INDICATOR, INDICATED AIRSPEED, PITOT STATIC, MAXIMUM ALLOWABLE SPEED 50-650 KNOTS

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US Military Specs/Standards/Handbooks

Gives pitot-static, indicator, range 50 to 650 knots as listed on MS28048.

Committee	FSC 6610
DevelopmentNote	INACTIVE FOR NEW DESIGN 4/9/96
DocumentType	Standard
Pages	23
PublisherName	US Military Specs/Standards/Handbooks
Status	Current

MIL-I-5415 Revision C:1987	INDICATOR, AIR SPEED, PITOT STATIC PRESSURE GENERAL SPECIFICATION FOR
MIL-P-21563 Revision B:1962	POINT SYSTEM, FLUORESCENT, FOR AIRCRAFT APPLICATION (ASA)
MS33585 Revision B:1961	POINTER, DIAL, STANDARD DESIGN OF AIRCRAFT INSTRUMENT
MS28048 Revision B:1969	INDICATOR, INDICATED AIRSPEED, PITOT STATIC MAXIMUM ALLOWABLE SPEED, 50-650 KNOTS (ASG)
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