Power Setting Table - Piper Turbo Saratoga PA-32-301T Pilot's Manual

POWER SETTING TABLE
-
LYCOMING MODEL TIO-540-S1AD
300
HP ENGINE
Press. Std. 55% - 165 HP 65% -
195
HP
75%
-
225
HP Press.
Alt. Ft.
Temp.
Approx. Fuel Flow 12.3
GPH
Approx.
Fuel Flow 14.0 GPH Approx. Fuel Flow 16.5 GPH Alt. Ft.
°C
2200
2300 2400 2575
2300 2400 2575 2300 2400 2575
SL 15 24.4 23.8
23.3
22.3 27.5 27.0 26.1 31.1 30.7 29.9 SL
2000 11 23.6 23.0 22.4 21.4 26.7
26.0 24.9 30.3
-
29.6 28.3 2000
4000 7 23.0 22.5 21.9 21.0 26.0 25.2 23.7 29.8 29.0 27.5 4000
6000
3 22.5 21.9 21.3 20.3 25.6
24.7 23.1 29.5 28.5 26.9
6000
8000
-1
22.2 21.7 21.1 20.2 25.3
24.5 22.8 29.2 28.3 26.7 8000
10,000
-5
21.8 21.3 20.7 19.8 24.8
24.0 22.6 28.9 27.9 26.3
10,000
12,000
-9
21.5 21.0
20.5
19.7
24.7
-
23.9 22.6 28.8 27.9 26.5 12,000
14,000
-13
21.4 21.0 20.2 19.3 24.6 23.9 22.7 28.8
27.9 26.5
14,000
16,000
-17
21.3 20.7 20.0 18.8 24.5 23.8 22.7 28.8 27.9 26.5 16,000
N 18,000
-21
21.3 20.6 19.8 18.5 24.5 23.7 22.7
27.9 26.5 18,000
20,000
-25
21.3 20.5 19.6 18.1 23.7 22.7
- -
26.5 20,000
To maintain
constant
power,
correct
manifold
pressure
approximately
1% MAP for each 6°C variation in induction air
temperature
from
standard altitude
temperature.
Add manifold
pressure
for
air temperatures
above standard; subtract
for temperatures below
standard. Observe maximum allowable manifold
pressure
limitations.