WING TRIM MECHANISM
Contents
1. Voltage supply 9 14V Nominal force 300 kg Maximum force 1000 kg Consumption current at nominal force 10A Travel 60 or 92 mm Emergency travel 70 or100 mm Complies with IP54 Moving speed 15 mm sec Operating mode Short term repeated Temperature range 15 455 C Time to failure relay 500000 turn ons terminal switch 100000 turn ons electric motor 1000 hours Dimensions Diam 48 x 371 mm Weight 1 425 kg NOTE In the power supply system of the trim device it is necessary to have a 15A safety fuse The trim device consists of travel mechanism rear bracket front bracket electric wiring with connectors control switch and safety fuse 2 Installing the Trim Device on the Aircraft To install the trim device the wing has to be mounted and raised on the trike For correct trim device operation the backup loop has to be connected so that it passes once over the keel and back to the pylon see photo Make sure the back up loop will not hang to the keel tube details and will not restrict the trim mechanism movement Connect the trim device to the rear bracket on the keel tube using the pin and a safety ring To connect the front bracket of the trim device move the control bar all the way backwards to set it against the front seat positioning the keel tube in right position for sliding the front bracket of the trim into the hangblock of the wing Watch out for your2. fingers Fix the front bracket in place with the pin and a safety ring NOTE It may be helpful to stand behind the wing on a small ladder and use a soft rope loop around the top of the mast and to use this with one hand for leverage while with the palm of the other hand push the keel tube of the wing to slide the wing just enough to line up the front bracket to go in easily into the hangblock It may also be helpful to use a soft rubber or plastic mallet to tap the front trim bracket pin lightly in Connect the pin to the socket connector of the trim device wiring Check the trim device operation in most forward and aft position Set the trim device in take off position which is 20 30mm from the most aft position Fix the electrical wire of the trim device with a plastic hose clamp 3 Removing the Trim Device from the Aircraft WARNING THE TRIM DEVICE CAN BE MOUNTED OR DISMOUNTED FROM THE AIRCRAFT ONLY WHEN THE WING IS ATTACHED TO THE TRIKE IN ITS FLYING POSITION RAISED ON THE TRIKE LOWERING AND REMOVING THE WING FROM THE TRIKE BEFORE THE TRIM DEVICE HAS BEEN DISMOUNTED WILL LEAD TO THE TRIM DEVICE AND BRACKETS DAMAGE Apply park brake if available Set the trim device to the aft position and then slightly forward 10 15mm from the most aft position Disconnect the pin from the socket connector of the trim device wiring Disconnect the rear bracket of the trim device Disconnect the front bracket of the
3. 000 10 Bomt 2 6 72 OCT131120 80 12 Nut M6 self locking DIN 985 5 Pin 6x77 74 13 Safety Ring SBR1519 4 MP 010 000 Tlodnuce u Gama 6 Pin 8x32 29 16 Washer M8 DIN 125 8 PRF 15 357 000 14 Splint 2 0 x 25 SBS2025 B3am uH6 Ne 2 PRF 15Tr 150 000 AD 18 MP 003 000 lodnucb u Gama N doxym 12 Nut M6 self locking DIN 985 15 Washer M6 DIN 125 11 Boxr 6 69 OCT131160 80 19 MP 012 000 3 MP 004 000 6 Pin 8x32 29 13 Safety Ring SBR1519 MP 001 000 AD Keel Tube with Linear Actuato Konupoban al Popmam A3 Kou Ha 3qesMe Lat Tlep6 npumen 1 PRF 15 190 000 AD 7 PRF 15 317 000 10 Bosr 2 6 72 OCT131120 80 2 PRF 15Tr 150 000 AD 12 Nut M6 self locking DIN 985 12 Nut M6 self locking DIN 985 15 Washer M6 DIN 125 11 Boxr 6 69 OCT131160 80 19 MP 012 000 5 Pin 6x93 90 13 Safety Ring SBR1519 3 MP 004 000 4 MP 011 000 Tlodnuce u Gama 6 Pin 8x32 29 15 Washer M8 DIN 125 8 PRF 15 357 000 14 Splint 2 0 x 25 SBS2025 18 MP 003 000 6 Pin 8x32 29 13 Safety Ring SBR1519 B3am uH6 Ne MP 002 000 AD N doy 0206 09Keel Tube with Linear Actuator Fr2 1 2 Konupo an Popmam A3 lo nucs u Gama Kou Ha 3qesMe Lat Tlep6 npumen 1 PRF 15 190 072 AD 7 PRF 15 317 000 10 Bonr 2 6 72 OCT131120 80 12 Nut M6 self locking
4. CTIVATE THE TRIM DEVICE ACTIVATION SWITCH AND THE CONTROL BAR POSITION DOES NOT MOVE STOP ITS USE AND TRY AND MOVE THE CONTROL BAR BACK AND FORTH SLIGHTLY TO MAKE THE HANGBLOCK SQUARELLY ALIGNED UNCOCKED ONCE ALIGNED YOU CAN ACTIVATE THE TRIM DEVICE AGAIN THERE SHOULD BE NO PROLONGED OPERATION OF THE ACTIVATION SWITCH IF THE CONTROL BAR POSITION DOES NOT SEEM TO CHANGE IT IS RECOMMENDED TO CLEAN THE KEEL TUBE WITH A SOFT RAG TIME AFTER TIME AND SPRAY IT WITH A SILICONE SPRAY IN PLACE WHERE THE HANGBLOCK MOVES NOTE In case of the trim device failure in most forward position it is recommended to use flat with no obstacles landing field which is long enough for landing due to increased landing approach speed 5 Maintenance and Storage The trim device is maintenance free However few simple rules will help you to maintain the trim device in good condition The trim device has to be positioned at 10 15mm from the most rear position for storage Wipe off the trim device carefully with the soft clean rags from any mildew or dirt before storage Store the trim device in its bag in a dry area The recommended storage temperature is 5 25 deg C If your trim device failed to operate check the safety fuse Do not attempt to dismount or repair the trim device and contact your dealer or Aeros directly for replacement if necessary Have fun Fly safe Aeros Ltd Koa Ha Y3 Wee WT Tlep6 npumen 1 PRF 15 180 000 AD 7 PRF 15 317
5. DIN 985 5 Pin 6x86 83 13 Safety Ring SBR1519 4 MP 011 072 Tlodnuce u Gama 6 Pin 8x32 29 16 Washer M8 DIN 125 8 PRF 15 357 000 14 Splint 2 0 x 25 SBS2025 B3am uH6 Ne 2 PRF 15Tr 150 000 AD 18 MP 003 000 11 bont 6 69 OCT131 12 Nut M6 self locking DIN 985 15 Washer M6 DIN 125 160 80 19 MP 012 000 3 MP 004 000 6 Pin 8x32 29 lodnucb u Gama N dokym lo206 04Keel Tube with Linear Actuator Fr2 USA Konupoban 13 Safety Ring SBR1519 MP 002 072 AD MIEREA Popmam A3
6. WING TRIM MECHANISM OWNER SERVICE MANUAL Manufactured by AEROS Ltd Tel 380 44 455 41 20 Post Volynskaya St 5 Fax 380 44 455 41 16 Kiev 03061 E mail aerosint aerosint kiev ua UKRAINE http www aeros com ua CONTENTS 1 Specifications of the Trim Device 2 Installing the Trim device on the Aircraft 3 Removing the Trim device from the Aircraft 4 Trim Device Operation 5 Maintenance and Storage Definitions Definitions used in this Manual such as WARNING CAUTION and NOTE are employed in the following context WARNING OPERATING PROCEDURES TECHNIQUES ETC WHICH IF NOT FOLLOWED CORRECTLY MAY RESULT IN PERSONAL INJURY OR DEATH CAUTION OPERATING PROCEDURES TECHNIQUES ETC WHICH IF NOT STRICTLY OBSERVED MAY RESULT IN DAMAGE TO THE AIRCRAFT OR ITS INSTALLED EQUIPMENT NOTE Operating procedures techniques etc which considered essential to highlight The trim device mechanism is designed for trimming your aircraft in pitch Please read and be sure you thoroughly understand this manual before operating your trim device Be sure you are thoroughly familiar with the trim device and the contents of this manual before initial operation It is important that you visit us regularly at http Avww aeros com ua In case of any doubts or questions contact your local dealers or Aeros We wish you a safe and enjoyable flying career Aeros Ltd 1 Specifications of the Trim Device
7. trim device and remove the trim device from the wing 4 Trim Device Operation Trim device switch should be activated in wings level attitude only not during turns To activate loosen grip on the control bar to allow control bar position to move and press the activation switch For take off and landing the trim device position is 20 30 mm 1 1 25 inch from most aft position visual check For cruise trim the aircraft on desired cruise speed with the trim device The travel range of 60 or 92 mm is sufficient for trimming the aircraft in the horizontal straight flight After the trim device has reached the most forward or aft positions its travel automatically stops The control switch is mounted and labeled on the aircraft Version of the trim device control switch position is shown on the photo WARNING THE TRIM DEVICE IS DESIGNED TO OPERATE IN HORISONTAL FLIGHT DURING TAKE OFF AND LANDING ONLY WARNING IT IS NOT RECOMMENDED TO USE THE TRIM DEVICE IN MOST FORWARD POSITION IN TURBULENT AIR IN ORDER TO AVOID EXCEEDING MAX LOAD FACTOR CAUTION DO NOT LEAVE THE TRIM DEVICE IN MOST FORWARD OR AFT POSITION FOR LONG PERIOD OF TIME CAUTION THE TRIM DEVICE PUSHES THE HANGBLOCK AT THE BOTTM SO IT IS NOT A CENTER PUSH SYSTEM BECAUSE OF THIS IN CERTAIN RARE CIRCUMSTANCES IT IS POSSIBLE THAT THE TRIM DEVICE PUSHES AT THE BOTTOM BUT THE HANGBLOCK DOES NOT MOVE AT THE TOP AND REACHES A SLIGHT ANGLE AND GETS COCKED IF YOU A
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