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Cessna U206 - SECTION 2. LIMITATIONS; CENTER OF GRAVITY AND WEIGHT LIMITS; AIRSPEED AND MANEUVER LIMITS

Cessna U206
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ISSUE DATE:
PO Box 2119
265 Shannon Lane
Priest River ID 83856
Page
5 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 2. LIMITATIONS
CENTER OF GRAVITY LIMITS:
Center of Gravity Range: (inches aft of reference datum –front face of
firewall)
(+42.1) to (+47.4) at 3744 lbs. Maximum G.W.
(+36.5) to (+47.4) at 2600 lbs. or less with a straight line
variation between points given.
WEIGHT LIMITS:
Maximum Ramp or Dock: 3755 lbs.
Maximum Take-off Floats: 3744 lbs.
Maximum Landing Floats: 3661 lbs.
Maximum Take-off Wheels: 3735 lbs.
Maximum Landing Wheels: 3550 lbs.
Maximum Weight in Baggage Compartment: NO CHANGE
Maximum Weight in Float Baggage Compartment: 100 lbs. each
AIRSPEED LIMITS:
MPH
CAS
MPH
IAS

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