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DYNAMIC WT9
5.1.3 Procès verbal de pesée et de l'équilibrage des gouvernes
AEROSPOOL
Prievidza
DYNAMIC WT9
Control surface
Aileron
Right
Left
Arm l = 255 mm
( the distance between rotation axis of the control surface and weighting point )
Note:
Elevator
Right
Left
Arm
l = 230 mm
( the distance between rotation axis of the control surface and weighting point )
Note:
Rudder
Arm l = 325 mm
( the distance between rotation axis of the control surface and weighting point )
Note:
Wing flap
Right
Left
The static moment is measured on root rib at arm distance l = 315 mm.
Note:
Checking static moment of the control surfaces are within the approved tolerances.
Prievidza, date ........................
Date: Novembre 2003
CHECKING CONTROL SURFACES WEIGHTS
Registration:
Without balancing
Specified values
weight (kg)
st. moment
( Ncm)
0,77- 0,95
70 – 100
0,77- 0,95
1,00-1,20
60-85
1,00-1,20
1,50- 1,90
40- 70
2,50- 3,30
180-220
2,50-3,30
DYNAMIC WT9
MANUEL D'UTILISATION, D'ENTRETIEN ET DE REPARATION
AND BALANCING
S/N:
With balancing
Specified values
weight (kg)
st. moment
( Ncm)
1,00-1,25
20-60
1,00-1,25
1,15-1,40
30- 68
1,15-1,40
1,75- 2,25 -40 do -20
3,50-4,70
-20do+25
3,50-4,70
.....................................................
Checking carried out by
Date:
Real values
weight (kg)
st. moment
( Ncm)
Section 5
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