T-45C TS, ADV & IUT ENG-07
Aircraft Fuel System
3.
Gravity refueling operation
a.
Location: capped filler on top of fuselage tank
Sg 2, fr 12
4.
Safety warnings
Safety Warnings
a.
Refueling must be stopped immediately if fuel is
discharged through main vent above tail cone
b.
Refueling pressure not to exceed 50 psi
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 2
Lesson Organization
NOTE: The T-45 does not have fuel dumping capability.
FUEL SYSTEM
A.
System status
* Major component
identification
* Operational characteristics
* Controls, switches,
and indicators
* Aircraft interfaces
4
3
2
5
Sg 3, fr 3
1
6
Fig 3: Fuel System
7
0
N2 RPM
102
F.F
Status Indications
FF
4529
20
P.P.H x 1000
10
FQTY
1389
INT
30
N1 RPM
104
0
LB
x 100
TAT C
36
EPR
2.02
T6 C
832
H
S
I
HPC PRESS
141
PLA
87
A
D
I
MENU
D
N
OFF
Figure 3: FUEL SYSTEM STATUS INDICATION
Original (9-98)
Page 7-14
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