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MIL-I-5392A
INDICATOR, AIRSPEED, PITOT STATIC, TYPE K-3
Year: 1956
Abstract: This specification covers one type of pitot static, sensitive, maximum allowable speed, range 40 to 400 knots, airspeed indicator, designated Type K-3. Intended Use: The Type K-3 airspeed indicator covered by this specification is intended to indicate the airplane's speed and the maximum allowable speed as set by the Mach number adjustment at the rear of the case. This is accomplished by the use of two pointers.
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| contributor author | AIR FORCE - 84 - Air Force Sustainment Center - Warner Robins | |
| date accessioned | 2017-09-04T15:12:14Z | |
| date available | 2017-09-04T15:12:14Z | |
| date copyright | 20803 | |
| date issued | 1956 | |
| identifier other | LWPIDAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho179893FD081D527369727A00D52FAB6A/handle/yse/10671 | |
| description abstract | This specification covers one type of pitot static, sensitive, maximum allowable speed, range 40 to 400 knots, airspeed indicator, designated Type K-3. Intended Use: The Type K-3 airspeed indicator covered by this specification is intended to indicate the airplane's speed and the maximum allowable speed as set by the Mach number adjustment at the rear of the case. This is accomplished by the use of two pointers. | |
| language | English | |
| title | MIL-I-5392A | num |
| title | INDICATOR, AIRSPEED, PITOT STATIC, TYPE K-3 | en |
| type | standard | |
| page | 15 | |
| status | Active | |
| tree | AIR FORCE - 84 - Air Force Sustainment Center - Warner Robins:;1956 | |
| contenttype | fulltext |