MS14168 Tire, Pneumatic, Aircraft, 22 X 6.6-10

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INCH-POUND

MS14168A(AS)

12 July 1996

SUPERSEDING MS14168(AS)

21 May 1976

MS SPECIFICATION SHEET

TIRE, PNEUMATIC, AIRCRAFT, 22 X 6.6-10

This specification is approved for use by the Naval Air Systems Command, Department of the Navy, and is available for use by all Departments

and Agencies of the Department of Defense.

The requirements for acquiring the product described herein shall consist of this specification sheet and the issue of MIL-T-5041 listed in that issue of the Department of Defense Index of Specifications and Standards (DoDISS) specified in the solicitation.

SIZE	PLY	STATIC	VERT	INFL	BURST	BEAD	WEIGHT	STATIC	TREAD	MOLD	DEFLC
	RATING	LOAD	LOAD	PRESS	PRESS	WIDTH	LB.	UNBAL	3/	SKID	+3%
	1/	RATING	LB.	PSI	PSI	IN.	MAX.	+1/2 OZ.		DEPTH	-4%
		LB.		RATED	MIN. 2/	MAX.				MIN.

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22 X 6.6-10 22TL 14,150 60,000 304 1400 1.75 32.0 15 RIB 0.22 32

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1/ TL = tubeless

2/ New tire

3/ The tire shall have not less than three and not more than five grooves. The tread grooves shall be shaped, insofar as practicable, so that foreign objects will not become trapped between the ribs.

TIRE DATA

The tire shall meet the following envelope dimensions for a new tire at rated inflation and a grown and thrown tire at 400 psi inflation.

TIRE DIMENSIONS (INCHES) RATED INFLATION

GROWN AND THROWN

MIN MAX MAX

OUTSIDE DIAMETER	21.60	22.20	23.30
SECTION WIDTH	6.40	6.80	7.14
SHOULDER DIAMETER	-	20.00	20.60
SHOULDER WIDTH	-	6.00	6.30

AMSC N/A 1 of 5

FSC 2620

DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.