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GB/T 42045-2022: Aircraft jacking pads
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| Standard ID | Contents [version] | USD | STEP2 | [PDF] delivered in | Standard Title (Description) | Status | PDF |
| GB/T 42045-2022 | English | 119 |
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Aircraft jacking pads
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GB/T 42045-2022
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PDF similar to GB/T 42045-2022
Standard similar to GB/T 42045-2022 GB/T 23420 GB/T 24713.2 GB/T 24713.1 Basic data | Standard ID | GB/T 42045-2022 (GB/T42045-2022) | | Description (Translated English) | Aircraft jacking pads | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V50 | | Classification of International Standard | 49.100 | | Word Count Estimation | 6,651 | | Date of Issue | 2022-10-14 | | Date of Implementation | 2022-10-12 | | Issuing agency(ies) | State Administration for Market Regulation, China National Standardization Administration | GB/T 42045-2022: Aircraft jacking pads---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
Aircraft jacking pads
ICS 49.100
CCSV50
National Standards of People's Republic of China
aircraft headrest
Published on 2022-10-12
2022-10-12 Implementation
State Administration for Market Regulation
Released by the National Standardization Administration
directory
Preface I
1 Scope 1
2 Normative references 1
3 Terms and Definitions 1
4 Requirement 1
Appendix A (Informative) Types of Aircraft Headliners (Imperial Measurement Units) 3
foreword
This document is in accordance with the provisions of GB/T 1.1-2020 "Guidelines for Standardization Work Part 1.Structure and Drafting Rules of Standardization Documents"
drafted.
This document is revised and adopted ISO 43.2016 "Aircraft Head Pad".
Compared with ISO 43.2016, this document has the following structural adjustments.
a) The first paragraph of Chapter 4 corresponds to part of the scope of Chapter 1 in ISO 43.2016;
b) Appendix A corresponds to ISO 43.2016, Chapter 4, Paragraph 3, "Table of Imperial Metric Units for Aircraft Headliner Types".
Please note that some content of this document may be patented. The issuing agency of this document assumes no responsibility for identifying patents.
This document is proposed and managed by the National Aircraft Standardization Technical Committee (SAC/TC435).
This document is drafted by. Shanghai Aircraft Customer Service Co., Ltd., Commercial Aircraft Corporation of China Ltd., Commercial Aircraft Corporation of China Ltd.
Responsible for the company Shanghai Aircraft Design and Research Institute, Shanghai Aviation Industry (Group) Co., Ltd., AVIC XAC Civil Aircraft Co., Ltd., AVIC
Fly South China Aircraft Industry Co., Ltd., Zhuhai Xiangyi Aviation Technology Co., Ltd.
The main drafters of this document. Li Chongxiang, Feng Zihan, Wang Zhengxin, Ma An, Huang Shasha, Chen Yong, Zhou Xianghua, Yin Penggang, Wang Yongmei, Cao Tao,
Yang Lei.
aircraft headrest
1 Scope
This document specifies the shape and dimensions of aircraft roof pads and the minimum surrounding space for the roof pad.
This document applies to the design and use of aircraft roof pads.
2 Normative references
There are no normative references in this document.
3 Terms and Definitions
There are no terms and definitions that need to be defined in this document.
4 Requirements
There are seven types of aircraft roof pads, each of which specifies its shape, size and minimum surrounding space.
The aircraft roof pad shall conform to the shape specified in Figure 1, as well as the dimensions, minimum surrounding space and corresponding bearing loads specified in Table 1.imperial aircraft
See Table A.1 in Appendix A for the parameters of the top cushion type.
Figure 1 Schematic diagram of the aircraft roof pad
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