T-45A UJPT, E2-C2, ADV, & IUT Eng-05
Fuel System
c.
Refueling flow rate not to exceed 180
US gallons per minute
d.
Aircraft must be grounded during
refueling procedures
III. Controls, switches, and indicators 1.4.7.3
Sg 3, fr 1
Lesson Organization
NOTE: The T-45A does not have fuel dumping
capability.
A.
System status
Sg 3, fr 2
1.
FUEL FLOW indicator gauge
4
3
20
2
5
10
1
6
INT
30
7
0
LB
0
FF
a.
Location: left instrument panel, both
X 100
PPHX1000
cockpits
b.
Function: indicates rate of fuel flow to
engine combustion chamber in pounds
FUEL SYSTEM STATUS INDICATORS
per hour
(1) Direct measure of volumetric fuel
flow
(2) Corrected for fuel density
2.
FUEL QUANTITY indicator gauge
a.
Location: right instrument panel, both
cockpits
b.
Function: needle indicates fuel
remaining in 100-pound increments
(uses capacitance-type measuring
Sg 3, fr 3
system)
GTSFIRE
MSTR
E T/RM
G P
CABINALT
ALERT
OILPRESS
OXYGEN
c.
No fuel quantity indicator test system
HYDFAIL
BRAKEPRESS
(what you see is what you get)
SEATUNARMED
CNP
AOY
TAILPIPEHOT
SLATS
HYD1PRESS
ACINVERTER
HYD2PRESS
EA
C
R TETN
A XE D
AVIONICSHOT
B.
Warning/advisory
FUELLOW
PARKBRAKE
LPPUMP
N S W LSR
OE H T
FUELPRESS
CONTRAUG
ACCEL
ANTI-SKID
1.
FUEL LOW caution light
FUEL SYSTEM CATION LIGHTS
(8-03) Original
Page 5-17
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