Cessna 208B - Airstart; Engine Flameout During Flight; Starter Assist (Preferred Procedure)

CESSNA SECTION 3
MODEL 2088 (675 SHP) EMERGENCY PROCEDURES
I ENGINE FAILURES (Continued)
ENGINE FAILURE DURING FLIGHT (Continued)
10.Electrical Load - REDUCE as follows:
A. Avionics Bus 2 Switch
- OFF.
B. Flashing Beacon
-OFF.
C. Strobe Lights - OFF.
D. Ice Protection (if installed)
- CONSIDER (if pitot heat is
required, pull the RIGHT
PlTOT HEAT circuit breaker and turn
pitot heat switch ON).
E. Vent Fans
- OFF.
F. GEN CONT and GEN FIELD Circuit Breakers
- PULL (top row,
last two breakers on forward end).
G. Autopilot Circuit Breaker - PULL (third row from bottom,
second breaker from forward end.)
-
11.Landing - Refer to Emergency and in^ Without Engine Power
checklist.
ENGINE FLAMEOUT DURING FLIGHT
1. If Gas Generator Speed (Ng) Is Above 50%:
A. Power Lever - IDLE.
6. Ignition Switch -ON.
C. Power Lever - AS DESIRED after satisfactory relight as
evidenced by normal
ITT and N
D. lgnition Switch
- OFF if cause offlameout has been corrected.
2. If Gas Generator Speed (N,) Is Below 50%:
A. Fuel Condition Lever - CUTOFF.
B. Refer to Airstart checklists for engine restart.
AIRSTART
STARTER ASSIST (Preferred Procedure)
1. Electrical Load - REDUCE.
2. Standby Power Switch (if installed)
- OFF.
3. Avionics Power Switches - OFF.
4. Ignition Switch - NORM.
~~,
5. Air Conditioner (if installed) - OFF.
6. Bleed Air Heat Switch -OFF.
7. Emergency Power Lever - NORMAL.
-I 8. Power Lever - IDLE.
~,
9. Propeller Control Lever - MIN RPM.
10.Fuel Condition Lever - CUTOFF.
=,
11.Fuel Shutoff - ON (push in).
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