49.120 – Cargo equipment – PDF Standards Store ?u= Wed, 06 Nov 2024 01:19:20 +0000 en-US hourly 1 https://wordpress.org/?v=6.7.1 ?u=/wp-content/uploads/2024/11/cropped-icon-150x150.png 49.120 – Cargo equipment – PDF Standards Store ?u= 32 32 ISO/TR 8647:1990 ?u=/product/publishers/iso/iso-tr-86471990/ Wed, 06 Nov 2024 01:19:20 +0000 Dégradation en environnement des textiles utilisés dans les équipements de retenue du fret aérien
Published By Publication Date Number of Pages
ISO 1990-07 24
]]> Dégradation en environnement des textiles utilisés dans les équipements de retenue du fret aérien
Published By Publication Date Number of Pages
ISO 1990-07 24
]]> ISO/PAS 21100:2011 ?u=/product/publishers/iso/iso-pas-211002011/ Wed, 06 Nov 2024 01:07:27 +0000 Air cargo unit load devices — Performance requirements and test parameters
Published By Publication Date Number of Pages
ISO 2011-10 42
]]> 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.

]]> ISO 9788:2017 ?u=/product/publishers/iso/iso-97882017/ Wed, 06 Nov 2024 00:30:05 +0000 Air cargo — Double stud tie-down fittings — Design and testing requirements
Published By Publication Date Number of Pages
ISO 2017-12 18
]]> ISO 9788:2017 specifies the geometry, performance and testing requirements for a double stud tie-down fitting assembly, having a load capacity of 22 250 N (5 000 lbf), when installed in rail or track conforming to ISO 7166.

Other materials than those specified can alternatively be used, provided the performance and testing requirements of this document are complied with.

Double stud tie-down fittings are intended to be used as either:

a) loose items to be attached to an air cargo pallet's track or an aircraft's floor rail in order to constitute a tie-down arrangement together with cargo restraint straps meeting the requirements of ISO 16049-1 or cargo restraint slings (steel cables) meeting the requirements of ISO 20291-1,

b) or permanently attached tie-down components of pallet nets meeting the requirements of ISO 4115 or ISO 4170.

In this case, where deemed appropriate, the stud geometry can alternatively conform to ISO 7166, and the breaking strength requirement can be limited to the value necessary to meet the net's airworthiness approval/certification in accordance with ISO 21100.

Single stud tie-down fittings are not covered by this document.

They nevertheless can, where deemed appropriate, use the same stud geometry alternatively to the stud configuration specified in applicable ISO 7166.

]]> ISO 9788:1990 ?u=/product/publishers/iso/iso-97881990/ Wed, 06 Nov 2024 00:30:05 +0000 Air cargo equipment — Cast components of double stud fitting assembly with a load capacity of 22 250 N (5 000 lbf), for aircraft cargo restraint
Published By Publication Date Number of Pages
ISO 1990-12 8
]]> Deals with the geometry and requirements for assemblies, when installed in rail conforming to ISO 7166. Other materials than those specified in 4.2 may alternatively be used, provided the performance and testing requirements of this standard are complied with. Includes definitions, certification and testing, designation and identification.

]]> ISO 9031:1987 ?u=/product/publishers/iso/iso-90311987/ Wed, 06 Nov 2024 00:20:18 +0000 Équipement pour le fret aérien — Systèmes de manutention des unités de charge — Symboles pour la représentation graphique
Published By Publication Date Number of Pages
ISO 1987-07 8
]]> The symbols given herein are applicable to all aircraft cargo-handling systems for underfloor as well as for main-deck systems. The conveyance, guidance, restraint, power drive unit and the degree of automation for the total cargo-handling system can be depicted using the symbols. Each cargo symbol consists of a basic symbol, which represents basic functions. It characterizes a component function, but not the detail design and manufacturing method.

]]> ISO 8268:1987 ?u=/product/publishers/iso/iso-82681987/ Wed, 06 Nov 2024 00:09:06 +0000 Air cargo equipment — Automobile transport devices — Basic requirements
Published By Publication Date Number of Pages
ISO 1987-02 16
]]> Provides functional, dimensional, structural and environmental requirements for devices used to transport automobiles in wide-body aircraft. These devices are intended to be used in conjunction with pallets compatible with existing aircraft restraint systems or with pallets matching the width of automobiles to ensure maximum use of aircraft volume. The devices shall be easily convertible so that they can carry general cargo on return haul flights.

]]> ISO 7715:1985 ?u=/product/publishers/iso/iso-77151985/ Tue, 05 Nov 2024 23:59:48 +0000 Air cargo equipment — Ground handling and transport systems for unit load devices — Minimum requirements
Published By Publication Date Number of Pages
ISO 1985-09 10
]]> Includes minimum performance and compatibility requirements for these systems for air cargo unit load devices, used to service civil wide body freight aircraft. Is applicable to equipment, designed to deal with main deck unitized cargo in the form of intermodal containers and other compatible unitized load devices.

]]> ISO 7716:1985 ?u=/product/publishers/iso/iso-77161985/ Tue, 05 Nov 2024 23:59:48 +0000 Équipement pour le fret aérien — Véhicules de transport d'unités de charge (VTU) — Caractéristiques fonctionnelles
Published By Publication Date Number of Pages
ISO 1985-09 12
]]> La présente Norme internationale spécifie les caractéristiques fonctionnelles minimales des châssis porte-unités de charge de type 3 et de classe A, conformément à la terminologie adoptée dans l'ISO 7715. Elle spécifie également les caractéristiques fonctionnelles des véhicules de transport d'unités de charge pour fret aérien capables de circuler dans les zones de traitement d'aéroports et sur les voies de circulation publiques et d'assurer le transbordement des unités de charge sur les matériels de manutention à rouleaux et vice versa.

]]> ISO 7166:1985 ?u=/product/publishers/iso/iso-71661985/ Tue, 05 Nov 2024 23:52:12 +0000 Aircraft — Rail and stud configuration for passenger equipment and cargo restraint
Published By Publication Date Number of Pages
ISO 1985-08 6
]]> Specifies the geometry and the partial dimensions of these parts used for securing passenger equipment and for cargo restraint, necessary to ensure interchangeability of these items. Individual strength requirements will determine the complete rail shape, such as incorporating the standard section integrally into an I-beam extrusion. The overall shape of the studs above the top of the rail will depend upon the application.

]]> ISO 6968:2005 ?u=/product/publishers/iso/iso-69682005/ Tue, 05 Nov 2024 23:50:00 +0000 Aircraft ground equipment — Lower deck loader — Functional requirements
Published By Publication Date Number of Pages
ISO 2005-11 12
]]> ISO 6968:2005 specifies the functional requirements for a self-propelled loader capable of raising air cargo unit load devices (ULDs) with base dimensions and maximum mass as specified.

The requirements of ISO 6968:2005 were determined based on generally recognized assumptions with regard to the normally intended use of aircraft ground support equipment, when used on the ramp of international civil airports in order to handle, service or maintain civil transport aircraft; and with regard to the environmental (surface, slope, weather, lighting, operating rules, staff qualification, etc.) conditions prevailing on the ramp area of the majority of international civil airports.

]]>