Cessna 402C - Page 94

SECTION 4
NORMAL PROCEDURES
AFTER LANDING
(AMPLIFIED PROCEDURES)
(r~'·402C
MOOEl
1. Auxil iary Fuel Pumps - LOW during landing roll.
2. Cowl Fl aps - OPEN.
3. Wing Flaps - UP.
Maximum braking effectiveness is obtained by applying full even pressure
to the toe brakes without locking the wheels and applying full back pres-
sure to the control column. This procedure is recommended only for emer-
gency
stops as excessive brake pad and tire wear will occur. Maximum brake
wear occurs
at high speed. This brake wear can be reduced using aerody-
namic braking supplemented with the use of wheel brakes. Maximum aerody-
namic braking occurs with the wing flaps fully extended and the control
wheel held aft to keep the nose off the runway as long as possible.
After leaving the active runway, the wing flaps should be retracted. Be
sure the wing flaps switch is identified before placing it in the UP posi-
tion. The auxiliary fuel pump switches are turned to LOW during the land-
ing roll.
SHUTDOWN \lOlvv~ s;4~ c-k.J=:- I'.~ S"T'fl~~ See't.9 ~-
1. Parking Brake - SET if brakes are cool.
2. Avi on; cs Bus Switch - OFF.
3. All Switches Except Battery, Alternator and Magneto Switches - OFF.
4. Auxiliary Fuel Pumps - OFF.
~ NOTE __.
The fuel pumps must be turned OFF prior to stopping
engines.
5. Throttles - IOLE.
6. Mixtures - IOLE CUT-OFF.
7. Battery and Alternators - OFF.
8. Magneto Switches - OFF, after engines stop.
9. Control Locks - INSTALL.
10. Fuel Selectors - OFF if a long period of inactivity is anticipated
(Feel For Oetent).
11. Cabin Door - CLOSE after checking internal upper door handle stowed
in the lock plate.
With the mixture levers in IDLE CUT-OFF, the fuel flow is effectively
blocked at the fuel metering unit. Thus, it is unnecessary to place the
fuel selectors in the OFF position if the airplane is receiving nonnal
usage. However, if a long period of inactivity is anticipated, the fuel
selectors should be turned OFF to preclude any possible fuel seepage that
might develop through the metering valve.
I
To preclude battery discharge when the airplane is temporarily inactive,
refer to FLYABLE STORAGE, Section 8, for servicing instructions.
1 November 1979
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