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