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SECTION 3 / USAGE 

 

Wing Assembly (Rigging) 
 

The wing assembly is the start of a thorough PREFLIGHT. The assembly operation must be 
carried out unhurriedly, without using force and methodically: 
 

• 

position the wing nose into wind, open the cover 

• 

Turn the wing over, Control frames on the ground (on canvas, grass, a smooth surface) 

• 

remove the cover  

• 

fit the king-post to the keel,  between the cross spar tensioning cables (2)  

• 

hang the upper-longitudinal rear cable near the king-post, without crossing the cables 

Note: the part small diameter of the hook will be directed upwards (3) 

• 

position the nose batten on the head of the CHC 6 front screw  

• 

pull the leading edges outwards, grasping them in the middle, without raising or forcing 
them (1) 

• 

pull the control frame outwards, checking that no cable passes inside the frame 

• 

fit the control bar using the M8 bolt (wing nut + safety ring) 

Note: preferably position the wing nut towards the nose of the wing so as not to tear the front 
seat cover when the control bar rests against it 

• 

slide upper wing surface battens into their respective sleeves 

Note: the leading edge batten ends are ‘colour-coded’, red for the port (left) side and black, 
green or white, for the starboard (right) side 

• 

check the position of the side and longitudinal cables 

• 

pull on the cross spars tensioning cables  

Note: to facilitate this operation, raise the tip of one of the leading edges to knee height (i.e. 
give the wing a little dihedral) 

• 

lock the tension lever (or goose neck) using the pit-pin (2). 

Note: the end of the tension lever is divided, lock it immediately. On the level of the king post, 
the left tensioning cable of must be higher than that located on the right. 

• 

tighten the upper surface battens, pass the shock-cord in double (4, 5). 

• 

raise the wing by the back of the keel, by making it swivel on its bar of control 

• 

tension the front cables and lock the tension lever using the pit-pin. 

• 

place the nose of the gently on the ground, nose into wind 

• 

slip the under-surface battens into their respective sleeves (6, 8). 

Note: the batten tip is spoon shaped, with the hollow side, cupped towards the leading edge 
(7). Red tip to the left; black, white or green, to the right 

• 

insert the washout tubes (dive sticks) in the leading edge 

• 

close the wing ends 

• 

attach the nose cap.  

Note: the absence of the nose cap creates an internal pressure variation in the wing which 
causes fundamental changes in the wing profile and makes the wing heavier to control. 

 

Note: in moderate or strong winds secure the wing by its nose. 

 

Attaching the wing to the Airframe 

 
See the Airframe Instruction manual. 
 

Wing Disassembly (De-rigging) 

 
Follow the Wing Assembly procedure, except in reverse. Before placing the wing on the ground, 
the hang bracket protection on the top of the control frame must be fitted to the keel and the under-
surface battens and the hang block remove (10). Before folding up both sides of the wing, to 
withdraw the washout tubes from their sockets and fold back them along the leading edge. 

 

MAUT DYN 450 

Edition : June 2005 

Section : 3 - 01 

Summary of Contents for DYNAMIC 450

Page 1: ...WING INSTRUCTION AND MAINTENANCE MANUAL DYNAMIC 450 MAUT EN DYN 450 Edition June 2005 Copyright DTA DTA ULM AU Wing n Model Year...

Page 2: ...DTA improves its production constantly and reserves the right to modify the specification the drawing the characteristics the model and or the equipment in the interests of Quality Assurance without i...

Page 3: ...Diagram 2 01 2 02 2 03 JUNE 05 SECTION 3 USE Wing Assembly Disassembly Wing Photographs assembly disassembly Hang Bracket Position Washout Tension Dissymmetry Vibrations Modifications PREFLIGHT Wing...

Page 4: ...he aircraft or to add elements by modifying the estimate of weight will check that the identification registration card is valid and that the identification markings a minimal height of 50 cm for Fran...

Page 5: ...in fast flight and 30 cm from the front strut in slow flight in hang bracket position n 2 CF section 3 03 Note The person s who choose s to use a non DTA airframe will assume ALL the responsibilities...

Page 6: ...3 Plan Views MAUT EN DYN 450 Edition June 2005 Section 1 03...

Page 7: ...g cables Control frame Cross spar left Inner leading edge LEFT Lower side cable Upper side cable Lower rear cables Cross spar cable tensioning lever Keel Outer leading edge sleeve LEFT Washout tube Fr...

Page 8: ...h 110 km h Horizontal maximum speed VH 115 km h 126 km h 138 km h 130 km h 138 km h Landing distance 70 m 70 m 70 m 70 m 70 m Landing distance from 15 m 190 m 190 m 190 m 190 m 190 m Minimum rate of...

Page 9: ...h 110 km h 110 km h 110 km h Horizontal maximum speed VH 126 km h 138 km h 130 km h 138 km h Landing distance 75 m 75 m 75 m 75 m Landing distance from 15 m 195 m 195 m 195 m 195 m Minimum rate of fal...

Page 10: ...LM is NOT designed for Aerobatic flight Inverted flight is completely prohibited Beyond these limits Bank 60 pitch 45 the loss of stability or of control structural failure or tumbling could occur Koc...

Page 11: ...the wing a little dihedral lock the tension lever or goose neck using the pit pin 2 Note the end of the tension lever is divided lock it immediately On the level of the king post the left tensioning...

Page 12: ...1 2 3 4 5 6 7 8 9 10 MAUT DYN 450 Edition June 2005 Section 3 02...

Page 13: ...y close to the wing s stall speed Control deflections must be subtle The effort required to pull the control bar in will be more significant than in hang position n 2 At MTOW in position n 4 full fron...

Page 14: ...ord on this side Vibration the appearance at high speed of a vibration of the wing trailing edges is a result of insufficient tension on the shock cord of the battens where the vibration occurs Modifi...

Page 15: ...ashout tube dive stick is correctly inserted in the leading edge tube then immediately close the hatch again Walking towards the keel and visually check the batten position and the shock cord 5 Open t...

Page 16: ...ack towards the pilot in order to preserve a trajectory parallel with the runway Let the Microlight ULM accelerate up to 80 km h before climbing out The climb out airspeed should not be lower than 75...

Page 17: ...face disturbs the air flow The stall angle of the wing will be decreased The associated stall speed will increase by approximately 10 km h If you wipe the leading edges before the flight wipe both sid...

Page 18: ...traviolet radiation emitted by the sun and reflected by the moon cause the ageing of the fabric and the seams As far as possible park your aircraft under shelter out of the sun between flights Four up...

Page 19: ...onditions of use of the aircraft given to the purchaser The breaking of any regulatory provisions of the Civil Aviation Code or any related legislation of the country of registration of the aircraft h...

Page 20: ...ASTIC CENTERING RING KEEL E2195 RIGHT LEADING EDGE REAR SECTION 450 E7177 CHC 6X80 12 CONTROL FRAME CHANNEL KEEL E2196 LEFT LEADING EDGE REAR SECTION 450 E7178 CHC 6X37 8 CONTROL FRAME SIDE UPPER KNUC...

Page 21: ...Maintenance Log Date Hours Operations carried out Sign MAUT DYN 450 Edition June 2005 Section 5 02...

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