Textron Cessna 172R - Page 202

SECTION
6
WEIGHT
&
BALANCE
/
EQUIPMENT
LIST
CESSNA
MODEL
172R
ITEM
DESCRIPTION
WEIGHT
AND
MOMENT
TABULATION
SAMPLE
AIRPLANE
YOUR
AIRPLANE
Weight
(lbs.)
Moment
(Lb-ins.
/1000)
Weight
(lbs.)
Moment
(Lb-ins.
/1000)
1.
Basic
Empty
Weight
(Use
the
data
pertaining
to
your
airplane
as
it
is
presently
equipped.
Includes unusable
fuel
and
full
oil)
1639
64.4
2.
Usable Fuel
(At
6
Lbs./Gal.)
53
Gallons
Maximum
35
Gallons
(To
reduced
fuel
indicator
tab)
210
10.1
3.
Pilot
and
Front
Passenger
(Station
34
to
46)
340
12.6
4.
Rear
Passengers
220
16.0
5.
*Baggage
Area
1
(Station
82
to
108;
120
Lbs.
Max.)
48
3.4
6.
*Baggage
Area
2
(Station
108
to
142;
50
Lbs.
Max.)
7.
RAMP
WEIGHT
AND
MOMENT
(add
columns)
2457
106.5
8.
Fuel allowance
for
engine
start,
taxi
and
runup
-7.0
-0.3
9.
TAKEOFF
WEIGHT
AND
MOMENT
(Subtract
Step
8
from
Step
7)
2450
106.2
|
1
0.
Locate
this
point
(2450
at
1
06.2)
on
the
Center
of
Gravity
Moment
Envelope,
and
since this
point
falls
within
the
envelope,
the
loading
is
acceptable.
*
The
maximum
allowable
combined
weight
capacity
for
baggage
areas
1
and
2
is
120
pounds.
Figure
6-5.
Sample
Loading
Problem
(Sheet
1
of
2)
6-12
Feb
28/00
All manuals and user guides at all-guides.com