I
THIS DATA APPLICABLE ONLY TO AIRPLANES WITH LYCOMING
O-235-12C ENGINE.
FOR
AIRPLANES WITH ENGINE MODIFIED TO
O-235-N2C,
REFER
TO DATA
IN
SECTION 9 SUPPLEMENT.
SECTION
5
PERFORMANCE
CONDITIONS:
1670
Pounds
RANGE PROFILE
45
MINUTES RESERVE
37.5
GALLONS USABLE FUEL
Recommended
Lean
Mixture for Cruise
Standard Temperature
Zero
Wind
NOTES:
CESSNA
MODEL 152
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
2.8 gallons.
3.
Performance
is
shown for an airplane equipped with
speed
fairings
which
increase
the cruise speeds by approximately
two
knots.
5-16
1-
w
w
LL
w
C
::>
1-
5
<
12.000
::::::::::,:_"T"
1
~-:,.11:~::r::_,::~,:
.....
,r-..-=::_"T
80
--.-...,...."T",_-,-,,.....
l-+-t--t-1-+-~/
~
~02.t--''-+--t-' ... ,
,..
... · KTA,S_,_,_
1--1--t--+-1-+tP/,_
,_
KT
AS
94
_,_
10,000
'-.~
KTAS--
"'.A
---~'#+-t--H-+-t-t-+-.-+-t-H-+-+--+-~
--~~,~t--t-+-H--t-+-11-+-t--+---tt-t-+-+-+--t-1
8000
t-+-+-tt---+-+-i---i!H---t-a--+-H-
......
-+-+-1
107 _
~100
79
--
KTAS
- -KTAS-+-.,_~
...
.._. ......
KTAS--
i---+-+-o+-+-+-+-+-+--+--+-,...91
6000
t-t-+tt-r--+-r-t--tr-+--+--t--~
KT
AS-+-,_-+-
...
I I I
I I I
1---+-+-+-+-+-++-+--+-+-..-89
--+-<,-+-+--r
.,KTAS
4000
H--+-+-+--1--iiH-+-t--+-r-t-+-i-½-+-+-+-+-i
-a:
>103
a:
~97
-a:
---a:
~78
--
~
KTAS
~
-KTAS-~
---;
KTAS--
0
LI-.!....
0
I I
O -
--O->--+--+--+--<
a.
LlJ_
a.
I
a.
a.
2000
~:::=:~
I
~
,-
-~
~-t--t--t--t-t
#!?
I I
:8
\ \
:lJ
---~
-"-100
71
94
111
87
T
-11
+-
7~TAS,7J,KTAS
M1,KTAST
vKTAS-
S.L.
·-
..
550
600 650
700
75<,
RANGE
- NAUTICAL MILES
Figure
5-8.
Range
Profile
(Sheet
2
of
2)
1
July
1978
Revision
1 -
31
March
1983
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