Cena s DPH / bez DPH
Hlavní stránka>BS ISO 21100:2020 Air cargo unit load devices. Performance requirements and test parameters
Sponsored link
sklademVydáno: 2020-07-07
BS ISO 21100:2020 Air cargo unit load devices. Performance requirements and test parameters

BS ISO 21100:2020

Air cargo unit load devices. Performance requirements and test parameters

Formát
Dostupnost
Cena a měna
Anglicky Zabezpečené PDF
K okamžitému stažení
8990 Kč
Čtěte normu po dobu 1 hodiny. Více informací v kategorii E-READING
Čtení normy
na 1 hodinu
899.00 Kč
Čtěte normu po dobu 24 hodin. Více informací v kategorii E-READING
Čtení normy
na 24 hodin
2697.00 Kč
Anglicky Tisk
Skladem
8990 Kč
Označení normy:BS ISO 21100:2020
Počet stran:56
Vydáno:2020-07-07
ISBN:978 0 580 93367 7
Status:Standard
Popis

BS ISO 21100:2020


This standard BS ISO 21100:2020 Air cargo unit load devices. Performance requirements and test parameters is classified in these ICS categories:
  • 49.120 Cargo equipment
  • 49.100 Ground service and maintenance equipment

This document specifies the minimum requirements for airworthiness approval of air cargo pallets, nets and containers, generally designated as air cargo unit load devices (ULD).

This document is intended to provide a uniform technical reference for air cargo unit load devices approval. As a prerequisite, it is presupposed that the applicable general civil aviation requirements and the aircraft manufacturer’s approved Weight and Balance Manual are followed.

This document 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 9,0 g forward ultimate inertia force of § 25.561(b) (3) (ii).

This document applies to airworthiness approved air cargo unit load devices intended for carriage on board civil transport category airplanes type certificated under EASA CS-25 or 14 CFR Part 25, or equivalent.

This document exclusively applies to unit load devices airworthiness approval and testing parameters. It does not apply to aircraft design or aircraft operating requirements, which are provided by the approved Weight and Balance Manual for each aircraft type.

Other aspects that do not directly pertain to air cargo unit load devices airworthiness approval and testing are not covered by this document and are defined in other International Standards (see Bibliography), e.g.:

  1. ULD design specifications,

  2. ULD in service damage limits,

  3. ULD restraint malfunction limitations,

  4. ULD test methods,

  5. ULD load distribution models,

  6. ULD maximum allowable contours,

  7. ULD CG (centre for gravity) location control means,

  8. ULD pressure equalization methods,

  9. ULD utilization guidelines.

Air cargo unit load devices qualified prior to publication of this document were approved in accordance with the requirements of ISO 8097:2001. This document is intended as a TSO approval reference for all new models of unit load devices in the sizes and types it covers, in replacement of ISO 8097. For air cargo unit load devices the size or type of which is not covered in this document, see the requirements of ISO 8097:2001, if their size or type is contained therein, or other equivalent criteria, if not.

NOTE 1

ISO 8097 is based on USA National Aerospace Standard NAS 3610 revision 10:1990, Specification for Cargo Unit Load Devices.

NOTE 2

The requirements for cargo covers are not defined in this document, except insofar as net restraint is incorporated therein.