T-45A UJPT, E2-C2, ADV, & IUT Eng-01
Introduction to NATOPS & T-45A Configuration
E.
Flaps/slats, speed brakes 1.4.19.3.1.1
NOTE: Since during normal operation full slat
extension occurs with any half or down flap
condition, reference to slats is omitted in some
subsequent discussion of flaps.
1.
Description: flaps inboard at trailing edge
of each wing, slats full span on leading
edge of wing, and speed brakes on each
side of aft fuselage
2.
Function
a.
Flaps augment lift at lower airspeeds
b.
Slats decrease stall speed and
increase aircraft control and stability
c.
Speed brakes increase drag to reduce
airspeed rapidly during flight and to
allow increased power setting in
landing configuration
F.
Landing gear system 1.5.4.1.1.1.2
Sg 3, fr 6
1.
Description: retractable, tricycle-type gear
Strut Door
Trunnion Door
a.
Each wing-mounted main gear
consists of strut assembly, trailing arm
Forward Door
suspension unit, conventional split-hub
Drag Brace Fairing
wheel, and single tire
Trailing Arm Door
Inner (Wheelwell) Door
Fixed Strut Door
T-45A LANDING CONFIGURATION
b.
Nose gear: conventional forward-
retracting shock strut, dual tire system
with mountings for launch bar,
holdback fitting, and lighting
assemblies
2.
Function: supports and cushions aircraft
during stresses of land-based or carrier
launches and landings
(8-03) Original
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