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
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