Piper Arrow PA-28R-201 Pilot Operating Handbook page 159

PA-28R-201, ARROW
6.7 WEIGHT
AND
(a) Add the weight of all items to be loaded to the basic empty weight.
(b) Use the Loading Graph
allitems to be carriedin the airplane.
(c) Add the moment
moment.
(d) Divide the total moment
location.
(e) By using the figures of item (a) and item (d) (above), locate a point
on the C.G. range and weight graph (Figure 6-15). If the
within the C.G. envelope, the loading meets the weight and balance
requirements.
Basic Empty Weight
Pilotand Front Passenger
Passengers (Rear Seats)
Fuel (72 Gallons Maximum)
Baggage (200 Lbs. Maximum)
Weight (2758 Lbs.
Ramp
Maximum)
Fuel Allowance For Engine
Start, Taxi, and Run-Up
due to Retraction
Moment
of Landing Gear
Takeoff Weight (2750 Lbs.
Maximum)
The center of gravity (C.G.) of this sample loading problem is at 89.04 inches
aftof the datum line.Locate this point (89.04) on the C.G. range and weight
graph. Since this point falls within the weight
meets the weight and balance requirements.
iT IS THE
RESPONSIBILITY
THAT
TO ENSURE
LOADING
SAMPLE
12, 1995
ISSUED: JULY
HB-PQY, Page: 6-9-(0)
BALANCE DETERMNATJON
(Figure 6-13) to determine the moment
of allitems to be loaded to the basic empty weight
by the total weight to determine the C.G.
OF THE
THE AIRPLANE IS LOADED
PROBLEM
Figure 6-9
WEIGHT AND
FOR
FLIGHT
Arm
Datum
Weight
(Lbs) (Inches)
1890 84.8
340.0
80.5
170.0 118.1
294 95.0
64 142.8
2758 88.76
-8
95.0
2750 89.04
C,G. envelope, this loading
AND AIRCRAFT
PILOT
PROPERLY.
(NORMAL CATEGORY)
REPORT:
Issued: JULY 12, 1995
SECTION 6
BALANCE
of
point falls
Aft
Moment
(In-Lbs)
160272
27370
20077
27930
9139
244788
-760
819
244847
OWNER
VB-1612
dc-Q
6-9