MIL-I-21718 Base Document:1958
Current
The latest, up-to-date edition.
Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots
20-11-1958
Important note : Users cannot be edited or removed once added to your Multi user PDF.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.
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