Cessna 402C - Page 70

SECTION 3
EMERGENCY PROCEDURES (AMPLIFIED PROCEDURES)
6~'402C
MODEL
AIR INLET OR FILTER ICING EMERGENCY PROCEDURES
1. Al ternate Ai r Control (5) - PULL OUT.
2. Propel ler( s) .- INCREASE (2550 RPM For Normal Crui se).
3. Mixture(s) - LEAN as required.
PROPELLER SYNCHROPHASER
ENGINE INOPERATIVE PROCEDURE
I. Propeller Synchrophaser - OFF (Optional Syst6n).
SYNCHROPHASER FAILURE
I. Propeller Synchrophaser - OFF (Optiona' System).
2. Propeller Synchrophaser Circuit Breaker - PULL (Optional Systan).
EMERGENCY EXIT WINDOW OPENING
The forward cabin window on the right side of the passenger compartment
should be opened as follows:
I. Emergency Release Handle Plastic Cover - PULL OFF.
2. Safety Clip - PUSH FORWARO.
3. Emergency Release Handle - PULL FULL AFT.
4. Emergency Exit Window - PUSH OUT and UP until the up-lock brace
holds the window open.
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NOSE BAGGAGE DOOR OPEN ON TAKEOFF
If a baggage door ;s left unlatched, it may open as the nose ;s raised
on takeoff. The door will not hit a propeller nor will there be any unus-
ual handling characteristics. If sufficient runway remains for a safe
abort, the airplane should be stopped. If the decision is made to continue
the takeoff, maintain airspeed below 120 KIAS and return for landing as
soon as practical. Avoid lowering the nose abruptly which could throw
loose objects out of the compartment.
SPINS
Intentional spins are not pennitted in this airplane. Should a spin
occur, however, the following recovery procedures should be employed:
I. Throttles - CLOSE IMMEDIATELY.
2. Ailerons - NEUTRALIZE.
3. Rudder - HOLD FULL RUODER opposite the direction of ro,ation.
4. Control Wheel - FORWARD BRISKLY, 1/2 turn of spin after applying.
full rudder.
5. Inboard Engine - INCREASE POWER to slow rotation. (If Necessary).
I
November 1979
Revision 4 - 1 December 1983
3-31