Cessna 402C - Page 43

SECllON 3
EMERGENCY PROCEDURES
(ABBREVIATED PROCEDURES)
ENGINE FAILURE DURING FLIGHT (Speed Below VMCA )
MODEL 402C
1. Rudder - APPLY towards operative engine.
2. Power - REDUCE to stop tum.
3. Pilch Attitude - LOWER NOSE to accelerate above YMCA)
4. Inoperative Engine Propeller - FEATHER.
5. Operative Engine· INCREASE POWER as airspeed increases above YMCA.
6. Inoperative Engine - SECURE.
7. Trim Tabs - ADJUST 50 bank toward operative engine with approximately 1/2 bail
slip indicated on the turn and bank indicator.
8. Operative Engine Cowl Flap· AS REQUIRED.
ENGINE INOPERATIVE LANDING
1. Fuel Selector - MAIN TANK (Feel For Detent).
2. Auxiliary Fuel Pump· ON (Operative Engine).
3. Alternate Air Control - IN.
4. Mixture - FULL RICH or lean as required for smooth operation.
5. Propeller Synchrophaser - OFF (Optional System).
6. Propeller - FULL FORWARD.
7. Approach - 108 KIAS with excessive altitude.
8. Landing Gear - DOWN within gliding distance of field.
9. Wing Flaps - DOWN when landing is assured.
10. Speed - DECREASE below 95 KIAS only ~ landing is assured.
11. Air Minimum Control Speed - 80 KIAS.
ENGINE INOPERATIVE GO-AROUND (Speed Above 95 KIAS)
WARNING
Level flight may not be possible for certain combinations of
weight, temperature and altitude. In any event, do not attempt
an engine inoperative go-around after wing flaps have been
extended beyond 15
0
.
1. Throttle· FULL FORWARD (39.0 Inches Hg.).
2. Wing Flaps - UP.
3. Positive Rate-ot-Climb - ESTABLISH.
4. Landing Gear - UP.
5. Cowl Flap - OPEN.
6. Cimb at One Engine Inoperative Best Rate-of-Climb Speed - 104 KIAS.
7. Trim Tabs - ADJUST
50 bank toward operative engine with approximately 1/2 bail
slip indicated on the tum and bank indicator.
3-4 1 November 1979