR PANEL.SDR AWXA200301333Actuator · bindingDURING C-03 CHECK VERIFICATION FLT AFTER T/O PILOTS OBSERVED AN ELAC 1 & 2 PITCH FAULT FOLLOWED BY A REPORT THAT STAB JAMMED & STAB TRIM WHEELS WERE HARD TO MOVE. MAINT R&R THS ACT IAW A320 AMM. LEAK AND OPERATIONAL TEST OF THE THS ELECTRICAL CONTROL GOOD IASDR QXEA200301308Actuator · failedPDX-ON FLIGHT 2289, IDA-SEA FLIGHT DIVERTED TO PDX DUE TO PITCH TRIM CAUTION INFLIGHT. PITCH TRIM INOPERATIVE. TRIM INDICATION SHOWING FULL NU POSITION. OCCURRED AT FL 240 AT 240 KIAS; AUTO PILOT DISENGAGED WITH AUTO TRIM FAIL MESSAGE ON PFD. REMOVED AND REPLASDR 2003FA0001234Actuator · stuckDURING FINAL APPROACH, FLAPS WOULD NOT EXTEND BEYOND 35 DEGREES TO THE NORMAL 39 DEGREES, NOR COULD THE FLAPS RETRACT. LANDING WAS UNEVENTFUL. IT WAS LATER DISCOVERED THAT HORIZ STAB ACT (WHICH BEGINS TO MOVE HORZ STAB DOWN WHEN FLAPS GO BEYOND 10 DEGREES) WSDR DM42003F00000Nut · crackedSUBJECT HORIZONTAL STABILIZER ACTUATOR: RECEIVED WITH A CRACKED NUT WITH METAL PARTICLES ON SCREW SECTION AD 200-15-15.SDR 2003UALA00679Turnbuckle · unsafetiedHORIZONTAL STABILIZER ADJUSTMENT TURNBUCKLE FORWARD OF CABLE DRUM IN FORWARD EQUIPMENT AREA NOT SAFETY WIRED. MAJOR REPAIR ACCOMPLISHED, SAFETY WIRED TURNBUCKLE.SDR SWIA200312348Actuator · malfunctionedSTAB CH2 HSTA C/B POPPED WHEN POWERING A/C UP. WOULD NOT RESET. REMOVED AND REPLACED HSTC MOTOR CONTROL UNIT AND ACTUATOR IAW 27-42-01. OPS CHECKS GOOD. MCU P/N: 7062-3 S/N OFF: 113.SDR SWIA200312305Control Unit · malfunctionedSTAB TRIM CH 2 INOPERATIVE, WILL NOT ENGAGE. REPLACED HSTA AND MOTOR CONTROL UNIT AND REMOVED AND REPLACED FO'S DISCONNECT SWITCH IAW 27-40-00. P/N: 8396-3 S/N OFF: 806SDR SWIA200312368Actuator · failedHORIZONTAL STAB TRIM FAILS CHANNEL 2 ON PREFLIGHT TEST. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT. OPS CHECK GOOD IAW RII 27-415. MOTOR CONTROL UNIT PN: 7062-3 SN OFF: 961 SN ON: 218.SDR SWIA200312272Actuator · failedPITCH FEEL CB POP OUT IN FLIGHT CH NR 1. REMOVED AND REPLACED NR 1 ACTUATOR-LINEAR IAW MM 27-31-23. OPS CHECKS GOOD.SDR SWIA200312250Actuator · malfunctionedSTAB CH 1 INOP STATUS MESSAGE OCCURRED; WAS RESETTABLE, BUT REOCCURRED. STAB TRIM CAUTION AND MACH TRIM CAUTION ALSO OCCURRED AFTER RESETTING CHANNEL 1; ALSO RESETTABLE.REMOVED AND REPLACED HSTA AND MCU IAW CRJ MM 27-42-01. OPS CHECK GOOD. P/N: 7062-3 S/N SDR DL767030701Actuator · brokenDURING A LUBE VISIT (1T188), AN AMT FOUND THE LOWER ICE SCRAPER RING FROM THE STAB TRIM ACTUATOR BALL NUT BENT AND OUT OF PLACE. IT WAS FOUND AT THE BOTTOM OF THE BALLSCREW. THE ACTUATOR PART NUMBER IS 251T4310-1. THE PART NUMBER OF THE SCRAPER IS B18834-7R. RSDR QXEA200300893Actuator · malfunctionedPDX- ON FLIGHT 2315 SEA TO EUG, DIVERTED TO PDX DUE TO ON CLIMBOUT OF SEA AT 6,000 FEET ACCELERATING TO 240 KTS, "PITCH TRIM" CAUTION LIGHT ILLUMINATED. NO OTHER CAUTION LIGHTS ILLUMINATED. ELEVATOR TRIM POINTER WENT TO FULL NU AND ELEVATOR TRIM WAS INOPERATIVSDR SWIA200312203Actuator · malfunctionedSTAB TRIM AND MACH TRIM WILL NOT ENGAGE ON GROUND. REMOVED AND REPLACED HSTA & MCU IAW MM 27-40-00. OPS CHECK OK.MCU P/N: 7062-3 S/N OFF: 829.SDR MEX2003295Actuator · failedFLT 113 - TIJ-GDL - AIRTURN BACK DUE TO RIGHT CONTROL STABILIZER DID NOT OPERATE AND LEFT CONTROL STABILIZER WORKED INTERMITTENTLY. DURING REVSION THE SW S10-19 WAS DETECTED WITH OCCASIONAL FAIL. THE S10-19 AND BRAKE OVERRIDE SW S10-20 WERE REPLACED IAW MM 2SDR 03FDEA01047Trim Motor · contaminatedUPON APPLICATION OF POWER UP FOR TAKEOFF THE STABILIZER MOVED FROM 7.3 TO 5.4. AFTER REJECTED TAKEOFF WHILE ON TAXIWAY STABILIZER, RESET TO 7.3. UPON SUBSEQUENCY TAXI THE STAB MOVED BY ITSELF TO 9.2 AND THEN BACK TO ABOUT 5. T/S AND FOUND NR 2 TRIM MOTOR C/SDR IMJ2003F00001Motor · inoperativeCREW NOTICED SECONDARY TRIM (ON AUTOPILOT) DID NOT SEEM TO BE WORKING PROPERLY IN CRUISE. DISENGAGED AUTOPILOT AND TRIED TO TRIM MANUALLY. FOUND TRIM INOPERATIVE IN PRIMARY, SELECTED SECONDARY AND CONFIRMED IT WAS INOPERATIVE ALSO. AIRCRAFT WAS IN COMPLIANCSDR CA030526005Actuator · malfunctioned(CAN) HOLDING AT FL200 200KTS ELAC2 PITCH FAULT FOLLOWED BY A/P OFF, ALTN LAW AND ELAC 1PITCH FAULT. ECAM SHOWED STAB JAM BUT MAN. PITCH TRIM OK. DIR LAW ON MLG DOWN PITCH TRIM IN MAN STILL AVAIL. A/C HANDLING QUALITY WAS GOOD. NO FAULT LTS ON ELAC2/1 ON O/HEASDR SWIA200311923Actuator · malfunctionedAFTER TAKEOFF AND CLIMBING THROUGH 500 FT AGL, THE STAB CH1 INOP MESSAGE ILLUMINATED. RAN QRH PROCEDURE. MESSAGE PERSISTED. INSTALLED SERVICEABLE HORIZONTAL STABILIZER ACTUATOR IAW MM 27-42-01 AND RII 27-415. OPS CHECK GOOD. NO DEFECTS NOTED. ALSO INSTALSDR ARWA20030402Rotary Actuator · jammedRIGHT SUIT CASE HANDLE JAMMED IN FORWARD POSITION AND COULD NOT BE MOVED EVEN WITH C/B PULLED. REMOVED AND REPLACED RIGHT LONGITUDINAL TRIM SERVO ACTUATOR IAW MM 27-41-10. OPERATIONAL CHECK NORMAL IAW MM 27-40-0.SDR 2003F00150Actuator · defectiveHORIZONTAL TRIM ACTUATOR WOULD NOT ACTUATE IN EITHER THE PILOT/CO-PILOT/AUX POSITION. FOUND ACTUATOR TO BE BAD.
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