JASC 2711

Service difficulty reports · 415

Reports filed under 2711 · Aileron Tab 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 = '2711'
  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 MASA2010021200134Trim Panel · faultyACFT ROLLS LEFT WITH FULL RT TRIM. REPLACED AILERON RUDDER TRIM PANEL.Feb 12, 2010 · N505MJ · Cndair CL6002C10SDR 2010F00024Tab · mismanufacturedRECEIVED NEW AILERON TRIM TAB FROM VENDOR. TAB WAS A NEW PART FROM THE MFG. INCOMING INSP NOTED THE RIVETS THAT SHOULD HAVE BEEN INSTALLED TO SECURE THE ACTUATOR HORN TO THE TAB WERE MISSING. THERE IS ALSO A ROW OF RIVETS, ALONG THE HINGE LINE, THAT WERE MISSFeb 2, 2010 · N221CJ · Beech 1900DSDR MASA2010011300040Power Supply · malfunctionedAILERON TRIM FULL RT WING DOWN-MRR AILERON TRIM FULL RT WING DOWN. PROBLEM OCCURS WITH AUTO P, PLACED ON MEL. POSSIBLE FCC 822-1308-320 ON REQ TO CLT ALSO POSSIBLE AILERON TRIM POWER SUPPLY PS644. ADS PROGRAM IS OPEN FOR THIS. RESET SYS OPS NORMAL. DEFECTJan 13, 2010 · N508MJ · Cndair CL6002C10SDR 2009FA0001046Actuator · looseDURING MX ON 510-0032 WHILE CARYING OUT SB510-27-01 A LOUD RATTLE WAS NOTICED FROM INSIDE THE LT AILERON PRIOR TO REFIT. THE NOISE SOUNDED LIKE MUTIPLE LOOSE ITEMS TOWARDS THE INBD END OF THE AILERON. ON REMOVAL OF THE AILERON TRIM ACTUATOR ACCESS PANEL (532Nov 26, 2009 · N814WS · Cessna 510SDR UALA2009102303308Actuator · faultyRIGHT AILERON TRIM PROBLEM, RTFL. REPLACED LATERAL TRIM ACTUATOR. OP CHECK OKAY. MOTOR SPEED NORMAL. CHK'D FOR ELEVATOR PCU HYD BYPASSING, NO BYPASSING NOTED. PERFORMED ELEVATOR FEEL CHK, WITHIN LIMITS. PERFORMED ELEVATOR SERVO TEST, CHK'D FOR ELEVATOR PCU FOROct 23, 2009 · N508UA · Boeing 757222SDR DXTA2009101603812Actuator · failedAILERON TRIM KNOB FROZEN IN NEUTRAL POSITION ,WILL NOT TURN. REMOVED AND REPLACED AILERON TRIM TAB ACTUATOR IAW MM 27-10-71, OPS CHECKS AND FUNCTIONAL CHECKS GOOD.Oct 15, 2009 · N817QS · Raythn HAWKER800XPSDR AALA20090928TUL15Trim Tab · splitRIGHT TAB TRIM TRAILING EDGE SPLIT OPEN. REPAIRED TRAILING EDGE UNDER SRM 51-70-01A.Sep 28, 2009 · N483A · Doug DC982SDR QXEA2009082700635Trim Panel · malfunctionedBOI - ON TAKEOFF AILERON YOKE INPUT REQUIRED 20 TO 30 DEGREE RIGHT AILERON FOR WINGS LEVEL. FUEL WAS BALANCED AND TRIMS WERE NORMAL. NEUTRAL AILERON YOKE WOULD PUT A/C IN 20 TO 30 DEGREE LEFT BANK AS SPEED INCREASED IN CLIMB AND CRUISE AILERON YOKE ANGLE TO Aug 23, 2009 · N403QX · Bombdr DHC8402SDR CA090908004Rod End · brokenAILERON TRIM INOP AND AP MISTRIM MESSAGE. AP DISCONNECTED AND MISTRIM CONFIRMED. FOUND TRIM TAB FULL UP (LWD) DEFLECTED AND MOVEABLE WITH FINGER. TRIMMING WITH ACTUATOR ONLY IN UP DEFLECTION POSSIBLE. FOUND AILERON TRIM ACTUATOR ROD END BOKEN OFF. TRIM TAB Aug 20, 2009 · Dhav DHC8301SDR UALA2009070101891Module · faultyEICAS MSG STAB TRIM DISPLAYED & STAB TRIM LIGHT ILLUMINATED. STABILIZER TRIM RATE NORMAL. FOUND LT STAB TRIM AIL LOCKOUT MOD FAULT. REPLACED LT SAM. COMPLETED MCDP GRND TEST 65 STAB TRIM AND AIL LOCKOUT TEST, ALL TEST PASS. NO FAULT INDICATIONS.Jul 1, 2009 · N642UA · Boeing 767322SDR UALA2009070101885Actuator · failedAILERON TRIM INOPERATIVE. REPLACED AILERON RUDDER TRIM PANEL RUDDER TRIM SYSTEM, OP CHECK OK, AILERON SYSTEM NO HELP. NEED AILERON TRIM ACTUATOR. AILERON TRIM ACTUATOR, OPS CHECKS GOOD.Jun 29, 2009 · N543UA · Boeing 757222SDR SWIA200922181Rod · corrodedLEFT AILERON TRIM TAB RODS CORRODED. (C CHECK) REPLACED ROD ENDS PER AMM.Jun 17, 2009 · N292UX · Emb EMB120ERSDR 2009FA0000525Actuator · intermittentFLIGHT CREW REPORTED LT ROLL TRIM PANEL INTERMITTENTLY NOT OPERATING. CONFIRMED PILOT SQUAWK, FOUND ACTUATOR INTERMITTENTLY NOT RUNNING WITH EITHER DUAL OR SINGLE SOURCE SELECTED. VERIFIED POWER INPUTS TO ACTUATOR CONNECTOR NORMAL. REPLACED ACTUATOR WITH OVJun 17, 2009 · N400MV · Raythn 400ARAYTHEONSDR HALA2009051900181Trim System · out of toleranceOPEN - ETOPS SIGNIFICANT SYSTEM - ACFT FLYS OUT OF TRIM, NEEDS RT AILERON 2 DEGREES RT RUDDER, 2 DEGREES FOR STRAIGHT AND LEVEL, SAME IN A/P MODE. PERFORMED AILERON TRIM CONTROL OPERATIONAL TEST PER AMM 27-11-00-715-002 STEPS A-G, PERFORMED RUDDER TRIM CONTROMay 19, 2009 · N585HA · Boeing 7673G5SDR UALA2009043001253Actuator · faultyAILERON LOCKOUT EICAS MESSAGE. REPLACED RIGHT AILERON LOCKOUT ACTUATOR AND FSEU.Apr 28, 2009 · N659UA · Boeing 767322SDR CA090420001Spring · looseUPON CARRYING OUT C-CHECK, INSPECTION 543E, THE LT AILERON SPRING TAB INBD HINGE (ON REAR SPAR OF AILERON) WAS FOUND WORN TO THE POINT THAT IT WAS NO LONGER SUPPORTING THE TAB. ONLY THE OUTBOARD AND CENTER HINGES WERE SUPPORTING THIS SPRING TAB- EXTREMELY LOOApr 10, 2009 · Dhav DHC8102SDR CA090415005Actuator · failed(CAN) WHILE ON THE GROUND THE AILERON TRIM WAS RUN TO THE STOP. IT THEN FAILED AND INSP REVEALED THAT THE ELECTRICAL WIRE HAD SEPARATED AT THE TRIM ACTUATOR WHERE THE WIRE IS FLEXED BACK AND FOURTH AS THE ACTUATOR MOVES. THE ACTUATOR WAS REPLACED.Mar 4, 2009 · Pilats PC1245SDR HALA2009022400065Control Unit · malfunctionedIN ORDER AND RIGHT RUDDER TRIM. ON CONFIG PAGE NO FLT CONTROL ABNORMALITIES. REPLACED AILERON/RUDDER TRIM CONTROL UNIT PER AMM 27-11-01-400-801. OPS CK FUNCTIONAL CK PER AMM 27-11-01-720-801, CK OK FOR SVC.Feb 24, 2009 · N478HA · Boeing 717200SDR TRBA2009018Actuator · failedEXCESSIVE VIBRATION NOTED IN CONTROL COLUMN AFTER TAKEOFF. INCREASED WITH INCREASED SPEED. NOTED IN CABIN, MORE IN FORWARD PORTION. REMOVED AND REPLACED LT AILERON TRIM ACTUATOR IAW ATR 72 JIC NR 27-12-71. OPERATIONAL CHECK GOOD.Feb 3, 2009 · N536AT · Aerosp ATR72212ASDR C2XA09CL015Switch · stickingEWR FLIGHT NR 2879 THE CREW REPORTED A ROLL TRIM SWITCH STUCK IN FLIGHT. THE ACFT DIVERTED AND LANDED IN CLE. MX INSPECTED AND CLEANED AND LUBRICATED THE ROLL TRIM SWITCHES. OPS CHECKS WERE GOOD. A COMPANY ECTM WORKSHEET WAS ISSUED AND THE TRIM SWITCH WAS Feb 3, 2009 · N11192 · Emb EMB145XRSDR QXEA2009010600003Trim System · frozenSEA - ON LEVEL OFF AT CRUISE ALT, AS SPEED INCREASED TO 280 3/4 OF AILERON TRIM REQUIRED TO KEEP AIRCRAFT LEVEL. REDUCING AIRSPEED TO 170 OR SO THE AILERON TRIM ALMOST CENTERED. PERFORMED GVI OF LT AND RT AILERONS, FOUND ICE 1/8 INCH THICK ON LT WING FROM OTJan 2, 2009 · N400QX · Bombdr DHC8402SDR QXEA2008121901253Trim System · out of adjustDURING CLIMB AND CRUISE MORE THAN HALF AILERON TRIM IS REQUIRED TO MAINTAIN WINGS LEVEL. DURING SLOW SPEEDS AND FLAPS AT 35 TRIM IS NORMAL. AIRCRAFT IS CONTROLLABLE DURING ALL PHASES OF FLIGHT. LT WING IS HEAVY WING. FERRY TO PDX FOR REPAIRS. INSPECTED AILDec 18, 2008 · N402QX · Bombdr DHC8402SDR ASOA200801368Trim System · malfunctionedA/C YAWED EXCESSIVELY TO THE RIGHT DURING FLIGHT, THE A/C WOULD NOT STAY TRIMMED. AFTER ENGAGING THE AUTOPILOT, THE AUTOPILOT HAD DIFFICULTY MAINTAINING THE FLIGHT CONTROL INPUTS. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. (AILERON TRIM SYSTEMOct 19, 2008 · N855AS · Cndair CL6002B19SDR SWIA200820002Trim System · stuckAILERON TRIM WOULD NOT MOVE RIGHT WING DOWN. FLT 6111. REPLACED AILERON/RUDDER TRIM PANEL IAW 27-12-4. OPS CHECKS GOOD IAW 27-11-00 AND 27-22-00. P/N: CC670-51114-3. Aug 29, 2008 · N702SK · Cndair CL6002C10SDR DXTA200803227Trim System · malfunctionedCLIMBING THROUGH FL230 AT 270 KNOTS INDICATED, "RETRIM L WING DOWN" AT THE TIME THE AP WAS DISENGAGED, AND THE ACFT REQUIRED 50 PERCENT LT AILERON TRIM. (S)Aug 15, 2008 · N950QS · Cessna 750SDR SWIA200819859Control Panel · malfunctionedAILERON TRIM STICKS AND WILL NOT TRIM TO THE RIGHT. (FLIGHT NR 6052) REPLACED AILERON/RUDDER TRIM CONTROL PANEL IAW AMM 27-12-10. Jul 9, 2008 · N934SW · Cndair CL6002B19SDR 2008UALA03091Module · malfunctionedRUDDER RATIO & AILERON LOCKOUT EICAS MSG. FLIGHT DIVERTED. REPLACED LT STAB TRIM AILERON LOCKOUT MODULE (SAM). SHOP FINDINGS: NFFMay 29, 2008 · N648UA · Boeing 767322SDR COMA0860230Actuator · faultyFLIGHT 9657 - HESITATION FELT IN CONTROLS WHEN TURNING RIGHT, AUTO-PILOT OFF, ALL HYDRAULICS ON, PILOT AND CO-PILOT SIDES. DECLARED EMERGENCY, RETURNED TO CVG, LANDED WITHOUT INCIDENT. REPLACED AILERON TRIM ACTUATOR. NO FURTHER DEFECTS.Apr 20, 2008 · N784CA · Cndair CL6002B19SDR 2008UALA02671Control Module · malfunctionedRUDDER TRIM INOP INTERMITTENT. PER CREW INBOUND CREW, AC REQUIRED FREQUENT RETRIMMING AND AT TIMES, RUDDER TRIM WOULD BE INOP AND OTHERS IT WOULD TRIM NORMALLY, ALL AT CRUISE. OCCURRED ON THE GROUND AS WELL AFTER ARRIVAL. SUSPECT INTERMITTENT TRIM COMMAND FRApr 18, 2008 · N545UA · Boeing 757222SDR 2008F00013Trim Tab · bindingAILERONS BINDING ON TAKEOFF AFTER GEAR RETRACTION (BEFORE TAKEOFF CONTROL CHECK) NORMAL. FOUND THAT THE AILERON SPRING TAB MECHANISM WAS BINDING PREVENTING MOVEMENT OF THE TAB SYSTEM WHICH IN TURN INCREASED THE FORCES REQUIRED TO MOVE THE AILERONS.Apr 7, 2008 · N7780B · Doug DC6ASDR 2008FA0000348Actuator · malfunctionedIN CONJUNCTION WITH REPAIRS FOR UNCOMMANDED ROLL, TRIM ACTUATION AT KMDW REPLACED RT ROLL TRIM ACTUATOR (HBC PN 390-3810090010) WITH RAPID SUPPLIED REPAIRED UNIT. ATTEMPTED TO PERFORM ROLL TRIM FUNCTIONAL CHECKS IAW THE 390 MM 27-10-00-501 AFTER ACTUATOR REPLAMar 18, 2008 · N837JM · Raythn 390SDR WGEA200800040Trim System · malfunctionedWHILE HAND FLYING, AILERON TRIM DOES NOT SEEM TO WORK TO THE RIGHT EVEN WITH FULL DEFLECTION. OK TO THE LEFT. TRIM INDICATION MOVES OK. SUPPLEMENTAL INFORMATION, PERFORMED AILERON TRIM FUNCTIONAL TEST IAW EA500 AMM 27-00-00 SUB TASK 27-00-00-071. ALL CHECKMar 4, 2008 · N163DJ · Eclips ECLIPSEEA500SDR WGEA200800044Spring · damagedREPLACED AILERON TRIM SPRING WITH NEW TRIM SPRING IAW AMM 27-11-20. PERFORMED AILERON TRIM SYSTEM ADJUSTMENT/TES IAW AMM 27-00-01. SYSTEM TEST AND CHECKS GOOD, NO DEFECTS NOTED. ITEM 1. FLIGHT WAS UNSATISFACTORY. AT 220KTS 82 PERCENT OF TRIM WAS REQUIREDMar 2, 2008 · N142DJ · Eclips ECLIPSEEA500SDR 2008UALA01168Control Rod · faultyAILERON TAB CONTROL RODS ARE FAULTY. REPLACED CONTROL RODSFeb 29, 2008 · N382UA · Boeing 737322SDR DXTA20082899Control Module · malfunctionedAFTER 15 MINS OF CRUISE FLT AT FL400 (MACH TRIM OFF) AND (PRI STAB TRIM FAIL) MESSAGE KEPT DISPLAYING AND RESETTING. REMOVED DEFECTIVE ECM P/N 4214-0021-11N S/N 3125, INSTALLED UNIT MODIFIED BY MFG SERVICE, IAW MM CHAP 72-40-00. OPERATIONAL CHECKS GOOD.Feb 25, 2008 · N975QS · Cessna 750SDR HNAA0800024Lever · wornIN FLIGHT AIRCRAFT IS DIFFICULT TO TURN LEFT AND SPOILER NR 1 PUSH OFF LIGHT ILLUMINATES WHEN MAKING RIGHT TURNS. FOUND WIRES ON RIGHT HAND SPOILER CLUTCH UPPER MICRO SWITCH, REPAIRED WIRES AND RIGGED MICRO SWITCH. INSPECTED LEFT AND RIGHT AILERONS AND SPRINJan 2, 2008 · N906HA · Dhav DHC8102SDR DXTA200702611Indication Sys · malfunctionedEXTREME FORWARD FORCE, ON YOKE, USED TO KEEP AIRCRAFT CONTROL ON TAKEOFF. FOUND TRIM POINTER MIS-INDEXED IN TRIM WHEEL. RE-INDEXED POINTER TO PROPER POSITION. ELEVATOR TRIM SYSTEM OPS CHECKS GOOD AT THIS TIME. WORK DONE IAW CE-560XL M/M 27-32-01Nov 13, 2007 · N631QS · Cessna 560XLSDR HYIA12111Rod · corrodedLEFT AILERON TRIM TAB CONTROL ROD WAS FOUND TO BE CORRODED. CORROSION WAS FOUND TO BE BEYOND MANUFACTURERS LIMITS. ROD WAS REMOVED AND REPLACED.Oct 6, 2007 · N14834 · Aerosp ATR42320SDR CA071010008Actuator · seized(CAN) DURING A 50 HOUR ROUTINE INSPECTION MAINTENANCE PERSONEL DISCOVERED THAT THE AILERON TRIM WAS NOT MOVING. UPON INSPECTION OF THE SYSTEM IT WAS DISCOVERED THAT THE AILERON TRIM ACTUATOR WAS SEIZED. THE ACTUATOR WAS REMOVED AND DISSASSEMBLED. THERE WAS INTOct 3, 2007 · Beech 1900DSDR FDKA200710519Trim System · stiffFDM 6041 JFK (1921 PHX LCL) - AILERON MIS TRIM AND AILERON GOT STIFFER WITH SLOWER AIRSPEED DURING APPROACH. MX COULD NOT DUPLICATEOct 3, 2007 · N853MJ · Emb EMB145LRSDR QXEA200701404Trim Tab · out of adjustSEA - DURING INITIAL CLIMB FROM 34R WITH A LEFT QUARTERING HEADWIND AILERON CONTROL WAS STIFF WHEN APPLYING LEFT ROLL. WITH 2 SHORT TAPS OF LWS AILERON TRIM DIFFICULTIES SEEMED TO DISAPPEAR AT 2K FT A RIGHT TURN WAS INITIATED AND THIS TIME THERE WAS DIFFICULTYSep 10, 2007 · N358PH · Dhav DHC8202SDR 2007UALA03602Aileron · bindingAILERONS SLIGHT BINDING WHEN COMING OUT OF A RIGHT TURN.Sep 6, 2007 · N308UA · Boeing 737322SDR QXEA200701385Tab · out of adjustSEA - DURING CLIMB AND CONTINUING DURING CRUISE, THE AMOUNT OF FORCE NEEDED TO TURN THE AIRCRAFT TO THE LEFT WAS MORE THAN USUAL. THE AMOUNT OF FORCE REQUIRED INCREASED WITH INCREASING AIRSPEED TO THE POINT OF BEING INCREDIBLY DIFFICULT AT HIGH SPEEDS. ON THESep 5, 2007 · N358PH · Dhav DHC8202SDR CA070827009Actuator · stiff(CAN) PILOT COMPLAINED ABOUT AILERON STIFF TO MOVE AND WOULD OCCASIONALLY STICK IN THE FULL RT POSITION. UPON MAINTENANCE TROUBLESHOOTING IT WAS NOTICED THAT THE LT AILERON TRIM ACTUATOR THAT WAS RECENTLY REPLACED, APPROXIMATLY 80 HOURS PREVIOUS, WAS AGAIN STAug 8, 2007 · Frchld 22C7ASDR SWAA073333Rod End · corrodedDURING SCHEDULED SERVICE CHECK, FOUND AILERON ROD END CORRODED IN RT MLG W/W. REMOVED AND REPLACED ROD END PER MM.Jul 5, 2007 · N650SW · Boeing 7373H4SDR HALA0700234Control System · malfunctionedETOPS SIGNIFICANT SYSTEM, AILERON TRIM UNITS TO THE LEFT DURING TAKEOFF,CLIMB AND APPROACH. OK DURING CRUSE SEGMENT. PERFORMED OPERATIONAL TEST AILERON AND AILERON TRIM, TRIM CONTROL SYSTEM PER AMM 27-11-00-715-002. OPERATION NORMAL.May 31, 2007 · N587HA · Boeing 76733ASDR QXEA200700515Control Panel · malfunctionedSEA- UNABLE TO TRIM THE AILERONS TO THE LEFT. MAINTENANCE REPLACED THE AILERON/RUDDER TRIM CONTROL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.Mar 31, 2007 · N600QX · Cndair CL6002C10SDR DJFA2007038Trim Switch · stickingTRIP NR 1160942 CREW REPORTED ROLL TRIM RUNAWAY. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. MAINTENANCE FOUND THE ROLL TRIM SWITCH STUCK. THE SWITCH WAS REPLACED.Mar 30, 2007 · N455CW · Beech 400ASDR COMA0760292Control Panel · faultyFLIGHT 5689 - CONFIG AILERON MASTER WARNING MESSAGE RECEIVED. REPLACED AILERON TRIM CONTROL PANEL. NO FURTHER DEFECTS.Mar 26, 2007 · N987CA · Cndair CL6002B19SDR FDKA200702090Actuator · malfunctionedFDM 6201 JFK-PWM (1128 PHX LCL). AILERON TRIM WILL GO FULL LEFT AND WILL NOT RETURN TO NEUTRAL. MX REMOVED AND REPLACED ACTUATOR.Feb 27, 2007 · N804LR · Dhav DHC8102
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