Cessna P206A-E - SECTION 6. WEIGHT AND BALANCE; SAMPLE LOADING PROBLEM

ISSUE DATE:
PO Box 2119
265 Shannon Lane
Priest River ID 83856
Page
27 of 38
8/23/10
INCORPORATED
FILE NO.
REVISION
DATE
TITLE: Supplemental Airplane Flight Manual
A-10060
03/04/15
SUBTITLE:
Cessna 206 on Model 3400 Floats
REVISION: D
FAA Approved
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.
Arm
Weight Moment
Arm Weight Moment
Inches Pounds lb.-ins./1000 Inches Pounds lb.-ins./1000
(1) Basic Empty Weight 38.94 2660 103.58
(2) OIL -20.8 17 -0.35
(3) Usable Fuel (MAX 65) 47 gallons 48 283 13.58
(4) Pi lot and Copilot (STA. 34 TO 48) 37 340 12.58
(5) PASSENGERS + BAGGAGE
CENTER Row Passengers (STA. 69 TO 79) 70 340 23.80
AFT Row Passengers (STA. 92 TO 100) 100 0 0.00
AFT BAGGAGE (STA. 109 TO 145; 120LBS MAX
)
127 50 6.35
(6) NO SEATS CARGO AREAS
CARGO "A" (STA. 10 TO 50) 37
0 0.00
CARGO "B" (STA. 50 TO 84) 78 0 0.00
CARGO "C" (STA. 84 TO 109)
105 0 0.00
CARGO "D" (STA. 109 TO 145)
127 0
0.00
(7) OPTIONAL CARGO POD (STA. 10 TO 85) 47
0 0.00
(300 LBS. MAX)
(8) FLOAT CARGO LOCKERS (STA. 15 TO 51) 32.4 50 1.62
(100LBS. MAX EACH SIDE)
(9) Ramp CG, Weight And Moment 43.1 3740 161.2
(10) Available useful Load @ 3744 GW 4
(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.
SAMPLE AIRPLANE
YOUR AIRPLANE
SAMPLE LOADING PROBLEM
CESSNA 206 WITH AEROCET AMPHIBIOUS 3400 SERIES FLOATS