AS1614C Main Line Aircraft Tow Bar Attach Fitting Interface

Reaffirmed

08/24/2010

Features
Issuing Committee
Scope
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/AS1614C
Pages
5
Citation
SAE International Technical Standard, Main Line Aircraft Tow Bar Attach Fitting Interface, SAE Standard AS1614C, Reaffirmed August 2010, Revised October 2003, Issued August 1981, https://doi.org/10.4271/AS1614C.
Additional Details
Publisher
Published
Aug 24, 2010
Product Code
AS1614C
Content Type
Technical Standard
Status
Reaffirmed
Language
English

Revisions