-
-
Available Formats
- Options
- Availability
- Priced From ( in USD )
-
Available Formats
-
- Immediate download
- $180.00
- Add to Cart
-
- Printed Edition
- Ships in 1-2 business days
- $207.00
- Add to Cart
Customers Who Bought This Also Bought
-
ISO/PAS 15594:2004
Priced From $123.00 -
ISO/PAS 3930:2009
Priced From $200.00 -
ISO 30004:2012
Priced From $223.00 -
ISO 28004-2:2014
Priced From $166.00
About This Item
Full Description
ISO/PAS 21100:2011 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 of FAR Part 25, except for the 9,0g forward ultimate inertia force of § 25.561 (b) (3) (ii).
ISO/PAS 21100:2011 applies to airworthiness approved air cargo unit load devices intended for carriage on board civil transport category airplanes of the type certificated under EASA CS-25 or FAR Part 25, or equivalent regulations.
ISO/PAS 21100:2011 applies exclusively to unit load device airworthiness approval and testing parameters. It does not apply to either aircraft design or aircraft operating requirements, which are provided by the approved Weight and Balance Manual for each aircraft type.
Document History
-
ISO 21100:2020
Air cargo unit load devices - Performance requirements and test parameters- Most Recent
-
ISO 21100:2014
Air cargo unit load devices - Performance requirements and test parameters- Historical Version
-
ISO/PAS 21100:2011
viewing
Air cargo unit load devices - Performance requirements and test parameters- Historical Version