SOLOY TURBINE PAC
SECTION 2
POHS CESSNA T206H/206H
LIMITATIONS
2-9
F.A.A. Approved
November 14, 2014
CENTER OF GRAVITY LIMITS
Center of Gravity Range:
Forward:
33.0 inches aft of datum at 2500 lbs.
or less, with straight line variation to
42.5 inches aft of datum at 3600 lbs.
Aft:
49.7 inches aft of datum at all
weights.
Reference Datum:
Lower portion of front face of
firewall.
MANEUVER LIMITS
This airplane is certificated in the normal category. The normal
category is applicable to aircraft intended for non-aerobatic operations.
These include any maneuvers incidental to normal flying, stalls (except whip
stalls), lazy eights, chandelles, and turns in which the angle of bank is not
more than 60
.
Aerobatic maneuvers, including spins, are not approved.
FLIGHT LOAD FACTOR LIMITS
Flight Load Factors:
*Flaps Up:
+3.8g, -1.52g
*Flaps Down:
+2.0g
*The design load factors are 150% of the above, and in all
cases, the structure meets or exceeds design loads.
KINDS OF OPERATION LIMITS
Flight into known icing conditions is prohibited.
The systems mentioned below must be activated for flight or
ground operation in the following conditions:
A. Engine inlet anti-ice must be on in visible moisture at an OAT
of 5
C (41
F) and below.
B. Engine alternate air must be on in visible moisture at an OAT
of 1
C (34
F) and below.
UNCONTROLLED
COPY