MIL-A-9207B

ANALYZER, IGNITION AND VIBRATION, AIRCRAFT RECIPROCATING ENGINE

contributor author	AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City
date accessioned	2017-09-04T18:16:58Z
date available	2017-09-04T18:16:58Z
date copyright	20374
date issued	1955
identifier other	HODJDAAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho1513AF679D40AC4261598F1EFDEC014A/handle/yse/199835
description abstract	This specification establishes the requirements for two types of ignition and vibration analyzers suitable for use as a test cell or flight line instrument. It shall include provisions for ignition analysis on either high or low tension ignition systems and shall also provide suitable vibration harnesses, pickups, and leads for complete vibration analysis for those engine types specified herein. The ignition and vibration analyzer shall be of the following types: Type I - Nonportable Type II - Portable. Intended Use: The Engine Analyzers described by this specification, contain the basic Analyzer Instrument. They are designed to detect, locate, and identify reciprocating aircraft engine abnormalities as well as to indicate normal engine operation. The type I equipment will be used in the test cell while the Type II is primarily intended for flight line use.
language	English
title	MIL-A-9207B	num
title	ANALYZER, IGNITION AND VIBRATION, AIRCRAFT RECIPROCATING ENGINE	en
type	standard
page	18
status	Active
tree	AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City:;1955
contenttype	fulltext