MIL-I-5392A

INDICATOR, AIRSPEED, PITOT STATIC, TYPE K-3

contributor author	AIR FORCE - 84 - Air Force Sustainment Center - Warner Robins
date accessioned	2017-09-04T15:12:14Z
date available	2017-09-04T15:12:14Z
date copyright	20803
date issued	1956
identifier other	LWPIDAAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/10671
description abstract	This specification covers one type of pitot static, sensitive, maximum allowable speed, range 40 to 400 knots, airspeed indicator, designated Type K-3. Intended Use: The Type K-3 airspeed indicator covered by this specification is intended to indicate the airplane's speed and the maximum allowable speed as set by the Mach number adjustment at the rear of the case. This is accomplished by the use of two pointers.
language	English
title	MIL-I-5392A	num
title	INDICATOR, AIRSPEED, PITOT STATIC, TYPE K-3	en
type	standard
page	15
status	Active
tree	AIR FORCE - 84 - Air Force Sustainment Center - Warner Robins:;1956
contenttype	fulltext