Mooney M20M - Page 44

SERVICE
AND
MAINTENANCE
MANUAL
M20M
MOONEY
AIRCRAFT
CORPORATION
12.
Record
weights
and
measurements
and
compute
the
basic
weight
and
CG
as
follows:
LC/G
LM/R
-13
-LM
a.
CG
Forward
of
Main Wheels
LBS
X
IN.
i
LBS.
1N.
Weight
Nose
Distance
Between
Total
Weight
of
CG
Forward
of
Main
Nose
Wheel
Aircraft
Main
Wheels
Axel Centers
OIVN)
(LM/N)
ONT)
(Lhn)
b.
CG
Aft of Datum
(Station
O)
IN.
131N.
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
(Emptr
Axles
(Horizontal)
Datum
Weight
CG)
(LM/R)
(CONSTANT)
(LM)
(LC/G)
NOTE:
REF,POINT
REFERENCE LEVEL REF,
(NOSE
GEAR
DATUM(STA,O> (LEVELING SCREWS>
TRUNNION
STA,
-13>
I
1~
I
I
MEASUREMENTS
C/
/r
Lm/n
LM/R
INCHES/CM
Wn
Wr
WI
LM/N
INCHES/CM
Nose Jack Point
Sta.
-5.866
Main
Jack Point
Sta.
56.658
WEIGHT AND
BALANCE DIAGRAM FIGURE
8-2
8-00-01
4-99
OLDWILLWAYNE