V45 航空仪表 标准查询与下载
共找到 902 条与 航空仪表 相关的标准，共 61 页
This AS covers vertical velocity instruments which display the rate of change of pressure altitude of an aircraft, as follows: type A - direct reading, self-contained, pressure actuated; type B - electrically or electronically operated, self-contained, pressure actuated; and type C - electrically or electronically operated, input from a remote pressure sensor. The range of operation of the instrument and the altitude range when applicable shall be as marked on the instrument face or nameplate. This Aerospace Standard (AS) establishes the minimum performance standards for vertical velocity instruments for aircraft use.
Vertical Velocity Instrument (Rate-of- Climb)
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996-01-01
- 实施
This SAE Aerospace Standard (AS) applies to all temperature instruments used in aircraft applications and environments. The word instruments as used in the Standard encompasses only the display device and does not include the temperature sensors. Examples of the types of instruments covered are as follows: 1.1 temperature instruments using a resistance temperature detector for temperature sensing; 1.2 temperature instruments using a thermocouple for temperature sensing; 1.3 temperature instruments using an averaging thermocouple harness for temperature sensing; 1.4 temperature instruments receiving an input from a signal conditioning unit; 1.5 temperature instruments receiving an input from another temperature instrument; and 1.6 temperature instruments receiving an input from other temperature sensing devices. This document establishes the essential minimum performance requirements for electrical type temperature instruments primarily for use on aircraft which may subject the instruments to environmental conditions specified herein.
Minimum Performance Standard Temperature Instruments
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996-01-01
- 实施
This notice should be filed in front of MIL-I-S7928B(USAF), dated 1 November 1978.
INDICATOR, ATTITUDE, TYPE ARU-51/A
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996-01-01
- 实施
This commercial item description covers a 3-inch, solid state, self-contained attitude indicator intended to provide a standby attitude display for transport aircraft.
INDICATOR, ATTITUDE, THREE INCH, SOLID STATE, SELF-CONTAINED
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996-01-01
- 实施
This notice should be filed in front of MIL-A-S1403(USAF), dated 15 June 1967.
ALTIMETER-ENCODER, AAU-21/A
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996-01-01
- 实施
This notice should be filed in front of MIL-A-27198B(USAF), dated 29 December 1987.
ALTIMETER, PRESSURE AAU-7/A
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996-01-01
- 实施
This notice should be filed in front of MIL-1-25479A(USAF), dated 26 October 1987.
INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.0, TYPE ME-5
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996-01-01
- 实施
This notice should be filed in front of MIL-I-25355B(USAF), dated I June 1993.
INDICATOR, INSTRUMENT LANDING, AIRPORT RUNWAY
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996-01-01
- 实施
MIL-F-63231 [AR], dated 17 August 1979, with amendment 2 dated 26 April 1984 has been reviewed and determined to be valid for use in acquisition.
INDICATOR, INSTRUMENT LANDING, AIRPORT RUNWAY
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996-01-01
- 实施
This notice should be filed in front of MIL-I-27673C(USAF), dated 12 February 1993.
INDICATOR, TRUE AIRSPEED AVU-15/A
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996-01-01
- 实施
This notice should be filed in front of MIL-1-21718(AER), dated 20 November 1958, and Amendment -1, dated 9 October 1959.
INDICATOR, AIRSPEED, PITOT-STATIC, MAXIMUM ALLOWABLE SPEED, 40-400 KNOTS
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996
- 实施
This notice should be filed in front of MK-I-21735A(AS), dated 3 1 January 1969, and Notice 1, dated 7 December 1987.
INDICATOR, AIRSPEED AND MACH NUMBER, PITOT STATIC, 60 TO 650 KNOTS
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996
- 实施
This notice should be filed in front of MIL-I-7906A(AS), dated 15 June 1961, Amendment 2,dated 10 January 1980, and Notice 1, dated 8 July 1987.
INDICATOR, GYRO HORIZON, MANUALLY CAGED, ELECTRIC, TYPE MB-1
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996
- 实施
MIL-I-21203A(AS) is inactive for new design and is no longer used, except for replacement purposes.
INDICATOR, ATTITUDE, SPHERICAL, DIRECT READING, FAST ERECTING, ELECTRIC GYRO
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996
- 实施
This notice should be filed in front of MIL-I-Z3832A(AS), dated 25 June 1980.
INDICATOR, TACHOMETER, TRIPLE POINTER, HELICOPTER
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996
- 实施
MIL-S-23535(AS) is inactive for new design and is no longer used, except for replacement purposes.
SYSTEM, INTEGRATED FLIGHT INSTRUMENTATION
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996
- 实施
This notice should be filed in front of MIL-I-81496(AS), dated 15 April 1968, and Amendment 1, dated 15 October 1968.
INDICATOR, ATTITUDE, 2-INCH ID-1602/A
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996
- 实施
MIL-I-23524A(AS) is inactive for new design and is no longer used, except for replacement purposes.
INDICATOR, ATTITUDE-DIRECTOR, REMOTE, ID 1329A(V)
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996
- 实施
This CID covers a non-luminous battery-generator voltage indicator(voltmeter) for 28 volt(V)(nominal) direct current(dc) electrical systems.
INDICATOR, VOLTAGE: BATTERY-GENERATOR, 28 VOLT DC (NOMINAL) (METRIC)
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996
- 实施
This notice should be filed in front of MIL181186(AS), dated 1 July 1966.
INDICATOR, RATE OF FUEL FLOW SYNCHRO TYPE, MS90360
- ICS
- 49.090
- CCS
- V45
- 发布
- 1996
- 实施
