FIRE PROTECTION
Description
Aircraft Operations Manual
7.1
PAGE
10
Apr 01/15
A11989
A
L ENG
OIL PRESS
A
B
C
D
1
2
3
4
5
6
7
8
9
10
1
2
3
4
5
6
7
8
9
10
L ENG
FIRE
AVIONIC
SMOKE
CARGO
SMOKE
LAV
SMOKE
CABIN
PRESS
R ENG
FIRE
R ENG
OIL PRESS
L TAIL P
HOT
R TAIL P
HOT
PROP
BRAKE
AUTO
TRIM
AUTO
COARSEN
CONFIG
PITCH
TRIM
RUDDER
LIMIT
L FIRE
DET FAIL
R FIRE
DET FAIL
FUEL
ELEC
ICE
PROT
ENGINE
FLAPS
AIRCOND
PARK
BRK ON
HYDR
EMER LTS
UNARMED
OXYGEN
DOORS
AVIONICS
VENT
AVIONICS
A
−
SKID
INOP
L STALL
FAIL
GUST
LOCK
PUSHER
SYSTEM
R STALL
FAIL
CENTRAL WARNING PANEL
A
L/R ENG FIRE light (red)
Comes on flashing for an engine fire
condition.The light will remain on as long
as the fire exists.
AVIONIC/LAV/CARGO SMOKE light (red)
A light comes on to indicate a smoke condi-
tion in the respective compartment. The
light will remain on as long as the smoke
condition exists.
L/R TAIL P HOT light (red)
Comes on to indicate a tail pipe overtem-
perature. The light will remain on as long
as there is an overtemperature.
L/R FIRE DET FAIL light (amber)
Comes on flashing to indicate a short cir-
cuit in the engine fire detection loop. The
light will remain on as long as there is a
short circuit.
Fig. 5 Fire protection
−
controls and indicators
