JASC 2740

Service difficulty reports · 2,126

Reports filed under 2740 · Stabilizer Control System, 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 = '2740'
  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 GLBA20110307FStructure · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RT STABILON OB TIP DAMAGED WHILE PARKING IN HANGER. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-55-005. MATERIALS UTILIZED ARE INCLMar 5, 2011 · N218YV · Beech 1900DSDR C2XA11IA038Trim Switch · inoperativeMCI - FLIGHT 6208, THE CREW REPORTED THE F/O'S PITCH TRIM SWITCH WAS INOPERATIVE. THE AIRCRAFT RETURNED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE F/O'S PITCH TRIM SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRMar 1, 2011 · N14148 · Emb EMB145XRSDR USAA2011022890885Unknown · malfunctionedFLT 1222 - CLT-BWI - EMERGENCY LANDING - EXPERIENCED PROBLEMS WITH STABILIZER, EXTREME AIRFRAME BUFFET INCURRED. COMPLETED TASK CARDS 26T00027002 (ELEVATOR AND AILERON SERVO CONTROLS), 26T00027003 (OPERATIONAL TEST OF RUDDER SERVO, STAB TRIM, AND CARGO SMOKE Feb 24, 2011 · N762US · Airbus A319112SDR 2011FA0000222Jackscrew · out of positionDURING O/H, MX PERFORMED ON THE SCREW JACK ASSY, FE140 SN 125, IDENTIFICATION OF THE WRONG POSITIONING OF THE RATCHET WHEEL (ITEM 3-620 OF CMM 27-44-13), ASSEMBLED ON THE OPPOSITE POSITION COMPARED TO THE SPEC MENTIONED ON THE CMM 27-44-13. LETTER LT-S9-11-10Feb 18, 2011 · N807FD · Airbus A310324SDR UALA2011021600800Actuator · failedTRIMMABLE HORIZ STABILIZER ACTUATOR FAILED JAMMING TEST. START REMOVING THS ACTUATOR. ACCOMPLISHED UP TO ITEM NR 5. COMPLETED INSTALLATION OF THS ACTUATOR. INSPECTED THE INSTALLATION OPERATION, SAFETY AND SECURITY OF THE THS ASSY.Feb 14, 2011 · N408UA · Airbus A320232SDR SIMA201103805Control Unit · malfunctionedON FLIGHT 4243 THE CREW DECLARED AN EMERGENCY ON APPROACH TO ORD FOR A MAIN PITCH TRIM FAIL. THE STANDBY WAS OPERABLE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT Feb 6, 2011 · N907AE · Emb EMB145LRSDR IXXA110011OWarning Light · false activationDURING CRUISE, NOTICE EICAS MESSAGE WITH CODE 27-48-03-00 STABILIZER TRIM DISPLAYED AND STABILIZER TRIM LIGHT ILLUMINATED WITH STABILIZER TRIM OPERATES AT HALF SPEED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX PERFORMED PROCEDURES IN FIM 27-4Jan 30, 2011 · N763CX · Boeing 767232SDR REXA201100080Control Unit · malfunctionedSTAB TRIM RUNAWAY ON DEPARTURE. AIR RETURN TO JFK. QRH COMPLETED. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. PERFORMED OPS CHECK ON HSTCU. OPS CHECK GOOD. OK FOR SERVICE.Jan 29, 2011 · N8886A · Cndair CL6002B19SDR C2XA11CL028Trim Switch · faultyIAD FLT 5977 - THE CREW REPORTED CAPTAINS PITCH TRIM SWITCH WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE TRIM SWITCH AND OPERATIONAL CHECKS WERE GOOD.Jan 28, 2011 · N12166 · Emb EMB145XRSDR C2XA11CL023Trim Switch · faultyORD FLT 5871 - THE CREW REPORTED A MAIN PITCH TRIM FAIL MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CAK AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER'S PITCH TRIM SWITCH. OPERATIONAL CHECKS WERE GOOD.Jan 22, 2011 · N14174 · Emb EMB145XRSDR 2011FA0000049Shaft · mismanufacturedLOOKING UNDER 10X YOU CAN SEE MACHINE MARKS ON THE THREADS OF THE SHAFT PREVENTING THE SHAFT FROM THREADING INTO THE TRIM BARREL. 4 IN STOCK ALL ARE FROM DATE 3/19/10 WITH A BATCH NR OF 6641D28J ALL WITH SAME DEFECT. USED A SHAFT WITH A DIFFERENT BATCH NR ANJan 18, 2011 · N914PA · Piper PA28181SDR C2XA11CL012Trim Switch · faultyCLE FLT 2051 THE CREW REPORTED A PITCH TRIM MAIN INOP MESSAGE ON THE EICAS DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS PITCH TRIM SWITCH. ALSO REPLACED THE HORIZONTAL STAB ACTUATOR. OPERATIONAL CHECKS WERJan 14, 2011 · N17159 · Emb EMB145XRSDR C2XA011TY005Control Unit · malfunctionedTHE "PITCH TRIM MAIN INOP" EICAS MESSAGE ON CLIMBOUT AFTER TAKEOFF. REMOVED AND REPLACED HSCU IAW EMB 145XR AMM 27-40-01, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.Jan 14, 2011 · N17159 · Emb EMB145XRSDR FDEA201101120128Computer · faultedPITCH FEEL NR 2 FAULTED TURNED IT OFF FOR APPROX (1) MINUTE RESET AND FAULT WENT AWAY. (2) MINUTES LATER IT FAULTED AGAIN IAW ECAM/QRH TURNED IT OFF AND COMPLIED W/QRH. FOUND FAULT LIGHT ON NR 2 COMPUTER FLC R & R IAW MM 27-23-26-4.Jan 12, 2011 · N741FD · Airbus A300B4622RSDR IPXA11664037Control Cable · icedCREW REPORTED STAB FAULT INBOUND. MX INSP FOUND LARGE AMOUNT OF ICE WITH PULLEY AND CABLE DAMAGE IN TAIL OF ACFT. FOUND ICE IN STAB AND THE CABLE DRUMS FOR THE STAB INDICATION WERE BROKEN. R & R RT POSITION MODULE CABLES AND LOWER TERMINAL ASSY/ TURNBUCKLEJan 6, 2011 · N315UP · Boeing 76734AFSDR IPXA1664037Control Cable · damagedCREW REPORTED STAB FAULT INBOUND. MX INSP FOUND LARGE AMOUNT OF ICE WITH PULLEY AND CABLE DAMAGE IN TAIL OF ACFT. FOUND ICE IN STAB AND THE CABLE DRUMS FOR THE STAB INDICATION WERE BROKEN. (OPEN)Jan 6, 2011 · N315UP · Boeing 76734AFSDR DXTA2011010504396Actuator · inoperativeIMMEDIATELY AFTER TAKEOFF, PRIMARY TRIM AND AUTOPILOT FAILED. SECONDARY TRIM OPERATED NORMAL. R & R PRIMARY STAB ACTUATOR WITH AN O/H UNIT. R & R ACTUATOR CONTROL UNIT WITH AN O/H UNIT. COMPLIED WITH ALL RIGGING PROCEDURES AND OPS CHECK. OPS CHECK GOOD. Jan 3, 2011 · N301QS · Cessna 680CESDR ASOA201100006Switch · malfunctionedSTAB TRIM CH1 AND CH2 DISCONNECTED ON T/O MACH TRIM WILL NOT ENGAGE AND A/P PITCH TRIM CAUTION MSG. FOLLOWED QRH AND RETURNED TO DEPARTURE GRND PROX FLAP OVRD SWITCH SELECTED. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) R & R PILOT SIDE HODec 30, 2010 · N919EV · Cndair CL6002B19SDR 2010FA0001266Control Cable · brokenLOWER FWD STABILATOR CONTROL CABLE, THREADED ROD END BROKE AT THE SAFETY WIRE WRAP WHERE IT THREADS INTO THE TURNBUCKLE THE ONLY THING HOLDING CABLE TOGETHER WAS A SINGLE STRAND OF .041 SAFETY WIRE.Dec 29, 2010 · N2155H · Piper PA32300SDR USAA20101227SB208Circuit Breaker · trippedDFW - ON CLIMBOUT FROM DFW, CREW REPORTED THE STAB OUT OF TRIM LIGHT CAME ON AND WITH AUTO PILOT ON, WOULD NOT TRIM. WITH AUTO PILOT OFF, STAB TRIM WILL WORK. FLIGHT RETURNED TO FIELD AT DFW AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MDec 27, 2010 · N155AW · Boeing 7373G7SDR C2XA10CL204Control Unit · intermittentABE FLT 6041 THE CREW REPORTED A MAIN PITCH TRIM INOP MESSAGE ON THE EICAS. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.Dec 21, 2010 · N16178 · Emb EMB145XRSDR DXTA2010120904356Stabilizer · failedHORIZ STAB FAILED IN FLIGHT IN ICING CONDITIONS. RESET CIRCUIT BREAKER HORIZONTAL STAB PROTECT, COMPLIED WITH GROUND TEST OF HORIZONTAL STAB HEAT SYS IAW MM 30-12-00-201. GROUND CHECKED GOOD.Dec 8, 2010 · N141QS · Raythn 400ARAYTHEONSDR C2XA10IA315Trim Switch · inoperativeIAH - FLIGHT 2347 THE CREW REPORTED THE PITCH TRIM TO BE INOPERATIVE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE F/O'S PITCH TRIM SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPRNov 27, 2010 · N11181 · Emb EMB145XRSDR GTIA1000111Actuator · leakingEXTERNAL LEAK FOUND ON THE THS ACTUATOR. R & R THE THS ACTUATOR.Nov 26, 2010 · N507NK · Airbus A319132SDR CA101026005Control Unit · failed(CAN) DURING A 100 HR IN-HANGAR INSPECTION, THE AIRCRAFT PITCH TRIM OPS CHECK FAILED, AS FOLLOWS: WITH BOTH CHANNELS ENGAGED, STAB TRIM EICAS INDICATION DOES NOT AGREE WITH ACTUAL STABILIZER POSITION. EICAS INDICATION OF 3.0 WITH STAB AT FULL DEFLECTION, EICOct 20, 2010 · Cndair CL6002B19SDR SIMA201028802Trim System · malfunctionedON FLIGHT 4508 THE CAPTAIN ACTIVATED THE PITCH TRIM ON SHORT FINAL AND RECEIVED MASTER A WARNING MICAS "PTRIM MAIN INOP". BOTH CAPTAIN’S AND FIRST OFFICER’S TRIM INOPERATIVE BUT BACKUP SYSTEM WORKED PROPERLY. THE CAPTAIN DECLARED AND EMERGENCY. THE AIRCRAFTOct 13, 2010 · N846AE · Emb EMB135KLSDR UALA2010100803756Rod End · wornVIBRATION-NOISE ENCOUNTERED IN FLIGHT. DATA VIBRATION REPORT CHECK LIST OBTAINED FROM FLIGHT CREW, TSM DECISION TABLE COMPLETED, ELEV & RUDDER HAD THE TWO HIGHEST SCORES. TROUBLESHOT VIBRATION WITH INFO GIVEN. FOUND RT AND LT OTBD ELEVATOR ACTUATOR ROD ENDS WOOct 8, 2010 · N470UA · Airbus A320232SDR AALA20100929BOS01Module · leakingBOS - CREW REPORTED AIRCRAFT LOSING RIGHT HYDRAULIC QUANTITY. EMERGENCY DECLARED RETURNED BOS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEAK ON STAB CONTROL MODULE. REPLACED MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION.Sep 28, 2010 · N173AN · Boeing 757223SDR DXTA2010092204250Actuator · inoperativeAFTER TAKEOFF, FLAPS WERE SELECTED TO ZERO POSITION RESULTING IN A STAB MISCOMP, A HYD PRESS, AND A MC LIGHT. UPON LANDING, STAB CONFIRMED NOT TO MOVE FULL UP OR DOWN. TROUBLESHOT TO INOPERATIVE STAB ACTUATOR. REPLACED ACTUATOR WITH MODIFIED UNIT IAW MM. OPSSep 21, 2010 · N647QS · Cessna 560XLSDR C2XA10RI114Control Unit · inoperativeFLIGHT 2968 - BOS - FLIGHT CREW REPORTED MAIN AND BACK UP TRIM INOPERATIVE AT FL350, AND NOSE PITCHED UP 3 DEG. EWR MX REMOVED AND REPLACED PITCH TRIM ACTUATOR AND HORIZONTAL STABILIZER CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPRSep 13, 2010 · N14148 · Emb EMB145XRSDR USAA2010091692003Stabilizer · jammedFLT 399 LAS-PHX - RTF - AIRCRAFT EXPERIENCED FLIGHT CONTROL STABILIZER JAM UPON TAKEOFF ROTATION. CREW DECLARED AN EMERGENCY AND RETURNED TO LAS. MAINTENANCE REMOVED AND REPLACED THE TRIMMABLE HORIZONTAL STABILIZER.Sep 11, 2010 · N655AW · Airbus A320232SDR SIMA201025002Trim Switch · failedON FLIGHT 2841 DISPATCH REPORTED THAT IMMEDIATELY AFTER TAKEOFF THE FIRST OFFICER STARTED TRIMMING AND GOT NO RESPONSE. SEVERAL SECONDS LATER, GOT A PITCH TRIM MAIN INOPERABLE EICAS MESSAGE. THE CREW ELECTED TO RETURN TO DFW AND LANDED WITHOUT INCIDENT. THESep 5, 2010 · N636AE · Emb EMB145LRSDR 2010FA0001003Control Cable · brokenCABLE DIAMETER 0.0700, OEM CABLE DIAMETER: 0.0665. LARGER DIAMETER CABLE CAUSES IMPROPER RESTING OF CABLE INTO TRIM BARREL GROOVE, CAUSING OVER EXTENDING OF OVERALL DIAMETER AS WELL AS "WOBBLE" ON THE RAISED SECTION. ONCE INSTALLED, AND DUE TO CLOSE CLEARANCSep 2, 2010 · N971AC · Piper PA28161SDR NSVA2010149Trim System · malfunctionedRETURNED TO GATE DUE TO THE PITCH TRIM LIGHT ILLUMINATED. PERFORMED OPS CHECK OF THE PITCH TRIM SYSTEM. OPS CHECKED GOOD.Sep 1, 2010 · Bombdr DHC8402SDR DBCA2010083000028Actuator · failedON DEPARTURE, HORIZONTAL STABILIZER WOULD NOT TRIM. DIVERTED, LANDING WAS UNEVENTFUL. INSPECTED BY MFG TECHNICIANS DETERMINED FAULT WAS CAUSED BY INTERNAL FAILURE OF HORIZONTAL STABILIZER TRIM ACTUATOR.Aug 30, 2010 · N919CH · Israel ASTRASPXSDR DXTA2010082304202Control Module · malfunctionedSTAB TRIM RESPONDS INTERMITTENTLY AND WITH LIMITED RESPONSE TO BOTH PILOT AND CO-PILOT PRIMARY TRIM SWITCH INPUTS. SWITCHED TO SECONDARY TRIM WITH SAME RESULTS. NEVER RECEIVED AN ASSOCIATED AMBER CAS MESSAGE. R & R HORIZ STAB TRIM ELECTRONIC CONTROL MODULE. Aug 20, 2010 · N984QS · Cessna 750SDR AALA20100725DFW08Trim Motor · inoperativeDFW - PRIMARY LONGITUDINAL TRIM INOPERATIVE AFTER TAKEOFF. ALTERNATE TRIM WORKED AND PRIMARY TRIM DID NOT WORK USING NOSE DOWN. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PRIMARY STAB TRIM MOTOR AND CAPTAINS PRIJul 25, 2010 · N457AA · Doug DC982SDR UALA2010072602649Lockout · malfunctionedL FMC FAILURE & STAB TRIM EICAS, RTFL. STAB TRIM LIGHT ON O/H AS WELL AS EICAS MESSAGE. REPLACED STAB TRIM - AILERON LOCKOUT MODULE. ACP MCDP TEST 65. TEST OK. ACCOMPLISHED STAB TRIM CONTROL OPS TEST IAW MM. ALL TESTS PASSED.Jul 24, 2010 · N644UA · Boeing 767322SDR DXTA2010071504155Control Cable · brokenON DESCENT FOR APPROACH, THE PITCH TRIM LIGHT ON THE PFD CAME ON. AFTER DISCONNECTING AUTOPILOT, THE ELECTRIC TRIM DID NOT MOVE THE TRIM WHEEL. PITCH TRIM CIRCUIT BREAKER REMAINED IN. TRIM WHEEL AND INDICATOR MOVED MANUALLY WITH LITTLE RESISTANCE. ON POST FLIGJul 14, 2010 · N611QS · Cessna 560XLSDR UALA2010071202482Trim System · malfunctionedCREW REPORT: STAB TRIM EICAS ON TAXI OUT. CYCLED STAB TRIM CTRL C/B'S NO HELP, CYCLED FLT CTRL ELEC LT & RT 1&2 C/B'S FAULT CLEARS & STAYS OUT WHEN MOVING CAPT'S ELECT STAB TRIM SWITCHES. LIGHT & EICAS MSG RETURN WHEN F/O'S STAB TRIM SWITCHES ARE USED. STAJul 12, 2010 · N657UA · Boeing 767322SDR SIMA201019403Control Unit · inoperativeON FLIGHT 2772 DURING THE CLIMB THE CREW REPORTED, RECEIVED A PITCH TRIM INOP MESSAGE ON EICAS. UNABLE TO RESET FOLLOWING THE AIRCRAFT OPERATING MANUAL PROCEDURES. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO FTM LANDING WITHOUT INCIDENT. THE AIRCRAFT WASJul 11, 2010 · N640AE · Emb EMB145LRSDR DXTA2010071204148Trim System · looseON TAKEOFF WITH PITCH TRIM IN TAKEOFF RANGE REQUIRED EXCESSIVE AFT YOKE FORCE TO GET NOSE OFF GROUND. AFTER AIRBORNE FULL NOSE UP TRIM APPLIED & REQUIRES EXCESSIVE AFT YOKE FORCE AT 200 KTS. UPON INITIAL INSP, FOUND ELEVATOR TRIM TAB IN FULL NOSE UP POSITIONJul 9, 2010 · N371QS · Cessna 560CESSNASDR UALA2010071202458Terminal · brokenRT STAB POSITION TRANSMITTER CABLE TERMINAL ASSY IS BROKEN. REPLACED RT STAB POS. TRANSMITTER CABLE TERMINAL ASSY AND ACPD CABLE ADJUSTMENT. OP CHECK GOOD.Jul 9, 2010 · N660UA · Boeing 767322SDR FDKA2010070700172Pitch Control · malfunctionedPITCH TRIM MAIN INOP. RESET MAIN PITCH TRIM, OPS GOOD.Jul 7, 2010 · N829MJ · Emb EMB145LRSDR REXA201000096Switch · jammedCREW RECEIVED A STAB TRIM/MACH TRIM CAUTION MESSAGE ON CLIMBOUT AT 5000 FT AND WERE UNABLE TO RESET. RETURNED TO IND. UPON ARRIVAL MAINTENANCE VERIFIED DISCREPANCY AND FOUND F/O'S DISCONNECT SWITCH JAMMED WHICH WAS VERIFIED THROUGH MDC CODE 270 BIT 14. CLEAJul 3, 2010 · N8783E · Cndair CL6002B19SDR C2XA10RI087Trim Switch · brokenFLIGHT 2476 - EWR - FLIGHT CREW REPORTED BACK UP PITCH TRIM SWITCH INOPERATIVE. CREW PERFORMED AIR RETURN UNEVENTFULLY. EWR MX REMOVED AND REPLACED SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.Jun 24, 2010 · N19554 · Emb EMB145LRSDR A6WA201040451Switch · malfunctionedSTAB TRIM (BOTH CHANNELS) AND MACH TRIM CAUTION MSG, C/W QRH AND WOULD NOT RESET. R & R F/O`S STAB TRIM DISCONNECT SWITCH IAW AMM 27-41-30. ALL OPS CKS GOOD AT THIS TIME.Jun 18, 2010 · N430AW · Cndair CL6002B19SDR SIMA201016803Control Unit · malfunctionedON FLIGHT 2958 AT APPROXIMATELY 1000 FEET DURING THE FINAL APPROACH WITHOUT THE AUTO PILOT ON THE CREW PUT THE LANDING GEAR DOWN AND THE PITCH TRIM STARTED TO RUN THE NOSE DOWN BY ITSELF. THE CREW PUSHED AND HELD THE INHIBIT BUTTON AND THE TRIM STOPPED AT 2Jun 15, 2010 · N923AE · Emb EMB145LRSDR SWIA201024413Mcu · malfunctionedSTAB TRIM RUNAWAY AFTER TAKEOFF. (FLT 6732) REPLACED MCU AND MOTOR NR 1. P/N 7074-5, S/N OFF 430, P/N 8489-713-2, S/N OFF 1072.Jun 9, 2010 · N705SK · Cndair CL6002C10SDR VNAA2010061000003Control Unit · malfunctionedCREW REPORTED STAB TRIM AND MACH TRIM CAS MESSAGES DISPLAYED IN CRUISE CLIMB AFTER DEPARTURE FROM CLT. AIRCRAFT LANDED IN CAK WITHOUT INCIDENT. MAINTENANCE INSPECTED THE MAINTENANCE DIAGNOSTIC COMPUTER (MDC), RESET THE HORIZONTAL STABILIZER TRIM CONTROL UNITJun 6, 2010 · N241PS · Cndair CL6002B19
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