共找到 168 条与 环境条件 相关的标准,共 12 页
(Copies of the referenced federal and military specifications, standards, and handbooks are available from the Department of Defense Single Stock Point, Defense Printing Service Detachment Office, Building 4-D,700 Robbins Avenue, Philadelphia, PA 19111-5094.)
RING, RETAINING, EXTERNAL, INVERTED (TAPERED SECTION TYPE)
(Copies of the referenced federal and military specifications, standards, and handbooks are available from the Department of Defense Single Stock Point, Defense Printing Service Detachment Office, Building 4-D,700 Robbins Avenue, Philadelphia, PA 19111-5094.)
RING, RETAINING, INTERNAL, INVERTED (TAPERED SECTION TYPE) [Refer To: ASME B18.24.3, ASME B18.24.3]
MS90708C, dated 28 June 1995, is hereby reinstated and may be used for acquisition.
RING, RETAINING, EXTERNAL INTERLOCKING [Superseded By: ASME B18.24.3, ASME B18.24.3]
MS16633C, dated 24 April 1990, is hereby reinstated and may be used for acquisition.
RING, RETAINING, EXTERNAL,"E" (REDUCED SECTION TYPE) [Refer To: ASME B18.24.3, ASME B18.24.3]
MS16625C, dated 13 AUGUST 1968, is hereby reinstated and may be used for acquisition.
RING, RETAINING, INTERNAL, BASIC (TAPERED SECTION TYPE) [Refer To: ASME B18.24.1, ASME B18.24.1]
MS16629D, dated 20 APRIL 1990, is hereby reinstated and may be used for acquisition.
RING, RETAINING, INTERNAL, BOWED (TAPERED SECTION TYPE) [Refer To: ASME B18.24.3, ASME B18.24.3]
MS16630, dated 11 APRIL 1989, is hereby reinstated and may be used for acquisition.
RING, RETAINING, EXTERNAL, BEVELED (TAPERED SECTION TYPE) [Refer To: ASME B18.24.3, ASME B18.24.3]
AN166401THRUAN166700 Rev 3 remains inactive for new design, however, the document is valid for acquisition when needed.
RING, RETAINING, INTERNAL, BEVELED (TAPERED SECTION TYPE) [Refer To: ASME B18.24.3, ASME B18.24.3]
MS16634, dated 2 May 1990, is hereby reinstated and may be used for acquisition.
RING, RETAINING, EXTERNAL, BOWED"E" (REDUCED SECTION TYPE) [Refer To: ASME B18.24.3, ASME B18.24.3]
MS16624C, dated 18 April 1990, is hereby reinstated and may be used for acquisition.
RING, RETAINING, EXTERNAL, BASIC (TAPERED SECTION TYPE)
This document provides guidance for a means of showing compliance with regulations for protection against lightning direct effects for aircraft of conventional design, as well as for those involving advanced composite structures or other new technologies. This guidance also applies to those aspects of aircraft systems and components not addressed in the regulations covering the protection of electrical/electronic systems (for example, FAR/JAR xx.1316) or fuel systems (for example, xx.954). The guidance provided in this document applies to initial designs as well as modifications.
Aircraft Lightning Direct Effects Certification
This is an extended environment-resisting hybrid construction (metal and nonmetallic inner shell components, nonmetallic coupling nut) backshell. Metallic components are finished with olive drab cadmium plate over a suitable underplate. Nonmetallic components are uncoated for corrosion resistance
CONNECTOR, ACCESSORIES, ELECTRICAL, BACKSHELL ENVIRONMENTAL, 90 DEG. EMI/RFI HYBRID CONSTRUCTION, CATEGORY 3C
This is an extended environment-resisting hybrid construction (metal and nonmetallic inner shell components, nonmetallic coupling nut) backshell. Metallic components are finished with olive drab cadmium plate over a suitable underplate. Nonmetallic components are uncoated for corrosion resistance.
CONNECTOR, ACCESSORIES, ELECTRICAL, BACKSHELL ENVIRONMENTAL, STRAIGHT EMI/RFI HYBRID CONSTRUCTION, CATEGORY 3C
This users manual provides additional information and references relevant to identifying: (1) acceptance criteria for the indirect effects of lightning compliance approaches, (2) verification (analysis and test) methods including those associated with multiple stroke and multiple burst and (3) recommended design options to optimize needed system immunity to lightning indirect effects. Equipment hazards addressed include those due to the indirect effects on equipment mounted on the aircraft exterior and equipment located within the aircraft interior as well as all associated interconnecting wiring. This document has specific application toward those topics and subsystems addressed in ARP5413 but also provides additional guidelines in the application of those tests identified in DO- 160/ED-14, Section 22. This users manual expands on the topics introduced in ARP5413, Certification of Aircraft Electrical/ Electronic Systems for the Indirect Effects of Lightning. Guidelines are provided which explain the approaches to compliance with the US Federal Aviation Regulations (FAR) and the European Joint Airworthiness Regulations (JAR). Discussions are applicable to all categories of airplanes and rotorcraft. This material as well as the Aerospace Recommended Practices (ARPs) it supports are not intended to provide mandatory approaches to compliance. In many cases, the path to compliance may use one or more of several methods. Applicants for Federal Aviation Administration (FAA) or Joint Aviation Authority (JAA) approval may elect to demonstrate compliance through alternative methods found acceptable by the FAA/JAA.
User?s Manual for Certification of Aircraft Electrical/Electronic Systems for the Indirect Effects of Lightning
Environmental Conditions
Environmental Conditions
Support for Character-Oriented Applications
Support for Character-Oriented Applications
Support for Bit-Oriented Applications
Support for Bit-Oriented Applications
MIL-S-81824, dated 31 August 1998, is hereby reinstated and may be used for acquisition.
SPLICE, ELECTRIC, PERMANENT, CRIMP STYLE, COPPER, INSULATED, ENVIRONMENT RESISTANT
MS90708C, dated 28 June 1995, has been reviewed and determined to be valid for use in acquisition.
RING, RETAINING, EXTERNAL INTERLOCKING [Superseded By: ASME B18.24.3, ASME B18.24.3]
Training Requirements for Flight Training Equipment Support Personnel
Training Requirements for Flight Training Equipment Support Personnel
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