Cessna T188C - Page 71

MODEL 188 &T188 SERIES SERVICE MANUAL
jacent to the seat.
This control handle has a MANUAL
3-29. BAGGAGE
AREA. The area aft of the firewall
and AUTOMATIC
position. In the AUTOMATIC
posi- and forward
of the hopper on airplane Serials
thru
tion, the reel allows slow movement of the pilot, locking 18800832 may be equipped with a removable floor and
only against sudden movement. Locking, automatically tie-downs. Beginning with airplane Serial 18800833
moves the control to the MANUAL
position and all
the equipment installation in the
area does not permit
movement is restricted. After the emergency, this the floor installation.
handle may again be moved to the AUTOMATIC posi-
tion. Beginning with Airplane serial 18800833 a new 3-30. BAGGAGE DOORS. (See figure 3-4.)
1.5 g's
inertia reel may
be installed in
the airplane.
This
reel does not incorporate
the manual locking and
release 3-31. DESCRIPTION.
The baggage doors, located
aft
handle. Both
systems require no lubrication
or adjustment. of the firewall
on either side of the fuselage are
hinged
Shoulder
harnesses
should be replaced
in accordance
at the
top to swing up
for access to forward
hopper area
with the provisions in Section 2. and baggage area prior to airplane Serial 18800833.
3-27.
CANOPY PADDING.
(See
figure 3-8.) The
3-32.
REMOVAL
AND INSTALLATION.
canopy padding consists of a
1/4 inch black ensolite cover
a. Unlock the wing stud fasteners
and remove the
on the
crash pad, also urethane bumper
pads bonded to fasteners
common to the upper half
of door hinge.
the tubular structure above
the cabin door, down
the b. Remove
door assembly.
corner
doorposts, across the tubular
structure behind c. Install
by reversing above procedures.
When in-
the pilots head, and across the
lower door seal.
stalling a new door, some trimming
to fit the opening
and some forming of the door edge to fair with the
3-28. WIRE
CUTTERS AND CABLE
DEFLECTORS. fuselage may
be necessary thru airplane Serial
188-
(See figure 3-8.) Wire cutter blades are installed on the 00832. Beginning with airplane Serial 1880833 these
landing gear strutsand in front
of the windshield. Deflector
doors are bonded assembly and
forming the door edge
cable
is installed from the back of the
canopy to a fitting at is not permissible,
as it could cause material
separation.
the forward
upper end
of the fin thru
airplane Serial
18801374.
Beginning with airplane
Serial 18801375 the 3-33.
SEAT RAIL INSPECTION. A
special inspec-
deflector
cable is attached
to the
upper end
of the
tion
of seat
rails should
be conducted
each
50 hours.
windshield cutter
blade, which is extended
to the top of the See figure
309 for inspection procedures.
canopy.
The cable tension
is set at 15
to 20 pounds tension
on either installation.
Temporary Revision 2 - Oct 3/94 3-17