Table Of Toroues; Engine Mounting; Wing Mounting; Horizontal Stabilizer - Beechcraft TRAVEL AIR 95 Shop Manual

TABLE OF TOROUES
ENGINE MOUNTING
Engine mount
bracket bolts 265
to 290
inch-pounds
(on nut)
(Prior
to
TD-534
except
TD-506)
(at
firewall)
245
to 265
inch-pounds
(on nut)
(TD-506, TD-534
and after)
305
to
325 inch-pounds
(on
bolt head)
Engine
shock mount
bolts 475
plus or minus
25 inch-pounds
WING MOUNTING
Upper front
wing mounting
2480-2600 inch-pounds
(wet torque)
bolt
Upper
rear wing
mounting
1180-1300
inch-pounds (wet toruge)
bolt
Lower rear
wing
mounting
2480-2600 inch-pounds
(wet torque)
bolt
Lower
forw
a rd w
i
ng
2880-3000 inch-pounds
(wet torque)
mounting bolt
VERTICAL STABILIZER
Front
and rear spar
mounting
50-70 inch-pounds
bolts
HORIZONTAL STABILIZER
The
mounting
bolts in the
50-70 inch-pounds
front
and rear spar and
the
bolt that
attaches
the elevator
horn hinge to the
rear spar
bracket.
PROPELLER
650-675 inch-pounds
LANDING GEAR
Main
gear
brace
support
arms
200-250 inch-pounds
Main
gear
hinge bolts
250-800 inch-pounds
Main
wheel
halves
Goodyear
140
inch-pounds
Cleveland
150
inch-pounds
Nose
wheel
halves
Goodyear
83 inch-pounds
Cleveland 90 inch-pounds
Brake attach bolts 50 inch-pounds
When torque wrench adapters are used, compensation must be
made for the extra leverage
gained;
new indicator
readings
must be
calculated before
the wrench
is
used.
To figure the desired lower readings
which
will
4-8
C4