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|  MIL-T-18232B(AS)
3.1.6
(cont)
Length, maximum:
Reference line level
feet
On handling truck
feet
Length from hoisting sling to farthest after part
of tail, reference line level, rudder neutral,
elevator down
feet
Distance from wing mean aerodynamic quarter-chord
point to horizontal tail mean aerodynamic
quarter-chord point
feet
Distance from wing mean aerodynamic quarter-chord
point to vertical tail mean aerodynamic
quarter-chord point
feet
Propeller clearance (normal):
Reference line level
inches
Propeller diameter
feet
3.1.7
CONTROL SURFACE MOVEMENTS. - Control surface movements on
each side of neutral position for full movement as limited
by stops shall be as specified in the detail specification. (Not to be used for
inspection purposes.)
Rudder
degrees
right
degrees
left
Rudder tab or trim surface
degrees
right
degrees
left
Elevators or movable stabilizer
degrees
above
degrees
below
Elevators tab or trim surface
degrees
above
degrees
below
Ailerons
degrees
above
degrees
below
Aileron tab
degrees
above
degrees
below
3.1.8
SIMPLICITY. - The design shall provide for a maximum of
simplicity commensurate with other criteria.
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