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GB/T 42045-2022Aircraft jacking pads (English PDF)

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Issued by

State Administration for Market Regulation, China National Standardization Administration

Level / Type

National · Recommended

Issue date

October 12, 2022

Implementation date

October 12, 2022

Scope

GB/T 42045-2022 (Aircraft jacking pads) is available as an English-translated PDF.

GB/T 42045-2022 — 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.

Document preview — GB/T 42045-2022

National Standard of the People's Republic of China

ICS
49.100
Classification
V 50

Issued by: State Administration for Market Regulation, China National Standardization Administration

Contents

  • foreword
  • 1 Scope
  • 2 Normative references
  • 3 Terms and Definitions
  • 4 Requirements

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.

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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This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — all pages — is available in the English PDF.

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