P92 Eaglet
Flight Manual
Revision Date: 12-14-2007
Revision Number: 1.00
Doc n° 27-13-100-00
26
SECTION 2
OPERATING LIMITATIONS
2 Introduction
Section 3 includes operating limitations, instrument markings, and basic placards necessary for safe operation of the P92
Eaglet, its engine, standard systems and standard equipment.
2.1.1
Airspeed Limitations
Airspeed limitations and their operational significance are shown below:
SPEED
KIAS
REMARKS
V
NE
Never exceed speed
134
Never exceed this speed in any operation
V
NO
Maximum Structural
Cruising Speed
106
Never exceed this speed unless in smooth air, and then only with caution
V
A
Maneuvering speed
93
Do not make full or abrupt control movements above this speed as this may
cause stress in excess of limit load factor
V
FE
Maximum flap
extended speed
68
Never exceed this speed for any given flap setting
V
H
Maximum speed
120
Maximum speed in level flight at max continuous power (MSL)
V
X
Best Angle Climb
60
The speed which results in the greatest gain of altitude in a given horizontal
distance
V
Y
Best Rate Climb
68
The speed which results in the greatest gain of altitude in a given time
2.1.2
Airspeed Indicator Markings
Airspeed indicator markings and their color code are explained in the following table:
MARKING
KIAS
SIGNIFICANCE
White arc
43 – 68
Flap Operating Range (lower limit is 1.1 V
SO
, at maximum weight and upper
limit is maximum speed permissible with full flaps)
Green arc
48 – 106
Normal Operating Range (lower limit is 1.1 V
S1
at maximum weight and flaps
at 0° and upper limit is maximum structural speed V
NO
)
Yellow arc
106 – 134
Operations must be conducted with caution and only in smooth air
Red line
134
Maximum speed for all operations
