ISO 11077:2014 pdf download.Aircraft ground equipment- De-icers—Functional requirements.
NOTE Lower temperatures, requiring special design and operating measures, can be agreed between manufacturer and purchaser. See Note in the Introduction.
4.2 Functions
4.2.1 The primary function of the de-icer shall be to apply heated dc-icing/anti-icing fluid from a variable height boom to the surfaces of stationary aircraft while traversing their perimeter. A hose shall also be fitted for ground use. The vehicle shall be acceptable for use around terminal gate areas, airport service roads, and aircraft service ramps.
NOTE A secondary function can also be to provide access when required to high elevation parts of the aircraft.
4,2.2 The maximum width and overall height with the boom in the stowed position shall be kept to a minimum. The maximum overall width should be minimum comp,flihle with stability objectives, and the overall height in the stowed position shall not exceed 4.0 m (13 ft. tin). Overall turning radius in this position should not exceed 12 m (40 It), though maximum possible manoeuvrabillty is recommended.
NOTE Over the road regulations In a ma)orlty of states allow a maximum width of 2,5 m (8 ft 2 1/2 In). A number of states allow 2.6 m (8 ½ ft) width. Conversely, some local road traffic regulations can require narrower widths. Depending on the airport of use. a lower height can also be necessary. See Note in the Introduction.
4.2.3 On an appropriate self-propelled chassis with an enclosed driver’s cabin, meeting the requirements oI4J. the deIcer shall provide
a) an aerial device with operator’s cabin or basket. Including safe access means from the ground In the stowed position, meeting the requirements of 4.4.
b) (a) fluid storage and supply tank(s), large enough to accommodate the fluid capacity necessary for servicing slandard.body and/or wlde.body or large capacity aircraft as required by the purchaser. meeting the requirements of 4.5.2. and
c) fluid pumping systems for applying heated de-icing fluid and heated or unheated anti-icing fluid to aircraft surfaces, meeting the requirements of 4.5.1.
4.2 Functions
4.2.1 The primary function of the de-icer shall be to apply heated dc-icing/anti-icing fluid from a variable height boom to the surfaces of stationary aircraft while traversing their perimeter. A hose shall also be fitted for ground use. The vehicle shall be acceptable for use around terminal gate areas, airport service roads, and aircraft service ramps.
NOTE A secondary function can also be to provide access when required to high elevation parts of the aircraft.
4,2.2 The maximum width and overall height with the boom in the stowed position shall be kept to a minimum. The maximum overall width should be minimum comp,flihle with stability objectives, and the overall height in the stowed position shall not exceed 4.0 m (13 ft. tin). Overall turning radius in this position should not exceed 12 m (40 It), though maximum possible manoeuvrabillty is recommended.
NOTE Over the road regulations In a ma)orlty of states allow a maximum width of 2,5 m (8 ft 2 1/2 In). A number of states allow 2.6 m (8 ½ ft) width. Conversely, some local road traffic regulations can require narrower widths. Depending on the airport of use. a lower height can also be necessary. See Note in the Introduction.
4.2.3 On an appropriate self-propelled chassis with an enclosed driver’s cabin, meeting the requirements oI4J. the deIcer shall provide
a) an aerial device with operator’s cabin or basket. Including safe access means from the ground In the stowed position, meeting the requirements of 4.4.
b) (a) fluid storage and supply tank(s), large enough to accommodate the fluid capacity necessary for servicing slandard.body and/or wlde.body or large capacity aircraft as required by the purchaser. meeting the requirements of 4.5.2. and
c) fluid pumping systems for applying heated de-icing fluid and heated or unheated anti-icing fluid to aircraft surfaces, meeting the requirements of 4.5.1.
