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GB/T 24713.1-2009 English PDF

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GB/T 24713.1-2009: Aircraft -- Tow bar attachment fittings interface requirements -- Part 1: Main line aircraft
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Basic data

Standard ID GB/T 24713.1-2009 (GB/T24713.1-2009)
Description (Translated English) Aircraft -- Tow bar attachment fittings interface requirements -- Part 1: Main line aircraft
Sector / Industry National Standard (Recommended)
Classification of Chinese Standard V50
Classification of International Standard 49.100
Word Count Estimation 6,698
Date of Issue 2009-11-30
Date of Implementation 2010-07-01
Quoted Standard CCAR 25
Adopted Standard ISO 8267-1-2005, IDT
Regulation (derived from) National Standard Approval Announcement 2009 No.14 (Total No.154)
Issuing agency(ies) General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China, Standardization Administration of the People's Republic of China
Summary This standard specifies the drawbar connection (when normal operation from the auxiliary landing gear when towing) interface requirements auxiliary landing gear conventional tricycle landing gear on the aircraft. This section applies to the largest mass shutdown in CCAR 25 airworthiness certification of more than 50 000 kg (110 000 lb) trunk aircraft. This section does not apply to the largest mass shutdown for CCAR 25 airworthiness certification is not more than 50000 kg (110 000 1b) of the aircraft. Such planes defined in Part 2 of this standard.

GB/T 24713.1-2009: Aircraft -- Tow bar attachment fittings interface requirements -- Part 1: Main line aircraft


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. Aircraft Tow bar attachment fittings interface requirements Part 1. Main line aircraft ICS 49.100 Vp 50 National Standards of People's Republic of China GB/T 24713.1-2009/ISO 8267-1.2005 Aircraft tow bar connector interface requirements Part 1. route aircraft (ISO 8267-1.2005, Aircraft-Towbarattachmentfittingsinterface requirements, Part 1. Mainlineaircraft, IDT) Posted 2009-11-30 2010-07-01 implementation Administration of Quality Supervision, Inspection and Quarantine of People's Republic of China Standardization Administration of China released

Foreword

GB/T 24713 "aircraft tow bar connector interface requirements" is divided into two parts. --- Part 1. route aircraft; --- Part 2. regional aircraft. This is Part 1 GB/T 24713 of. This section identical with ISO 8267-1.2005 "Aircraft tow bar connector interfaces Requirements - Part 1. trunk aircraft. " For ease of use, this standard made the following editorial changes. a) the scope of the order of paragraphs have been adjusted; b) Normative references by the FAR/JAR25.509 to CCAR25; c) Remove international standards foreword, introduction and objectives; d) with a decimal point "." instead of as a decimal point "." This part is proposed by the China Aviation Industry Corporation. This part of the aircraft by the National Standardization Technical Committee (SAC/TC435) centralized. This section drafted by. China Integrated Technical Institute Airlines, China Aviation Industry Corporation First Aircraft Design and Research Institute. The main drafters of this section. Normal Anon, Wang, Wang kai-kai, Li Yong, Lvguang Lin. GB/T 24713.1-2009/ISO 8267-1.2005 Aircraft tow bar connector interface requirements Part 1. route aircraft

1 Scope

This section GB/T 24713 specifies the drawbar coupling auxiliary landing gear conventional tricycle landing gear on the aircraft (when viewed from the auxiliary Landing gear traction normal operation) interface requirements. This section applies to CCAR25 airworthiness certification of quality is greater than the maximum downtime 50000kg (1100001b) trunk aircraft. Maximum mass shutdown This section does not apply to CCAR25 airworthiness certification is not more than 50000kg (1100001b) aircraft, these flying Machine defined in Part 2 of this Standard. The purpose of this section is graded according to the quality of the aircraft (aircraft quality determines the drawbar load) of the tow bar connector standardized interfaces to Ensure the drawbar standard connector can be used within or close to the quality classification of the quality grading of all aircraft types, thereby reducing the use of Type of traction rod. When a series of existing or anticipated aircraft types across two quality grade, they should use the same interface to connect drawbar and Consider using the standard size series high quality grade. This section applies to all new aircraft in the trunk section of this publication put into use or design.

2 Normative references

The following documents contain provisions which, through reference GB/T 24713 in this section constitute provisions of this section. For dated reference documents Member, all subsequent amendments (not including errata content) or revisions do not apply to this section, however, encouraged to reach under this section Parties to research agreement to use the latest versions of these documents. For undated reference documents, the latest versions apply to this section. CCAR25 transport aircraft airworthiness standards

3 Terms and Definitions

The following terms and definitions apply to this section. 3.1 The maximum stopping mass greater than 50000kg (110000lb) of passenger and cargo aircraft. 3.2 The maximum stopping mass greater than 10000kg (22000lb) and less than or equal 50000kg (110000lb) of passenger and cargo aircraft. 3.3 MRW Plane left the parking position when the maximum permissible mass under their own power or traction, including the maximum take-off mass (MTOW) and slide Fuel reserve amount.

4 Requirements

4.1 connector position Connections shall be designed to be directly connected to the drawbar in front of the auxiliary landing gear. Where applicable, the auxiliary rear landing gear can be set GB/T 24713.1-2009/ISO 8267-1.2005

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