Cessna 152 - Page 79

CESSNA
MODEL
152
THIS
DATA
APPLICABLE ONLY TO AIRPLANES
WITH
LYCOMING
I
O-235-UC
ENGINE. FOR AIRPLANES WITH ENGINE MODIFIED TO
O-235-N2C, REFER TO
DATA
IN SECTION 9 SUPPLEMENT.
SECTION
5
PERFORMANCE
CONDITIONS:
1670 Pounds
ENDURANCE
PROFILE
46
MINUTES
RESERVE
24.6
GALLONS USABLE FUEL
Recommended Lean Mixture for Cruise
Standard Temperature
NOTES:
1. This chart allows for the fuel used for engine start, taxi, 1Bkeoff and climb, and the
time during climb as shown
in
figure 5-6.
2.
Reserve fuel
is
based on
45
minutes
at
45%
BHP
and
is
2.8 gallons.
12,000
10,000
---l~'
1
---/:,
--
f}
--~
__
,-::.
""""'
=;,
I-
8000
w
w
LL
w
6000
0
::>
I-
j::
..I
<(
4000
2000
_a:
-~lii
~
.._a:
-
>-I---
a:
>--
w w
w
-3:
-~3:
I---
3:
>-I---
3:
-
-
_Q
->-2
I---I---
2
2
~-
Q.
-"ii!-
--"ii!-
~-
"ii!--
...........
~
"ii!-
,_._
-'°
~~~
~
in
I----
r-.
~
I
I
S.L. 3
4
5
6
ENDURANCE - HOURS
Figure
5-9.
Endurance
Profile
(Sheet
1
of
2)
1
July
1978
Revision
1 -
31
March
1983
5-17