EasyManua.ls Logo

Learjet 24D - ENGINE FIRE EXTINGUISHING

Default Icon
373 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
steady. Returning the switch to NORM extin-
guishes the lights.
EXTERIOR EXTINGUISHER
DISCHARGE INDICATORS
Two colored disc indicators are flush-mounted
in the side of the fuselage below the left en-
gine pylon (Figure 8-3). The red disc covers
the thermal discharge port. It will be ruptured
if one or both thermal relief valves have re-
leased bottle pressure. The yellow disc will be
ruptured if either bottle is discharged by de-
pressing an illuminated ARMED light. The
integrity of the two discs is checked during the
external preflight inspection.
ENGINE FIRE
EXTINGUISHING
EXTINGUISHER CONTAINERS
Two spherical extinguishing agent contain-
ers are located in the tailcone area. Both con-
tainers use common plumbing to both engine
cowlings via shuttle valves, providing the air-
plane with a two-shot system. The chemical
agent in the containers, monobromotrifluo-
romethane (CF
3
Br), is not corrosive, and its
discharge will not necessitate cleaning of the
engine and cowl areas.
The containers are plumbed to each engine
cowling to provide the airplane with a two-shot
system. The containers will fully discharge in
one to two seconds. A pressure gage mounted
on each container indicates the charge of the
container. A thermal relief valve on each con-
tainer is plumbed to a thermal (red) discharge
indicator to relieve bottle pressure when bot-
tle temperature reaches 217ºF.
Access to the fire-extinguishing container is
through the tailcone door.
OPERATION
When a FIRE light illuminates (or flashes), it
indicates a fire or overheat condition in the re-
spective engine cowling. The pilot should first
place the thrust lever of the affected engine to
CUT OFF, then proceed with the AFM proce-
dures. A brief description of system operation
is as follows:
Airplanes With Glareshield
Warning Lights
Lifting the guard and depressing the red FIRE
warning light applies 28 VDC to close the hy-
draulic and fuel shutoff valves, and on airplanes
SNs 24-350 and subsequent and 25-227 and
subsequent, it closes the associated bleed-air
8-3
FOR TRAINING PURPOSES ONLY
LEARJET 20 SERIES PILOT TRAINING MANUAL
FlightSafety
international
Figure 8-2. FIRE DET Test Switch
Figure 8-3. Fire Extinguisher Discharge
Indicators

Table of Contents

Related product manuals