SAE ARP4806A
Current
The latest, up-to-date edition.
Aerospace - Deicing/Anti-Icing Self-Propelled Vehicle Functional Requirements
Hardcopy , PDF
English
17-08-2022
Important note : Users cannot be edited or removed once added to your Multi user PDF.| DocumentType |
Standard
|
| Pages |
8
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
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.
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