This part of ISO 20683 is applicable to towbarless aircraft towing vehicles (TLTVs) interfacing with the noselanding gear of civil transport aircraft with a maximum ramp mass comprised between 10 000 kg and 50 000 kg (22 000 lb and 110 000 lb), commonly designated as “regional aircraft”. The requirements for main line transport aircraft with a higher maximum ramp mass are specified in ISO 20683-1, which is not applicable to TLTVs which were manufactured before its date of publication.
This part of ISO 20683 specifies general design requirements, testing and evaluation requirements, maintenance, calibration, documentation, records, tracing and accountability requirements in order to ensure that the loads induced by the tow vehicle not exceed the design loads of the nose gear or its steering system, or reduce the certified safe life limit of the nose gear, or induce a stability problem during aircraft push back and/or maintenance towing operations.
This part of ISO 20683 specifies requirements and procedures for towbarless tow vehicles (TLTVs) intended for aircraft push-back and gate relocation or maintenance towing only. It is not intended to allow for dispatch (operational) towing (3.7). Dispatch towing imposes greater loads on nose gears and aircraft structure due to the combination of speed and additional passenger, cargo, and fuel loads.
This part of ISO 20683 does not apply to towbarless towing vehicles interfacing with aircraft main landing gear.
NOTE TLTV designers should also take into account the requirements of documents referenced in Bibliography.