Cessna 402C - Page 131

DC -40 -30 -20 -10 0 10 20 30 lIU :JU
I ' , , , ! ! , , ,
I iii , i I I
of -40 -20 0 20 40 60 80 100 120
52847043 OUTSIDE AIR TENPERATURE
4-\-+-1 j-._
a..-, , ._. I·.
~ •. _I- .ril
liI:0
~~V'
~
o
I'.)
n
""'
m m
"'0
(j='
",0
;::Z
}> '"
Z
o
m
400 Ft/r1 n
350 FtlM n
200 FtlM n
800
FtlM n
Subtract values listed
below from value
obtained in above
graph.
Effects for a
combination
of gear,
flap or wlndmilling
propeller may be
obtained by adding the
effects for each.
Approximate
Effect of
Configuration on One
Engine Inoperative
Rate-at-Cl imb.
lnoperat i
ve
Engine
Windmilling
Gear
Down
Flaps Down 150
Flaps Down 45
0
NOTE:
o
~
CONDITIONS:
1. 2700 RPM and 39.0 Inches Hg.*
2. Mixture - CHECK Fuel Flow In
White Arc. *
3. Landing Gear· UP.
7 z 4. Wing Flaps - UP.
'i: 5. Inoperative Propeller
;:::- FEATHERED.
6 u- 6. Wings Banked 50 Toward Operative
Engine With Approximately 1/2
Ball 51 ip Indicated on the Turn
and Bank Indicator.
Cowl Flaps - CLOSED on
Inoperative Engine.
8
9
~ 7.
, ::
u
~ *ABOVE 12.000 FEET. USE PLACARDED
3 ti.. MANIFOLD PRESSURE AND CLIMB FUEL
~ FLOW,
a
-2
-1
-3
10
t±:. _,
5000
5500
F;gure 5-15
6500 6000
II'EIGHT - POUNDS
~. I I 1J'!'+++-+-I'
6850
t-+++-t-I,II' :t.IC-t-;
r--;-,
-=-"':T
la'
101
97
92
87
. i;
CLIMB SPEEI
KIAS
6850
6500
6000
5500
5000
WEIGHT-
POUNDS
i++-
H
g ,
o
- 8
~
~
~ 16
go
~ 12
~
l- 12*
;:::
::i. 14
r
~ SL
~
o
o
~-
o
5.
o
n
~z
00
, <
o '"
3 3
iSg
, ~
~
O~
,,~
~~