Engine Emergencies; Engine Fire During Start Or Shutdown - Bell BHT-206L3-FM-1 LongRanger-III Flight Manual

DOT APPROVED
Table 3-2. Caution lights (Cont)
BHT-206L3-FM-1
PANEL
WORDING
R/FUEL PUMP
FAULT CONDITION CORRECTIVE ACTION
Right pump of the dual Descend below 6,000 feet pressure
boost pump assembly altitude if flight permits. Land as
failed. soon as practical
IF BOTH FUEL BOOST PUMPS FAIL,
UNUSABLE FUEL MAY BE AS HIGH
AS 160 POUNDS (73 KILOGRAMS)
DUE TO INABILITY TO TRANSFER
FUEL FROM FORWARD CELLS.
I
L/FUEL PUMP Left pump of the dual boost Descend below 6,000 feet pressure
pump assembly failed. altitude if flight permits. Land as
soon as practical.
3-4. ENGINE EMERGENCIES
3-5. ENGINE FIRE DURING START
OR SHUTDOWN
*INDICATIONS:
1. Excessive TURB OUT TEMP.
2. Visible smoke or fire.
*PROCEDURE:
1. Throttle - Closed.
2. FUEL VALVE switch - OFF.
-
3. STARTER switch - Press to
motor engine until TURB OUT
TEMP stabilizes at normal
temperature.
4. Shut down and exit helicopter.
3-6.
ENGINE FIRE DURING
FLIGHT
*INDICATIONS:
1. Smoke.
2. Fumes.
3. Fire.
*PROCEDURE:
1.
2.
3.
4.
5.
6.
Throttle - Closed.
Immediately enter autorotation.
FUEL VALVE switch - OFF.
BAT switch - OFF.
GEN switch - OFF.
Execute autorotative descent and
landing.
Rev. 3 3-5