Introduction to T-45C Configuration
T-45C TS, ADV & IUT ENG-01
b.
High gain provides +/- 65 degrees either side
of center for aircraft parking
c.
When launch bar is extended, nose wheel is
disengaged. NWS steering may be selected by
pressing and holding the NWS button but travel
is limited to +/- 20 degrees either side of center.
3.
Control location
a.
NWS button: control stick, both cockpits
b.
Paddle switch: control stick, both cockpits
c.
Rudder pedals: provide electro-mechanical
directional input to NWS to steer aircraft
J.
Launch bar system 1.4.12.3.1.1
1.
Description: electrically controlled, hydraulically
extended, and mechanically retracted launch bar
2.
Function: connects aircraft to catapult shuttle during
catapult launches
3.
Control location: LAUNCH BAR switch--below
EMER GEAR handle, lower left instrument panel,
fwd cockpit only
K.
Arresting hook system 1.4.13.3.1.1
Sg 3, fr 11
1.
Description: extended by gravity with nitrogen
Fig 10: Arresting
damper and retracted hydraulically
Hook Operation
2.
Function: extended hook engages deck arresting
cable or field arresting gear to stop aircraft
3.
Control location
a.
Arresting HOOK handle: right instrument panel,
both cockpits
(9-98) Original
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