Cessna 206H - MINIMUM ENGINE TORQUE FOR TAKEOFF

SOLOY TURBINE PAC SECTION 5
POHS CESSNA T206H/206H PERFORMANCE
5-8
F.A.A. Approved May 23, 2003
MINIMUM ENGINE TORQUE FOR TAKEOFF
CONDITIONS:
1. Power – TAKEOFF
2. Propeller – 1810 RPM
3. Engine Air Induction System – NORM
NOTES:
4. The torque indicated below is the minimum value for which takeoff
performance in this section can be obtained.
5. Torque on this chart shall be achieved without exceeding 810C TOT or
105% N
1
.
EXAMPLE: OAT 16C
Pressure Altitude 4000 Ft.
Minimum Engine Torque Acceptable 85 PSI
Figure 5-4. Minimum Engine Torque For Takeoff
RANGE IN NAUTICAL MILES
RANGE IN NAUTICAL MILES
110
100
90
80
70
60
50
40
20
10
0
ENGINE TORQUE IN PSI
OUTSIDE AIR TEMPERATURE
O
C
8000
6000
4000
2000
S.L.
PRESSURE
ALTITUDE IN FEET
ISA -20
0
C
ISA
ISA +20
0
C
-20
-15
-10
-5
0
5
10
15
20
25
30
35
40
UNCONTROLLED
COPY