Cessna 402C Pilot Operating Handbook page 133

SECTION 5
PERFORMANCE
MODEl402C
ENGINE INOPERATIVE SERVICE
CEILlNG~=:::::;l
CONOITIONS:
1. Engine Inoperative Climb Configuration.
NOTE:
1. Engine Inoperative service ceil ing is the maximum
altitude where the a; rp 1ane has the capabi 1ity of
climbing 50 feet per minute with one engine inoper-
ative and feathered.
2. Increase indicated service ceil ing 100 feet for
I
each 0.10 inch Hg. altimeter setting greater than
29.92.
3. Decrease indicated service ceil ;ng 100 feet for
each 0.10 inch Hg. a1tilneter setting less than
29.92.
4. This chart provides perfonnance infonnation to aid
in route selection when operating under FAR 135.181
and 91.119 requirements.
50 0 0
>--
<BS
w
w 550 0 87
1([
~
20
<BS 4S
0
60 00 ' 92
I(
0
0
<BS [4S
~
6500 ' 97
I(
w
68 <8S [4S
0 So <8 ' 101
=>
S
15
S
'1
1(/4S
>--
01
~
1(/4S
«
w
'"
=>
~
~
w
'"
10
~
co
z
~
~
w
'-'
w
"'
5
,.
'"
w
~
SL
°C
-40 -30 -20 -10
0 10 20
30 40 50
I
I
I
I
I
I
I
I I
I
I
I
I
I
I
I
of
-40 -20 0
20 40 60
80
100
120
OUTSIOE AIR TEMPERATURE
Figure 5-17
52847015
1 tJovember 1979