Effectivity: 914 Series BRP-Powertrain page 2-3
OM Edition 2 / Rev. 1 April 01/2011
d05036.fm
Critical flying alti-
tude
available boost pressure
Airbox tempera-
ture
Oil pressure
Oil temperature
EGT exhaust gas temperature
Up to the stated critical flight altitude the re-
spective 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
Intervention temperature 72 °C (160 °F)
Intervention temperature * 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)
Max. 7 bar (102 psi)
For a short period admissible at cold start.
Min. 0.8 bar (12 psi) (below 3500 rpm)
* 1.5 bar (22 psi)
Normal 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
Max. 130 °C (266 °F)
Min. 50 °C (120 °F)
normal operating temperature approx. 90 to 110 °C (190 - 230 °F)
Max. 950 °C (1742 °F)
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