CESSNA
SECTION
3
MODEL
208B
(675
SHP) EMERGENCYPROCEDURES
ENGINE FAILURE
(Continued)
GROUND DISTANCE
-
NAUTICAL MILES
.,
Figure
3-1.
Maximum Glide
~,
While gliding toward a suitable landing area, an effort should be made
.,
to identify the cause of the power loss. An engine failure might be
=,
identified by abnormal temperatures, mechanical noises or high
vibration levels in conjunction with the power loss. A flameout will be
.~-,
noticed by a drop in ITT, torque and
%
Ng.
-3
CAUTION
-,
DO NOT ATTEMPT TO RESTART AN ENGINE THAT IS
DEFINITELY KNOWN TO HAVE FAILED.
(Continued Next Page)
=-,
1
Revision
23
U.S.
3-29
To Next Page