Cirrus SR20 - Page 221

Cirrus Design Section 7
SR20 Airplane and Systems Description
P/N 21399-004 7-37P/N 21399-004 7-37
Figure 7-7
Engine Controls and Indicating
Density Alt 8000 Ft
Oat 31°F -1°C (ISA +0°C)
8
Engine Instruments
Engine Controls
9
10
7
1345 6
LEGEND
1. Percent Power
2. CHT
3. Tachometer
4. EGT
5. Manifold Pressure
6. Oil Temperature
and Pressure
7. Alternate Air Control
8. Power Lever
9. Friction Control
10. Mixture Control
2
SR20_FM07_3008A
Revision A1