MIL-I-5419 Revision B:1969
Current
Current
The latest, up-to-date edition.
INDICATOR, INDICATED AIRSPEED, PITOT STATIC, MAXIMUM ALLOWABLE SPEED 50-650 KNOTS
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PDF
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Important note : Users cannot be edited or removed once added to your Multi user PDF.Gives pitot-static, indicator, range 50 to 650 knots as listed on MS28048.
| Committee |
FSC 6610
|
| DevelopmentNote |
INACTIVE FOR NEW DESIGN 4/9/96
|
| DocumentType |
Standard
|
| Pages |
23
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| MIL-I-5415 Revision C:1987 | INDICATOR, AIR SPEED, PITOT STATIC PRESSURE GENERAL SPECIFICATION FOR |
| MIL-P-21563 Revision B:1962 | POINT SYSTEM, FLUORESCENT, FOR AIRCRAFT APPLICATION (ASA) |
| MS33585 Revision B:1961 | POINTER, DIAL, STANDARD DESIGN OF AIRCRAFT INSTRUMENT |
| 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 |
| 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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