T-45A UJPT, E2-C2, ADV, & IUT Eng-01
Introduction to NATOPS & T-45A Configuration
2.
Function
Sg 3, fr 15
O
N
OFF
a.
Converts engine compressor bleed air
N
to conditioned air and distributes it to
cockpit ventilation, pressurization, and
W
H
E
O
N
L
S
1
N
BARO
2
3
+
OFF
SET
SET
W
AT
UO
BUNO165059
4
5
E
6
DEP
-
DAY
BRT
C
K
30
4
6
VCR
7
-
S
8
+
9
20
2
8
gUNITS
AUTO
MD
OE
O
0
DCL
ENT
0
R
C
L
DT
AA
O
F
F
F
0
10
0
1
MSTR
MS28025
F
FIRE
2
-
4
-
ALERT
O
N
defog systems
PUSH
SETO
T
0
1
0
LANDING
1 2
I
2
0
PUSHHARD
0
8
9
1
2
I
5
4
GEAR
2
1
U 5
.
P
FT./MIN.
3
0
6
0
5
5
0
7
5
6
4
3
MM
PERCENT
0
6
FLAPS/SLATS
1
1
1
0
9
1
4
HOOK
0
1
2
5OW000
D x1N
.
9
0
4
0
OO
ALT
12
HARNESS
9
3
R.P.M. 5
CODE
8
0
0
4
5
1
5
2
8
ANT-SKID
SPDIBRAKES
8
4
OFF
0
7
0
6
0
7
5
2
TAKE
OFF
6
A
A
/
G
N
U
5
3
2
3
5
3
34
7
G
L
10
20
5
CONTR-SGID
ANTIAUK
G
A
/
10F
00T
INHG
3
0
N
2
5
29 2
33
3 O
S 3
C
4
6
FLAPS/SLATS
4
3
5
1
2
4
ROCKETS
1
T
O
X
S
N
100FT
6
4
1
6
3
INT
TI
RM
BMS
OB
GTS
K
0
5
N
5
LB
0
3
2
CANOPY
ROTATION
0
7
5
0
F O
0
X0
10
1
EGT
7
GSIE
TF
R
HARNESS
F
F
.
OFF
CX100
1
0
F
0
8
ETM
GP
R
/
CBNL
AIAT
SA
ET
LSTA
RSTA
P.P.HX1000
7
40
L A
S
T
RSTA
SD
P
BK
R
OILPRESS
OXYGEN
SPDBRKFULL
6
AM
R
AM
R
HDA
YFL
I
GNRTR
EEAO
EEG
MR
JETT
30
1
5
0
HO
OK
20
LAUNCH
BAR
5000
100
GUN
BRKPRESS
ECA
4000
READY
PS
UH
SAUAMD
ETNRE
CANOPY
MANUALFUEL
RETRACT
AAAT
RLTIRUDE
D
3000
TOJETT
1777
2
0
0
2000
0
2
GUN
TAILPIPEHOT
SLATS
1000
ASM
MT
RR
HYD1PRESS
ACINVERTER
LA
BR
NS WLSR
OE H T
RANGE
COURSE
LA
BR
ANTI-SKID
FEET
N
OFF
3 1
800
300
HYD2PRESS
C
A
E
2
ETN
XED
3
3
3
0
6
400
CLIMB
LT
TEST
S E
A
F
RATEXTEND
AVIONICSHOT
NAV
PUSH
FELW
ULO
PRBAE
AKRK
VOL
SQL
FREQ/(CHAN)
U
A
M
BRT
OEST
T
O
O
H
F
5
1
F
1
DI
VE
LPM
PUP
NOSEWHLSTR
F
OFF
F
M
2
F
CDI
NAVCM
OM
CM
OM
FE
UL
PES
RS
CT
O
N
R
A
U
G
V\U
H
RA
ED
R
T
/
T/RDG
F
&
S
1
2
TONETEST
F
PRGSETLA
E
OD
O
F
TEST
VOR/ILS
W
F
D
W
F
D
W
F
D
ACL
CE
ANTI-SKID
G
MAN
A
C
T
A
T
F
A
T
F
A
T
F
S
2
4
3
INTR/EXT
HG
D
CRS
2
1
CHANSEL
MODE
LIGHTS
b.
Provides cooled bleed air to avionics
AIR
FOD
LO
MIP
DATA
RCDR
HG
D
DG
U
3
P
0
S
S6
S
0
-
+
COMP
SLV
FA
LP
1/2
H
A
3
0
N60N
R
PL
UL
OFF
BRT
OFF
BRT
D
W
N
S
OFF
A-COLL/STROBE
LAT
CONSOLE
WARN/CAUT
AL-
C L
O
DIMSELECT
LGE
DGA
3
0
R
DO
OR
2
0
4
0
OFF
CB
AI
N
NS
OE
OFFBRT
LF
ET
1
0
PRES000LT
X1SA
5
0
HOT
RH
GT
I
0
VORTACANMKR
OM
CM
EME
RGF
LAP
I
M
C
S
OD
CL
C
NO
U
P
RM
ICSA
O
1
2
N
bay for equipment cooling
RCVR
M
L
O
R
TN
OE
T
M
DOW
N
D
N
FLIGHT INSTRUMENTS
FLIGHT INSTRUMENTS
P.
Flight instruments 1.4.5.3.1.1
1.
Description: consists of airspeed, vertical
speed, compass, altimeter, and attitude
indicating systems
2.
Function
a.
Provide primary flight performance data
b.
Provide navigation information
c.
Provide backup instrumentation
d.
Mach/airspeed indicator
e.
Vertical speed indicator (VSI)
f.
Standby attitude indicator (AI)
g.
Attitude director indicator (ADI)
h.
Horizontal situation indicator (HSI)
i.
Standby compass
j.
k.
Clock
l.
Radar altimeter
(8-03) Original
Page 1-26
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