Upper Forward Wing Bolt Installation - Beechcraft TRAVEL AIR 95 Shop Manual

**95-110025-1
WASHER
(CHECK FOR A SMOOTH
105090A032-10K
WASHER
*95-110021
WASHER
(POSITION
OUTER RADiUS AND WITH COUNTERSINK
TOWARDS
POSITION RADIUS TOWARD
BOLT
HEAD)
FITTING)
12NB126
NUT
NAS
152-3T M BOLT
OR
131790-1
BOLT
DRAIN
HOLE
FUSELAGE
FITTING
WING
FITT1NG
***
NAS143-12
WASHER
*NAS143-12
WASHER
WET
BOLT
TORQUE: 2480 TO
2600
INCH-POUNDS. COAT THE COMPLETE BOLT,
NUT.
WASHERS, WING FITTING
BOLT
BORES, AND EXPOSED
BOLT
THREADS WITH MIL-C-16173,
GRADE
2
CORROSION PREVENTIVE COMPOUND.
*TD-3
thru
TD-24
**TD-2. TD-25
thru TD-721
***AN
NAS143-12
WASHER MAY BE USED BETWEEN THE NUT AND THE
NAS143-12 OR 95-110025-
1
WASHER
TO PROVIDE BOLT
GRIP ADJUSTMENT.
95-31-68
Figure 4-1. Upper Forward Wing Bolt Installation
44