ARP4806A Aerospace - Deicing/Anti-Icing Self-Propelled Vehicle Functional Requirements

Canceled

08/17/2022

Scope
Content

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.

Rationale
Content
This document was incorporated into ARP1971D.
Meta TagsDetails
DOI
https://doi.org/10.4271/ARP4806A
Pages
8
Citation
SAE International Recommended Practice, Aerospace - Deicing/Anti-Icing Self-Propelled Vehicle Functional Requirements, SAE Standard ARP4806A, Cancelled August 2022, Issued October 1994, https://doi.org/10.4271/ARP4806A.
Additional Details
Publisher
Published
Aug 17, 2022
Product Code
ARP4806A
Content Type
Recommended Practice
Status
Canceled
Language
English

Revisions