Raytheon Beech Baron E55 - Page 167

Raytheon
AiKraft
Company
BARON
55
AND
58
SHOP
MANUAL
Chart
1
I
Wing
Bolt Wrenches and
Torque
Adapters
BOLT PART WRENCH PART NUT PART
NUT
TORQLIE
POSITION NUMBER
NUMBER NUMBER
ADAPTER
LOWER
FORWARD 1309098279
TS1222-3
EB144
or
50-590014
1
TC-I
thru
TC-1442,
ZEB1845-144
TE-I
thru
TE-862,
TH-1 thru TH-234.
131790-3
TC-1443
and
After,
TE-863 and
After,
TH-235 and
After.
UPPER
FORWARD
131790-1
TS1222-3
(9/16
12NB126
TS
1171-2
inch
hex)
TO-i thru
TC-2358,
TS1222-4
(1/2
TE-\
thru
TE-1 t
82,
inch
hex)
TH-I
thru
TH-1192.
EB126 TS1176-2
TC-2359
and
After,
TE-1183
and
After,
TH-1193
and
After.
UPPER
AFT 1309098274
TS1222-4 128108
TS1171-1
50-590013
LOWER
AFT
1309098280
TK1817-922-4
12N8126
or
TS
1171-2
or
1
I
LH6422T-1
26
TS
1176-10
CAUT~ON:
There
should
be
no
bolt
binding during
removal
or
installation.
Do
not
drive
or
screw
a
bolt
in
or
out
of
the
fittings.
If
wing
bolt
binding
is
encountered,
place
the
airplane
on a
three
point jack
and
raise
the
airplane
until
the
wheels
are
clear
(see
Section 2
forjacking
instructions).
Place
a
suitable
cradle
under
each
wing
and
a
tail stand under the
aft
portion
of
the
fuselage.
Defuel
the
wing,
loosen
the
remaining
bolts and
reposition
the
wing
until the
bolt
moves
freely
through
the
fittings.
Replace
the
soft
aluminum
washers between
the
upper
fittings
and
torque
the
bolts
as
instructed
under
WING
INSTALLATION.
II
bolt
binding
is
not
encountered and
the
wing
is
not
shifted,
replacement
of
the
soft
aluminum
washers
between the
upper
wing
attach
fittings
is
not
required.
NOTE:
Raytheon
Aircraft
Company supplies
wing
attach
hardware
(bolts
and
nuts)
that
have
been
given
an
additional
magnetic particle
inspection
since
manufacture.
These
components
may
be
identified
by
the
green
dye
on
the
head
of
the bolt
and
on
the
nut.
WARNING:
Use
only
the
components
specified
in the
applicable
Illustrations. DO
NOT INSTALL
THE
BLACK
P/N
H-20
NUTS,
These
nuts
have
been
dry
film
lubricated
with
molybdenum
disumde.
When
I
MIL-C-16173
Grade
II corrosion
preventive
compound
is
added
to
these
nuts,
the
additional
lubrication
may
cause
improper
preload
in
the bolt
when
it
is
tightened
to
the
wet
torque
values
specified
in
figures
8,
9, in,
and 11,
E23
SECTION
3
Dec
19