NAVY - MIL-I-21718
INDICATOR, AIRSPEED, PITOT-STATIC, MAXIMUM ALLOWABLE SPEED, 40-400 KNOTS
active
| Organization: | NAVY |
| Publication Date: | 20 November 1958 |
| Status: | active |
| Page Count: | 17 |
scope:
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.
intended Use:
The indicator covered by this specification is intended for use on high speed aircraft to give an indication of airspeed and Mach number on a single dial.
Document History
October 9, 1996
INDICATOR, AIRSPEED, PITOT-STATIC, MAXIMUM ALLOWABLE SPEED, 40-400 KNOTS
A description is not available for this item.
October 9, 1959
INDICATOR, AIRSPEED, PITOT-STATIC, MAXIMUM ALLOWABLE SPEED, 40-400 KNOTS
A description is not available for this item.
MIL-I-21718
November 20, 1958
INDICATOR, AIRSPEED, PITOT-STATIC, MAXIMUM ALLOWABLE SPEED, 40-400 KNOTS
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.