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 98FDEA00141Actuator · jammedON T/O AT FLAPS UP TRIM JAM AT 7.2 DEG NOSE UP. BOTH PICKLE SWITCH AND MANUAL TRIM SUITE CASE HANDLES, BUT NO MOVEMENT. CKD CIRCUIT BREAK AND RAN STAB INOP (2.5-12) NO HELP. TRIED BOTH AUTOPILOT, NO HELP. DUMP 110,000 LBS OF FUEL AND RETURN TO KANSAI. ON SDR 99ZZZX9Actuator · misinstalledDURING INSPECTION ATTEMPT TO LUBRICATE THE LEFT ELEVATOR TRIM ACTUATOR, DETERMINED THE PART NUMBER AND GREASE ZERT LOCATION WAS THAT OF THE RIGHT SIDE PART.SDR CA980318010Actuator · ratcheting(CAN) PITCH TRIM ACTUATOR FOUND OUT OF LIMITS WHILE DOING FAA AD 97-23-01.SDR AU980065Fitting · cracked(AUS) HORIZONTAL STABILISER PITCH TRIM ACTUATOR FITTING CRACKED.SDR PNSA980101Actuator · malfunctionedWHILE F/O WAS TRIMMING AIRCRAFT, AIRCAFT PITCHED UP SHARPLY AND TRIM CONTROL COULD NOT BE REGAINED BY FO, CAPT OR OVERRIDE SYSTEM. FLIGHT CREW OVERPOWERED THE FLIGHT CONTROLS AND A SAFE LANDING WAS ACCOMPLISHED. STABILIZER WAS FOUND IN THE FULL NOSE UP POSISDR 97ZZZX4827Actuator · failedTHE PILOT REPORTED THE PITCH TRIM ACTUATOR FAILED IN THE STANDBY MODE. AIRCRAFT SYSTEMS WERE CHECKED AND FOUND TO BE OK. REPLACED THE PITCH TRIM ACTUATOR WITH A NEW UNIT. SUBMITTER STATED THIS IS THE 4TH ACTUATOR TO BE INSTALLED SINCE JANUARY, 1997. THE AUSDR UPS97624812Actuator · inoperativeHORIZONTAL STABILIZER TRIM (NORMAL AND ALTERNATE) INOP DURING DESCENT INTO ONT TRIM STOPPED AT 4 ANU STAB TRIM BEGAN OPERATING AT 4000 FT STAB TRIM OPERATED NORMALLY AT 4000FT. AUTOPILOT EICAS MESSAGE WAS DISPLAYED PRIOR TO STAB TRIM. REMOVED AND REPLACED STSDR CA971113063Actuator · inoperative(CAN) HORIZONTAL STAB TRIM ACTUATOR FAILED 1.7 HRS AFTER INSTALLATION. ACTUATOR WAS PREVIOUSLY SENT IN FOR REPAIR OF MAIN TRIM MOTOR AND FAILED IN THE MAIN TRIM MOTOR SIDE AGAIN. INVESTIGATION FOR CAUSE OF THE FAILURE IS CURRENTLY IN PROGRESS.SDR 9719519926Drive Motor · failedPRIMARY LONGITUDINAL TRIM FAILED AFTER TAKEOFF. CIRCUIT BREAKERS H3, H4, H7, H8, H12, AND H14 WERE ALSO OPEN. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED PRIMARY DRIVE STABILIZER MOTOR, OPERATIONAL CHECK NORMAL.SDR 97ZZZX4285Actuator · malfunctionDURING PREFLIGHT, DISCOVERED THE SECONDARY TRIM OPERATED BACKWARDS. THE OVERHAULED ACTUATOR WAS INSTALLED 5 HOURS PREVIOUSLY. SUBMITTER STATED REVIEW OVERHAUL, FUNCTIONAL TEST AND QUALITY CONTROL PROCEDURES AT ELECTROMECH TECHNOLOGIES. FOLLOW MM PROCEDURES SDR COMA9760166Actuator · failedSTABILIZER CHANNEL 1 INOP MESSAGE ON EICAS. REPLACED THE HORIZONTAL STABILIZER ACTUATOR.SDR 97UAL900424Actuator · failedSTABILIZER MAIN ELECTRIC TRIM SLOW. CRUISE TRIM OK. FORWARD TRIM STALLS OUT, AFT TRIM OK. BRAKE ASSEMBLY SEEMS TO BE INOPERATIVE. COULD NOT MANUALLY CRANK STABILIZER TRIM FULL NOSE DOWN. ALSO, TRIMS ELECTRIC NOSE DOWN VERY SLOWLY. *S/D* REPLACED MAIN TRSDR COMA9760099Trim Actuator · malfunctionHORIZONTAL STABILIZER WILL ONLY TRIM NOSE DOWN 5 UNITS. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.SDR CA970505017Actuator · failed(CAN) ECAM MESSAGES, STABILIZER TRIM AND MACH TRIM APPEARED ON TAKEOFF ROLL AT 110 KNOTS. TAKEOFF REJECTED. HORIZONTAL STABILIZER TRIM ACTUATOR FOUND AT FAULT.SDR WRLA97010Motor · crackedDURING INITIAL CLIMB-OUT, FLIGHT CREW NOTED NR 3 HYDRAULIC SYSTEM FLUID QTY LOSS. FLIGHT CREW ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND STAB TRIM MOTOR HOUSING CRACKED. REPLACED TRIM MOTOR. SDR 9705012204Trim Brake · malfunctionedDURING APPLICATION OF THRUST POWER, TAKEOFF WAS ABORTED TO THE HEAVY STICK PRESSURES. TAKEOFF WAS ABORTED AT 140 KNOTS AND PERFORMED WITH NO INCIDENTS. REPLACED STABILIZER TRIM BRAKE MECHANISM, MAIN STABILIZER TRIM ACTUATOR, AND R27 NOSE UP STABILIZER TRIM RSDR COMA9760039Actuator · malfunctioned'CON FIG.' STABILIZER TRIM WARNING DURING TAKEOFF. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.SDR DLL12970207Actuator Bolt · brokenWHILE WORKING A AUTOPILOT, DISCOVERED D-SYS HORIZONAL STAB HYDRAULIC ACTUATOR LOWER ATTACH BOLT BROKEN. REPLACED PER MAINTENANCE MANUAL 27-41-28.SDR COMA9760022Trim Actuator · inoperativeA/P PITCH TRIM MESSAGE DURING FLIGHT STAB. CHANNEL NR 1 MESSAGE AT SAME TIME. REPLACED HSTA AND MCU.SDR COMA9660224Actuator · malfunctionCONFIG WARNING DURING TAKEOFF. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.SDR 9625632707Actuator · inoperativeDURING CLIMBOUT, MAIN ELECTRIC STABILIZER TRIM WENT INOPERATIVE. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED STABILIZER TRIM ACTUATOR, OPERATIONAL CHECK OK.SDR CA961112027Nut Tubes · failed(CAN) DURING PERIODIC INSPECTION, PITCH TRIM NOTED MAKING LOUD GRINDING NOISES. ACTUATOR REPLACED. TEAR DOWN INDICATED THAT THE NUT TUBES WERE REPLACED AT OVERHAUL. AD 93-15-02R2 REQUIRES THAT THE OPERATOR DETERMINE IF THE NUT TUBE ASSEMBLY WAS REPLACED AND IFSDR 97ZZZX2715Actuator · brokenTHE BROKEN STABILIZER JACK SCREW WAS FOUND DURING A 400-HOUR AIRFRAME INSPECTION. ISRAEL AIRCRAFT IND RELEASED A MANDATORY SB RECENTLY TO INSPECT COMPONENTS WITHIN 50 HOURS OR AT THE NEXT INSPECTION. SUBMITTER'S CONCERN IS THE METHOD THAT IS USED TO DETECT ASDR 97ZZZX2714Actuator · brokenUPON INSPECTION FOUND LEFT HAND JACK SCREW ON PITCH TRIM ACTUATOR S/N 7082-08AA BROKEN. HIGH CYCLES AND HEAVY USE OF THRUST REVERSERS CAUSE VIBRATION IN THE TAIL WHICH COULD HAVE RESULTED IN THIS FAILURE. INSTALLED 4-3-86. LANDINGS SOH, 3,457.SDR 96ZZZX5153Bearing · leaking greaseSTAB ACTUATOR CLUTCH BEARINGS MIGRATE SMALL AMOUNT OF GREASE THAT COATS THE SLIP RING AND BRUSHES REDUCING D.C. CURRENT TO THE CLUTCHES EFFECTING THE UNITS OUTPUT TORQUE.SDR DHL96703003Actuator · jammedSTABILIZER TRIM JAMMED FROM TOP OF DESCENT, WOULD NOT STRIM NOSE UP. COMPLIED WITH ALTERNATE PROCEDURE. CLEANED AND LUBED STAB TRIM JACKSCREW DUE TO EXCESSIVE MOISTURE. REPLACED MAIN STAM ACTUATOR, ACTUATED STAB TRIM FULL TRAVEL AND NO DEFECTS NOTED.SDR 96ZZZX3733Actuator · shaft shearedDURING A 600-HOUR ROUTINE INSPECTION, NOTED A PORTION OF THE HORIZONTAL STABILIZER WAS STRIKING THE FUSELAGE AND CAUSING PAINT DAMAGE. AFTER FURTHER INVESTIGATION DETERMINED THE PITCH TRIM ACTUATOR SHAFT HAD SHEARED. THE PITCH TRIM ACTUATOR IS ATTACHED TO THSDR 9613193247Actuator · malfunctionedDURING CLIMBOUT AT APPROXIMATELY 600 FEET AGL, RECEIVED 'F/CTL ELAC 2 PITCH FAULT' ACCOMPANIED BY UNCOMMANDED 2 TO 3 DEGREE PITCH DOWN INPUTS AND SLUGGISH PITCH RESPONSE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. SDR CA960910005Lock Pin · sheared(CAN) ACTUATOR HAD REFURBISHED NUTS AND SHAFTS INSTALLED AT PREVIOUS OVERHAUL INSPECTION AT 3000 HOURS FOUND RH SHAFT FREE END PLAY AT MID POINT OF TRAVEL WAS APPROXIMATELY 0 010, LEFT SHAFT FREE END PLAY NEGLIGIBLE, LEFT ROD END ASSEMBLY INNER SHAFT COULD BESDR USAAD96062Trim Motor · failedPIT/EWR - FLT 936 - PRIMARY TRIM DOES NOT TRIM FORWARD. RETURNED TO FIELD. REPLACED PRIMARY TRIM MOTOR AND TRIM BRAKE RELAYS. (X)SDR COMA9660994Trim Actuator · malfunctionSTABILIZER TRIM CHANNEL 1 INOPERATIVE MESSAGE ON EICAS. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.SDR COMA9660993Trim Actuator · malfunctionHORIZONTAL STABILIZER CHANNEL 1 WILL NOT ENGAGE. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.SDR COMA9630078Actuator · failedTHE MAIN PITCH TRIM IS INOP. REPLACED THE PITCH TRIM ACTUATOR.SDR AU960415Actuator · failed(AUS) HORIZONTAL STABILISER PRIMARY TRIM ACTUATOR FAILED INTERNALLYSDR COMA9660042Actuator · failedSTABILIZER TRIM CHANNEL ONE IS INOP. REPLACED THE STABILIZER TRIM ACTUATOR.SDR 96ZZZX1638Motor · misassembledON 2-27-96, TWO HORIZ STAB ACTUATOR MOTORS, SN AH-57563 AND SN AH-57871, WERE RECEIVED FROM REPAIR STATION AFTER INSPECTION AND VERIFICATION IAW REF AD AND AIRBUS AOT REFERENCED THEREIN. THESE MOTORS WERE ASSEMBLED TO AN A310 TAILPLANE ACTUATOR, PN 47142-203,SDR CA960131003Shaft · loose(CAN)ACTUATOR HAD REFURBISHED NUTS AND SHAFTS INSTALLED AT OVERHAUL. DURING ROUTINE INSPECTION AT 2800 HOURS IN SERVICE SOME FREE PLAY WAS NOTED. HOWEVER, AT REMOVAL FREE PLAY WAS 0.009 BOTH LH AND RH. ALS O THE ROD END ASSEMBLY HAD FREE PLAY DUE TO THE LOCK NSDR 9520753208Packing · leakingFLIGHT CREW SENT ACARS MESSAGE NOTIFYING OF GREEN HYDRAULIC SYSTEM LOW LEVEL. THE LANDING GEAR WAS MANUALLY EXTENDED, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT ELEVATOR GREEN SERVO CONTROL ACTUATOR FILTER SDR QXEA9500426Actuator · malfunctionedALW - FIRST OFFICER NOTED TRIM-IN-MOTION BEEP, BUT HAD NO STABILIZER TRIM AFTER FLAPS WERE SELECTED TO FULL. TRIM SELECTED TO CAPTAIN'S SIDE AND STILL NO TRIM. AIRCRAFT LANDED IN ALW WITHOUT FURTHER INCIDENT.SDR COMA9560614Trim Act · defectiveHORIZONTAL STABILIZER CHANNEL 2 IS INOP. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.SDR CA951206013Actuator · failed(CAN)INBOARD TRIM SWITCH WHICH SHOULD OPERATE ORAL TRIM ALARM, ALLOWED ACTUATOR TO RUN, BUT THE STABILIZER DID NOT MOVE. ACTUATOR REPLACED.SDR CA951122015Actuator Screw · worn(CAN)LEFT AND RIGHT HAND TRIM ACTUATOR SCEWS WORN WHERE THEY SIT IN THE BEARING. SUBMITTER SUGGESTS INSTALLING KIT P/N SK 185-27 WHICH INCLUDES AN INSPECITON PANEL AND LUBRICATION PROVISIONS.SDR COMA956096Hsta · failedHORIZONTAL STABILIZER TRIM CHANNEL NR 2 INOP. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.SDR COMA9560571Trim Actuator · failedHORIZONTAL STABILIZER TRIM CHANNEL NR 1 INOPERATIVE MESSAGE ON EICAS. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.SDR COMA9560553Trim Actuator · defectiveHORIZONTAL STABILIZER CHANNEL NR 2 WILL NOT ENGAGE. REPLACED THE STABILIZER TRIM ACTUATOR.SDR 95ZZZX4467Actuator · failedPITCH TRIM ACTUATOR, SN 187, FAILED 16 FLIGHT HOURS AFTER INSTALLATION. SN 186 WAS INSTALLED IN ITS PLACE, AND IT FAILED ON THE FOLLOWING DAY (EXACT NUMBER OF HOURS IN USE AFTER INSTALLATION UNKNOWN AT THIS STATION).SDR 95ZZZX4466Actuator · failedPITCH TRIM ACTUATOR, SN 187, FAILED 16 FLIGHT HOURS AFTER INSTALLATION. SN 186 WAS INSTALLED IN ITS PLACE, AND IT FAILED ON THE FOLLOWING DAY (EXACT NUMBER OF HOURS IN USE AFTER INSTALLATION UNKNOWN AT THIS STATION).SDR COM20386Actuator · failedSTABILIZER CHANNEL 1 INOP STATUS MESSAGE ON CIRCUIT BREAKER TRIPPED. REPLACED THE HORIZONTAL STABILIZER ACTUATOR AND MOTOR CONTROL UNIT.SDR 95ZZZX4287Actuator · failedINTERMITTENT PITCH TRIM FAIL INDICATION. TIME IN SERVICE OF THIS REPAIRED PART - 16.8 HOURS. THIS IS THE FOURTH FAILURE OF THIS PART ON THIS AIRCRAFT.SDR 95ZZZX3821Actuator · failedREPAIRED UNIT FROM CRS-BS4R087M REINSTALLED, 6-8-95. TEST FLIGHT AT ALTITUDE FAILED. UNIT STILL GOING INOP AFTER COLD SOAKING. REINSTALLED RENTAL UNIT AND RETURNED S/N 222 TO VENDOR 6-14-95. CONDITION CAUSE UNKNOWN AT THIS TIME.
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