共找到 548 条与 航空器及其附件综合 相关的标准,共 37 页
This specification establishes the performance, operating characteristics, design features, detailed interface configuration definitions, and installation envelopes for a gas turbine auxiliary power unit (APU) with a government furnished equipment (GFE) electrical generator attached.
POWER UNIT AUXILIARY, S-3A AIRCRAFT EQUIPMENT SPECIFICATION FOR
Specifies general requirements for aircraft, suitable for use in nominal 28 V d. c. systems, or 115/200 V, 400 Hz a c. systems, having the characteristics specified in ISO 1540. Two classes of switches are specified: class 1: switches for use in unprotected positions on aircraft; class 2: switches intended for less arduous environments.
Aircraft; Proximity switches; Part 1 : General requirements
Provisions for Automatic Test Equipment
Provisions for Automatic Test Equipment
Provisions for Automatic Test Equipment
Provisions for Automatic Test Equipment
This document establishes the minimum performance and design characteristics for a Hybrid Test System (HTS). The HTS will be used for functional and diagnostic test of analog and hybrid Units Under Test (UUTs) within a variety of weapon systems either currently in inventory or projected for subsequent introduction into inventory.
HYBRID TEST SYSTEM
Removable aircraft emergency towing and mooring rings.
Removable aircraft emergency towing and mooring rings. Strengthened type.
Specification for general requirements for equipment for use in aircraft. Introduction
本标准适用于各型航空发动机经试车验收后至运输和贮存中的封存防锈。
Aircraft engine dry air storage
Steel, carbon in accordance.vith pr.acuremmt mpecific atim. Steel, c.rrnsion. Resisci ccordmce with procurement .pecificatim.
SLEEVE, COMPRESSION, TUBE FITTING, 37 DEGREE FLARED [Refer To: SAE J514, SAE J514, SAE J514, SAE J514, SAE J514]
Tins Intel national Standard specifics tests to evaluate the effects of temperature variations on components or equip-ment used in an craft. The tests have limited application and should only be specified in the relevant equipment specifi-cation when the thermal effects due to a change of tem-perature are significant to the operation of the equipment. The tests will enable equipment manufacturers to demonstrate that then equipment — when exposed to changes of temperatuie — will continue to function, and/or suivive. Two categories of test are described : 1) Temperature variations generally applicable to equipment likely to be subjected to gradual changes in atmospheric temperature, and 2) Thermal shock - generally applicable to equipment likely to be subjected to rapid or instantaneous changes in atmosphenic temperature. The tests are not suitable for equipment installed in locations wheie the heat transfer rate is greatly increased by high velocity ot tutbulent an movement (for example external to the aircraft or in intake or supercharger ducting), where the temperatuie change affects only certain paits or surfaces of the equipment (for example radomes, windscreens, etc.), nor are they applicable to equipment which is subject to thermal shock by contact with a hot fluid (for example hydraulic components). For such equip-ment the lelevant equipment specification shall detail the appiopriate test to be conducted.
Specification for general requirements for equipment for use in aircraft - All equipment - Environmental conditions - Change of temperature
This list has been prepared for use by or f a the Government in-the procurement of products c6ver.d by th.
STARTER; ELECTRIC, CONSTANT CURRENT, DC
Provisions for Automatic Test Equipment
Provisions for Automatic Test Equipment
Built-In Test Equipment (BITE)
Built-In Test Equipment (BITE)
Automatic Test Equipment Provisions
Automatic Test Equipment Provisions
Built-in Test Equipment (BITE)
Built-in Test Equipment (BITE)
Provisions for Automatic Test Equipment
Provisions for Automatic Test Equipment
Automatic Test Equipment Provisions
Automatic Test Equipment Provisions
Built-In Test Equipment (BITE)
Built-In Test Equipment (BITE)
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