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Tecnam P92 Eaglet - Approved Maneuvers; Flight Crew; Kinds of Operations; Maneuvering Load Factor Limits

Tecnam P92 Eaglet
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P92 Eaglet
Flight Manual
Revision Date: 12-14-2007
Revision Number: 1.00
Doc n° 27-13-100-00
30
2.1.17 Approved Maneuvers
This aircraft is intended for non-aerobatic operation only. Non-aerobatic operation includes:
Any maneuver pertaining to “normal” flight
Stalls (except whip stalls)
Lazy eights
Chandelles
Turns in which the angle of bank is not more than 60°
Acrobatic maneuvers are not approved
1 ½ turn spins for flight instruction only with trained CFI
Recommended entry speeds for each approved maneuver are as follows:
Maneuver Speed (KIAS)
Lazy eight 93
Chandelle 93
Steep turn (max 60°) 93
Stall / Spin Slow deceleration (1 Knots/sec)
Warning
Limit load factor could be exceeded by moving the flight controls abruptly to full control deflection at a speed above V
A
(93 KIAS, Maneuvering Speed).
2.1.18 Maneuvering Load Factor Limits
Maneuvering load factors are as follows:
Flaps
+4 -2
35° +1.9 0
2.1.19 Flight Crew
Minimum crew for flight is one pilot seated on the left side.
2.1.20 Kinds of Operations
The airplane, in standard configuration, is approved only for day VFR operation with terrain visual contact. Minimum
equipment required is as follows:
Altimeter
Airspeed Indicator
Heading Indicator
Fuel Gauges
Oil Pressure Indicator
Oil Temp. Indicator
Cylinder Heads Temp. Indicator
Outside Air Temp. indicator
Tachometer
Chronometer
First Aid Kit
Hand-held fire extinguisher
Emergency hammer
For further standard equipment refer to section 6.

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