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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MIL-S-62520

At root ---- At construction tip (theoretical extended sec-

tion at tip) : ----

(Note: When an airfoil section other than a NACA section is used, the airfoil section shall be compared with the most nearly equivalent NACA section, or data similsr to that available for NACA sections shall be presented.)

Incidence (degrees):

At root .

At construction tip ----

Sweepback at percent chord, degrees ---- Dihedral, degrees ---- Aspect Ratio ----

Ailerons :

Span ---- Chol·d (average percent wing chord) ---- Tab dimensions ---- Distance from plane of symmetry to centroid

of aileron area ---- The amount of the aerodynamic and static

balance shall be specified, in percent, and

the coefficient of dynamic balanctf'given ----

Spoilers:

Span ---- Chord (average percent wing chord) .: ---- Position of leading edge (average percent

"ring chord) ----

High lift and drag increasing device:

Type --- Span, exclusive of cutouts (percent .of wing

span) ---- Chord (average percent wing chord) ----

Speed brakes :

Span		----
Chord		----
Location	,	----

Tail:

Horizontal :

Span ----

Chord --- Airfoil section designation and thickness ---- Tab dimensions ---- Tab location : ----

The amount of the aerodynamic and static balance shall be specified, in percent, and

the coefficient of dynamic balance given....----