Standard

SAE AS1614C

Aug 2010 Withdrawn

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Language English

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Abstract

This SAE Aerospace Standard (AS) specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft with a maximum ramp weight higher than 50 000 kg (110 000 lb), commonly designated as “main line aircraft”. Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft weight category (which determines tow bar forces) in order to ensure that one single type of tow bar with a standard connection can be used for all aircraft types within or near that weight category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used.

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Standard from SAE International
Published: August 24 2010
Withdrawn: April 8 2021
Document type: IS
Pages
ISBN:

Publisher: SAE International
Distributor: SAE International

Product Relations

Replaced by: SAE AS1614D
Replaces: SAE AS1614B

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Version history Related Corrigenda and Amendments (0)

Version history History (2)

SAE AS1614C

SAE AS1614B

Abstract

Products specifications

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