Section 6. Weight And Balance - Cessna 206 Series Supplemental Manual

ISSUE DATE:
8/23/10
REVISION
TITLE:
DATE
SUBTITLE:
03/04/15

SECTION 6. WEIGHT AND BALANCE:

The airplane equipped with Aerocet 3400 amphibious seaplane floats must
be loaded in accordance with the limitations in Section 2. These are shown
as an aircraft weight/moment envelope or an aircraft weight versus c.g.
location chart.
Note: It is the responsibility of the airplane owner and pilot to
insure that the airplane is loaded properly.
SAMPLE LOADING PROBLEM
(1) Basic Empty Weight
(2) OIL
(3) Usable Fuel (MAX 65)
(4) Pilot and Copilot (STA. 34 TO 48)
(5) PASSENGERS + BAGGAGE
CENTER Row Passengers (STA. 69 TO 79)
AFT Row Passengers (STA. 92 TO 100)
AFT BAGGAGE (STA. 109 TO 145; 120LBS MAX )
(6) NO SEATS CARGO AREAS
CARGO "A" (STA. 10 TO 50)
CARGO "B" (STA. 50 TO 84)
CARGO "C" (STA. 84 TO 109)
CARGO "D" (STA. 109 TO 145)
(7) OPTIONAL CARGO POD (STA. 10 TO 85)
(300 LBS. MAX)
(8) FLOAT CARGO LOCKERS (STA. 15 TO 51)
(100LBS. MAX EACH SIDE)
(9) Ramp CG, Weight And Moment
(10) Available useful Load @ 3744 GW
(11) Located the (9) point (3740 @ 161.2) on the Center of Gravity Moment Envelope, and since this point
falls within the evelope, the loading is acceptable.
* Maximum allowable cargo loads will be determined by the type and number of tie-downs used, as well as
by the airplane weight and C.G. limitation. Floor loading must not exceed 200lbs. per square foot.
FAA Approved
INCORPORATED
Supplemental Airplane Flight Manual
Cessna 206 on Model 3400 Floats
CESSNA 206 WITH AEROCET AMPHIBIOUS 3400 SERIES FLOATS
Arm
Inches
38.94
-20.8
47 gallons 48
37
70
100
127
37
78
105
127
47
32.4
43.1
PO Box 2119
265 Shannon Lane
Priest River ID 83856
SAMPLE AIRPLANE
Weight Moment
Pounds lb.-ins./1000
2660 103.58
17 -0.35
283 13.58
340 12.58
340 23.80
0 0.00
50 6.35
0 0.00
0 0.00
0 0.00
0 0.00
0 0.00
50 1.62
3740 161.2
4
Page
27 of 38
FILE NO.
A-10060
REVISION: D
YOUR AIRPLANE
Arm Weight Moment
Inches Pounds lb.-ins./1000