Mooney M20R - Weight and Balance Diagram

SERVICE AND MAINTENANCE MANUAL
M20R
MOONEY
AIRCRAFT
CORPORATION
13. Record
weights
and
measurements
and
compute
the basic
weight
and CG
as
follows:
LCIG
LM/R
-13
LNI
a.
CG Forward of Main Wheels
LBS
X
IN.
O
LBS.
IN.
Weight
Nose
Distance
Between
Total
Weight
of
CG Forward of
Main
3
Nose
Wheel
Aircraft
Main
Wheels
Axle
Centers
O/VN)
(LM/N)
<wr,
(LM)
b.
CG
Aft of Datum
(Station O)
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
irunnion
to
Datum
(Empty
Axles
(Horizontal)
Datum
Weight CG)
(LMIR)
(CONSTANT)
(LM)
(LC/G)
NOTE:
Empty weight
includes
unusable
fuel
and full
oili(8
Qts.)
and is
computed
with
gear
down
and
flaps
up.
REF,PDINT
REf~ERENCE
LEVEL
REF,
<NOSE
GEAR DATUM(STA,O)
(LEVELING
SCREWS>
TRUNNION
STA,
-13~
1
1CI_3
I
c/g-´•3-Lm
1/ I
MEASUREMENTS
Lm/r
LM/R
Lm/n
INCHES/CM
Wn
Wr
WI
INCHES/CM
WEIGHT
AND
BALANCE
DIAGRAM
FIGURE 8-2
8-00-01
REV. 10-98
Island Enterprises