Technical Data; Operating Limits - Rotax 914 series Installation Manual

8) Technical data

To maintain clarity, only data relevant for engine installation and operation will be stated in
the Manual.
◆ NOTE:
8.1)

Operating limits

1. Engine speed .......................... see Operators Manual 914 Series, sec. 10.1.
2. Manifold pressure:................. see Operators Manual 914 Series, sec. 10.1.
3. Acceleration: .......................... see Operators Manual 914 Series, sec. 10.1.
4. Critical flight level ................. see Operators Manual 914 Series, sec. 10.1.
5. Oil pressure: .......................... see Operators Manual 914 Series, sec. 10.1.
6. Oil temperature: ..................... see Operators Manual 914 Series, sec. 10.1.
7. Cyl. head temperature: .......... see Operators Manual 914 Series, sec. 10.1.
8. Exhaust gas temperature: ..... see section 11.1
9. Airbox temperature: .............. see section 16.1
10. Range of starting temperature: see Operators Manual 914 Series, sec. 10.1
11.Fuel pressure: ........................ see Operators Manual 914 Series, sec. 10.1.
12.Banking of plane deviation from the effective vertical:
See Operators Manual 914 Series, sec. 10.1.
The engine design is for a conventional, non-aerobatic, fixed wing tractor or pusher
type configuration with the oil return port in the optimum position (see section 13.5).
With this consideration the engine is properly lubricated in all flight profiles.
The resulting bank angle b (depending on acceleration/deceleration) may never
exceed the max. bank angle.
◆ NOTE:
Fig. 6
08405
Effectivity: 914 Series
Edition 2 / Rev. 0
INSTALLATION MANUAL
Connecting dimensions, filling capacities, drive and reduction ratios, electric
output etc. can be found in the respective chapter of engine installation or
other relevant engine documentation. (see section 4.4)
Pitch or role angle α is not equal with β, except stabilized condition
(without acceleration).
max. 40°
Fig. 7
07191
BRP-Rotax
F2
F1
Fr
max. 40°
α
pitch or roll
β
current bank angle
F1 gravity
F2 acceleration
Fr result of F1 and F2
July 01/2008
page 27