CRUISE
&
RANGE DATA CONDITIONS:
1.
All Cruise and Range Data tables allow for:
a
climb
out at 200 horsepower to 3000 feet; a continued climb
at maximum power (power boost on), full-rich mixture,
and best rate-of-climb airspeed to cruise altitude; a
cruise to destination at the specified power and mixture
setting; and
a
45-minute fuel reserve
at
the same al-
titude and power setting. The data is also based
ona
-
gallons of usable fuel, standard atmosphere, and no
wind. Takeoff weight
is
ounds or
E!g
pounds.
2,
The data
is
taken from flight tests at full-rich mixture
settings above 75 percent rated power and at best-power
mixture settings for cruise at 75 percent rated power or
less. (For
best.power mixture, setEGT at 100°F below
peak EGT on rich side of peak.
)
3.
When interpolating the cruise and range data for non-
standard conditions, note that each
PO0F increase above
standard temperature will cause a one percent reduction
in horsepower, while each
1O0~
decrease below standard
temperature will cause
a
one percent increase in horse-
power.
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