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

飞机牵引杆连接件接口要求第1部分：干线飞机

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Issued by

Standardization Administration of China

Level / Type

National · Recommended

Issue date

November 30, 2009

Implementation date

July 1, 2010

Scope

GB/T 24713.1-2009 is the English-translated version of 飞机牵引杆连接件接口要求第1部分：干线飞机.

GB/T 24713.1-2009 — 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.

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Document preview — GB/T 24713.1-2009

National Standard of the People's Republic of China

ICS: 49.100
Classification: V 50

Issued by: Standardization Administration of China

What this standard covers1
Document data2
Standards quoted by this document3

What this standard covers

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.

Document data

International classification (ICS): 49.100.

Chinese classification (CCS): V50.

Estimated length of the Chinese original: 6,626 words.

Adopted international standard: ISO 8267-1-2005, IDT.

Standards quoted by this document

CCAR 25

......
This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 4 pages — is available in the English PDF.

Referenced standards

Normative references

GB/T 24713

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