EasyManua.ls Logo

Cessna 402C - Page 96

Cessna 402C
336 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
RPM
TO
SIMULATE
CRITICAL (LEFT)
ENGINE
INOPERATIVE
AND
FEATHERED
CONDITIONS:
1.
Propellers
in
Low
Pitch
(Full
Forward
Position).
2.
Manifold Pressure Adjusted to Obtain Proper
RPM,
ZU>
om
Al()
;:::J
~O
rZ
,,~
Al
o
()
m
o
C
Al
m
U>
~
20
~
18
~
016
0
214
~
12
0
~
10
~
8
""
~ 6
~
4
LIaH4
iii
tllO<H1
iii
I I I
UH1"0
!
ISA
~
2
~
SL
~
\"r.S-
'f..\~
()~.
reP
qmr::'{..\~s
\0"
t-\"r.
S
\\(',
j;
;::
"
r
'ii
in
o
"
Al
o
()
m
o
C
Al
"'
!'J
°c
-40 -30 -20 -10 0
10
20
30
40
I ! I I I I I I I
I I I I ( 1 1
of
-40 -20 0
20
40
60
80 100
OUTSIDE
AIR
TEMPERATURE
,
,
,
)
\
)
1400 1600
Figure 4-3
\
)
~
1800 2000
PROPELLER
SPEED
-
RPM
}
2200
l
2400
~0
~~v
~
o
N
c.J

Related product manuals