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MIL-I-5418 Revision B:1963

Current

Current

The latest, up-to-date edition.

Indicator, Airspeed, Pitot Static, Sensitive, 50-650 Knots

Available format(s)

PDF

Published date

08-01-1963

£13.91
Excluding VAT

Gives design and performance requirements for the procurement of one type of indicator, range 50 to 650 knots.

DevelopmentNote
INACTIVE FOR NEW DESIGN 4/9/96
DocumentType
Standard
Pages
17
ProductNote
NEW CHILD NOT 2 2019 IS NOW ADDED.
PublisherName
US Military Specs/Standards/Handbooks
Status
Current

This specification covers certain design and all performance requirements for the procurement of one type of sensitive pitot static airspeed indicator, range 50 to 650 knots.

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MS33585 Revision B:1961 POINTER, DIAL, STANDARD DESIGN OF AIRCRAFT INSTRUMENT (NO S/S DOCUMENT)
MS28047 Revision E:1984 INDICATOR, INDICATED AIRSPEED, PITOT STATIC, 50-650 KNOTS (NO S/S DOCUMENT)
MIL-D-70327 Base Document:1959 DRAWINGS, ENGINEERING AND ASSOCIATED LISTS
MS33558 Revision C:1968 Numeral and Letters, Aircraft Instrument Dial, Standard Form of
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FED-STD-595 Revision C:2008 Colors Used in Government Procurement (S/S By SAE-AMS-STD-595)
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£13.91
Excluding VAT