SAE ARP4806 PDF
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AEROSPACE – DEICING/ANTI-ICING SELF-PROPELLED VEHICLE FUNCTIONAL REQUIREMENTS
Description
This document specifies the general functional and performance requirements for a self-propelled, boom type aerial device equipped with an aircraft deicing/anti-icing fluid (ADF) spraying system. The unit shall be highly maneuverable for deicing and anti-icing all exterior surfaces of wide-body and narrow-body aircraft, e.g., B747 and DC9. The vehicle shall be suitable for day and night operations. The vehicle and all associated systems shall operate satisfactorily under the temperature conditions between -40 and 50 °C (-40 and 122 °F) and in continuous humidity of up to 100%.
It is not within the scope of this document to specify a comprehensive set of technical design criteria for aircraft deicing/anti-icing vehicles but only those relating to functional and performance requirements.
History
| ARP4806A | 2022-08-17 | Latest | Canceled |
| ARP4806 | 1994-10-01 | Historical | Issued |
| ISSUING COMMITTEE | G-12E Equipment Committee |
|---|---|
| DATE | 1994-10-01 |
| DOI | |
| ISCURRENT | |
| PAGE | 7 |
| PUBLISHER | SAE International |
| REVISED | ISSUED |
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