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|  MIL-T-18232B(AS)
3.1.5
AREAS. - Areas shall be specified in the detail specification.
(Not to be used for inspection purposes.)
Wing area, total, including ailerons,
and
square feet of fuselage
square feet
Aileron area, aft of hinge, including over-
hanging external balance forward of hinge,
total including
square feet of tab area
square feet
Horizontal tail area, total
square feet
Stabilizer, to elevator hinge, including
square feet of fuselage and
square
feet of contained elevator balance
square feet
Elevator, aft of hinge, including
square
feet of overhanging external balance forward
of hinge and
square feet of tab area
square feet
Vertical tail area, total
square feet
Fin, to rudder hinge, including
square
feet of contained rudder balance
square feet
Rudder, aft of hinge, including
square
feet of overhanging external, balance forward
of hinge and
square feet of tab area
square feet
3.1.6
DIMENSIONS AND GENERAL DATA. - Dimensions and general data
shall be as specified in the detail specifications (Not to
be used for inspection purposes.)
Wings:
Span, maximum
feet
Chord (Streamwise):
At root
inches
At construction tip (theoretical extended
section at tip)
inches
Span with external stores
feet
Mean aerodynamic (leading edge located
inches aft of
reference datum)
inches
Airfoil Section:
At root
At construction tip (theoretical extended
section at tip)
Airfoil thickness (percent chord)(streamwise
or perpendicular to sweep of 1/4 chord line):
At root
percent
At construction tip (theoretical extended
section at tip)
percent
Average (frontal area divided by wing area)
Incidence:
At root
degrees
At construction tip
degrees
At mean aerodynamic chord
degrees
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