I
THIS DATA APPLICABLE ONLY TO AIRPLANES WITH LYCOMING
0-235-UC
ENGINE.
FOR
AIRPLANES WITH ENGINE MODIAED TO
0-235-N2C,
REFER
TO DATA IN SECTION 9 SUPPLEMENT.
SECTION
5
PERFORMANCE
CONDITIONS:
1670 Pounds
ENDURANCE
PROFILE
46
MINUTES RESERVE
37
.5
GALLONS USABLE FUEL
Recommended Lean Mixture for Cruise
Standard Temperature
NOTES:
CESSNA
MODEL
152
1. This chart allows for the fuel used for.engine start, taxi, takeoff
ar1d
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.
I-
w
w
IL
w
0
::,
I-
j:::
.J
<(
5-18
12,000
I
10,000
lq
kr
R,
--
~J
-....,,
==~
8000
6000
4000
2000
--
---
IC IC
IC
IC
--w
--
-w
w
w
--3:
--
-3:
3:
3:
--2
-2
0
0
--
II-
II-
>--,P.
--
-,p.
'IP.
~
r--~
_It)
It)
--
lU>
It)
,¢
I
I
I
S.L. 5
6
7
8
9 10
ENDURANCE - HOURS
Figure
5-9.
Endurance
Profile
(Sheet
2
of
2)
1
July
1978
Revision
1 -
31
March
1983
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