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Cessna 402C - Page 135

Cessna 402C
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TIME,
FUEL
AND
DISTANCE
TO
CLIMB
-
CRUISE
CLIMB
~
~
~'~
~"
~'"
vv'v
-S>VS
S)S)Rl
Rl~
,ff I $
,<.0'0(;;5
<.0""<;:)
'<;,"0"'3
1l
(Jl
rnrn
" 0
"
-<
0-
" 0
;::2
l>
en
2
o
rn
CO
-40 -30 -20 -10 0
10
20
30
40
I I I I I I I I I
iii
1 r i I
FO
-40 -20
0 20 40 60
80
100
OUTSIDE
AIR
TH1PERATURE
B18
~
16
o
'"
,
14
~
o
~
12
;:
;:t
10
~
~
c;
8
~
~
6
4
~
-i}?1:
-
..
;-.
+-
o 5 10
15
20 25
TUtE
TO
cur1B -
MINUTES
I J I I I I
I
I I I 1 I r I l I I
o
10
20
30
40
50
60 70
80
90
100
FUEL
TO
CLIMB
-
POUNDS
I I I
I I I I I I I
o
10
20
30
40
50
60
DISTANCE
TO
CLIMB
-
NAUTICAL
rULES
(ZERO
WIND)
Figure 5-19
CONDITIONS:
1.
2450
RPN
and
29.5
Inches
Hg.
2. Landing Gear -
UP.
3,
Wing
Flaps -
UP.
4.
Cowl
Flaps -
AS
REQUIRED.
5.
Airspeed
- 120
KIAS.
6. Mixtures -
Recom·
mended
Fuel
Flow.
NOTE:
1.
Time,
fuel
and
dis-
tance
for
the
c1
imb
are
determined
by
taking
the
differ-
ence between
the
ai
rport
altitude
and
initial
cruise,
alti-
tude
conditions.
2.
For
total
fuel
used,
add
35
pounds
for
start,
taxi and
takeoff.
~0
~~(
~
o
52847019 N
C")