SOLOY TURBINE PAC SECTION 2
POHS CESSNA T206H/206H LIMITATIONS
2-3
F.A.A. Approved May 23, 2003
INTRODUCTION
This Supplement contains the information required to be furnished
to the pilot by FAR Part 23 and must be carried in the airplane during flight
operations. It also provides additional information, which will assist in
operating the airplane at its maximum efficiency.
Compliance with the limitations section is mandatory.
AIRSPEED LIMITATIONS
Airspeed limitations and their operational significance are shown in
Figure 2-1.
V
MO
Maximum operating
speed:
Do not exceed in any
operation.
V
A
Maneuvering speed:
3600 pounds
2950 pounds
2300 pounds
Do not make full or
abrupt control
movements above
this speed.
V
FE
Maximum flap
extended speed:
to 10 flaps
10 to 40 flaps
Do not exceed these
speeds with the given
flap setting.
Maximum
window open speed:
Do not exceed this
speed with window
open.
Figure 2-1. Airspeed Limitations