MIL-L-85314/4A

LIGHT SYSTEMS, SUBSONIC AIRCRAFT, ANTI-COLLISION, STROBE, FUSELAGE MOUNTED RED SOURCE AND WING TIP MOUNTED WHITE SOURCE

contributor author	NAVY - AS - Naval Air Systems Command
date accessioned	2017-09-04T15:18:35Z
date available	2017-09-04T15:18:35Z
date copyright	06/30/1983
date issued	1983
identifier other	MQQPDAAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/18264
description abstract	This detail specification together with the general specification cover the requirements for a fuselage mounted, red, strobe anti-collision light system, and a wing tip mounted, white, strobe, anti-collision light system, for large subsonic aircraft. The classification (types) of the light systems shall be as specified in the general specification.
language	English
title	MIL-L-85314/4A	num
title	LIGHT SYSTEMS, SUBSONIC AIRCRAFT, ANTI-COLLISION, STROBE, FUSELAGE MOUNTED RED SOURCE AND WING TIP MOUNTED WHITE SOURCE	en
type	standard
page	14
status	Active
tree	NAVY - AS - Naval Air Systems Command:;1983
contenttype	fulltext