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MIL-I-21718 Base Document:1958

Current

Current

The latest, up-to-date edition.

Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots

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PDF

Published date

11-20-1958

US$20.00
Excluding Tax where applicable

Design and performance criteria for a pitot static, maximum allowable airspeed indicator, range 40 to 400 knots.

DevelopmentNote
INACTIVE FOR NEW DESIGN 9/10/96
DocumentType
Standard
Pages
20
PublisherName
US Military Specs/Standards/Handbooks
Status
Current

This specification covers certain design requirements and all performance requirements for one type of pitot static, maximum allowable airspeed indicator, range 40 to 400 knots.

MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
FED-STD-1 Revision A:1972 STANDARD FOR LABORATORY ATMOSPHERIC CONDITIONS FOR TESTING
MS33585 Revision B:1961 POINTER, DIAL, STANDARD DESIGN OF AIRCRAFT INSTRUMENT
MS33558 Revision C:1968 NUMERAL AND LETTER, AIRCRAFT INSTRUMENT DIAL, STANDARD FORM OF
QQ-C-320 Revision B:1974 CHROMIUM PLATING (ELECTRODEPOSITED)
MIL P 7936 : LATEST PARTS AND EQUIPMENT, AERONAUTICAL, PREPARATION FOR DELIVERY
MIL C 5541 : E CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS
MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
MIL-P-6906 Revision B:1969 PLATE, IDENTIFICATION AIRCRAFT
MIL-P-116 Revision J:1988 PRESERVATION, METHODS OF
QQ-P-416 Revision F:1991 PLATING, CADMIUM (ELECTRODEPOSITED)
FED-STD-595 Revision C:2008 COLORS USED IN GOVERNMENT PROCUREMENT
QQ-N-290 Revision A:1971 NICKEL PLATING (ELECTRODEPOSITED)
MIL-S-7742 Revision D:1991 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR

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