
Handbuch Slingsby T21 - BGA 782
Seite 33 von 35
Thl. J&(J( Is$ued with A.L. No.
S,
Oeumber.
" 950
A.I.4J09A.',VoJ.
"
I
"
Part
2
Section '2
ASSEMBLY. DISMANTLING AND REMOVAL
L IST
OF CONT�NT
S
.
General
...
: :
.
Moln plones
.Tall plone
Alferon control ...
.
Spoiler control
..
..
ASSEMBLY
.
�
.
.
�
. ....
Para.
,
.... . :" 1
3
4
5
6
Elevator control....
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.
.
..
';'
'
.
.
.
.
.
,
'\"
t9!rinvs
,�....
•
......
-,
...
.
.
Ailerons
'
Rudder
E/�'v�to,
.REMOVAL·
.... .
. .. ,
'�""
.... ,,.,.�
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.
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.
. "'- .....
;,;
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..
,
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.""
Para.
7
8
�.
10
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1 1
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•
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12
LIST OF
'
ILLUSTRATIONS
Ma;n components
.....
,
,,'
....
Main·plane auachmenu
Gt!lnt!lral
'
.
.
Flf·
I
•
1
1 .
::The purpose
of this
'
.
chapter
.
ds
�
to
describe. the method
o
f
.
·
assembling t,the.
glider from its main components ·a.ndnthe
removaL of individual. items of the '.main
components. Neither the p,ismantling " of
the complete glider; nor.: the assembly or
individual , items is described, since theso
arc::mainly reversals oC .the
"
particul
�
assembly or removal opcrati9ns. but. where
this ,is nof
�
the :case
it
i� described
'
i;
'
l
�
t
he
r�levant .paragraph.
2:
'The: glider is so design
e
d that it can
easily be assembled and dismantled without
the use of special tools ilnd equipment
other than fusela£e trestles, It nOnTIallv
Tall'runlc and toll IIdd oUachments
CockPlc comrals and lond'n, wheel detail)'
;
..
.
..
will'�
bel'
receiyed;.broken I.down.; into the
[P1l9�ving
.
:
c
oqlponents
'
:
nil';
and
I
rudder
d
�.t all:
t�;
.PQ,rt
·ana.
:Siarbo�d ',Wi.iigsj iq�mpl<tte:
WIth
/fhli
!
pla.n�
't
f'
and
,
..
'elevator:· ass'emblcd to-
utcther as onc
unit.
.
fMjlin-plane!\struts�
W)ng" roQt fairing:
Tail
plane-to-fm fairings:
'f
.
,
.
.
.
.
.
,
.
' �
A�tachment" and locking',pins' (these are
'nonnallyt! packed ' in " a
'
canvas bag
stowed in -the cockpit).
.
ASSEMBLY
·
MAIN PLANES
.
'\.:.
.
.
-
..
-
,
.
.
.
3.
,
.;
The method. of assemb
l
ing
'
the '.main
planes
to
the fuselage is as follows
:'-:" ' , '1
I
; '. , .' I' j'
(I)
Support the fuselage in tbe rigging
position
(Pari 2,
5,,1. 3,
Cllap
.
•
1),
either by one man holding it at the
side
oC
the
cockpit
or in fuselage
trestles
(Pori
2,
Sect.
I/�Chap: 1):".\"
(2)
!
Attach the' two
struts to
the · fuselage
�
with
;
diameter
shackle
'
pins,
'
inserting them' from the
front.
p
Lock
the
attachment pins with
,;mCety, pins and rest the outboarc;l ends
of the struts on the �round. ·
.
rI.
••
•
'.
..
�
'(3\
.
'
.
With .on
e
.
man;at
...
t e
wing tip. one
under
,th_e
ma;n spar at. the ... wing. root
and'.'one· man'lsteadying the 'wing at
the ''roaPI tr
a
ilin
g
,
l
ed
g
e, lift . the ' star
board wing and align the "wing root
attachment jiltings with . tbe .attach·
ments 'pn the
'fuselage
neck.
I
l1i
riisert t
h
e m';';n;''s
p
ar--attac!tiPent pin ;
.
.
frami the port
oC the fuselage by the:..man .who
was steadying
�!Ige. Lock
�qe
:
at��
A
Aqi�.�t:
�·.�afety. pin.
(?)
AHach
;
;
.the
.
•
\�ng"�trut
Ip,
tbe main
plane with a half-inch diameter shackle
F.S·II
R E S T R I C T E D
Содержание BGA 782
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