| Name |
Description |
Abstract |
Status |
Publication date |
Edition |
Number of pages |
Technical committee |
ICS |
| ISO 6833:1983 |
Air cargo — Minimum requirements for future wide-body aircraft cargo systems and compartments (intermodal) |
|
Withdrawn |
1983-06 |
Edition : 1 |
Number of pages : 13 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 6965:1982 |
Aircraft — Self-propelled gantry for lifting air cargo containers and outsize cargoes — Functional requirements |
Gives the requirements for a gantry capable of raising from the ground, transporting and stacking two high: corner fitting equipped air/surface intermodal containers per ISO 1496/7, surface container, equipped with 8 corner fittings per ISO 1161 and various pieces of outsize cargo. The methods and devices used to lift corner fitting containers with the unit shall comply with ISO 3874.
|
Withdrawn |
1982-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 10537:2010/Amd 1:2015 |
Space data and information transfer systems — Encapsulation service — Amendment 1 |
|
Withdrawn |
2015-07 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 6966-1:2005 |
Aircraft ground equipment — Basic requirements — Part 1: General design requirements |
ISO 6966-1:2005 specifies the minimum general design requirements applicable to aircraft ground support equipment in order to ensure
definition of aircraft ground support equipment general requirements for designers;effective operation of aircraft ground support equipment.
The requirements of ISO 6966-1:2005 apply to any piece of aircraft ground support equipment used on airports.
ISO 6966-1:2005 does not intend to provide all the design requirements applicable for aircraft ground support equipment. Other requirements apply, and can be found in separate standards:
ISO 6966-2 specifies the safety-related requirements applicable to all aircraft ground support equipment;ISO 4116 specifies the additional requirements applicable for conveying surfaces of those pieces of aircraft ground support equipment intended for handling and loading of baggage and cargo unit load devices (ULDs);specific standards, listed in the Bibliography, define the functional and performance requirements for certain types of aircraft ground support equipment.
ISO 6966-1:2005 does not apply to unmodified general-use transportation vehicles such as automobiles, vans, buses and flat-bed trucks when used on airports.
|
Published |
2005-11 |
Edition : 1 |
Number of pages : 15 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 6966-2:2005 |
Aircraft ground equipment — Basic requirements — Part 2: Safety requirements |
ISO 6966-2:2005 specifies the minimum design requirements applicable to all aircraft ground support equipment in order to ensure
safety of staff operating or maintaining the equipment or in its vicinity;protection of aircraft against interference or damage.
The requirements of ISO 6966-2:2005 apply to any piece of aircraft ground support equipment used on airports.
ISO 6966-2:2005 does not provide all the design requirements applicable for aircraft ground support equipment. Other requirements apply, and can be found in separate standards:
ISO 6966-1 specifies the general, other than safety related, design requirements applicable to all aircraft ground support equipment;ISO 4116 specifies the additional requirements applicable for conveying surfaces of those pieces of aircraft ground support equipment intended for handling and loading of baggage and cargo unit load devices;specific standards, listed in the Bibliography, define the functional and performance requirements for certain types of aircraft ground support equipment.
|
Withdrawn |
2005-11 |
Edition : 1 |
Number of pages : 16 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 6966-2:2014 |
Aircraft ground equipment — Basic requirements — Part 2: Safety requirements |
ISO 6966-2:2014 specifies the minimum design requirements applicable to all aircraft ground support equipment (GSE) in order to ensure safety of staff operating or maintaining the equipment or in its vicinity, and protection of aircraft against interference or damage.
ISO 6966-2:2014 does not apply to automotive vehicles or parts thereof approved for public vehicles, when used on aircraft ground support equipment for the purpose for which they are designed.
|
Published |
2014-08 |
Edition : 2 |
Number of pages : 27 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 6966:1982 |
Aircraft — Basic requirements for aircraft loading equipment |
|
Withdrawn |
1982-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 6966:1993 |
Aircraft — Basic requirements for aircraft loading equipment |
Specifies the basic mechanical, electrical, hydraulic and pneumatic requirements as well as requirements for materials, workmanship, national codes of practice, safety, environment, mobility, transport, maintenance, manuals and optional features.
|
Withdrawn |
1993-12 |
Edition : 2 |
Number of pages : 9 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 6967:1983 |
Aircraft — Wide body aircraft main deck container/pallet loader — Functional requirements |
|
Withdrawn |
1983-11 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 6967:1994 |
Aircraft — Wide body aircraft main deck container/pallet loader — Functional requirements |
Specifies the requirements for a self-propelled loader capable of raising pallets and containers with base dimensions and maximum weights according to the table. Gives information on structure and overall dimensions, platform design, guide rails and stops, platform operation and loading, mobility and stability and controls.
|
Withdrawn |
1994-09 |
Edition : 2 |
Number of pages : 4 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 6967:2006 |
Aircraft ground equipment — Main deck loader — Functional requirements |
ISO 6967:2006 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 6967:2006 were determined based on generally recognized assumptions with regard to the normally intended use of aircraft ground 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.
|
Published |
2006-02 |
Edition : 3 |
Number of pages : 7 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 6968:1994 |
Aircraft — Wide body aircraft lower deck container/pallet loader — Functional requirements |
Specifies the requirements for a self-propelled loader capable of raising pallets and containers with base dimensions and maximum weights according to the table. Gives information on structure and overall dimensions, platform design, guide rails and stops, platform operation and loading, mobility and stability and controls.
|
Withdrawn |
1994-09 |
Edition : 2 |
Number of pages : 4 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 6968:2005 |
Aircraft ground equipment — Lower deck loader — Functional requirements |
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.
|
Published |
2005-11 |
Edition : 3 |
Number of pages : 7 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 7166:1985 |
Aircraft — Rail and stud configuration for passenger equipment and cargo restraint |
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.
|
Published |
1985-08 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 7715:1985 |
Air cargo equipment — Ground handling and transport systems for unit load devices — Minimum requirements |
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.
|
Published |
1985-09 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 7716:1985 |
Air cargo equipment — Unit load devices transport vehicle (UTV) — Functional requirements |
Specifies minimum requirements for type 3, class A, air cargo unit load device chassis in accordance with the terminology defined in ISO 7715. Outlines the requirements for a transport vehicle, capable of carrying unit load devices over airport and public roads and transferring them to/from rollerized handling equipment.
|
Published |
1985-09 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 8268:1987 |
Air cargo equipment — Automobile transport devices — Basic requirements |
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.
|
Published |
1987-02 |
Edition : 1 |
Number of pages : 12 |
Technical Committee |
49.120
Cargo equipment
|
| ISO/TR 8647:1990 |
Environmental degradation of textiles used in air cargo restraint equipment |
|
Published |
1990-07 |
Edition : 1 |
Number of pages : 17 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 9031:1987 |
Air cargo equipment — Handling systems for unit load devices (ULDs) — Symbols for pictorial representation |
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.
|
Published |
1987-07 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.120
Cargo equipment
;
01.080.20
Graphical symbols for use on specific equipment
|
| ISO 9788:1990 |
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 |
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.
|
Withdrawn |
1990-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 3004-6:1986 |
Light gauge metal containers — Capacities and related cross-sections — Part 6: Open-top cans for milk |
|
Withdrawn |
1986-10 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
55.120
Cans. Tins. Tubes
|
| ISO 9788:2017 |
Air cargo — Double stud tie-down fittings — Design and testing requirements |
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.
|
Published |
2017-12 |
Edition : 2 |
Number of pages : 10 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 10254:1995 |
Air cargo and ground equipment — Vocabulary |
Defines 117 terms in English and French in the alphabetic order of the English versions. Alphabetic indexes in English and French are given the English index including all entries resulting from repositioning of the words in a term.
|
Withdrawn |
1995-01 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 10254:2016 |
Air cargo and ground equipment — Vocabulary |
ISO 10254:2016 defines the terms relating to air cargo and aircraft ground equipment, as used in the other International Standards in these areas.
NOTE The term "weight" is used throughout ISO 10254:2016 instead of the correct technical term "mass", in order to conform to current commercial usage.
The terms and abridged definitions of ISO 10254:2016 are primarily intended to provide uniform understanding of the International Standards prepared by TC20/SC9. However, it is intended that they be used in any other documents, manuals and standards in the areas of air cargo and airport ground equipment.
More detailed definitions are provided when needed in the "Terms and definitions" clause of the specific International Standards prepared by TC20/SC9.
The terms are listed in alphabetic sequence in the English language version. An index allows the identification of terms from their French or German expressions.
|
Published |
2016-07 |
Edition : 2 |
Number of pages : 49 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO/CD 10254 |
Air cargo and ground equipment — Vocabulary |
ISO 10254:2016 defines the terms relating to air cargo and aircraft ground equipment, as used in the other International Standards in these areas.
NOTE The term "weight" is used throughout ISO 10254:2016 instead of the correct technical term "mass", in order to conform to current commercial usage.
The terms and abridged definitions of ISO 10254:2016 are primarily intended to provide uniform understanding of the International Standards prepared by TC20/SC9. However, it is intended that they be used in any other documents, manuals and standards in the areas of air cargo and airport ground equipment.
More detailed definitions are provided when needed in the "Terms and definitions" clause of the specific International Standards prepared by TC20/SC9.
The terms are listed in alphabetic sequence in the English language version. An index allows the identification of terms from their French or German expressions.
|
Under development |
|
Edition : 3 |
|
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
|
| ISO 11995:1996 |
Aircraft — Stability requirements for loading and servicing equipment |
Specifies the criteria to be used to determine stability of aircraft loading and servicing equipment, including wind loads. Is intended to define uniform criteria, calculation and testing methods in order to provide a safe work environment under all predictable circumstances.
|
Published |
1996-06 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 12118:1995 |
Air cargo equipment — Identification of double-stud tie-down fittings having an omnidirectional rated load capacity of 22 250 N (5 000 lbf) or above |
Specifies an identification scheme for double-stud tie-down fittings having an omnidirectional rated load capacity of 22 250 N (5 000 lbf) or above in a rail conforming to ISO 7166. Applicable to all cargo tie-down fittings equipped with a movable plunger, regardless of material or method of fabrication.
|
Withdrawn |
1995-03 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 12174:1998 |
Space data and information transfer systems — Telecommand — Data management service — Architectural specification |
|
Withdrawn |
1998-07 |
Edition : 1 |
Number of pages : 39 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14186:2013 |
Air cargo — Fire containment covers — Design, performance and testing requirements |
ISO 14186:2013 specifies the minimum design and performance criteria and testing methods of fire containment covers (FCCs) used:
either in those cargo compartments of civil transport aircraft where they constitute one means of complying with applicable airworthiness regulations,
or on a voluntary basis, when deemed appropriate by operators to improve fire protection in aircraft cargo compartments where airworthiness regulations do not mandate their use.
|
Published |
2013-08 |
Edition : 1 |
Number of pages : 26 |
Technical Committee |
49.120
Cargo equipment
;
13.220.20
Fire protection
|
| ISO 16049-1:2001 |
Air cargo equipment — Restraint straps — Part 1: Design criteria and testing methods |
|
Withdrawn |
2001-07 |
Edition : 1 |
Number of pages : 17 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 16049-1:2013 |
Air cargo equipment — Restraint straps — Part 1: Design criteria and testing methods |
ISO 16049-1:2013 specifies the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical rated ultimate tension load capability of 22 250 N (5 000 lbf), as used by the airline industry in order to restrain on board civil transport aircraft during flight:
a) cargo loaded and tied down onto airworthiness approved air cargo pallets, themselves restrained into aircraft lower deck, main deck or upper deck cargo systems and meeting the requirements of ISO 8097 (NAS 3610) or ISO 21100, or
b) non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained ("floating") pallet into either lower deck, main deck or upper deck containerized cargo compartments of an aircraft.
The same restraint strap assemblies can also be used in other applications such as:
c) non-containerized (bulk loaded) baggage and cargo compartments,
d) to ensure cargo restraint inside an airworthiness approved air cargo container.
Compliance with ISO 16049-1:2013 provides one means of cargo restraint straps airworthiness approval by Civil Aviation Authorities under TSO/ETSO C-172, in addition to the other requirements therein.
|
Withdrawn |
2013-03 |
Edition : 2 |
Number of pages : 19 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 16049-1:2020 |
Air cargo equipment — Restraint straps — Part 1: Design criteria and testing methods |
This document specifies the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22 250 N (5 000 lbf) rated ultimate tension load capability, as used by the airline industry. These restraint straps are used in civil transport aircraft during flight for:
a) cargo loaded and tied down onto airworthiness approved air cargo pallets, themselves restrained into aircraft lower deck, main deck or upper deck cargo systems and meeting the requirements of ISO 8097 (NAS 3610) or ISO 21100, or
b) non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained ("floating") pallet into either lower deck, main deck or upper deck containerized cargo compartments of an aircraft,
c) the same restraint strap assemblies can also be used in other applications such as:
1) non-containerized (bulk loaded) baggage and cargo compartments;
2) to ensure cargo restraint inside an airworthiness approved air cargo container.
NOTE The ultimate loads allowable on the attachment points available in most aircraft bulk compartments and inside many air cargo containers are significantly lower than 22 250 N (5 000 lbf). This results in the restraint arrangements ultimate load capability being dictated by the weakest element, i.e. the attachment points: typical 22 250 N ultimate load restraint straps will therefore be in excess of the requirements for such applications.
Compliance with this document provides one means of cargo restraint straps airworthiness approval by Civil Aviation Authorities under TSO/ETSO-C172a, in addition to the other requirements therein.
|
Published |
2020-01 |
Edition : 3 |
Number of pages : 22 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 16049-2:2005 |
Air cargo equipment — Restraint straps — Part 2: Utilization guidelines and lashing calculations |
ISO 16049-2:2005 specifies utilization guidelines and principles to be used in strength calculation methods adequate to guarantee the effectiveness and ultimate load strength of tie-down/lashing arrangements used to restrain cargo on board civil transport aircraft during flight for either cargo loaded and tied down onto airworthiness certified air cargo pallets, themselves restrained into aircraft lower deck or main deck cargo systems meeting the requirements of ISO 8097; additional tie-down on aircraft structure when necessitated by pallet maximum gross mass or centre of gravity limits; non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained ("floating") pallet into either lower deck or main deck containerized cargo compartments of an aircraft; or individual pieces of load loaded in non containerized (bulk loaded) baggage or cargo compartments.
ISO 16049-2:2005 is applicable to cargo tie-down/lashing arrangements using exclusively air cargo restraint straps conforming to ISO 16049-1. Its general recommendations may be used for tie-down arrangements using other means (e.g. steel cables, rope, chains, other types of straps), but under the user's responsibility as to their adequacy and the strength calculations required.
ISO 16049-2:2005 is not applicable to the use of chains or other rigid devices for tie-down onto civil transport aircraft floor tracks. These devices are generally not recommended for use due to the possibility of generating excessive stresses in the aircraft structure, except where explicitly approved in the manufacturer's Authority approved Weight and Balance Manual.
ISO 16049-2:2005 is intended to provide industry recognized means of complying with Airworthiness Authorities general regulations applicable to load-securing on board civil transport aircraft (see FAR/JAR Parts 25), and aircraft manufacturers Authority approved Weight and Balance Manuals for each aircraft type as specified therein. It is not the intent of ISO 16049-2:2005 to specify when restraint straps should be used, but how they should be used. It does not, under any circumstance, supersede the requirements of any of the above documents that take precedence at all times.
|
Withdrawn |
2005-02 |
Edition : 1 |
Number of pages : 15 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 16049-2:2013 |
Air cargo equipment — Restraint straps — Part 2: Utilization guidelines and lashing calculations |
ISO 16049-2:2013 provides general utilization guidelines and calculation methods adequate to guarantee the effectiveness and ultimate load strength of tie-down/lashing arrangements performed to restrain cargo on board civil transport aircraft during flight:
a) cargo loaded and tied down onto airworthiness approved air cargo pallets, themselves restrained into aircraft lower deck or main deck or upper deck cargo systems meeting the restraint requirements of air cargo pallets approved in accordance with ISO 8097, (NAS3610) or ISO/PAS 21100, or
b) additional tie-down on aircraft structure when necessitated by pallet maximum gross mass or centre of gravity limits, or
c) non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained ("floating") pallet into either lower deck, main deck or upper deck containerized cargo compartments of an aircraft, or
d) individual pieces of load loaded in non-containerized (bulk loaded) baggage or cargo compartments.
ISO 16049-2:2013 applies to cargo tie-down/lashing arrangements using exclusively air cargo restraint straps conforming to ISO 16049-1. Its general recommendations may also be used for tie-down arrangements using other means (e.g. steel cables, rope, other types of straps), but under the user's responsibility as to their adequacy and the strength.
ISO 16049-2:2013 provides industry recognized means of complying with Airworthiness Authorities general regulations applicable to load securing on board civil transport aircraft (see 14 CFR Part 25 and EASA CS-25), and aircraft manufacturers Authority approved Weight and Balance Manuals for each aircraft type as specified therein. It is not the intent of this part of ISO 16049 to specify when restraint straps should be used, but how they should be used. It does not, under any circumstance, supersede the requirements of any of the above documents that take precedence at all times.
|
Withdrawn |
2013-05 |
Edition : 2 |
Number of pages : 14 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 16049-2:2020 |
Air cargo equipment — Restraint straps — Part 2: Utilization requirements and recommendations and lashing calculations |
This document aims at providing general utilization requirements and recommendations and calculation methods adequate to guarantee the effectiveness and ultimate load strength of tie-down/lashing arrangements performed to restrain cargo on board civil transport aircraft during flight:
a) cargo loaded and tied down onto airworthiness approved air cargo pallets, themselves restrained into aircraft lower deck or main deck or upper deck cargo systems meeting the restraint requirements of air cargo pallets approved in accordance with ISO 8097 (NAS3610) or ISO 21100, or
b) additional tie-down on aircraft structure when necessitated by pallet maximum gross mass or centre of gravity limits, or
c) non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained ("floating") pallet into either lower deck, main deck or upper deck containerized cargo compartments of an aircraft, or
d) individual pieces of load loaded in non-containerized (bulk loaded) baggage or cargo compartments.
This document applies to cargo tie-down/lashing arrangements using exclusively air cargo restraint straps conforming to ISO 16049-1. Its general recommendations may also be used for tie-down arrangements using other means (e.g. steel cables, rope, other types of straps), but under the user's responsibility as to their adequacy and the strength calculations required.
NOTE 1 Where tie-down is performed onto aircraft structure as per b) or c) above, additional restrictions can be stated in the aircraft's Authority approved Weight and Balance Manual.
NOTE 2 The use of chains, rods, or other rigid devices for tie-down onto civil transport aircraft floor tracks, which can generate excessive stress in the aircraft structure, is not part of the scope of this document. .
This document aims at providing industry recognized means of complying with Airworthiness Authorities general requirements applicable to load securing on board civil transport aircraft (see CCAR-25, JAS Part 3, 14 CFR Part 25 and EASA CS-25), and aircraft manufacturers Authority approved Weight and Balance Manuals for each aircraft type as specified therein. It is not the intent of this document to specify when restraint straps should be used, but how they should be used.
Meeting the methods requirements of this document is not alone sufficient to ensure flight safety: this document is based on the assumption that cargo tie-down will be designed, performed, and checked prior to aircraft departure in accordance with appropriate operating instructions conforming to the Weight and Balance Manual of the aircraft concerned, by competent, suitably trained, personnel as defined for example in ISO 9001:2015, 6.2.2 (see Clause 8).
|
Published |
2020-01 |
Edition : 3 |
Number of pages : 17 |
Technical Committee |
49.120
Cargo equipment
|
| ISO 21100:2014 |
Air cargo unit load devices — Performance requirements and test parameters |
The purpose ISO 21100:2014 is to establish the minimum requirements for airworthiness approval of air cargo pallets, nets and containers, generally designated as air cargo unit load devices.
ISO 21100:2014 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.
ISO 21100:2014 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.
ISO 21100:2014 exclusively applies to unit load devices 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.
|
Withdrawn |
2014-09 |
Edition : 1 |
Number of pages : 42 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO/PAS 21100:2011 |
Air cargo unit load devices — Performance requirements and test parameters |
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.
|
Withdrawn |
2011-10 |
Edition : 1 |
Number of pages : 37 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 21100:2020 |
Air cargo unit load devices — Performance requirements and test parameters |
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.:
— ULD design specifications,
— ULD in service damage limits,
— ULD restraint malfunction limitations,
— ULD test methods,
— ULD load distribution models,
— ULD maximum allowable contours,
— ULD CG (centre for gravity) location control means,
— ULD pressure equalization methods,
— 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.
|
Published |
2020-06 |
Edition : 2 |
Number of pages : 46 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 10537:2016 |
Space data and information transfer systems — Encapsulation service |
ISO 10537:2016 defines the Encapsulation Service in terms of:
a) the service primitives provided to the users of this service;
b) the protocol data units employed by the service provider; and
c) the procedures performed by the service provider.
It does not specify:
a) individual implementations or products;
b) the implementation of service interfaces within real systems;
c) the methods or technologies required to perform the procedures; or
d) the management activities required to configure and control the service.
|
Published |
2016-11 |
Edition : 2 |
Number of pages : 29 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 21785:2020 |
Air cargo unit load devices — Load distribution model |
This document defines the industry agreed model for load distribution on air cargo unit load devices (ULD) bases to apply the maximum allowable centre of gravity (C.G.) eccentricity.
Its purpose is to establish a common reference load distribution algorithm for:
a) comparable and repeatable ULD testing methods, or equivalent numeric simulations;
b) aircraft structure and cargo systems design assumptions, consistent with existing airframers practices; and
c) definition of operators unit load devices utilization rules and cargo build-up training programs.
It applies to all types of unit load devices intended for use on board civil transport aircraft and airworthiness approved in accordance with the performance requirements and testing parameters of either ISO 21100 or, as applicable, ISO 8097.
It also applies to non-airworthiness approved (non-certified) containers as defined in ISO 4118, the utilisation of which is controlled by the provisions of the aircraft type's Weight and Balance Manual and other airframe manufacturer's documents.
|
Published |
2020-02 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO/DIS 32312-11 |
Aircraft ground support equipment — Specific requirements — Part 11: Container/Pallet dollies and loose load trailers |
|
Under development |
|
Edition : 1 |
Number of pages : 21 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 4115:1980 |
Air-land cargo pallet nets — Specification and testing |
|
Withdrawn |
1980-10 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4115:1987 |
Air cargo equipment — Air/land pallet nets |
|
Withdrawn |
1987-05 |
Edition : 2 |
Number of pages : 7 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4115:1997 |
Air cargo equipment — Air/land pallet nets |
|
Published |
1997-12 |
Edition : 3 |
Number of pages : 6 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4117:1980 |
Air and air-land cargo pallets — Specification and testing |
|
Withdrawn |
1980-10 |
Edition : 1 |
Number of pages : 27 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4117:1993 |
Air and air/land cargo pallets — Specification and testing |
Gives dimensional, structural and environmental requirements for 2,44 m wide pallets to be used in freighter versions of high-capacity fixed wing aircraft and is intended to be compatible with the 2,44 × 2,44 m cross-section containers described in International Standards for air-land cargo containers. Pallet nets used in conjunction with these pallets are described in ISO 4115.
|
Published |
1993-02 |
Edition : 2 |
Number of pages : 24 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4118:1980 |
Non-certified lower deck containers for air transport — Specification and testing |
|
Withdrawn |
1980-10 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4118:1996 |
Non-certified lower-deck containers for air transport — Specification and testing |
Specifies the general design, performance and testing requirements for compartment-restrained lower-deck containers for air transport which do not require airworthiness certification.
|
Withdrawn |
1996-04 |
Edition : 2 |
Number of pages : 16 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4118:1996/Cor 1:1999 |
Non-certified lower-deck containers for air transport — Specification and testing — Technical Corrigendum 1 |
|
Withdrawn |
1999-10 |
Edition : 2 |
Number of pages : 1 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4118:2005 |
Air cargo — Non-certified containers for the lower deck of large-capacity aircraft — Specification and testing |
ISO 4118:2005 specifies the requirements for lower-deck containers in large-capacity aircraft which do not require airworthiness certification when loaded under the conditions of compartment restraint and/or, where applicable according to aircraft type, ISO 8097 (NAS 3610) equivalent base-plate restraint.
|
Withdrawn |
2005-10 |
Edition : 3 |
Number of pages : 32 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 10789:2011 |
Space systems — Programme management — Information and documentation management |
ISO 10789:2011 describes the processes and the requirements for the management of information/documentation within space programmes and projects.
The requirements specified in ISO 10789:2011 apply to and affect the customer and supplier at all levels.
When viewed from the perspective of a specific project context, the requirements defined in ISO 10789:2011 need to be tailored to match the specific requirements of the particular profile and circumstances of a project.
Defence information and documentation are not part of the scope of ISO 10789:2011.
|
Published |
2011-09 |
Edition : 1 |
Number of pages : 16 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 4118:2016 |
Air cargo — Non-certified lower deck containers — Design and testing |
ISO 4118:2016 covers the design, performance and testing requirements for lower deck containers for use in main line aircraft which do not require airworthiness approval/certification when loaded under the conditions of compartment restraint and/or where applicable according to the aircraft type's approved Weight and Balance Manual, ISO 8097 or ISO 21100 equivalent base plate restraint for these containers.
Aircraft Weight and Balance Manuals require non-certified containers be constructed then loaded in such a manner that neither the container nor its contents can become a hazard or damage the aircraft structure under flight conditions. Compliance with ISO 4118:2016 is one means of demonstrating compliance with these requirements.
Most sizes of containers covered by ISO 4118:2016 (base sizes K, L, P and Q) cannot physically be loaded and latched on aircraft main deck cargo systems. Base size A and M containers can, but are not allowed on aircraft main decks, which in general do not accept non-certified units. Accordingly, all containers covered by ISO 4118:2016 are intended to be used/installed exclusively in aircraft lower deck compartments
NOTE The metric equivalents for dimensions have been rounded up or down to the nearest millimetre, except in critical dimensions. Masses have been rounded up to the nearest kilogram and forces have been rounded up to the nearest 10 N. See introduction where it is deemed necessary to use exact values.
|
Published |
2016-07 |
Edition : 4 |
Number of pages : 37 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4128:1985 |
Aircraft — Air mode modular containers |
Lays down the dimensions and specifies the basic requirements for the specification and testing of containers to be used exclusively in conjunction with the air mode in freighter versions of high-capacity fixed-wing aircraft. Furthermore gives environmental criteria and marking requirements.
|
Published |
1985-09 |
Edition : 1 |
Number of pages : 16 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4170:1980 |
Interline air cargo pallet nets |
|
Withdrawn |
1980-10 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4170:1987 |
Air cargo equipment — Interline pallet nets |
|
Withdrawn |
1987-05 |
Edition : 2 |
Number of pages : 5 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4170:1995 |
Air cargo equipment — Interline pallet nets |
Specifies dimensional, structural and environmental requirements for nets used to secure cargo on aircraft pallets meeting the requirements of ISO 4117 or ISO 4171. Establishes six basic sizes of pallet nets.
|
Published |
1995-01 |
Edition : 3 |
Number of pages : 4 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4171:1980 |
Interline air cargo pallets |
|
Withdrawn |
1980-10 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 4171:1993 |
Air cargo equipment — Interline pallets |
The document establishes dimensional, structural and environmental requirements for pallets used to transport cargo in aircraft using nets meeting the requirements of ISO 4170. Includes design loads, operational criteria, resistance to local indentation, to bridging and resting and to impact loads, ball load capacity, performance on ball units, abrasion resistance for plastic-coated or magnesium-base materials, execution of tests and markings.
|
Published |
1993-09 |
Edition : 2 |
Number of pages : 8 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 6517:1982 |
Aircraft — Containers — Base-restrained certified containers for the lower deck of high capacity aircraft |
|
Withdrawn |
1982-02 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 6517:1992 |
Air cargo equipment — Base-restrained certified containers exclusively for the lower deck of high-capacity aircraft |
Covers the design, fabrication, performance and testing requirements for the containers. Basic functions of containers are the unitization of baggage, cargo or mail during ground handling and transportation, and the restraint of its contents in flight.
|
Withdrawn |
1992-08 |
Edition : 2 |
Number of pages : 13 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 6517:2013 |
Air cargo — Certified lower deck containers — Design and testing |
ISO 6517:2013 covers the minimum design and operational testing requirements for general purpose base-restrained containers exclusively intended for the lower deck compartments of main line civil transport aircraft, capable of being used by either airlines or shippers and requiring airworthiness authority approval (certification).
ISO 6517:2013 does not cover the performance requirements and ultimate load testing parameters for approval by airworthiness authorities (certification), which are covered in ISO 21100 or, for units approved prior to 2012, ISO 8097:2001. The design and operational testing requirements of ISO 6517:2013 are additional to those of these standards.
|
Published |
2013-07 |
Edition : 3 |
Number of pages : 21 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 8058:1985 |
Air cargo equipment — Air mode insulated containers — Thermal efficiency requirements |
|
Withdrawn |
1985-05 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 8058:1999 |
Air cargo — Insulated container — Thermal efficiency requirements |
This International Standard specifies the minimum operational requirements for thermal efficiency to ensure that
perishable cargoes in insulated standard airborne containers are kept in prime condition during the ground handling
and air transportation cycle for a maximum period of 36 h.
It is applicable to all insulated air cargo containers irrespective of their size and designation. It does not provide
details concerning refrigerated or heated containers and/or the methods and equipment used to obtain the required
thermal effect, such as cryogenic, gaseous or liquid fluids, or mechanical compressors/heaters.
NOTES
1 The term "perishable cargo" refers, for example, to dairy produce, fruit, vegetables, flowers, frozen foods, meat, fish, etc.,
requiring maintenance of specific temperature ranges during door-to-door transportation involving air transport.
2 It should be noted that throughout this document environmental (atmospheric) temperatures are expressed in commercial
values of degrees Celsius/Fahrenheit (°C/°F) and technical (scientific) temperatures are expressed in the International
Standard measure, kelvin (K). A temperature conversion table is given for convenience in annex A.
|
Published |
1999-04 |
Edition : 2 |
Number of pages : 9 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 8097:1986 |
Aircraft — Minimum airworthiness requirements and test conditions for certified air cargo unit load devices |
|
Withdrawn |
1986-10 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 8097:1993 |
Aircraft — Minimum airworthiness requirements and test conditions for certified air cargo unit load devices |
|
Withdrawn |
1993-08 |
Edition : 2 |
Number of pages : 2 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 8097:1995 |
Aircraft — Minimum airworthiness requirements and test conditions for certified air cargo unit load devices |
Lays down the minimum requirements and test conditions for certified cargo unit load devices in certified aircraft. Covers pallets, nets and containers for the class I and class II of aircraft loading and restraint systems.
|
Withdrawn |
1995-08 |
Edition : 3 |
Number of pages : 2 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 8097:2001 |
Aircraft — Minimum airworthiness requirements and test conditions for certified air cargo unit load devices |
This International Standard specifies the minimum requirements and test conditions for certified cargo unit load
devices to be installed in certified aircraft. It covers pallets, nets and containers intended for use with the following
classes of aircraft loading and restraint systems:
_ Class I: Unit load device restraint in conformity with all flight and ground load conditions, including 9g forward
emergency loading conditions.
_ Class II: All other unit load device restraints.
|
Published |
2001-08 |
Edition : 4 |
Number of pages : 3 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 9469:1991 |
Air cargo equipment — Unit load devices for transportation of horses |
Specifies the design and performance for two types of unit load devices; type 1: airworthiness certified structural unit (complying with ISO 8097), type 2: non-certified unit.
|
Published |
1991-12 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 10327:1995 |
Aircraft — Certified aircraft container for air cargo — Specification and testing |
|
Withdrawn |
1995-02 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 10327:2014 |
Air cargo — Main deck containers — Design and testing |
ISO 10327:2014 covers the minimum design and operational testing requirements for general purpose, base-restrained containers exclusively intended for the main or upper deck cargo compartments of main line civil transport aircraft, capable of being used by either airlines or shippers and requiring an airworthiness authority approval (certification).
ISO 10327:2014 does not cover the performance requirements and ultimate load testing parameters for airworthiness authorities approval (certification), which are covered in ISO 21100 or, for units approved prior to 2012, ISO 8097:2001. The design and operational testing requirements of ISO 10327:2014 are additional to the performance and certification testing requirements of these International Standards.
ISO 10327:2014 does not cover containers with an overall height of 1 625 mm (64 in) or less, that can be loaded on the lower deck compartments of main line civil transport aircraft, which are specified in ISO 6517, nor air-surface main deck containers, which are specified in ISO 4128 and ISO 8323.
|
Published |
2014-05 |
Edition : 2 |
Number of pages : 24 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 11242:1996 |
Aircraft — Pressure equalization requirements for cargo containers |
Describes the minimum safety requirements to be met by containers used to transport cargo by civil transport aircraft under normal pressure equalization during climb and descent and under emergency pressure equalization in the event of a sudden depressurization.
|
Published |
1996-06 |
Edition : 1 |
Number of pages : 12 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 14950:2004 |
Space systems — Unmanned spacecraft operability |
ISO 14950:2003 defines the essential properties pertaining to the operation of unmanned spacecraft and defines requirements and guidelines for spacecraft on-board functions in order to enable a specified ground segment to operate the spacecraft in any nominal or predefined contingency situation.
|
Published |
2004-02 |
Edition : 1 |
Number of pages : 24 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 16412:2005 |
Air cargo equipment — Air cargo pallets — Utilization guidelines |
ISO 16412:2005 specifies utilization guidelines to be applied when preparing air cargo pallets for carriage on board civil transport aircraft. It identifies the various concerns to be taken into consideration to ensure flight safety, and provides recognized industry standard methods to achieve it.
16412:2005 is applicable to any certified air cargo pallet built up from either a single or a number of pieces of commercial cargo, intended to be loaded on lower, main or upper deck of a civil transport aircraft, whether a freighter or a passenger-carrying aircraft. Its field of application includes all pallets prepared within ground premises, whether at a shipper's facilities or an airport cargo warehouse, including those intended to be loaded into the aircraft in a floating position. The provisions of ISO 16412:2005 may not entirely apply in the event of pre-embarked pallets. In such a case, it is up to the operator to identify and implement the applicable criteria.
16412:2005 is not intended to apply to air cargo pallets prepared for military transport aircraft, and does not take into account any specific criteria for military aircraft. Nothing, however, precludes it being used for guidelines in this case, it being the military operator's responsibility to identify and implement any additional applicable criteria.
|
Published |
2005-05 |
Edition : 1 |
Number of pages : 23 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 19281:2016 |
Air cargo — Fire resistant containers — Design, performance and testing requirements |
ISO 19281:2016 the minimum design and performance criteria and testing methods of passive fire resistant containers (FRCs) for carriage on aircraft main deck, to be used on either of the following:
a) in those cargo compartments of civil transport aircraft where they constitute one means of complying with applicable airworthiness regulations;
b) on a voluntary basis, when deemed appropriate by operators to improve fire protection in aircraft cargo compartments where airworthiness regulations do not currently mandate their use.
The fire resistant containers (FRCs) specified by this International Standard are intended to be used to contain and restrain unitized cargo for loading into either of the following aircraft main deck cargo compartments:
a) Class B aircraft cargo compartments according to CS-25, CCAR-25, JAS Part 3 or 14CFR Part 25 25.857 (b), in accordance a) or b) above;
b) Class E aircraft cargo compartments according to CS-25, CCAR-25, JAS Part 3 or 14CFR Part 25 25.857 (e), in accordance with b) above;
c) Class F aircraft cargo compartments according to CS-25 § 25.857(f) and AMC to CS-25.855 and 25.857, or 14CFR Part 25 § 25.857(f) and FAA Advisory Circular AC25.857-X, in accordance with a) above.
NOTE 1 Though nothing formally prevents a fire resistant container (FRC) from being carried in a lower deck Class C aircraft cargo compartment, it is not intended for this use since its fire containment capability would be redundant with that of the aircraft's fire detection and suppression system, which it could hamper. Consult current regulatory guidance materials and aircraft type's Weight and Balance Manual whenever available.
Containers are specified in this International Standard only insofar as their flammability requirements and fire resistance performance are concerned. They are not otherwise specified in this International Standard, but still require meeting the applicable general standards.
NOTE 2 See Clause 2 and 4.1 and 4.2 for applicable containers airworthiness approval and general design standards.
This International Standard does not cover requirements for fire detection or suppression devices. The specified fire resistant containers (FRCs) are passive devices capable of containing a fire for the specified duration by themselves.
NOTE 3 Nothing, however, prevents additional use of self-contained fire detection or suppression devices within fire resistant containers (FRCs), but such devices are not specified herein (see 4.5.5).
ISO 19281:2016 does not cover requirements for other types of fire resistant containers not specified therein.
The use of fire resistant containers meeting the requirements of this International Standard is not alone sufficient to ensure flight safety: this International Standard is based on the assumption that the approved fire resistant containers will be built up, installed, and checked prior to aircraft loading in accordance with appropriate operating instructions, by competent, suitably trained, personnel as defined for example in ISO 9001:2008, 6.2.2 (see 9.3).
|
Published |
2016-02 |
Edition : 1 |
Number of pages : 20 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO/CD 19281 |
Air cargo — Fire resistant containers — Design, performance and testing requirements |
ISO 19281:2016 the minimum design and performance criteria and testing methods of passive fire resistant containers (FRCs) for carriage on aircraft main deck, to be used on either of the following:
a) in those cargo compartments of civil transport aircraft where they constitute one means of complying with applicable airworthiness regulations;
b) on a voluntary basis, when deemed appropriate by operators to improve fire protection in aircraft cargo compartments where airworthiness regulations do not currently mandate their use.
The fire resistant containers (FRCs) specified by this International Standard are intended to be used to contain and restrain unitized cargo for loading into either of the following aircraft main deck cargo compartments:
a) Class B aircraft cargo compartments according to CS-25, CCAR-25, JAS Part 3 or 14CFR Part 25 25.857 (b), in accordance a) or b) above;
b) Class E aircraft cargo compartments according to CS-25, CCAR-25, JAS Part 3 or 14CFR Part 25 25.857 (e), in accordance with b) above;
c) Class F aircraft cargo compartments according to CS-25 § 25.857(f) and AMC to CS-25.855 and 25.857, or 14CFR Part 25 § 25.857(f) and FAA Advisory Circular AC25.857-X, in accordance with a) above.
NOTE 1 Though nothing formally prevents a fire resistant container (FRC) from being carried in a lower deck Class C aircraft cargo compartment, it is not intended for this use since its fire containment capability would be redundant with that of the aircraft's fire detection and suppression system, which it could hamper. Consult current regulatory guidance materials and aircraft type's Weight and Balance Manual whenever available.
Containers are specified in this International Standard only insofar as their flammability requirements and fire resistance performance are concerned. They are not otherwise specified in this International Standard, but still require meeting the applicable general standards.
NOTE 2 See Clause 2 and 4.1 and 4.2 for applicable containers airworthiness approval and general design standards.
This International Standard does not cover requirements for fire detection or suppression devices. The specified fire resistant containers (FRCs) are passive devices capable of containing a fire for the specified duration by themselves.
NOTE 3 Nothing, however, prevents additional use of self-contained fire detection or suppression devices within fire resistant containers (FRCs), but such devices are not specified herein (see 4.5.5).
ISO 19281:2016 does not cover requirements for other types of fire resistant containers not specified therein.
The use of fire resistant containers meeting the requirements of this International Standard is not alone sufficient to ensure flight safety: this International Standard is based on the assumption that the approved fire resistant containers will be built up, installed, and checked prior to aircraft loading in accordance with appropriate operating instructions, by competent, suitably trained, personnel as defined for example in ISO 9001:2008, 6.2.2 (see 9.3).
|
Under development |
|
Edition : 2 |
|
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 20291-1:2021 |
Air cargo — Restraint slings — Part 1: Design and testing |
This document specifies the design criteria and testing methods adequate to guarantee the ultimate strength and operational dependability of cargo restraint sling assemblies made of steel wire rope, with a 22,25 kN (5 000 lbf) rated ultimate load capability, as can be used by the airline industry in order to restrain on board civil transport aircraft during flight, including the following:
— cargo loaded and tied down onto airworthiness approved air cargo pallets, themselves restrained into aircraft lower deck, main deck or upper deck cargo systems and meeting the requirements of ISO 8097 (NAS 3610) or ISO 21100, or
— non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained ("floating") pallet into either lower deck, main deck or upper deck containerized cargo compartments of an aircraft, to be restrained onto aircraft structure attachment (tie-down) points.
Two types of wire rope restraint slings are defined:
a) type A: adjustable length restraint sling assemblies, including a tension retaining device and termination fittings attached to the wire rope end eyes;
b) type B: fixed length restraint sling extensions, to be used in conjunction with a type A cable; extensions are usually terminated at both ends by eyes, without additional fittings, and can be attached through hooks or shackles.
The cables specified in this document are intended exclusively for restraint purposes on board aircraft, and not for use as lifting slings.
|
Published |
2021-06 |
Edition : 1 |
Number of pages : 20 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 14951-1:1999 |
Space systems — Fluid characteristics — Part 1: Oxygen |
|
Withdrawn |
1999-09 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 20291-2:2021 |
Air cargo — Restraint slings — Part 2: Utilization requirements and recommendations and lashing calculations |
1.1 This document provides general utilization requirements and recommendations and calculation methods adequate to guarantee the effectiveness and ultimate strength of tie-down/lashing arrangements performed to restrain cargo on board civil transport aircraft during flight, including the following:
a) cargo loaded and tied down onto airworthiness approved air cargo pallets, themselves restrained into aircraft lower deck or main deck or upper deck cargo systems meeting the restraint requirements of air cargo pallets approved in accordance with ISO8097 (NAS 3610) or ISO 21100, or
b) additional tie-down on aircraft structure when necessitated by pallet maximum gross mass or centre of gravity limits, or
c) non-unitized individual pieces of cargo, or pieces of cargo placed onto an unrestrained pallet (floating pallet) into either lower deck, main deck or upper deck containerized cargo compartments of an aircraft,
when using for this purpose restraint slings (wire rope cables) specified in ISO 20291-1.
1.2 Restraint slings as specified in this document can also be used for permanent or semi-permanent attachment of a special purpose device, such as aircraft engine transport stand (see ISO 11241), horse stall (see ISO 9469), automobile transport device (see ISO 8268) or other, whether or not airworthiness approved, onto an aircraft pallet.
1.3 This document applies to cargo tie-down/lashing arrangements using exclusively air cargo restraint slings conforming to ISO 20291-1.
NOTE Where tie-down is performed onto aircraft structure as per 1.1 b) or c), additional restrictions can be stated in the aircraft's authority approved Weight and Balance Manual.
1.4 This document specifies industry recognized means of complying with airworthiness authorities general regulations applicable to load securing on board civil transport aircraft (see 14 CFR Part 25 and EASA CS-25, CCAR-25 or Japanese Airworthiness Standard Part 3), and aircraft manufacturers authority approved Weight and Balance Manuals for each aircraft type as specified therein.
1.5 The wire rope slings in this document are intended exclusively for restraint purposes on board aircraft and are not intended to be used as lifting slings for handling or any other purpose.
|
Published |
2021-06 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
|
| ISO 21894:2020 |
Air cargo — Cargo stopper devices — Design and testing |
This document specifies the design, performance and testing requirements for "Cargo Stopper" air cargo restraint accessories with a 22 250 N (5 000 lbf) rated load capacity, to be used in conjunction with air cargo restraint straps meeting ISO 16049-1 (TSO/ETSO ̶ C172), or air cargo restraint slings meeting ISO 20291-1, with the same rated load.
Cargo stopper devices designed to this document are intended to be used in either of the following typical instances:
a) to ensure restraint/tie-down of a piece of cargo that does not lend itself to either direct hooking of tie-down straps or passing a strap around without risk of slippage; a common example is long shaped cargo items with a narrow cross-section, whether or not overhanging from the pallet, individual or in bundles, e.g. pipes or beams; see ISO 16049-2:2020, 7.4;
b) to restrain cargo smaller than the pallet net's mesh, or identified as "piercing" cargo, presenting a hazard to the aircraft in the event of it being released during flight;
c) when a crate containing cargo, even though its cross-section is large enough to be directly tied-down with the pallet net or restraint straps, contains or can contain a heavy item, e.g. a piece of machinery, shaft, or similar, with a cross-section lower than the pallet net's mesh size;
NOTE Such "hidden" items have been known to break free from insufficiently strong crates when subjected to in-flight accelerations, then pass due to their small size through the net mesh restraining the crate and be released into the cargo compartment.
d) to assist in tying-down odd-shaped cargo pieces where it is difficult or not allowed to directly attach tie-down straps or pass them around the load in an effective manner.
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Published |
2020-02 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
55.180.30
Air mode containers, pallets and nets
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| ISO/FDIS 5879 |
Space systems — Launch vehicle/spacecraft separation ground test requirements for combined separation test, horizontal separation test and individual falling separation test |
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Under development |
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Edition : 1 |
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Technical Committee |
49.140
Space systems and operations
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| ISO/DTS 6434 |
Space systems — Design, testing and operation of a large constellation of spacecraft |
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Under development |
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Edition : 1 |
Number of pages : 10 |
Technical Committee |
49.140
Space systems and operations
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| ISO/CD TR 6832 |
Space systems — Development technology of a thermal vacuum chamber |
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Under development |
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Edition : 1 |
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Technical Committee |
49.140
Space systems and operations
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| ISO/CD 9490 |
Space systems — Space Traffic Coordination |
This recommended standard addressees protocols and operational Space Traffic Coordination (STC) requirements critical to ensure flight safety and mitigate collision risk, from pre-launch safety assessment through manoeuvre plans, on-orbit collision avoidance support services, and end of mission disposal. This standard levies requirements of an STC system that will facilitate the provision of high-availability, timely, comprehensive and sufficiently accurate services to support the safe, efficient, and sustainable use of space.
This STC standard addresses:
• Protocols for collection and exchange of data relevant to space safety;
• Protocols for creating, populating and operating an open architecture data repository to facilitate open data exchange;
• Data integrity measures and standards to ensure quality from diverse sources;
• Space Situational Awareness (SSA) data derived from multiple and diverse sources.
• Measures to safeguard proprietary or sensitive data;
• Owner-operator notification of flight plans and planned manoeuvres and sharing of orbital location data (ephemerides)
• Timely and actionable warnings; sharing of catalogue data, to predict close approaches;
• Interoperable formats to enable reliable messaging STC inputs and results, timely and actionable warnings, referencing extant CCSDS standards where applicable;
• Exchange of catalogue data to predict close approaches and assess options for operator collision avoidance manoeuvre plans.
• Formats to enable development of applications to leverage data and perform automated processes for collision avoidance.
• Data protection measures
• Coordination for satellites transiting Large Constellation (LC) radial shells
This standard requires flexibility to accommodate our deeper understanding of the impacts upon the space environment created by increased and emerging space activities and to benefit from technological advances and refined capabilities.
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Under development |
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Edition : 1 |
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Technical Committee |
49.140
Space systems and operations
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| ISO/CD 9621 |
Space systems — Methods to decide thermal vacuum test cycles of recurring production according to precipitation efficiency and reliability |
This standard provides technical methods to calculate the precipitation efficiency and liability of a flight hardware by measuring the screen effectiveness of thermal cycles. This standard can be applied, but not be limited to those recurring production, such as higher volume production or hardware of constellation programs, with a constant block of design, manufacture, as an option for those who wishes to modify or reduce the numbers of cycles with own database as a supplement standard of ISO 15864.
In case that the number of thermal cycles is agreed with the customer’s specified standard or determined by other means, this standard may be used as a supplement technical informative reference.
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Under development |
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Edition : 1 |
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Technical Committee |
49.140
Space systems and operations
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| ISO 14951-2:1999 |
Space systems — Fluid characteristics — Part 2: Hydrogen propellant |
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Withdrawn |
1999-09 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.140
Space systems and operations
;
71.100.20
Gases for industrial application
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| ISO 10784-1:2011 |
Space systems — Early operations — Part 1: Spacecraft initialization and commissioning |
A general definition of initialization is that it begins at separation of the spacecraft (SC) from the launcher. In some cases, a more exact definition will be that initialization begins in flight, upon planned change in mode or state of the SC from the launch configuration. Commissioning is completed when the SC, including its payload, is certified for initial mission operations. Prior to certification for mission operations, the SC is described as a test article in the three parts of ISO 10784. ISO 10784 does not include a requirement for contingency plans, but does include a statement of the need for contingency planning.
ISO 10784-1:2011 outlines general descriptive information for SC initialization and commissioning as might be appropriate for programme management, project engineering or programme test documentation. Since the SC is considered a test article at this phase of its operational life, ISO 17566 is used as a normative reference in constructing the initialization plan and the commissioning report. It provides SC manufacturers, SC operators and other stakeholders with a common language and form to verify and document spacecraft initialization and commissioning prior to normal SC mission operations.
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Published |
2011-12 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
49.140
Space systems and operations
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| ISO 10784-2:2011 |
Space systems — Early operations — Part 2: Initialization plan |
A general definition of initialization is that it begins at separation of the spacecraft (SC) from the launcher. In some cases, a more exact definition will be that initialization begins in flight, upon planned change in mode or state of the SC from the launch configuration. Commissioning is completed when the SC, including its payload, is certified for initial mission operations. Prior to certification for mission operations, the SC is described as a test article in the three parts of ISO 10784. ISO 10784 does not include a requirement for contingency plans, but does include a statement of the need for contingency planning.
ISO 10784-2:2011 provides SC manufacturers and operators with a specific form and format to write spacecraft initialization plans required to configure and verify the SC to perform normal mission operations. Since the SC is considered a test article at this phase of its operational life, ISO 17566 is used as a normative reference in constructing the initialization plan. It provides SC manufacturers, operators and other stakeholders with a common language and form to verify and document spacecraft initialization prior to normal SC mission operations.
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Published |
2011-12 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 10784-3:2011 |
Space systems — Early operations — Part 3: Commissioning report |
A general definition of initialization is that it begins at separation of the spacecraft (SC) from the launcher. In some cases, a more exact definition will be that initialization begins in flight, upon planned change in mode or state of the SC from the launch configuration. Commissioning is completed when the SC, including its payload, is certified for initial mission operations. Prior to certification for mission operations, the SC is described as a test article in the three parts of ISO 10784. ISO 10784 does not include a requirement for contingency plans, but does include a statement of the need for contingency planning.
ISO 10784-3:2011 outlines general descriptive information for SC initialization and commissioning as might be appropriate for programme management, project engineering or programme test documentation. Since the SC is considered a test article at this phase of its operational life, ISO 17566 is used as a normative reference in constructing the commissioning report. It provides SC manufacturers, SC operators and other stakeholders with a common language and form to verify and document spacecraft initialization and commissioning prior to normal SC mission operations.
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Published |
2011-12 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 10785:2011 |
Space systems — Bellows — Design and operation |
ISO 10785:2011 specifies general and detailed requirements for bellows used in space systems. It establishes requirements with regard to material, design, analysis, fabrication, material, testing, inspection and operation for space use.
ISO 10785:2011 is applicable to metallic bellows which are used as pressure bearing components and are integrated into a pressure system. ISO 10785:2011 is not applicable to engine bellows or valve bellows.
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Published |
2011-10 |
Edition : 1 |
Number of pages : 14 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 10786:2011 |
Space systems — Structural components and assemblies |
ISO 10786:2011 establishes requirements for the design; material selection and characterization; fabrication; testing and inspection of all structural items in space systems, including expendable and reusable launch vehicles, satellites and their payloads. When implemented for a particular space system, it will assure high confidence in achieving safe and reliable operation in all phases of its planned mission.
ISO 10786:2011 applies specifically to all structural items, including fracture-critical hardware used in space systems during all phases of the mission, with the following exceptions: adaptive structures, engines and thermal protection systems.
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Published |
2011-07 |
Edition : 1 |
Number of pages : 65 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 10788:2014 |
Space systems — Lunar simulants |
ISO 10788:2014 is a reference for quantitative measures of lunar simulants.
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Published |
2014-05 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11221:2011 |
Space systems — Space solar panels — Spacecraft charging induced electrostatic discharge test methods |
ISO 11221:2011 specfies qualification and characterization test methods to simulate plasma interactions and electrostatic discharges on solar array panels in space. ISO 11221:2011 is applicable to solar array panels made of crystalline silicon, gallium arsenide (GaAs) or multi-junction solar cells. ISO 11221:2011 addresses only surface discharges on solar panels.
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Published |
2011-08 |
Edition : 1 |
Number of pages : 44 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 10794:2011 |
Space systems — Programme management — Material, mechanical parts and processes |
ISO 10794:2011 defines the programme management requirements for material, mechanical parts and processes for projects covering mission definition, design, development, production and operations of space systems, including disposal.
ISO 10794:2011 covers the following:
management, including organization, reviews, acceptance status and documentation control;
selection criteria and rules;
evaluation, validation and qualification, or verification testing;
procurement and receiving inspection;
utilization criteria and rules.
ISO 10794:2011 applies to all space deliverable products and all programme phases.
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Withdrawn |
2011-08 |
Edition : 1 |
Number of pages : 50 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 10794:2018 |
Space systems — Programme management — Material, mechanical parts and processes |
This document defines the programme management requirements for material, mechanical parts and processes for projects covering mission definition, design, development, production and operations of space systems, including disposal.
This document covers the following:
— management, including organization, reviews, acceptance status and documentation control;
— selection criteria and rules;
— evaluation, validation and qualification, or verification testing;
— procurement and receiving inspection; and
— utilization criteria and rules.
This document applies to all space deliverable products and all programme phases.
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Published |
2018-05 |
Edition : 2 |
Number of pages : 46 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 10795:2011 |
Space systems — Programme management and quality — Vocabulary |
ISO 10795:2011 provides definitions of all common terms used in the area of space systems and operations. ISO 10795:2011does not contain terms specific to an individual International Standard in the area of space systems and operations, which are defined in that particular International Standard.
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Withdrawn |
2011-08 |
Edition : 1 |
Number of pages : 37 |
Technical Committee |
49.140
Space systems and operations
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
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| ISO 10795:2019 |
Space systems — Programme management and quality — Vocabulary |
This document provides definitions of all common terms used in the area of space systems and operations for programme management and quality. It does not contain terms specific to an individual International Standard in the area of space systems and operations, which are defined in that particular International Standard.
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Published |
2019-07 |
Edition : 2 |
Number of pages : 41 |
Technical Committee |
49.140
Space systems and operations
;
01.040.49
Aircraft and space vehicle engineering (Vocabularies)
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| ISO 10830:2011 |
Space systems — Non-destructive testing — Automatic ultrasonic inspection method of graphite ingot for solid rocket motors |
ISO 10830:2011 is applicable to the inspection of isotropic graphite ingots for use in solid rocket motors, in order to detect planar flaws oriented in various directions, using immersion testing by means of a single-probe, pulse-echo ultrasonic method.
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Published |
2011-07 |
Edition : 1 |
Number of pages : 25 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11103:1991 |
Space data and information transfer systems — Radio metric and orbit data |
Applies to civil space applications. The requirements specified are the technical recommendations made in: CCSDS 501.0-B-1 (issue 1) January 1987 which is adopted as an International Standard.
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Withdrawn |
1991-11 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11104:1991 |
Space data and information transfer systems — Time code formats |
Applies to civil space applications. The requirements specified are the technical recommendations made in: CCSDS 301.0-B-2 (issue 2) April 1990 which is adopted as an International Standard.
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Withdrawn |
1991-11 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11104:2003 |
Space data and information transfer systems — Time code formats |
ISO 11104:2003 specifies the requirements for time code formats for space data and information transfer systems for civil space applications.
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Withdrawn |
2003-12 |
Edition : 2 |
Number of pages : 43 |
Technical Committee |
49.140
Space systems and operations
|