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SAE AS 1614D:2026-02-12

Main Line Aircraft Tow Bar Attach Fitting Interface

Summary

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 pounds), 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.

Notes

/ Note: Revision D

Technical characteristics

Publisher SAE International
Publication Date 02/12/2026
Confirmation Date 04/08/2021
Page Count 5
Themes Aerospace
EAN ---
ISBN ---
Weight (in grams) ---
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