Reference
Modification-No.
- 0 -
Page
20
Date
1996 05 10
Install
914 F
40°
8) Technical data
To maintain clarity, only data relevant for engine installation and operation will be stated in
the Manual.
◆ NOTE: Connecting dimensions, filling capacities, drive and reduction ratios, electric
output etc. can be found in the respective chapter of engine installation.
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: around 1400 r.p.m.
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
available.
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
°
C (-13° F)
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.
Ill. 7
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