Cirrus DESIGN SR22T - Page 233

Cirrus Design Section 7
SR22T Airplane and Systems Description
P/N 13772-003 7-31
Figure 7-7
Engine Controls and Indicating
8
Engine Instruments
Engine Controls
9
10
1345 6
LEGEND
1. Percent Power
2. CHT
3. Tachometer
4. EGT
5. Manifold Pressure
6. Oil Temperature
and Pressure
7. Turbine Inlet Temperature
8. Power Lever
9. Friction Control
10. Mixture Control
2
SR22_FM07_3255
7
Original Issue