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GDMMBi²13-1G 

Version 0010 

Reflex bridles produce longitudinal stability when the wing is at zero or negative angles 
of  attack.  The  reflex  bridles  work  by  preventing  the  trailing  edge  of  the  wing  from 
moving  downward,  as  they  are  tethered  to  the  king  post  assembly.  When  the  wing  has 
any negative load on the top surface the rest of the lifting surface will move downward 
relative  to  the  trailing  edge,  effectively  creating  elevator  type  control  surfaces  that 
produce a positive pitching moment, helping to restore level flight. 

3.5.13  CORSET 

The  BioniX²  wing is  equipped  with  a configuration  command that  allows the setting of 
cruise speed and the simultaneous adaptation of the shape of the sail in order to offer the 
best maneuverability and the best performance depending on that speed. The command of 
the  CORSET  is  activated  by  a  system  of  pulleys  that  tighten  the  two  central  battens, 
acting  on  washout  and  reflex  of  the  profile  at  the  center  of  the  sail.  The  CORSET  is 
activated  by  means  of  a  control  level  located  on  the  right  A-frame  strut.  This  lever 
automatically locks in the selected position and activates a cone-shaped pulley on which 
is wound the fine cord of the command. 

3.5.14  Sail 

The  sail  comprises  the  lifting  surface  of  the  wing.  It  is  mainly  constructed  of  UV 
protected  Trilam  and  Dacron  polyester  fabric,  with  some  ABS  and  Mylar  material 
making up the leading edge  areas. The sail is  constructed from  many individual  panels, 
which are sewn together using polyester thread to form the required shape. The sail has 
attachment  points  sewn  into  it  to  attach  to  the  frame  at  various  points  and  to  hold  the 
battens in place. The sail also provides zippers that facilitate easy preflight inspection of 
all the members inside the double surface wing. The central part of the upper surface is 
composed  of  a  flexible  fabric  derived  from  neoprene  which  compensates  for  the 
differences of tension due to the CORSET system. This part plays no mechanical role and 
may easily be replaced thanks to the two zippers that hold it in place. 

In  as  much  as  possible  the  wing  must  be  stored  away  from  sunlight,  as  UV  rays  cause 
damage to the fabrics. 

3.5.15  Tip Fins 

The wing tip  fins contribute to  the stability of the wing in roll  and  yaw at  high speeds. 
They  are made of a carbon composite material  and attached to  the wing  by means of 3 
quarter-turn  screws.  Flexibly  mounted,  they  give  way  when  the  wing  is  placed  on  the 
ground so that the end of the leading edge supports the force of any wind. 

3.5.16  Special purpose equipment 

Training Bars 

The  training  bars  are  attached  to  the  control  bar  and  uprights  in  order  to  extend  the 
possibility to fly the aircraft from the back seat. They are supplied as an option for use by 
qualified flight instructors. 

 

 

Содержание BioniX2 13

Страница 1: ...G Version 0010 1 Maintenance Manual Wing Type B Bi io on ni iX X 1 13 3 615 Route de l A rodrome 07200 Lanas France Telephone 33 0 4 75 93 66 66 Fax 33 0 4 75 35 04 03 info aircreation fr http www air...

Страница 2: ...5 4 King Post 7 3 5 5 Tensioning U channel 7 3 5 6 Control Frame 7 3 5 7 Leading Edge 8 3 5 8 Cross Bars 8 3 5 9 Battens 8 3 5 10 Top and Bottom Side Wires 8 3 5 11 Top and Bottom Front Back Wires 8...

Страница 3: ...tling Procedure 18 5 2 2 Wing Reassembly Procedure 19 5 2 3 Sail Reinstallation 23 5 3 Inspection Notes 34 5 3 1 Tubing 34 5 3 2 Bolts 35 5 3 3 Cables Terminals 35 5 3 4 CORSET 36 5 3 5 Composites 37...

Страница 4: ...blication The latest amendments to this manual will be issued on the Air Cr ation website http www aircreation fr in PDF format This should be printed out and added to the manual The amendment table s...

Страница 5: ...quired as the continuing airworthiness of the aircraft depends on the competence of the person performing the maintenance If there are any doubts regarding the required and appropriate maintenance the...

Страница 6: ...s a ready reference to the conversion factors that have been used in this manual 1 Pound lb 0 4536 Kilogram kg 1 Pound per sq in psi 6 895 Kilopascal kPa 1 Inch in 25 4 Millimeters mm 1 Foot ft 0 3048...

Страница 7: ...e cross bars tensioning U channel is bolted to the keel with two bolts These bolts are used to attach the rear wires 3 5 6 Control Frame The control frame is constructed mainly from 6005 AT5 and 2017...

Страница 8: ...eption of those at the extremities of the wing which are in a carbon composite The battens are secured by batten pockets sewn into the sail Easyfit tighteners on the trailing edge allow for the quick...

Страница 9: ...of UV protected Trilam and Dacron polyester fabric with some ABS and Mylar material making up the leading edge areas The sail is constructed from many individual panels which are sewn together using p...

Страница 10: ...t D or left G An inversion can have serious consequences because it modifies the tip angle resulting in negative twisting of the tips and strong longitudinal instability 8 Finish sliding the rear lead...

Страница 11: ...ockwise Rotax 582 the center part must be offset to the Right If necessary reverse the direction of the control bar if it does not correspond to the engine used by removing the connecting screws with...

Страница 12: ...ing should be moved with the nose facing into the wind In windy conditions the nose must be kept low The windward tip should also be kept lower to avoid the wing rising 3 8 Transportation Storage Avoi...

Страница 13: ...of these components is dependent upon rigid adherence to maintenance schedules Air Creation will from time to time amend these maintenance checks as the service history of the aircraft evolves It is t...

Страница 14: ...ten clasps 3 3 3 Wing tip fins fittings condition quarter turn screws 3 4 3 4 3 4 Condition of Velcro strips of the fairings of the kingpost struts 4 4 4 Wires and attachment fittings for tension corr...

Страница 15: ...xtended storage periods 4 4 2 Inspection after Heavy Landing The main attachment point for the wing to the aircraft base should be inspected carefully for any permanent deformation of the U bracket th...

Страница 16: ...in contact with each other and then approximately turn more should be made The resulting fit should not allow any axial movement of the bolt in its location but will allow rotation using fingers of a...

Страница 17: ...se plates Tubes Bolt holes Profile of central battens Wires Replacement of all bolts nuts and push pins Inspection of sail accessories Factory test on one of the sailcloth samples Special Requirements...

Страница 18: ...e trailing edge Refer to drawing OP10 26CA Remove all of the pieces of the CORSET the pulley assembly on the hang bracket and the control lever on the right A frame strut Dismantle the front and the b...

Страница 19: ...te the male female joints with Teflon grease Lay the crossbar D140640 41 out in their approximate flying position slightly swept back ball and socket joint in the middle tapered ends outwards with tap...

Страница 20: ...rough it Mount the 4 crossbar securing lugs D074327 of the restraining straps to the end of the crossbar securing lugs but do not tighten yet Figure 5 6 Figure 5 5 Figure 5 6 4 Nose Plates Please refe...

Страница 21: ...tween the crossbar and the keel Figure 5 7 Apply threadlock and tighten the nuts holding the lugs of the restraining straps to the crossbar leaving enough slack to allow forceful rotation of the plate...

Страница 22: ...rease or silicone spray to lubricate the hang bracket as this will serve only to collect abrasive dirt after a short time in service Secure the adjustment sleeves RAP stop ring D263020 D263010 in the...

Страница 23: ...ogether still with the crossbar on top Figure 5 9 Figure 5 10 2 Fitting the Sail to the Airframe Lay out the sail in a straight line back from the end of the leading edges with the nose towards the st...

Страница 24: ...sail should now be completely on the frame with the wing tips close to the ends of the sail Check that all the tubes have passed down the leading edge side of the membrane Now remove the protective p...

Страница 25: ...gently then loosen by one turn to allow the tips to slide as the tension screw is adjusted Figure 5 16 Figure 5 15 Figure 5 16 Do not apply threadlock to the tensioning bolt screw FHC 6 45 B126410 Go...

Страница 26: ...t the tips of the wing if it is not centered Fasten the retaining straps of the sail to the end of the nose battens and the CORSET batten guides of the lateral batten of the trailing edge as shown in...

Страница 27: ...last restraining strap free to slide between the two screws The leather stops on the strap must be placed on either side of the plate on the inside of the strap to limit the travel Figure 5 24 Figure...

Страница 28: ...t they do not cross 9 Uprights Check that the wing is still opened out fully Slide the Corset cord through the right A frame upright and the plastic guides at their ends Figure 5 27 Assemble the uprig...

Страница 29: ...positioned at the front of the assembly The lower side cable N2 D203675 fixed on the outer drilling of the cross bar is positioned at the back of the assembly Apply threadlock and gently tighten the...

Страница 30: ...s Tip Battens Refer to drawing U028271 M130 Place the two carbon wing tip battens D190920 on the plastic lug attached to the tube of the leading edge and tighten them with the clasps P235020 Respect t...

Страница 31: ...e in the pockets Figure 5 34 Figure 5 33 Figure 5 34 Lock the back right strap of the hoist on the central right batten by means of a self tapping screw B1999010 Figure 5 35 Assemble secure the pulley...

Страница 32: ...7 Figure 5 38 Thread the fine cord in the four guides of the right A frame strut then on the pulley of the hang point bracket then wrap it around the pulleys of the hoist and through the hole in the a...

Страница 33: ...et when the handle is brought back from the most stretched fast position to the least stretched slow Finish closing the central neoprene joint of the upper surface with the help of the zippers put in...

Страница 34: ...d control bar deserves special attention the central heat shrink sleeve must be cut to allow inspection of the elbows of the tube A new sleeve will be replaced before reassembly Ensure that the areas...

Страница 35: ...rame bolts are High Tensile Bolts If it is necessary to replace any bolts or nuts it is important that the specifications of the original bolt are matched when a replacement is selected Never replace...

Страница 36: ...of the CORSET are wrapped around the battens in the openings made in the pockets The right back strap of the CORSET is blocked on the right batten by means of a Parker screw to prevent the hoist from...

Страница 37: ...factors requiring attention are fatigue wear UV exposure and heat Inspection Check for tears in the sailcloth or any loose or unraveled seams Check that none of the securing points straps eyelets secu...

Страница 38: ...pair tape such as used for registration letters if possible to both sides of the fabric This tape is available from Air Creation Any other significant damage should be discussed with Air Creation or a...

Страница 39: ...of the reflex lines Never adjust the internal membrane setting Never alter batten shape except to match the batten profile drawing The reflex lines are designed never to be adjusted and their primary...

Страница 40: ...et during the first factory tests of the wing according to the torque of the trike s engine and they are locked in position by a Parker screw This position can be checked by means of the positioning m...

Страница 41: ...fects of aging on the sail and improve its performance This action is not to be considered before a minimum of 300 hours of flight To do this just move the screw that positions the tensioning swan cat...

Страница 42: ...GDMMBi 13 1G Version 0010 42...

Страница 43: ...aightness_______________________________________ 2 Hang bracket fit and orientation hang bolt hole on rear face ___________________ 3 Backward hang point position _____________________________________...

Страница 44: ...en aluminum parts D264550 and D264540 _____ 6 Correct flying wire fitting and orientation No2 nearest to hinge Top rigging not fitted at this stage _________________________________________________ Wi...

Страница 45: ...se assembly ______________________________________________ Sat Unsat 1 Refer to drawing M030 and check area for correct assembly and security of all fastenings ________________________________________...

Страница 46: ...lateral carbon batten in place at luff line 2 Velcro fastened _________________________ Sail General ____________________________________________________ Sat Unsat 1 Carefully check sail all over for...

Страница 47: ...roceed with a second person One stays at the leading edge the other holding down the inner surface panel Fold the leading edge which is stiffened by the Mylar insert onto the sail 5 Take the keel pock...

Страница 48: ......

Страница 49: ...MBi 13 1G Version 0010 49 7 3 Maintenance Operation Board Wing Type ______________________ Serial Number _________________________ Date Hours Flown Type of Operation Performed Operator Name Address St...

Страница 50: ...GDMMBi 13 1G Version 0010 50 Date Hours Flown Type of Operation Performed Operator Name Address Stamp...

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