Mooney M20B - Page 55

Supplement
to
figares 14, 15,
16, 17,
and 18.
i-
t
CONTR~L
TRAVELS
AND
RIGGING
INFORMATION
FOR MOONEY
M
iOB
WING
FLAPS
Measured
from
ts~:ng
chord with
travel
board at
wing
station
147.75.
Take
off
position
O"
Tolerance
=t
1"
approach
and
landing
position
214/2"
Tolerance
1"
AII~ERONS
~asured
from
aileron chord
with
aileron in
the
static
position
with
travel board
at
wing
station 147.75.
Down
´•travel,
both
ailerons
80
Tolerance
1"
Uptrav’el,
eitheraileron,
may
vary
from
123/2"
to
17"
with
no
additional
tolerance.
Static
pcsition
0"
to
2"
down.
RUDDER
AND ~OSEWHEEL
Measured
from
fm
chord
with
travel
board
at
fin
station
13.5.
Left
travel
18"
Tolerance
=t
1"
Right
tra-irel
’18"
Tolerance
-t-
I"
With
rudder
pedals
in
neutral
and
with trim
assist
unit
(p/n
7038)
at
zero
spring
f’
travel,
rudder and nosewheel
settings
are
approximately
1"
right.
~easured with thrust
line
level,
(Door
sill
level).
Maximum
positive setting
I" to
21/20
negative
setting
31/2"
to
4Y20
ELEVATORS
Measured
from
stabilizer
chord with
travel
board
at stabilizer
station
16.0 and
with
stabilizer
at
O"
thrust
line.
’CTp
´•trave1’24"
Tolerance
-F-
1"
Down
travel
104/20
Tolerance
I-e
1"
ELEVATOR
TRIM
ASSIST
UNITS
With
stabilizer
set
at
maximum
ne,6ative
setting
to
thrust
line
44/2"),
adjust
trim
assist
units
(p/n
7038-1)
for elevator
up
angle
of
--18"
to --20" at
the
zero
spring
travel
position.
With the stabilizer
moved to
the
maximum
positive
setting
(j14/2’),
the
position
of
the
~elevators
at
the
zero
spring
travel
position
of
the
trim
assist
units
shouid
be
from
O"
to
+3"
down.
kIILOWABLE
FdEE PLAY
LIMITS
Fore
and
aft
allowable
movement
at
stabilizer
tip:
.12"
Vertical.allowable
movement
at
stabilizer
tip:
Vertical
allowable
movement
at
rudder
trailing
edge:
.08"
_AQ~
OLDWILLWAYNE