g.
THRU AIRCRAFT SERIALS 15072629, F15000738,
A15000277
AND
FA15000132 WHEN NOT MODIFIED
IN ACCORDANCE WITH
SK150-37
AND
WHEN NOT
MODIFIED IN ACCORDANCE WITH FIGURE
7-2,
SHEET
3.
(Refer
to
figure
7-2,
sheet
1.)
Screw
actuating
tube
(5) IN
toward
transmission
(8)
by
hand
to
its
shortest
length
(flaps
full
up
position).
Loosen
setscrew
(6)
securing
actuating
tube
(5)
to
nut
and
ball
assembly,
hold
nut
and
ball
assembly
so
that
it
will
not
move,
hold
RIGHT
flap
in
the
full
UP
position
and
adjust
actuating
tube
(5) IN
or
OUT
as
necessary
to
align
with
attachment
hole
in
drive
pulley
(14).
Tighten
setscrew
(6)
and
secure
tube
to
drive
pulley
with
bolt
(21).
h.
THRU
AIRCRAFT
SERIALS 15072629, F15000738,
A15000277
AND
FA15000132 WHEN MODIFIED IN
ACCORDANCE WITH
SK150-37
AND
WHEN NOT
MODIFIED IN ACCORDANCE WITH FIGURE
7-2,
SHEET
3.
(Refer
to
figure
7-2,
sheet
2.)
Operate
flap
motor
until
actuating
tube
(n)
is
IN
to
its
shortest
length
(flaps
full up
position).
Hold
RIGHT
flap
in
the
full
UP
position
and
check
actuating
tube
(5)
to
drive
pulley
(14)
attachment
holes
for
alignment.
Operate
flap
motor
toward
the
DOWN pOSition
until
bolt
(21)
can
be
installed
freely.
Loosen
setscrew
(6)
and
rotate
nut
and
ball
assembly
IN
against
transmission
(8).
Tighten
setscrew
(6)
and
bolt
(21).
i.
BEGINNING WITH
AIRCRAFT
SERIALS 15072630,
F15000739, A15000278, FA15000133
AND
ALL
AIR-
CRAFT
MODIFIED IN ACCORDANCE WITH FIGURE
7-2,
SHEET
3.
(Refer
to
figure
7-2,
sheets
2
and
3.)
Screw
actuating
tube
(5) IN
toward
transmission
(8)
by
hand
to
. 12±. 05
inches
between
switch
actuating
collar
(30)
and
transmission
as
illustrated
in
figure
7-2,
VIEW
B-B.
Loosen
setscrew
(6)
securing
ac-
tuating
tube
(5)
to
switch
actuating
collar
(30),
hold
actuating
collar
to
maintain.
12±.
05",
hold
RIGHT
flap
in
the
full
UP
position
and
adjust
actuating
tube
(5) IN
or
OUT
as
necessary
to
align
with
attachment
hole
in
drive
pulley
(14).
Tighten
setscrew
(6)
in
accordance
with
procedures
outlined
in
the following
note
and
secure
tube
to
drive
pulley
with
bolt
(21).
NOTE
Thru
Aircraft
Serials
15075326, F15001073,
A1500464
and
FA1500236:
Tighten
setscrew
(6).
Aircraft
Serials
1507532
thru
15075740,
F15001074
thru
F15001143, A1500465
thru
A1500499, FA1500237
thru
FA1500261:
Apply
grade
CV
sealant
to
setscrew
(6)
threads
and
torque
to 45
lb-in.
Beginning
with
Aircraft
Serials
15075741,
FI5001144,
A1500500, FA1500262: Apply
grade
CV
sealant
to
setscrew
(6)
threads
and
torque
to 60
lb-in.
If
actuating
tube
(5)
is
too long to
allow
attachment
to
drive
pulley
after
completion
of
steps
"g",
"h"
and
"i",
proceed
to
step
"j
".
j.
Disconnect
push-pull
rod
(15)
at
drive
pulley
(14),
then
connect
actuating
tube
(5)
to
drive
pulley.
k.
Manually
hold
RIGHT flap
in
full
UP
pOSition
and
readjust
push-pull
rod
(15)
to
align
with
attachment
hole
in
drive
pulley.
Connect
push-pull
rod
and
•
tighten
locknuts
or
castellated
nuts
and
install
7-10
Change
2
cotter
pins.
I
NOTE
The
right
flap
and
actuator
must
be
correctly
rigged
before
cables
and
left
flap
can
be
rig-
ged.
1. THRU
AIRCRAFT
SERIALS 15072629, F15000738,
A15000277
AND FA15000132 WHEN NOT MODIFIED
IN ACCORDANCE WITH FIGURE
7-2,
SHEET
3.
After
completion
of
step
"k",
with
flap
in
full
UP
position,
adjust
up-limit
switch
clamp
(7)
to
operate
switch
(3)
and
shut-off
electrical
power
to
motor
at
this
pOSition.
m.
BEGINNING WITH
AIRCRAFT
SERIALS 15072630,
F15000739, A15000278
AND FA15000133 AND
ALL
AIRCRAFT
MODIFIED IN ACCORDANCE WITH
FIGURE
7-2,
SHEET
3.
After
completion
of
step
"k",
with
flaps
in
full
UP
position,
loosen
setscrew
(27)
and
slide
up-limit
switch
adjustment
block
(28)
on
support
(31)
to
operate
switch
and
shut-off
electrical
power
to
motor
at
this
position.
Tighten
setscrew
(27).
n.
Manually
hold
LEFT
flap
full
UP
and
connect
control
cables
at
turnbuckles
(index
4,
figure
7-1).
Remove
reference
tags
previously
installed
in
step
"f"
as
turnbuckles
are
connected.
o.
With
flaps
full
UP,
adjust
turnbuckles
to
obtain
30±10
pounds
tension
on
cables.
Adjust
retract
cable
(19)
first.
NOTE
Ensure
cables
are
pOSitioned
in
pulley
grooves
and
cable
ends
are
pOSitioned
correctly
at
drive
pulleys
before
tightening
turnbuckles.
p.
Disconnect
push-pull
rod
at
left
drive
pulley.
Run
motor
to
extend
flaps
approximately
20
0
and
check
tension
on
each
flap
cable.
If
necessary,
re-
adjust
turnbuckles
to
maintain
30±10
pounds
tension
on
each
cable
and
safety
turnbuckles.
q.
Fully
retract
right
flap.
Manually
hold
left
flap
in
full
up
position
and
readjust
push-pull
rod
to
align
with
attaching
hole
in
drive
pulley.
Connect
push-
pull
rod
and
tighten
locknuts
or
castellated
nuts
I
and
install
cotter
pins.
NOTE
An
inclinometer
for
measuring
control
sur-
face
travel
is
available
from
the
Cessna
Service
Parts
Center.
Refer
to
figure
6-4.
r.
Mount
an
inclinometer
on
one
flap
and
adjust
to
0
0
•
Extend
flaps
and
check
down
angle
as
follows:
s.
THRU
AIRCRAFT
SERIALS 15072629, F15000738,
A15000277
AND FA15000132 WHEN NOT MODIFIED
IN ACCORDANCE WITH FIGURE
7-2,
SHEET
3.
After
completion
of
steps
"a"
thru
"r",
the
flap
down
angle
Should
be
as
specified
in
figure
1-1.
Repeat
down
angle
check
on
opposite
flap.
t.
BEGINNING WITH
AIRCRAFT
SERIALS 15072630,
F15000739, A15000278, FA15000133
AND
ALL
AIR-
CRAFT
MODIFIED IN ACCORDANCE WITH FIGURE
7-
2,
SHEET
3.
After
completion
of
steps
"a"
thru
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