CONTROLS
PRIMARY
CONTROLS
Push- pull tubes with self-aligning r o d end bearings
actuate t h e p r i m a r y flight control s u r f a c e s .
loaded interconnect device indirectly joins t h e a i l e r o n
and r u d d e r control s y s t e m s t o a s s i s t in l a t e r a l stability
during flight maneuvers. Control s u r f a c e gap s e a l s
minimize airflow t h o u g h t h e hinge s l o t s and r e d u c e
d r a g .
CONTROLS
F o r pitch
control, the e n t i r e empennage pivots on
t h e t a i l cone attachment points t o i n c r e a s e o r d e c r e a s e
t h e horizontal s t a b i l i z e r angle, T h i s design allows
t r i m establishment with minimum control s u r f a c e de-
t r i m indicator on the console indicates
s t a b i l i z e r t r i m
flight, forward rotation
of
t r i m
Rowers
nose; r e a r w a r d rotation
r a i s e s
nose.
WING
The
control
a r e c e s s on the right s i d e
of the
control console and o p e r a t e s the
ally- actuated wide-span
f l a p s , Moving
control.
t o t h e
U P
position, r e t r a c t s the
The position of
the f l a p s can
be
noted f r o m the flap position
located adjacent t o the t r i m indicator.
the
control in the down position moves the flaps down until
t h e d e s i r e d position
is
r e a c h e d , r e l e a s i n g the
s t o p s
Limit
prevent
t r a v e l above o r below t r a v e l limits.
SYSTEM
A
mounted on t h e
s u r f a c e of t h e
wing, picks up a i r s p e e d indicator r a m a i r .
A heated
prevents
tube icing when flying
in
laden a i r .
s y s t e m d r a i n
i s located on t h e
forward bottom skin of
wing just outboard of t h e
wing fillet. Static posts on e a c h s i d e of the
cone
Содержание M20J 1978
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