Critical Flying Altitude; Airbox Temperature; Oil Pressure; Oil Temperature - Rotax 914 Series Operator's Manual

Critical flying alti-
tude
Airbox tempera-
ture

Oil pressure

Oil temperature

EGT

Effectivity: 914 Series
OM Edition 2 / Rev. 1
available boost pressure
NOTICE
WARNUNG
Take-off performance
Continuous performance
Intervention temperature
Intervention temperature
Max.
NOTICE
Min.
Normal
Max.
Min.
normal operating temperature
exhaust gas temperature
Max.
BRP-Powertrain
Up to the stated critical flight altitude the re-
spective manifold pressure is available.
up to max. 2450 m (8000 ft.) above
sea level
up to max. 4875 m (16000 ft.) above
sea level
72 °C (160 °F)
* 88 °C (190 °F)
* 914 F starting with S/N 4,420.200
(TCU TNr. 966741)
* 914 UL starting with S/N 4,417.598
(TCU TNr. 966471)
7 bar (102 psi)
For a short period admissible at cold start.
0.8 bar (12 psi) (below 3500 rpm)
* 1.5 bar (22 psi)
2.0 to 5.0 bar (29 to 73 psi) (above
3500 rpm)
* 1.5 to 5.0 bar (22 to 73 psi)
* 914 F up to S/N 4,420.085
* 914 UL up to S/N 4,417.665
130 °C (266 °F)
50 °C (120 °F)
approx. 90 to 110 °C (190 - 230 °F)
950 °C (1742 °F)
page 2-3
April 01/2011