共找到 902 条与 航空仪表 相关的标准,共 61 页
This specification covers a time-temperature controlled, chemically activated, irreversible indicator card for use with time-temperature sensitive, limited shelf life products.
INDICATOR, TIME-TEMPERATURE, CARD CHEMICALLY ACTIVATED, METRIC
This amendment forms a part of Military Specification MIL-I-81049A, dated 29 June 1972, and is approved for use by all Departments and Agencies of the Department of Defense.
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION
This amendnient forms a part of Military Specification MIL-I-5099B dated 13 December 1968.
INDICATOR CABIN AIR PRESSURE, 1-7/8 INCH DIAL, TYPE MA-1
This amendment forms a part of Military Specification MIL-1-7906, dated 15 June 1961.
INDICATOR, GYRO HORIZON, MANUALLY CAGED, ELECTRIC, TYPE MB-1
This specification covers air transportable, air-droppable, helicopter transportable, diesel-engine-driven, elevating scrapers.
SCRAPER, ELEVATING, SELF-PROPELLED, 9 CUBIC YARD MINIMUM HEAPED CAPACITY, SECTIONALIZED AND NON- SECTIONALIZED
本标准适用于保护航空仪表显示部分用的平面睞
Specifications for aviation instrument glass
The equipment covered by this specification is a Self-contained Vertical Gyro Indicator System for Military Aircraft.
INDICATOR, ATTITUDE REFERENCE SELF-CONTAINED, 3-INCH, ID-1791/A
This specification covers one type of enginetorquemeter indicator for turboprop engines.
INDICATOR, TORQUEMETER, AEU-13/A
This amendment forms a part of Military Specification MIL-I-81508(AS) dated 5 December 1966.
INDICATOR PLUG, FOR MISSILE PROPELLANTS
This amendment forms a part of Military Specification MIL-I-21685(AER) dated 10 November 1958 and has been approved by the Naval Air Systems Command, Department of the Navy.
INDICATOR, COMPASS REPEATER, ROTATING DIAL, TYPE MW-2
THE RELATIV€ POSITION OF THE CONNECTORS SHALL BE AS SHOWN, THEMARKINGS SHALL BE PERMANENT. AT LEAST 1/8 INCH HIGH CONFORMING TO hi533558 AND CLEARLY INDICATE THE CONNECTOR TO WHICH THEY APPLY. OIMENSIONS IN INCHES. FOR DESIGN FEATURE PURPOSES, THIS STANDARD TAKES PRECEDENCE OVER PROCUREMENT DOCUMENTS REFERENCED HEREIN.I. REFERENCED DOCUMENTS SHALL BE OF THE ISSUE IN EFFECT ON DATE OF INVITATIONS FOR BIO.
INDICATOR, TACHOMETER, TRIPLE POINTER, HELICOPTER
This British Standard specifies the general design and performance requirements for pressure altimeter systems having a combined counter and single pointer presentation in two forms as follows. (a) Type A. A panel-mounting indicator associated with its own internal or external pressure sensing mechanism. (b) Type B. As type A but incorporating an encoder for altitude reporting purposes. Provision is made for instrument systems operating over an indicated range of -2000 ft to +80 000 ft (geopotential) or such other range as may be declared. The design includes a barometric pressure setting facility and may include provision for applying corrections for the aircraft static pressure system error.
Specification for counter and pointer, servo type, pressure altimeter systems
This amendment forms a part of Military Specification MIL-I-9443D, dated 16 March 1972, and is approved for useby all Departments and Agencies of the Department of Defense.
INDICATOR, TEMPERATURE, THERMOCOUPLE, ENGINE EXHAUST, TYPE MJ-2
This amendment forms a part of Militam Specification Sheet MIL-E-l/U+Ol(USAF) dated 27 Januars 1971.
INDICATOR, BEARING-DISTANCE-HEADING ID-1103A/ARN
The equipment covered by this specification is a tape type vertical scale indicator set for engine performance indication.
INDICATOR SET, VERTICAL SCALE
This amendment form a part of Military Specification MIGI-7071B, dated 25 February 1972, and is approved for use by all Department6 and Agencies of the Department of Defense.
INDICATOR, TEMPERATURE, THERMOCOUPLE, HERMETICALLY SEALED, GENERAL SPECIFICATION FOR
This specification covers the requirements for a 2-inch red and whiten tegrallylighted , vertical velocity indicator having a range of from O to 6,000 fpm climb and descent, designated AAU-l8/A.
INDICATOR, VERTICAL VELOCITY AAU-18/A, INTEGRALLY LIGHTED
This specification covers the requirements far one typdkremote attitude director indicator (ADI) designated ARU-Tl/A.
INDICATOR, ATTITUDE, TYPE ARU-51/A
This amendment forms a part of Military Specification MIL-I-25645D(USAF) dated 25 September 1970.
INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR
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