IN-FLIGHT ENGINE/PROPS

Question 1

DECOUPLING OF ENGINE AND PROPELLER

Answer 1

IF RECOUPLE FAILS:

*1 PERFORM ENGINE FIRE/FAILURE/SHUTDOWN IN FLIGHT PROCEDURE

Question 2

PROPELLER PUMP LIGHT(S) - STEADY

Answer 2

*1 POWER LEVER- MAX (P)

*2 MAINTAIN AT LEAST 135 KCAS- (P)

IF NORMAL GOVERNING:

*3 PERFORM ENGINE FIRE/FAILURE/SHUTDOWN IN FLIGHT PROCEDURE- (P,CP)

Question 3

FAIL TO FEATHER PROCEDURE

Answer 3

*1 CONDITION LEVER- FEATH (P)

*2 FX OVRD SWITCH- TOGGLE AND HOLD TO COMPLETE FEATHER (P)

IF PROPELLER DOES NOT FEATHER:

*3 POWER LEVER (OPERATING ENGINE)- AS REQUIRED (P)

*4 CONFIGURATION- GEAR UP, FLAPS 10, MAX RUDDER 20 (P,CP)

*5 (AR) RUDDER STOP- SWITCH TO MAN AND DEC TO MINIMUM AIRSPEED (CP)

*6 AIRSPEED- AS REQUIRED (P)

Question 4

DUAL-ENGINE FAILURE DURING FLIGHT

Answer 4

*1 MAINTAIN 150KCAS, CLEAN- (P)

*2 POWER LEVERS- SLIGHTLY ABOVE FLT IDLE (P)

*3 CONDITION LEVER (L OR R)- GRD STOP THEN AIRSTART (P,CP)