MIL-S-6252 Specifications, Detail, Fixed Wing Aircraft, Preparation Of S/S By Mil-Std-832This specification contains instruction to be followed in the preparation of detail specifications for the complete aircraft.

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]IIL-S-6252D

Distance from wing MAC quarter chord point to horizontal tail MAC quarter chord point ----

Distance from wing MAC quarter chord point to vertical tail MAC quarter chord point ----

AugJe between reference line and wing zero-lift

line ----

Ground angle, degrees ---- Propeller clearance, (Normal design) loading

condition:

Reference line level, landplane or amphibian ....----

Propeller diameter (to nearest inch) ----

Wheel size:

Main wheels ---- Bicycle wheels, front main--rear main ---

Auxiliary wheel (nose, tail, or other) ----

Tire size:

Main wheels ----

Bicycle wheels, front main--rear main ---- Auxiliary wheel (nose, tail, or other) ----

Tread of main wheels ---- Wheel base , ---~

Vertical travel of .axle from extended to fully

compressed position:

Main wheels ---- Nose wheel ---- Tail wheel (in normal trailing position) ----"'

Distance from main wheel contact point to center of gravity: Horizontal Distance:

At most forward c. g. --. at--· lbs gross wt.

At most aft c. g. -- at -- lbs gross wt.

Vertical Distance :

At most forward c. g. -- at -- lbs gross wt.

At most aft c. g. -- at --. -.

lbs gross wt.

Location of external stores from the aircraft

center line , --- .....

3.1. 7 Control movement and corresponding control surface move[ ments. (Items may be added, omitted, or modified in this paragraph to properly describe the aircraft. The following information is not to be used for inspection purposes.)

.Control and control surface movements on each side of neutral position for full movement, as limited by stops.