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SAE AS1614 Rev D

Current Revision

Main Line Aircraft Tow Bar Attach Fitting Interface

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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.

SDO SAE: SAE International
Document Number AS1614
Publication Date Jan. 2, 2016
Language en - English
Page Count 5
Revision Level D
Supercedes
Committee
Publish Date Document Id Type View
Jan. 2, 2016 AS1614D Revision
Oct. 14, 2003 AS1614C Revision
Dec. 1, 1994 AS1614B Revision
Oct. 1, 1982 AS1614A Revision
Aug. 1, 1981 AS1614 Revision