Raytheon Beech Baron E55 - Page 71

Ral~heon
AiKraft
Company
BARON
55
AND
58
SHOP
MANUAL
Table
1
TABLE
OF
TORQUES
(Continued)
Front
Spar Mounting
Bolts
and
Upper
Aft
Spar
160 to
190 in.-lbs
(Prior
to
TC-2457; TE-1202;
TH-14&1).
I
Mounting
Bolts
(Vertical
Stabilizer)
330
to
360 in.-lbs
(TC-2457
and
After;
TE-1202
and After:
TH-1484 and
After)
Lower Aft
Spar Mounting
Bolts
(Vertical
Stabilizer)
50
to
70 in.-lbs
(Prior
to
TC-2457;
TE-1202:
iH-l
484)
I
85
to
100 in.-lbs
(TC-2457
and
After,
TE-1202
and
After;
TH-1484
and
After)
Elevator
Horn
Hinge
Mounting
Bolts
50
to
70
in.-lbs
(Prior
to
TC-2457;
TE-
1202,
TH-~384)
30
to
40
in.-lbs;
Maximum of 70 in.-lbs
it
necessary
to
align
1
cotter
pin
holes.
(TC-2457
and
After,
TE-1202
and
After,
TH-1484
and
After)
WING SURFACE
CONTROLS
Push
Rod
to
Bellcrank
30
to
60 in.-lbs
Bellcrank
to
Structure
50
to
100
in.-lbs
I
AIR
CONDITIONER
Drive
Pulley
700
to
800 in.-lbs
LANDING GEAR
Main
Landing
Gear
Brace
Bolts
180
to
200 in.-lbs
I
Cross
Arm
to
Barrel
Attach
Bolts
80
in.-lbs
Main
Landing
Gear
Hinge
Bolts
250
to
690 jn.-)bs
Brake Back Plate
Attach
Bolts
80
to
90
in.-lbs
(For
Cleveland
Heavy
Duty
Brakes
only)
WHEEL HALF
ASSEMBLIES
(All
TC
and
TE)
Main Wheel
Assembly
140
in.-lbs
I
Nose Wheel
Assembly
83
in.-lbs
(AIITH)
Main
Wheel
Assembly
150
in.-lbs
Nose
Wheel
Assembly
90
in.-lbs
1
NOTE:
Be
sure
to
tighten
all
wheel
attach
bolts
evenly
to
make
certain the
assembly
is
not
warped.
E22
SECTION 1
Jun
30/i04Pege
17