Flap Removal; Flap Installation; Removing And Installing The Flap Motor; Visual Spar Cap Inspection - Beechcraft TRAVEL AIR 95 Shop Manual

THIS
ILLUSTRATION
REPRESENTS
A
TYPICAL SECTION OF
THE SPAR
CAP
AREAS TO BE INSPECTED FOR
INDICATORS OF
POSSIBLE CORROSION.
BOX SECTION SKIN
THE INDICATORS ARE
ALL SHOWN
IN ONE
AREA
AND ARE EXAGGERATED FOR CLARITY
ANY ONE OR ANY COMBlNATION OF THE
o INDICATORS
ARE CAUSE FOR FURTHER
SPAR CAP
NVESTIGATION.
CRACKS
o
RAISED AREAS
LEADING o
EDGE
SKIN
THIS
RivET
PATTERN
WILL
VARY
PAINT BLISTER ON DIFFERENT
MODELS
Visual
Spar Cap
Inspection
Figure 4-1E
NOTE
FLAP INSTALLATION
Uneven or raised
areas
on the spar caps may be a. Hold
the
flap in
position and
install
the
flap
detected by
sliding
the fingers over the surface, rollers
and the
bolts in
the
flap
track bracket.
by
moving a straight
edge over the
surface
or
by sighting
down the length
of the spar cap
surface. NOTE
Install the flap
track rollers
(four
rollers per
If
unusual conditions are encountered
that cannot
be
flap
and two rollers per track)
in
the
flap
track
resolved
locally, contact the Commercial
Service
brackets
with
the flanges facing
each other.
Department of Beech Aircraft Corporation for evaluation Use only the
wide
flanged
rollers in the aft
and
determination of corrective action that may be locations.
required.
b. Connect the bonding cable
and
install
the
bolt in
FLAP REMOVAL
the flap actuating
arm.
a.
Remove the bolt from the flap
actuating
arm.
REMOVING AND INSTALLING THE FLAP MOTOR
b. Remove the bonding cables from the flap tracks.
c. Remove the
bolts
from the flap track bracket
and
a. Remove the cabin front seats.
remove the
flap.
b.
Remove the access cover.
C4
4-6G