Effectivity: 914 Series BRP-Powertrain page 2-2
OM Edition 2 / Rev. 0 April 01/2010
d05036.fm
2.1) Operating limits
Performance Performance data relate to ISA (International Standard Atmo-
sphere).
Manifold pressure
NOTE: The stated pressure in the suction tube is al-
ways lower by the pressure loss in the carbure-
tors than the TCU controlled airbox pressure
and may be therefore subject bigger deviations.
Speed
Manifold pressure
Acceleration Limit of engine operation at zero gravity and in negative ”g” con-
dition.
Take-off performance 84.5 kW at 5800 rpm
Max. continuous performance 73.5 kW at 5500 rpm
Take-off performance 1300 hPa (38.4 in.HG)
*1320 hPa (39.0 in.HG)
Max. continuous performance 1150 hPa (34.0 in.HG)
*1180 hPa (34.9 in.HG)
*914 F starting with engine S/N 4,420.200 (TCU part no. 966741)
*914 UL starting with engine S/N 4,417.598 (TCU part no. 966471)
Take-off speed 5800 rpm (max. 5 min)
Max. continuous speed 5500 rpm
Idle speed min. 1400 rpm
Due to the control behavior an overshooting
of the manifold pressure is possible. But with-
in 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)
Max. 5 seconds at max. -0.5 g
To Next Page
Loading...
Need help?
General
