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| MIL-T-18232B(AS)
3.4.3
AILERONS. - The ailerons consist of the aileron panels with
attached fittings, trim tabs, control horns, hinge-pins, bolts
and nuts} or other fastenings, complete and ready for attachment of flight con-
trols. Aileron movement on either aide of the neutral position shall be such
that satisfactory control will result for all flight operations and specified
maneuvers of the target. Sufficient additional movement of the ailerons shall be
provided so that the limit of movement may be controlled by stops rather than by
jamming the hinges or the control surfaces proper. Servo limit switches may be
used as stops in lieu of mechanical stops.
3.4.4
LIFT AND DRAG INCREASING DEVICES. - High-lift or high-drag
increasing devices shall be provided when required by the
detail specification.
TAIL GROUP
3.5
3.5.1
DESCRIPTION. - The tail group includes stabilizers, elevators,
fins, rudders and trim surfaces. Auxiliary control devices
attached to any part of the tail group also shall be included in this group.
STABILIZER. - The stabilizer consists of panels complete with
3.5.2
attachments. Stabilizers maybe fixed or adjustable and shall
be easily removable. Stabilizers constructed as integral parts of the fuselage
shall be detachable as a unit with a portion of the fuselage.
ELEVATORS. - Elevators shall consist of the panels with
3.5.3
attached fittings, trim surfaces, control horns, hinge-pins,
bolts and nuts, or other fastenings ready for attachment to the stabilizer and
for attachment of flight controls.
ELEVATOR MOVEMENT. - The movement of the elevators shall be
3.5.3.2
adequate for the control for which the target is designed.
The elevator and rudder shall be so designed that there will be no mechanical
interference between the surfaces and other parts of the target for any combina-
tion of control-surface settings within the range of movements of the control
surfaces.
3.5.4
FINS. - Fins constructed as integral parts of the fuselage
shall be detachable as a unit with a portion of the fuselage.
RUDDERS. - Rudders shall consist of panels with attached
3.5.5
fittings, trim surfaces, integral, torque tubes, attached
levers, control horns, pins, bolts and nuts, or other fastenings ready for attach-
ment to the fin and for attachment of flight controls.
3.5.6
ELEVATOR AND RUDDER STOPS. - Sufficient additional movement
of the elevator and rudder shall be provided so that the limit
of movement may be controlled by stops or servo limit switches rather than by
jamming the hinges or the control surfaces proper.
BODY GROUP. - The body group consists of fuselage.
3.6
FUSELAGE
3.6.1
27
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