Cessna 402B 1973 - Climb Procedures; Normal Climb Operations; Maximum Performance Climb

AFTER
TAKEOFF
(4)
(a)
(1)
(2)
(3)
Brakes
-
APPLY
MOMENTARILY'
Landing
Gear
- RETRACT
Climb
Speed -
126 MPH IAS
(best
multi-engine
rate-of-climb
speed) or
(set
up climb
speed
as shown
in Normal
Climb
para-
graph).
Auxiliary,Fuel
PumPs -
OFF.
Cowl
Flaps
-
AS
REQUIRED.
CIIM
B
NORIIAAT
CLIMB
(1)
Power
-
25.5 inches Hg.
and
2450 RPM.
(2)
Airspeed
-
130
-
160 MPH IAS.
(3)
Mixture
-
Adjust
to
climb fuel
flow.
(4)
CowI
Flaps
- AS REQUIRED.
(5)
Auxiliary Frel
Purr'pi
-
ON
(above
12, OOO
feet altitude
td mini-
mize vapor formation).
I}1 AX
I'IA
U M
PER FOR'YI
A NCE
Ctl'tA
B
(1)
Power
- FuIl
throtile
and
2?00
RPM
below
16,000 feet.
Placarded
manifold
pressure
above
16,000
feet.
Airspeed -
126 MPH
IAS.
Cowl
Flaps -
AS REQUIRED.
Auxiliary
FueI
Pumps -
ON
(above
12,
000 feet
altitude
to
mini-
mize
vapor
formation).
CRU
ISING
(1)
Cruise
Power
-
15-29.5Inches
Hg
and 2100 -
2450RPM'
(2\
Mixtures
-
LEAN for
desired cruise fuel
flow
as
determined
from
your
Cessna
Model
40tB/402B'Power
Computer.
Recheck
mixtures.if
'power,
altitude or OAT
changes.
(3)
Cowl
Flaps
-
AS REQIIIRED'
(2)
(3)
(4)
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