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Air Creation BioniX2 13, Руководство по обслуживанию

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GDMMBi²13-1G 

Version 0010 

43 

7 

Appendix 

7.1 

Wing Inspection Forms 

7.1.1 

BioniX² 13 Wing Frame Stage Inspection (1) 

Wing serial number and registration:  _________________________________________  

General 

This stage inspection should be carried out when the wing frame has been 
assembled and is ready to be fitted in the sail. It is not possible to properly 
inspect once the sail has been fitted. 

Inspection schedule 

Nose plate assembly  _____________________________________________  Sat / Unsat 

1 

General assembly correct (check with drawings M030)  _______________________ 

               

2 

Plastic spacer washers in position between plates and tubes ____________________ 

               

3 

Nylon stop washers in position under the Nylstop nuts of the leading edge nose 
assembly ____________________________________________________________ 

               

4 

Check for over tightening (distortion of plates/tubes)  _________________________ 

               

5 

Length of the thread of bolt B168710 (nut not tightened at this stage)  ____________ 

               

6 

Correct position of nose-catch rail (pointing rearward from the bolts)  ____________ 

               

Leading edges  __________________________________________________  Sat / Unsat 

1 

Inspect both forward sections for damage and straightness _____________________ 

               

2 

Inspect both rear sections for damage and straightness ________________________ 

               

Keel __________________________________________________________  Sat / Unsat 

1 

Inspect for damage and straightness _______________________________________ 

               

2 

Hang bracket fit and orientation (hang bolt hole on rear face) ___________________ 

               

3 

Backward hang point position  ___________________________________________ 

               

4 

Stop rings not over tightened ____________________________________________ 

               

5 

Kingpost fitting correctly assembled and not over tightened ____________________ 

               

6 

Length  of  the  thread  of  bolts  B167010  (fixing  nuts  on  tensioning  rail  not 
tightened at this stage) _________________________________________________ 

               

7 

Transparent  protective  film  patches  of  the  keel  R108810  properly  glued  & 
positioned ___________________________________________________________ 

               

Crossbar central junction __________________________________________  Sat / Unsat 

1 

Check cross tubes for damage and straightness ______________________________ 

               

2 

Correct fitting of webbing hinge D074330__________________________________ 

               

3 

Check  that  the  crossbar  are  free  to  rise  up,  limited  by  the  straps  of  the  keel 
protection sleeve ______________________________________________________ 

               

4 

Correct  assembly  order  of  stainless  plates  (no  stagger,  check  with  drawings 
M040) ______________________________________________________________ 

               

5 

Thread showing through each nut on bolts B069410 (just) _____________________ 

               

6 

Centre  bolt  B086710  not  over  tightened  (cables  should  wiggle  freely),  correct 
length of aluminum spacer D252300 ______________________________________ 

               

7 

Tension cables direction (plastic over sleeves forwards) _______________________ 

               

8 

Leather/webbing protection sleeve D074328 correctly fitted and screws in  ________ 

               

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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