SAE ARP 4806-1994
航空航天.除冰/防冰自走车辆功能要求

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

SAE ARP 4806-1994 发布历史

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.

SAE ARP 4806-1994由美国机动车工程师协会 US-SAE 发布于 1994。

SAE ARP 4806-1994 在中国标准分类中归属于: V57 特种车辆，在国际标准分类中归属于: 49.100 地面服务和维修设备。

SAE ARP 4806-1994 发布之时，引用了标准

• ISO 6966-1993 航空器 飞机装载设备的基本要求
• SAE ARP 1247C-1993 

SAE ARP 4806-1994的历代版本如下：

• 1994年 SAE ARP 4806-1994 航空航天.除冰/防冰自走车辆功能要求

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标准号

SAE ARP 4806-1994

发布日期

1994年

实施日期

废止日期

无

中国标准分类号

V57

国际标准分类号

49.100

发布单位

美国机动车工程师协会

引用标准

ISO 6966-1993 SAE J 1211-1978 SAE AMS 1424 SAE AMS 1428 SAE ARP 1247C-1993 ATA 101

适用范围

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.