Mooney M20K - Page 49

SERVICE
AND
MAINTENANCE
MANUAL M20K
MOONEY
AIRCRAFT CORPORATION
12.
Record
weights
and measurements
and
compute
the basic
weight
and
CG
as
follows:
LC/G
LM/R-5
-LM
a.
CG
Forward
of
Main Wheels
LBS
X IN.
s
LBS.
IN.
Weight
Nose
Distance Between
Total
Weight
of
CG
Forward
of
Main
8
Nose Wheel
Aircraft
Main
Wheels
Axel
Centers
OYN)
(LMIN)
D~VT)
(LM)
b.
CG
Aft of
Datum
(Station
O)
IN.
5
IN.
IN.
IN.
Distance
from center
Distance
from Result of
computation
CG
(FUS
STA)
Nose
Gear
Trunnion
to
Nose
Gear
Above
(a.)
Distance
Aft
of
Center of
Main
Wheel
Trunnion
to
Datum
(Empty
Axles
(Horizontal)
Datum
Weight
CG)
(LMIR)
(CONSTANT)
(LM) (LC/G)
NOTE:
Empty
weight
includes
unusable
fuel and full oil
(8 Qts.)
and is
computed
with
gear
down
and
flaps
up.
REF.POINT
REFERENCE
LEVEL
REF.
(NOSE
GEAR
DANH<STA~O)
(LEVEUNG
SCRRJS>
TRUNNICIN
STA, -5)
1
1
I
1
M20K
r
_I
I
MEASUREMENTS
Lm/n
Wn Wr
LM/R
INCHES/CM
WI
LM/N
INCHES/CM
WEIGHT AND BALANCE DIAGRAM
FIGURE
8
2
8-00-01
OLDWILLWAYNE