O-235-N2C
ENGINE
MODEL
152
PILOT'S
OPERATING
HANDBOOK
SUPPLEMENT
CONDITIONS:
1670 Pounds
RANGE PROFILE
45 MINUTES RESERVE
37.5 GALLONS USABLE FUEL
Recommended Lean Mixture for Cruise
Standard Temperature
Zero Wind
NOTES:
1.
This chart allows for
the
fuel used for engine start, taxi, takeoff and climb, and
the
distance during climb as shown
in
figure 5-6.
2. Reserve fuel
is
based
on
45
minutes
at
45%
BHP
and
is
3.2
gallons.
3. Performance
is
shown for an airplane equipped with speed fairings which increase
the cruise speeds by approximately
two
knots.
I-
w
w
LL
w
C
::,
I-
i=
..J
<(
16
12,000
10,000
8000
6000
4000
2000
--
S.L.
500
-
'<d
I
1
'
I I
--
-
1:-,v"-
I
93
~OL
\
I
KTAS
-
-
-
~;t
102
A.:
-
KTAS
v)
.;;;,V/
'<./
"100
KTAS
I I
'\
104
97
90
KTAS
-KTAS
KTAS
a::
a::
a::
~
--
-w
--w
....--
~
--~
fr
--
a?
--2
~t
--*
--*
--1:a-
--:8
I
99
-
_93
86
✓
KTAS~
/K
TASj
KTAS
I I I I I
I \:.,
I I
550
600
650
700
RANGE - NAUTICAL MILES
Figure
3.
Range
Profile
(Sheet
2
of
2)
1
July
1978
Revision
1 -
31
March
1983
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