GB/T 42032-2022 English PDF

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GB/T 42032-2022: Requirement for design of civil aircraft load sheet
Status: Valid

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Basic data

Standard ID: GB/T 42032-2022 (GB/T42032-2022)
Description (Translated English): Requirement for design of civil aircraft load sheet
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: V01
Classification of International Standard: 49.020
Word Count Estimation: 22,262
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 42032-2022: Requirement for design of civil aircraft load sheet

---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.
Requirement for design of civil aircraft loadsheet ICS 49.020 CCSV01 National Standards of People's Republic of China Civil aircraft loading manifest design requirements Published on 2022-10-12 2022-10-12 Implementation State Administration for Market Regulation Released by the National Standardization Administration directory Preface I Introduction II 1 Scope 1 2 Normative references 1 3 Terms and Definitions 1 4 Basic requirements 1 5 Load table design requirements 1 6 Balance diagram design requirements 3 Appendix A (Informative) Example of Aircraft Loading Manifest 13 Appendix B (informative) Example 15 of the load table Appendix C (Informative) Example of Equilibrium Diagram 17

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. 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., Shanghai Aviation Industry (Group) Co., Ltd., Commercial Aircraft Corporation of China Ltd. Responsible companies Shanghai Aircraft Design and Research Institute, AVIC XAC Civil Aircraft Co., Ltd., AVIC Tongfei South China Aircraft Industry Co., Ltd., Zhuhai Haixiangyi Aviation Technology Co., Ltd. The main drafters of this document. Zhong Guangzhi, Guan Jiahuan, Tong Yu, Sun Baoquan, Ma An, Huang Shasha, Jiao Yanqiong, Luo Tingfang, Ma Yutao, Yang Yonghua, Yang Lei.

Introduction

The loading manifest is usually an important document provided to aircraft operators, one for each type of aircraft according to each cabin layout Load manifest. During the operation of the aircraft, the aircraft operator uses the loading manifest to calculate "weight, center of gravity, horizontal stabilizer trim angle" and other information, and provides information for each The flight of one flight provides the basis for release and is an important tool for stowage work. Provide aircraft operators with the design of loading manifests that meet regulatory and operational requirements based on aircraft weight balance data, customized requirements, etc. The process is an important part of the stowage work. Civil aircraft loading manifest design requirements

1 Scope

This document specifies the basic requirements for the design of the civil aircraft loading manifest, the design of the load table and the design of the balance chart. This document applies to the design of passenger aircraft loading manifests for civil aircraft. Other transport aircraft can be used for reference.

2 Normative references

There are no normative references in this document.

3 Terms and Definitions

The following terms and definitions apply to this document. 3.1 loading manifest loadsheet Records data related to aircraft load balance and files for weight center of gravity calculation. 3.2 Weight center of gravity envelope loading envelope It is composed of characteristic weights such as maximum zero fuel weight, maximum landing weight, and maximum take-off weight and their corresponding front and rear limits of the center of gravity. Closed geometry. 3.3 cut curtailment According to the possible influence of various factors on the center of gravity of the aircraft in operation, the front and rear limits of the airworthiness certificated weight center of gravity envelope are carried out. Downsize, the process of establishing a tighter weight center of gravity envelope.

4 Basic requirements

4.1 The design of the loading manifest shall include the load table and balance chart, see Appendix A. 4.2 The design of the loading manifest shall be calculated and compiled according to the weight balance data of the aircraft type, customized requirements and other data.

5 Load table design requirements

5.1 The design content of the load table should include but not be limited to the information given in Table 1.The schematic diagram of the load table is shown in Figure 1.The load table should be in a fixed format, see Appendix B. 5.2 The cargo compartments in the column of load calculation and space layout in Table 1 shall be designed according to the requirements of cargo compartments. ......

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