FUEL
Description
Aircraft Operations Manual
9/1.1
PAGE
13
Apr 01/15
A11646
B
TEST 1
STALL
FIRE
LAMPS FLAPS
UPR
LWR
AUTOCOARS
L
R
FUEL
L
R
BLD LEAK
L
R
SMOKE
FIRE SHORT
1
2
ACC
+
TEST 1 PANEL
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
AFT
FWD
RST
L
R
C
B
C
A
C
FIRE PROTECTION PANEL
FUEL light (amber).
Comes on flashing whenever a caution light as-
sociated with the fuel system comes on, except
for XFEED ON and CONN VLV OPEN.
FUEL test switch.
L
−
Left fuel quantity indicators shows ;
without mod. 2091: 950
50 lb (432
23 kg)
with mod. 2091:
1000
50 lb (455
23 kg)
Left fuel flow indicator shows 760
35 lb/h or
345
16 kg/h
R
−
same values as above for right instrument.
NOTE: This test determines that the fuel quantity sig-
nal conditioner and indicators perform accu-
rately to a pre
−
set capacitance (to give the sim-
ulated fuel quantity shown above). This test
does not check the integrity of the fuel probes
or ensure full and empty calibration nor does it
check that the actual fuel level is measured
correctly.
L/R ENG fire handle.
L/R engine fire handle, when pulled the fire shut-
off valve will close off the fuel supply to the en-
gine.
Fig. 8 Fuel system
−
fuel caution light, fuel test and fire shut off