
Handbuch Slingsby T21 - BGA 782
Seite 2 von 35
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se
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e
r
a
l gUlde,to,tbe
location of
all
cocKpit
�
co'ri
(fO\S
a":d inst��rp,en�l.:
..
�<?g�th.e�: wH,h
,
.
tbe
�
melhod of
.
operatlcg the controls where'
this
:is
not
abvious
..
·:.The
l
a
y
o
u
t
of
th
e
:
cockoit
i
s
"
i
II
u
s
l
r
3
t
e
d
in
fig,
1.
FLYING CONTROLS
, ... �;
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..
.
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.
;
.
2
.
.
:
.
The
glider
has
side-by;slde
s
e
a
t
i
o
'
g
for in:
'structor
and
pupil. The
m
a
i
n
tlying'cdD'trols
t
.
\
¥
hic�
·
are·
co
n
v
�
n
.
t
i
o
nal
:in
o
p
e
r
a
t
i
o
ri
·.
�
"
a
r
�
duphcated;
.
sub
sl
dlary
c
on
t
ro
l
s
,
'
f
or
the
'
lift
spoiler aDd
tow
re
l
e
a
s
e
,
'
are
easy.
reach 'of
b
O
l
h
the
instructor
and
LIFT
·
SPOILER 'CONTROL·
"
,
.
;
'
"
:
, -
•
•
•
..I
11
'
·
·
• . •••
,
.
...
.
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;3:��;The
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1
.
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ft
..
,
.
.
s
p
o
i
J
er
.
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c
o
n
tr
o
l
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�,
is �
·
.
�
e
D
t
r
a
l
l
y
.p
l
a
c
e
d
ID
�
the
Hoor
o
f
·
,'
.
t
h
e
.
cockpit:?,:
it
is
'
·
moved aft
to open
tbe spo
i
l
e
rs
:
'
,
T
h
e
control
:
.
:spring-loa·de4.nnd
.
inUSt"
.
D
C
':
held
',in
<the
�ired
.
o
p
e
n
.. position
'
;
,
·
iit
:
'
ma
Y
'
be�
r
�
ta
i
n
e
d
'
,!u.;:the
fully
open
.
'
pos
it
ioo
'
:-
when the�g
li
der
'
. �s
,
l
p,a�ked
'i
.
by
"
,
uSing
'
t
h
c
;
'
s
a
f
e
t
y harness
:i.as
,
r�taIQlng
"
�s
[
raps
:
::
Thc
:
:
sp
ol
ler
s
"
li
re
,
�
a
u
t
o
matically
'
I
o
c
k
e
d
"
i
n the
"
c
lo
s
e
d
"
'
p
o
s
i
t
i
on
16
prevent
them "
fl
oa
t
i
n
g
n.
in
.night:
.
TOW
:
nELEASE
;:
CONIROti
4.
:
The
Ott"rur tow
'
rele�se' b';'�k
i
s
,
m
o
u
�t�
:
d
in
'
t
h
e
nose�of the
fuselage
f
o
r
w
a
r
d
·
o
f the
froot
s
k
i
d
.
l
'
l
t
is
o
p
e
ra
t
e
d by
'
a;
c
a
b
l
e
terminating'\
in
'
a"
y
e
l
low-
p
a
i
n
t
e
d
{
kn
o
b
�
'
�enlrally,
p
l
a
c
ed
immedi.ately
b
e
l
o
w
·
.
th�
:
IOstrument panel;
the
knob must
be
'
pulled
sharply
to
r
e
,
l
e
as
e
the
tow cable,:�
A'
trans�
.
parent plastic
panel
is
.fitted
in
the
Boor of
the Cockpit, i
mm
e
d
i
a
t
e
l
y
above [he'release
',hook,
e
n
a
b
li
n
g
the
'
p
i
l
o
t
s
.
t
o see the tow
cable
: attachment
in
flight.
'
WARNING
.
'f!
'
,
.
; ,:
:i
It.
is
�ssentjQl'tb!]ftbe1
,
tow
�
11
cDble.
releQs�
·
"
rinti
·
26EY
/41)
both
for
wm�h
launching
".ero-tow,
.
The
use of
nny other
type
or'
rmg
mny
cause
jamming
and
failure of
,,:1
the
release,
-.
"
.
:"
,
'
"
�:"
11,
'
,
:
INSTRUMENTS
·
'
�.
5
'
:
"
Th
l
jn�
i
r
,
u
'
�ent
'
pa·tj.
'
eJ"
ca;ric5;.the
insrru.
�
�el?
ts.rs
b,��,Iij,
ip.
�.fi
g;\
be;:
tu
rn
�a
n
d
:s} I P
.
:11��JCato�IS
,?pcrated
tbe
'
power
;bbLDg
8upphed
.
.
..
by;dry.;batteries stowed
in
a
�o�ke
�
,o9�t��:;p�rt,
si��
,
of the
'
inst��ment
'panel;
It,lS
co
�
t
r
o
n
e
d
,
b
y
"
a
switch;
"
p
o
s
I
t
ro
n
e
d
,alongsid�:
lhe�.instrumeut,
which
"
is
m
o
v
e
d
I
down
:
fo
'
r
{
OFI
�
:
:
8Dd
up
'
for
T
h
e
i
n
s
t
r
u
-
.
'
rnent
'
is"intended
f
o
r
and inter
rmittentius�:
Hi.
bliod flying", and
"'
und
e
r
'
these
'
�coodi'ioas::t)le·:
p
ower
s
u
p
p
l
y
iudequatdor
�several
montllS,
use"
�6. ;;,Tbe:iun:i�"e.n"d;slip·
inaic'a'tor 'is'1e'ss'
sensi-,
r,
a
t
e
s
:'.'
o
f
�turn :tban
:
�t
,
teCt ,::t()';pow,ered
,
�
8Ircraft:¥.the;calibratlOO'IS as
:follows:....:;;;:
.
.
·,:
..
:
'
R
a
t
e
'
;?
l i
t{p
o
i
n
t
e
r
·
�
movement
.
.
/r':!:jn
.
.
rrom
'
.j�:';
zero
Y�'4
50":
d
eg:'
'
oer
"
m
i
n
u
t
e:'.�. ;r�;;\�:,,:��!' ','
fro
m
,
:��
�
'Zero)
1
deg��
per
minute,
::��-{��M::,
'ftop;'is
jeiicli�d"::'2,250
eg,'.'
,
•
'
s
e
at
;'
bearers
�
f
u
s
e
l
a
g
e
.
'
f
r
ame
"
behind
Q
!t
�
"
tbe
.
�T
u.�
�.
I�g
c
:,
fra
me
ron ';:�.to
.;\\:�IC�\
they}. re
strap
'·.!:'"�they 'are:'
not
.
"
,h
" �..
"
�
�:a'tftlie; hack' 'of
ihe
pi
lo
t
s
'
Mk.15
are
-:
not
(are.
jpl
ywood
:!
,
,
"
-
'
.
.
,
.
,HorlioQ bii
' .1.l; 'rV",
.
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1
!10.!,�'A·�ho'r zon:!bar;JI'fitled
,
o
n
;
t
h
e
aft
face
for
each
seal
,
posi
are
,
manually
,
a
d
ju
s
t
e
d
for
,
'
:
aircraft,'
is
::
'
in
'
rigging
:
'
position 'and
t
h
"
e
pilot
sitting in the
a
t
ti
t
u
d
e
;'he
n
o
r
m
a
l
l
y s.'dopt(when flying,�',;:rhe'pilot
��
will,
indicate"
(:
w
h
e
n
l
;
the'�
bar;, is:"rset
in
,lhe
�.
p
o
s
i
t
i
o
n
,
he
reauire{il to
,
be
,
l
o
c
k
e
d
:
.
.
Содержание BGA 782
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