Indicator, Airspeed and Mach Number, Pitot Static, 60 to 650 Knots

Available format(s)

PDF

Published date

01-31-1969

Publisher

US Military Specs/Standards/Handbooks

Gives a device for indicating airspeed and Mach number.

DevelopmentNote	INACTIVE FOR NEW DESIGN 9/10/96
DocumentType	Standard
Pages	25
PublisherName	US Military Specs/Standards/Handbooks
Status	Current

The indicator covered by this specification shall indicate airspeed and Mach number with the indicated airspeed range from 60 to 650 knots, Mach range from 0.4 to 2.0 Mach, at altitudes from - 1,000 to 50,000 feet, and as listed on MS28089.

MIL-I-5415 Revision C:1987	INDICATOR, AIR SPEED, PITOT STATIC PRESSURE GENERAL SPECIFICATION FOR
MIL-I-81400 Base Document:1966	INSTRUMENT, AIRCRAFT, GENERAL SPECIFICATION FOR
MS24367 Revision C:1971	LAMP, INCANDESCENT MINIATURE INTEGRAL LIGHTING
MS28089 Revision B:1969	INDICATOR, AIRSPEED AND MACH NUMBER, PIVOT STATIC, 60 TO 650 KNOTS
MIL STD 470 : B	MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS)
MIL-C-14806 Revision A:1969	COATING, REFLECTION REDUCING, FOR INSTRUMENT COVER GLASSES AND LIGHTING WEDGES
MS33558 Revision C:1968	NUMERAL AND LETTER, AIRCRAFT INSTRUMENT DIAL, STANDARD FORM OF
MS28105 Revision D:2006	COVER GLASS, AIRCRAFT INSTRUMENT DIAL
MS24515 Revision F:1979	LAMPS, INCANDESCENT, T-1, SUB-MIDGET FLANGED
MIL-L-27160 Revision C:1972	LIGHTING, INSTRUMENT, INTEGRAL, WHITE GENERAL SPECIFICATION FOR
MIL-STD-471 Revision A:1973	MAINTAINABILITY DEMONSTRATION
MS33737 Revision B:1988	NUT, SELF LOCKING, CLIP IN TYPE, INSTRUMENT MOUNTING
MIL-L-25467 Revision D:1977	LIGHTING, INTEGRAL, RED, AIRCRAFT INSTRUMENT, GENERAL SPECIFICATION FOR
MIL D 1000/1 : LATEST	DRAWING, ENGINEERING & ASSOCIATED DATA
FED-STD-595 Revision C:2008	COLORS USED IN GOVERNMENT PROCUREMENT
MIL-STD-785 Revision B:1980	RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION
MIL-STD-781 Revision D:1986	RELIABILITY TESTING FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION