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Standard

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

2022-08-17
CURRENT
ARP4806A
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.
Standard

Enclosed Operator’s Cabin for Aircraft Ground Deicing Equipment

2022-08-17
CURRENT
ARP5058B
This SAE Aerospace Recommended Practice (ARP) is intended to establish guidelines and design requirements for an enclosed cabin for both mobile deicers and fixed deicing equipment. The enclosed cabin is located at the end of the deicing boom.
Standard

Aircraft Deicing Vehicle - Self-Propelled

2019-02-13
CURRENT
ARP1971D
This SAE Aerospace Recommended Practice (ARP) covers requirements for a self-propelled, boom-type aerial device, equipped with an aircraft deicing/anti-icing fluid spraying system. The unit shall be highly maneuverable for deicing all exterior surfaces of commercial aircraft, of sizes agreed upon between purchaser and manufacturer, in accordance with AS6285. The vehicle shall be suitable for day and night operations.
Standard

Forced Air or Forced Air/Fluid Equipment for Removal of Frozen Contaminants

2015-01-22
CURRENT
AIR6284
This SAE Aerospace Information Report (AIR) covers forced air technology including: reference material, equipment, safety, operation, and methodology. This resource document is intended to provide information and minimum safety guidelines regarding use of forced air or forced air/fluid equipment to remove frozen contaminants. During the effective period of this document, relevant sections herein should be considered and included in all/any relevant SAE documents.
Standard

Aircraft Deicing Vehicle – Self-Propelled

2011-05-06
HISTORICAL
ARP1971C
This SAE Aerospace Recommended Practice (ARP) covers requirements for a self-propelled, boom type aerial device, equipped with an aircraft deicing/anti-icing fluid spraying system. The unit shall be highly maneuverable for deicing all exterior surfaces of commercial aircraft, of sizes agreed upon between purchaser and manufacturer, in accordance with SAE ARP4737. The vehicle will also be used for aircraft maintenance and inspection. The vehicle shall be suitable for day and night operations.
Standard

Enclosed Operator's Cabin for Aircraft Ground Deicing Equipment

2004-06-21
HISTORICAL
ARP5058A
This SAE Aerospace Recommended Practice (ARP) is intended to establish guidelines and design requirements for an enclosed cabin for both mobile deicers and fixed deicing equipment. The enclosed cabin is located at the end of the deicing boom.
Standard

ENCLOSED OPERATOR’S CABIN FOR AIRCRAFT GROUND DEICING EQUIPMENT

1996-06-01
HISTORICAL
ARP5058
This SAE Aerospace Recommended Practice (ARP) is intended to establish guidelines and design requirements for an enclosed cabin for both mobile deicers and fixed deicing equipment. The enclosed cabin is located at the end of the deicing boom.
Standard

AEROSPACE - DEICING/ANTI-ICING SELF-PROPELLED VEHICLE FUNCTIONAL REQUIREMENTS

1994-10-01
HISTORICAL
ARP4806
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.
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