Cessna 152 - Page 77

CESSNA
MODEL 11'-'-a
THIS DATA APPLICABLE ONLY TO AIRPLANES WITH LYCOMING I
0-235--l2C ENGINE. FOR AIRPLANES WITH ENGINE MODIFIED TO
O-235--NZC, REFER TO DATA IN SECTION 9 SUPPLEMENT.
SECTION 5
PERFORMANCE
CONDITIONS:
1670 Pounds
RANGE PROFILE
45 MINUTES RESERVE
24.5 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 6-6. .
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.
1-
w
w
LL.
w
0
::>
1-
j::
....I
<(
12,000 ,-,-,--,.--,-T-i~..,.,,,.-r- ........ .,.....,.-,--.---r-.,........,r-r-r-,
l-+-+--1-1-+-+-- '4J·,,. _ _.
1
,_.,._N.,50
KT AS-+--+-+-1
,__.-+--+--+-+-<f' r-. ~9~ ~T~~-+--+-+-<
t-+-+--+-+-<1- 0·1+1-+-.="'!k:- s -+-+--+-i
10
()()()1-+-+--1-1-+,{J ,~102 KTA
• J.::.,.l~......,e-i!c-H-1-+-f-+-+-+-1-+-i
-.J
t-+-+--+-+~,-+l-l-+-+l-+ll-l-+-fl-+-+----+-+-f--1
I((
80001-1-+-4-....j_l-,l-+.14---+-4-!.-l-ll-+-4-+-+-ll-+-+-I
107 KTAS.....,'.,.,,,-'-+-l+-t-+<-"•...,.,,,..,79 KTAS-+-+-+-1
100
'KT AS ,,,, 91 KT AS-+-+--+-<
6000t-t-+-+--Htt---c-+++--t-+t-t-tt-+-+--t-+-c-+--t--1
4000
97 KT AS :;tt---t-tt-t-+-t1H---tt:.,. 89 KT AS-,- -
103
KTA<" 78 KTAS_,__
>-+-+--+-ffi - ffi - ffi -ffi I+-+->--+-+--+-_,__,
>-+-+--+- 3: - 3: - 3: - 3: t+-+-<-+-+--+-+-1
2000 >-+-+- ..... 2 - 2 - 2 -2-+-<--+-+--+-+-I
--- * - * - * -*
- 100 ~ 94 l8 87 18 - ~ t--t-t-+--+-+-+-f
-KTAS,;;;i: KTAS, KTAS..._.... ........ _/77 KTAs--
S. L 300 350 400 450
RANGE - NAUTICAL MILES
Figure 5-8. Range Profile (Sheet 1 of 2)
1 July 1978
Revision 1 - 31 March 1983 5-15