Piper PA-32RT-300T User Manual

LANCE
II SERVICE
MANUAL
5-16.
STABILATOR
TRIM
CONTROLS.
5-17.
REMOVAL
OF STABILATOR
TRIM
ASSEMBLY
(FORWARD).
(Refer
to Figure
5-9.)
a.
To remove
the trim
control
wheel
assembly
and/or
the trim
control
cables,
first
remove
the panel
to
the aft
section
of the
airplane.
b.
If the
aft trim
cable
(12)
is not
to be
removed,
block
the
cables
at the
pulleys
(35)
in
the
upper
aft section
of the
fuselage
to prevent
them
from
unwrapping
from
the
trim
drum.
(Refer
to Figure
5-8.)
c.
Loosen
the cables
if the
trim
control
wheel
(1) is to
be removed
or
disconnect
if
the
cables
are
to be
removed.
Do this
at the
trim
cable turnbuckles
(10
and 11)
in the
aft
section
of
the fuselage.
d.
The control
wheel
(1)
with drum
(3)
may be
removed
by
the following
procedure:
1. Remove
the control
wheel
cover
by removing
the
cover
attaching
screws.
2.
The wheel
assembly
may
be removed
from
its mounting
brackets
(4)
by
removing
nut,
washer
and
bolt (7)
that secures
the
wheel
between
the
brackets.
Draw
the
wheel
from the
brackets.
Use
caution
not to damage
trim indicator
wire
(2).
3. Unwrap
the
left cable
(9) from
the drum.
4.
The wheel
and drum
are joined by
a push fit,
separate these
two items
with their
center
bushing
and unwrap
the right
cable
(8).
5. Tie the
cables
forward
to prevent
them
from slipping
back
into the
floor tunnel.
e.
The trim
control cables
(8 and 9)
may be removed
by the
following
procedure:
1. Remove
the
center seats,
and
the pilot
and rear
seats if desired.
2. Remove
the seat
belts attached
to the
forward floor
tunnel
by removing
attachment
nuts,
washers
and bolts.
3. Remove
the heater
deflectors
from each
side of the
aft end of
the forward
floor
tunnel
by sliding
the
deflector sideways
and
releasing
the retainer
spring.
4.
Unfasten the carpet
from the aft
portion of the forward
floor tunnel
and lay it
forward.
5. Remove
the tunnel
cover located
between
the trim control
wheel
and the spar
cover by
removing
attachment
screws.
6. Remove
the cable pulleys
(6) located in
the forward tunnel
by removing
the
cotter
pin,
washer
and clevis
pin
(5).
7. Remove
the floor panel
aft of the main
spar by removing
the panel attachment
screws
and seat belt
attachments.
Lift the panel
and remove from
airplane.
8. Remove the cable rub
blocks (39) located in the floor opening
on the aft side of
the main
spar by removing
the
block attachment
screws.
9. Remove the trim
plate located
on top of the forward
end of the aft
floor tunnel.
10. Remove
the carpet from the
aft floor tunnel.
11. Remove
the cover
plate from the
top of the aft floor
tunnel by removing
attachment
screws.
12. Remove
the cable
guard (38)
from the
underside
of the trim
cable pulleys
(36)
located in the
forward area of
the aft floor tunnel
by removing a
tinnerman nut and
withdrawing
the cable
guard.
13. Remove
the cable
guard plate
(33) from
the underside
of the
pulley cluster
(34)
located in the
aft area of the floor
tunnel by removing
the plate
attachment screws.
14.
Remove the
cable guard
from the
cable pulleys
(13) in
the aft lower
section of
the
fuselage forward of the
cable turnbuckles (10 and
11 ).
15. With
the cables disconnected
from the
trim control wheel,
draw the cable(s)
through the
floor tunnel.
Issued:
1/3/78
SURFACE
CONTROLS
1G9

Piper PA-32RT-300T Specifications

General

Brand	Piper
Model	PA-32RT-300T
Category	Aircrafts
Language	English