Technical Data; Operating Limits - Rotax 914 F 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
Take-off speed: ................................. 5800 r.p.m. (5 min.)
max. continuous speed: .................... 5500 r.p.m.
idle speed:
2. Manifold pressure:
Take off performance ................................ 1300 hPa (38,4 in.HG)
maximum continuous performance ........... 1150 hPa (34,0 in.HG)
3. Acceleration:
Time limit for engine operation at weightless condition and with negative gravity
acceleration: .............................................. max. 5 sec at max. -5 g
4. Critical flight level
Take off performance ................................ to max. 2450 m (8000 ft) ASL
maximum continuous performance ........... to max. 4500 m (16000 ft) ASL
ATTENTION: Up to the critical flight level the stated respective performance is
5. Oil pressure: ............................................ see chapter 13.2
6. Oil temperature: ....................................... see chapter 13.2
7. Cyl. head temperature: ............................ see chapter 12.2
8. Exhaust gas temperature: ...................... see chapter 11.1
9. Airbox temperature: ................................ see chapter 16.1
10.Range of starting temperature:
max. ................................. 50° C (122° F)
min. .................................. - 25
11.Fuel pressure: see chapter 14.2.
12.Banking of plane deviation from the ef-
fective vertical:
See ill. 7.
max. ................................. 40°
NOTE:
Up to this inclination the dry sump
lubrication system warrants adequate
lubrication in every flight situation.
Date
Page
1996 05 10
20
Connecting dimensions, filling capacities, drive and reduction ratios, electric
output etc. can be found in the respective chapter of engine installation.
around 1400 r.p.m.
available.
Install
914 F
°
C (-13° F)
Ill. 7
Reference
40°
Modification-No.
- 0 -