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(5) Brakes -- Release.
(6) Elevator Control -- Maintain slightly tail-low attitude.
(7) Climb Speed -- 88 MPH (with obstacles ahead).
(8) Landing Gear and Wing Flaps -- Retract (after obstacles are
cleared).
CLIMB.
NORMAL CLIMB.
(1) Airspeed -- 120 to 140 MPH.
(2) Power -- 24 inches and 2600 RPM.
(3)
Mixtures -- Lean to 78Ibs/hr. fuel flow.
(4) Cowl Flaps -- Open as required.
MAXIMUM PERFORMANCE CLIMB.
(1) Airspeed -- 114 MPH (sea level) to 108 MPH (10,000 feet).
(2) Power -- Full throttle and 2800 RPM.
(3) Mixtures -- Lean for altitude per fuel flow indicator placard.
(4) Cowl Flaps -- Open as required.
CRUISING.
(1) Power -- 15 to 25 inches of manifold pressure and 2200-2600
RPM. Select combination to give no more than 75%power.
(2) Cowl Flaps -- Closed.
(3) Elevator and Rudder Trim -- Adjust.
(4)
Mixtures - - Lean for cruise fuel flow as determined from your
Cessna Power Computer or the OPERATIONAL DATA in Section VI.
NOTE
If optional auxiliary fuel tanks are installed, auxiliary
fuel may be used after 60 minutes of flight.
It
is recom
mended that the left and right auxiliary fuel tanks be sel
octed at staggered intervals of at least 10 minutes. This
LET-DOWN.
(1) Mixtures -- Enrichen as required.
(2) Power -- As desired.
(3) Cowl Flaps -- Closed.
(4) Wing Flaps -- As desired ("UP" to "1/3" down below 160 MPH).
BEFORE LANDING.
(1) Fuel Selectors - Front Engine -- "LEFT MAIN. "
Rear Engine - - "RIGHT MAIN. "
(2) Landing Gear -- "DOWN" (below 160 MPH).
(3) Landing Gear Light -- Green.
(4)
Landing Gear Handle -- Check returned to neutral.
(5)
Mixtures -- Rich.
(6)
Propellers -- High RPM.
(7) Wing Flaps -- As deSired ("1/3" below 160 MPH, "1/3" to "FULL"
below 120 MPH).
(8) Airspeed -- 90 to 100 MPH (flaps extended).
(9) Elevator Trim -- Adjust as desired.
~
BALKED LANDING (GO-AROUND).
,
(1) Power -- Full throttle and 2800 RPM.
(2)
Wing Flaps -- Retract to "1/3" down.
(3) Trim -- Adjust.
(4) Cowl Flaps -- Open.
(5) Wing Flaps -- Retract to 0° after obstacles are cleared and a
safe altitude and airspeed are reached.
I
NOTE
w1ll avoid the possibility of both engines eventually stop
Do
not retract landing gear if another landing approach
till
from auxiliary fuel exhaustion at the same time.
is to be conducted.
1-7
1-'
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