Over deze norm
|Commissie||Lucht- en ruimtevaart|
The purpose of this International Standard is to establish specify the minimum requirements for airworthiness approval of air cargo pallets, nets and containers, generally designated as air cargo unit load devices. This International Standard defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint and occupant protection requirements of EASA CS-25 or 14 CFR Part 25, except for the 9,0g forward ultimate inertia force of § 25.561(b) (3) (ii). This International Standard applies to airworthiness approved air cargo unit load devices intended for carriage on board civil transport category airplanes type certificated under EASA CS-25, “Certification Specifications for Large Aeroplanes” or 14 CFR Part 25, “Airworthiness Standards - Transport Category Airplanes”, or equivalent regulations.
|Nederlandse titel||Aircraft ground equipment - Performance requirements and test parameters|
|Engelse titel||Aircraft ground equipment - Performance requirements and test parameters|