BRP ROTAX 914 Series, Руководство оператора

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Effectivity: 914 Series
Rev. 0 BRP-Rotax Page 2-3
August 01 2019
Engine speed
Take-off speed 5800 rpm (max. 5 min.)
Max. continuous speed 5500 rpm
Idle speed min. 1400 rpm
Manifold pressure
ATTENTION
Due to the control behavior an overshooting of the manifold
pressure is possible. But within 2 seconds this pressure has to
stabilize within the allowance.
Take-off performance max. 1350 hPa (39.9 in.HG)
Max. continuous performance max. 1200 hPa (35.4 in.HG)
Acceleration
Limit of engine operation at zero gravity and in negative “g“
condition.
Max. -0.5 g (max. 5 second)
Critical flying
altitude Available boost pressure
ATTENTION
Up to the stated critical flight altitude the respective manifold
pressure is available.
Take-off performance up to max. 2450 m (8000 ft)
above sea level
Continuous performance up to max. 4875 m (16000 ft)
above sea level
Airbox
temperature
Airbox temperature
Intervention
temperature
72 °C (160 °F)
* 88 °C (190 °F)
* 914 F starting with S/N 4420200
(TCU part no. 966741)
* 914 UL starting with S/N 4417598
(TCU part no. 966741)