MIL-I-5419 Revision B:1969
Current
The latest, up-to-date edition.
Indicator, Indicated Airspeed, Pitot Static, Maximum Allowable Speed, 50-650 Knots
27-02-1969
Gives pitot-static, indicator, range 50 to 650 knots as listed on MS28048.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN 4/9/96
|
| DocumentType |
Standard
|
| Pages |
24
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers a pitot-static, maximum allowable airspeed indicator, range 50-650 knots as listed on MS28048.
| MIL-I-5415 Revision C:1987 | Indicator: Air Speed, Pitot-Static Pressure, General Specification for (No S/S Document) |
| MIL-P-21563 Revision B:1962 | Paint System, Fluorescent, for Aircraft Application (No S/S Document) |
| MS33585 Revision B:1961 | POINTER, DIAL, STANDARD DESIGN OF AIRCRAFT INSTRUMENT (NO S/S DOCUMENT) |
| MS28048 Revision B:1969 | Indicator, Indicated Airspeed, Pitot Static Maximum Allowable Speed, 50-650 Knots (ASG) |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| MIL-STD-785 Revision B:1980 | RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION |
| MIL-STD-781 Revision D:1986 | RELIABILITY TESTING FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION |
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