SAE ARP4806

Aerospace - Deicing/Anti-Icing Self-Propelled Vehicle Functional Requirements.

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Standard:
  • ARP4806
Issued:
  • 1994-10-01
Issuing:
  • G-12e Equipment Committee
Scope:

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 degrees C (-40 and 122 degrees 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:
StandardPublishedRevisionStatus
ARP48061994-10-01LatestIssued
AKA:
  • SAE ARP 4806
Sector:
  • Aerospace
Topic:
  • Aircraft Operations
  • Icing and Ice detection

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