MIL-I-21718 Base Document:1958
Current
Current
The latest, up-to-date edition.
Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots
Available format(s)
PDF
Published date
20-11-1958
Publisher
Design and performance criteria for a pitot static, maximum allowable airspeed indicator, range 40 to 400 knots.
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