Slingsby BGA 782, Руководство пользователя

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Handbuch Slingsby T21 - BGA 782
Seite 28 von 35
FLYING CONTROLS
AILERON CONTROL
18.
The aileron control is rigged and ad·
justed in the following manner:-
(1) Set the control column vertical and
temporarily secure it in that position.
(2)
Check that a line drawn through the
push-rod attachment bolt holes in the
double lever at the aft end of the aileron
torque tube (aft of frame
4)
is horizontal.
(3)
Connect the lower ends of the push­
rods to the aileron torque tube lever and
the upper ends to the levers on the main
plane root ribs. and adjust the length of the
push-rods until the levers on the main
plane root ribs are parallel to the root ribs.
(4)
Connect the inboard cnds of the aileron
contl'ol cables to the control levers on the
root ribs (the longer link-plate is attached
to the lower arm of the lever) and · their
outboard ends to the aileron levers (the
cable with the shackled end is attached to
the lower lever).
(5)
Adjust 'he cables at the ,urnbuckles,
accessible through the panel on the under­
side of the main planes between ribs
5
and
6,
until the trailing edge of the aileron is in
line with the adjacent main plane: trailing
edge.
(6)
Check and adjust the aileron movements
as instructed in para. 14.
(7) Tension the cables to the limits given
in para.
23
and lock all adjustments and
connections.
(8)
Check the static friction load
(para. 27).
RUDDER CONTROL
19.
The rudder control is rigged and
adjusted in the following manner :-
(I)
Set the rudder pedals so that thc foot­
bars arc in line with the frame to which
the pedals are attached.
(2)
Connect the cablcs at the turnbuckJes
on the inboard rudder pedals and ut the
control levers on the rudder (the cable with
the shackled end is attached to the port
lever on the rudder and the starboard in­
board rudder pedaL)
(3)
Adjust the cables at the turn buckles
until the rudder is in line with the centre
.
line of the fuselage. -
(4)�heek and adjust the rudder movements
as
. instructed in para.
IS
and lock the
tumbuckJes and connections.
(5)
Check the static friction load
(para. 29).
ELEVATOR CONTROL
20.
The elevator control is rigged and
adjusted in tite following manncr:-
(1)
Set the control column vertical fore­
and-aft, and temporarily secure it in that
position.
(2J
Adjust the connecting tube between
the
control column cross-shaft and the control
lever on the front face of frame
4
until tile
centre of the top hole of the contro!" lever is
1 1 in. from the front face of the frame.
(3)
Connect the control cables at the turn.
buckles on the control levcr and at the lever
in the rear fuselage (the cable with the
shackled end is attached at the upper position
on both levers) and adjust them until a line
drawn from the pivot point of the lever
in
the rear fuselage to the top cabJe�attachment
hole is inclined forward at an angle of71 deg.
to the fuselage datum (the top surface of
the deck under the tail plane). The tail
plane must be removed for the purpose of
this adjustment.
(4)
Connect the elevator push�pllll rod from
the lever in the rear fuselage to the control
lever on the elevator, and �djust it until the
elevator is in its neutral position.
(5)
Check and adjust the elevator movcment
as instructed in para. 16.
(6)
Check the tension of the cables and
adjust to the limits given in para.
24;
lock
all adjustments and connections.
(7) Check the static friction load
(para. 28).
SPOILER CONTROL
21.
The spoiler control is rigged and
adjusted in the following manner:-
(I)
Connect the cable at the turnbuckle in
the cockpit, at the shackles at the port and
starboard wing roofs and an of the operating
levers in the main planes, and adjust the
tension of lite cables until they are rensonably
tigitt when the control lever is fu1Jy forward
against its stop.
(2)
Move the control lever in the co�kpit to
its full extent aft and check and adjust the
spoiler movement as instructed in para. 17.
(3)
Release the control lever and check that
the spoilers are flush with the upper surf�ce
of the main plane and that. the operatl.ng
levers in the main planes are In contact With
their stops.
R E S T R I C T E D