| Name |
Description |
Abstract |
Status |
Publication date |
Edition |
Number of pages |
Technical committee |
ICS |
| ISO 2435:1973 |
Nitrogen for use in aircraft |
Gives the pressure and characteristics of nitrogen, compressed in oil-lubricated equipment. Is not intended to cover nitrogen für use in oxygen systems. The gaseous nitrogen supply pressure shall ensure charging of aircraft systems up to 343 bar at 20 °C. The minimum purity shall be 98,5 % by volume. It shall contain not more than a total of O,OO5 mg of oil vapour and particulate matter per cubic decimetre of nitrogen at 15 °C and 1 013 mbar.
|
Published |
1973-12 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 2529:1973 |
Aircraft — Zones, access doors and panels — Referencing system |
|
Withdrawn |
1973-09 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 3174:1981 |
Aircraft — Connections for checking hydraulic systems by ground appliances |
|
Withdrawn |
1981-10 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 4116:1986 |
Air cargo equipment — Ground equipment requirements for compatibility with aircraft unit load devices |
Specifies requirements for those portions of ground and terminal handling equipment that will have a direct bearing on the life of the device for the purpose of preventing on due wear on the device. Covers requirements for conveyor systems, guides, stops and restraint hardware that are used on trucks, transporters, dollies, storage provisions, pallet build-up hoists, or other device-handling equipment. The devices can be containers, galley modules and pallets for aircraft galley and cargo systems.
|
Published |
1986-07 |
Edition : 2 |
Number of pages : 4 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 4153:1981 |
Aircraft — Pressure fuel dispensing system — Test procedure and limit value for shut-off surge pressure |
Includes a standard method for testing. The method specified and the limit value apply to all ground systems, fixed and mobile. Also, because these both are standardized, necessary knowledge is provided for aiding proper design of the aircraft fill control valve shut-off characteristics.
|
Published |
1981-11 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.050
Aerospace engines and propulsion systems
;
49.100
Ground service and maintenance equipment
|
| ISO 6858:1982 |
Aircraft — Ground support electrical supplies — General requirements |
Gives electrical output characteristics, and interface requirements, between an aircraft and ground support electrical supplies. Requirements for safety features are also included. The facilities covered by this International Standard are intended to supply power to an aircraft. In some cases the facility may also be capable of being used for aircraft engine starting.
|
Withdrawn |
1982-08 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.060
Aerospace electric equipment and systems
;
49.100
Ground service and maintenance equipment
|
| ISO 6858:2017 |
Aircraft — Ground support electrical supplies — General requirements |
ISO 6858:2017 specifies the electrical output characteristics and interface requirements between an aircraft and ground support electrical supplies. This includes all external electric power generation facilities, provided as part of a central source or in point-of-use application. Requirements for safety features are also included. Performance and safety issues under regional control are not addressed in this document. Requirements for ground traffic control purposes, such as towing points, identification and warning lights, etc. are also excluded.
The electrical characteristics relate to nominal 28 V DC and either 115/200 V or 230/400 V three-phase, 400 Hz AC outputs measured at the aircraft attaching connector as indicated in Figure 1.
|
Published |
2017-11 |
Edition : 2 |
Number of pages : 35 |
Technical Committee |
49.060
Aerospace electric equipment and systems
;
49.100
Ground service and maintenance 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 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 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 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 6966:1993 |
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 6968:1983 |
Aircraft — Wide body aircraft lower 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 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 12172:2003 |
Space data and information transfer systems — Telecommand — Data routing service |
ISO 12172:2003 specifies the common requirements which define the data routing service of a spacecraft telecommand. The intent of this document is to provide a common framework within which space agencies may implement compatible future spacecraft telecommanding systems.
|
Withdrawn |
2003-02 |
Edition : 2 |
Number of pages : 61 |
Technical Committee |
49.140
Space systems and operations
|
| 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 7717:1985 |
Aircraft — Four-wheel-drive tow tractors — Performance requirements factors for design |
Identifies and summarizes the various factors that shall be considered and evaluated by the design or specifying engineer in establishing performance requirements. Provides a summary of design factors as well as various tabulated design data and explanatory examples.
|
Published |
1985-03 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 7718-1:2009 |
Aircraft — Passenger doors interface requirements for connection of passenger boarding bridge — Part 1: Main deck doors |
ISO 7718-1:2009 specifies minimum requirements for dimensions and unobstructed space around main-deck passenger doors of future types of civil-passenger transport aircraft when they are intended to be compatible with the thousands of passenger boarding bridges and passenger transfer vehicles existing, or being planned, in airports worldwide.
ISO 7718-1:2009 is not applicable to existing models of civil transport aircraft, or derivative models with the same fuselage, for which the aircraft-mating section of passenger boarding bridges or passenger transfer vehicles is expected to be compatible with ISO 16004.
ISO 7718-1:2009 is not intended to restrict in any way the basic design of any future types of civil-passenger transport aircraft. However, it aims to clarify for aircraft-design engineers the design characteristics that would make it difficult, or impossible, for a new type of aircraft to connect adequately with existing airport passenger boarding bridges or passenger transfer vehicles.
If, on a future model, basic aircraft-design requirements impose certain dimensional characteristics that do not comply with ISO 7718-1:2009, one of the following will apply, and in each case, aircraft-handling constraints and operating costs will increase:
alternative methods of embarking/disembarking passengers (e.g. integral aircraft stairs) will need to be implemented; or
existing passenger boarding bridges and/or passenger transfer vehicles will need to be modified/reworked to some extent in the airports where this type of new aircraft will operate; or
additional interface devices/equipment will be needed to connect this type of new aircraft with existing passenger boarding bridges and passenger transfer vehicles.
|
Withdrawn |
2009-03 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 7718-1:2016 |
Aircraft — Passenger doors interface requirements for connection of passenger boarding bridge or passenger transfer vehicle — Part 1: Main deck doors |
ISO 7718-1:2016 specifies minimum requirements for dimensions and unobstructed space around main deck passenger doors of future types of civil-passenger transport aircraft when they are intended to be compatible with the thousands of passenger boarding bridges and passenger transfer vehicles existing, or being planned, in airports worldwide.
ISO 7718-1:2016 is not applicable to existing models of civil transport aircraft, or derivative models with entry into service up to year 2000 with the same fuselage, for which the aircraft-mating section of passenger boarding bridges or passenger transfer vehicles is expected to be compatible with ISO 16004.
It is not the intent of this document to restrict in any way the basic design of any future types of civil-passenger transport aircraft. However, it aims at clarifying, for aircraft-design engineers, the design characteristics which would make it difficult or impossible for a new type of aircraft to adequately connect with existing airport passenger boarding bridges or passenger transfer vehicles. If basic aircraft-design requirements impose on a future model certain dimensional characteristics not complying with this document, note that:
- either alternative methods of embarking/disembarking passengers will need to be implemented, such as integral aircraft stairs, etc.;
- or existing passenger boarding bridges and/or passenger transfer vehicles in the airports where such a new type of aircraft is to operate will require some degree of modification/reworking;
- or additional interface devices/equipment will be required in order to connect such a new type of aircraft with existing passenger boarding bridges and passenger transfer vehicles.
Each case results in increased aircraft-handling constraints and operating cost.
|
Published |
2016-12 |
Edition : 2 |
Number of pages : 3 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 7718-2:2009 |
Aircraft — Passenger doors interface requirements for connection of passenger boarding bridge — Part 2: Upper deck doors |
ISO 7718-2:2009 specifies minimum requirements for dimensions and unobstructed space around upper deck passenger doors of future types of civil-passenger transport aircraft when they are intended to be compatible with passenger boarding bridges existing, or being planned, in airports worldwide.
ISO 7718-2:2009 is not necessarily applicable to existing models of civil transport aircraft, or derivative models with the same fuselage. However, it is expected that the design of such aircraft types be taken into account in the design of passenger boarding bridges capable of upper deck servicing, in addition to ISO 7718-2:2009.
ISO 7718-2:2009 is not intended to restrict in any way the basic design of any future types of civil-passenger transport aircraft. However, it aims to clarify for aircraft-design engineers the design characteristics that would make it difficult, or impossible, for a new type of aircraft to connect adequately with existing airport passenger boarding bridges.
If, on a future model, basic aircraft-design requirements impose certain dimensional characteristics that do not comply with ISO 7718-2:2009, one of the following will apply, and in each case, aircraft-handling constraints and operating costs will increase:
alternative methods of embarking/disembarking passengers (e.g. integral aircraft stairs) will need to be implemented; or
existing upper deck passenger boarding bridges will need to be modified/reworked to some extent in the airports where this type of new aircraft will operate; or
additional interface devices/equipment will be needed to connect this type of new aircraft with existing upper deck passenger boarding bridges.
|
Withdrawn |
2009-03 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 7718-2:2016 |
Aircraft — Passenger doors interface requirements for connection of passenger boarding bridge or passenger transfer vehicle — Part 2: Upper deck doors |
ISO 7718-2:2016 specifies the minimum dimensional and unobstructed space requirements around future civil-passenger transport aircraft upper deck passenger doors when they are intended to be compatible with passenger boarding bridges planned in airports worldwide.
This document is not applicable to existing models of civil transport aircraft, or derivative models with entry into service up to year 2000 with the same fuselage, for which the aircraft-mating section of passenger boarding bridges or passenger transfer vehicles is expected to be compatible with ISO 16004. However, it is expected that the design of such aircraft types may be taken into account for design of passenger boarding bridges capable of upper deck servicing, in addition to this document.
It is not the intent of this document to restrict in any way the basic design of any future types of civil-passenger transport aircraft. It aims, however, at clarifying for aircraft design engineers the design characteristics which would make it difficult or impossible for a new type of aircraft to adequately connect with airport passenger boarding bridges. Should basic aircraft design requirements impose on a future model certain dimensional characteristics not complying with this document, note that:
- either alternative methods of embarking/disembarking passengers will need to be implemented, such as using the internal aircraft stairs, etc.;
- or upper deck passenger boarding bridges in the airports where such a new type of aircraft is to operate will require some degree of modification/reworking;
- or additional interface devices/equipment will be required in order to connect such a new type of aircraft with existing upper deck passenger boarding bridges.
Each case results in increased aircraft-handling constraints and operating cost.
|
Published |
2016-12 |
Edition : 2 |
Number of pages : 3 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 7718:1984 |
Aircraft — Connection of passenger loading bridge or transfer vehicle — Interface requirements in the vicinity of main deck passenger doors |
Specifies minimum dimensional and unobstructed space requirements around the doors of present and future public civil passenger transport aircraft when they are intended to be compatible with the thousands of passenger loading bridges and passenger transfer vehicles existing or being planned in airports worldwide. Is not intended to restrict in any way the basic design of any future types of such aircraft.
|
Withdrawn |
1984-11 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 7718:2003 |
Aircraft — Main-deck passenger doors — Interface requirements for connection with passenger-boarding bridge or transfer vehicle |
ISO 7718:2003 specifies minimum requirements for dimensions and unobstructed space around main-deck passenger doors of future types of civil-passenger transport aircraft when they are intended to be compatible with the thousands of passenger boarding bridges and passenger transfer vehicles existing, or being planned, in airports worldwide.
ISO 7718:2003 is not applicable to existing models of civil transport aircraft, or derivative models with the same fuselage, for which the aircraft mating section of passenger boarding bridges or passenger transfer vehicles should be made compatible according to ISO 16004.
|
Withdrawn |
2003-06 |
Edition : 2 |
Number of pages : 3 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 8267-1:2005 |
Aircraft — Tow bar attachment fittings interface requirements — Part 1: Main line aircraft |
ISO 8267-1:2005 specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) in conventional tricycle type landing gears of commercial civil transport passenger and freight aircraft.
Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft mass category (which determines tow bar forces) in order to ensure that a single type of tow bar with a standard connection can be used for all aircraft types within or near that mass category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used.
ISO 8267-1:2005 is applicable to all new models of main line aircraft within the specified maximum ramp mass range, entering service or designed after its date of publication.
ISO 8267-1:2005 is applicable to main line commercial transport aircraft of airworthiness certified under FAR/JAR Parts 25 with a maximum ramp mass greater than 50 000 kg (110 000 lb).
It does not apply to aircraft of airworthiness certified under FAR/JAR Parts 25 but with a maximum ramp mass less than or equal to 50 000 kg (110 000 lb), which are covered by ISO 8267-2.
|
Withdrawn |
2005-08 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 8267-1:2015 |
Aircraft — Tow bar attachment fittings interface requirements — Part 1: Main line aircraft |
ISO 8267-1:2015 specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) in conventional tricycle type landing gears of commercial civil transport passenger and freight aircraft.
Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft mass category (which determines tow bar forces) in order to ensure that a single type of tow bar with a standard connection can be used for all aircraft types within or near that mass category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used.
ISO 8267-1:2015 is applicable to all new models of main line aircraft within the specified maximum ramp mass range, entering service or designed after its date of publication.
ISO 8267-1:2015 is applicable to main line commercial transport aircraft of airworthiness certified under FAR/EASA-CS Parts 25 with a maximum ramp mass of > 50 000 kg (110 000 lb).
It does not apply to aircraft of airworthiness certified under FAR/EASA-CS Parts 25 but with a maximum ramp mass of ≤ 50 000 kg (110 000 lb), which are covered by ISO 8267‑2.
Where a family of existing or contemplated aircraft types bridges two mass categories, use a single tow bar attachment fitting interface for all of them, and consider the use of the standard dimensions for the higher mass category throughout the family.
NOTE As far as practical, this part of ISO 8267 was defined in order to be compatible with as many existing aircraft types as possible in the mass category concerned.
|
Published |
2015-10 |
Edition : 2 |
Number of pages : 5 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 8267-2:2005 |
Aircraft — Tow bar attachment fittings interface requirements — Part 2: Regional aircraft |
ISO 8267-2:2005 specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft.
Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft mass category (which determines tow bar forces) in order to ensure that a single type of tow bar with a standard connection can be used for all aircraft types within or near that mass category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used.
ISO 8267-2:2005 is applicable to all new models of regional aircraft within the specified maximum ramp mass range which enter service or are designed after its date of publication.
It does not apply to previously in service regional aircraft models, which present a considerable variety of tow bar attachment fittings. However, a simple retrofit modification is described that may make certain in-service fittings compatible with a tow bar head in conformity with ISO 8267-2:2005, where deemed appropriate in order to facilitate operation of such aircraft types at airports.
ISO 8267-2:2005 is applicable to regional commercial transport aircraft airworthiness certified under FAR/JAR Parts 25 with a maximum ramp mass less than or equal to 50 000 kg (110 000 lb). It does not apply to
aircraft airworthiness certified under FAR/JAR Parts 23 as commuter category aeroplanes;aircraft airworthiness certified under FAR/JAR Parts 25 but with a maximum ramp mass of greater than 50 000 kg (110 000 lb), which are covered by ISO 8267-1.
|
Withdrawn |
2005-08 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 9667:2017 |
Aircraft ground support equipment — Tow bars |
ISO 9667:2017 specifies dimensional and physical requirements of tow bar connections to tractor and aircraft (see Figure 1). It is applicable to any new type of commercial transport category aircraft tow bar designed or built after publication of ISO 9667:2017.
The purpose of ISO 9667:2017 is to standardize tow bar attachments to airplane and tractor according to the mass category of the towed aircraft, so that one tow bar head with different shear levels can be used for all aircraft that are within the same mass category and are manufactured in compliance with ISO 8267.
|
Published |
2017-07 |
Edition : 3 |
Number of pages : 8 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 12173:1998 |
Space data and information transfer systems — Telecommand — Command operation procedures |
|
Withdrawn |
1998-08 |
Edition : 1 |
Number of pages : 57 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 8267-2:2015 |
Aircraft — Tow bar attachment fittings interface requirements — Part 2: Regional aircraft |
ISO 8267-2:2015 specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft.
Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft mass category (which determines tow bar forces) in order to ensure that a single type of tow bar with a standard connection can be used for all aircraft types within or near that mass category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used.
ISO 8267-2:2015 is applicable to all new models of regional aircraft within the specified maximum ramp mass range which enter service or are designed after its date of publication.
It does not apply to previously in service regional aircraft models, which present a considerable variety of tow bar attachment fittings. However, a simple retrofit modification is described that may make certain in-service fittings compatible with a tow bar head in conformity with this part of ISO 8267, where deemed appropriate in order to facilitate operation of such aircraft types at airports.
ISO 8267-2:2015 is applicable to regional commercial transport aircraft airworthiness certified under FAR/EASA-CS Parts 25 with a maximum ramp mass of ≤ 50 000 kg (110 000 lb). It does not apply to
- aircraft airworthiness certified under FAR/EASA-CS Parts 23 as commuter category aeroplanes;
- aircraft airworthiness certified under FAR/EASA-CS Parts 25 but with a maximum ramp mass of > 50 000 kg (110 000 lb), which are covered by ISO 8267‑1.
Where a family of existing or contemplated aircraft types bridges two mass categories, use a single tow bar attachment fitting interface for all of them, and consider the use of the standard dimensions for the higher mass category, be it part of this part of ISO 8267 or ISO 8267‑1, throughout the family.
NOTE As far as practical, this part of ISO 8267 was defined in order to be compatible with as many existing aircraft types as possible in the mass category concerned.
|
Withdrawn |
2015-10 |
Edition : 2 |
Number of pages : 6 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 8267-2:2019 |
Aircraft — Tow bar attachment fittings interface requirements — Part 2: Regional aircraft |
This document specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft.
Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft mass category (which determines tow bar forces) in order to ensure that a single type of tow bar with a standard connection can be used for all aircraft types within or near that mass category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used.
This document is applicable to all new models of regional aircraft within the specified maximum ramp mass range which enter service or are designed after its date of publication.
It does not apply to previously in service regional aircraft models, which present a considerable variety of tow bar attachment fittings. However, a simple retrofit modification is described that may make certain in-service fittings compatible with a tow bar head in conformity with this document, where deemed appropriate in order to facilitate operation of such aircraft types at airports.
This document is applicable to regional commercial transport aircraft airworthiness certified under FAR/EASA-CS Parts 25 with a maximum ramp mass of ≤ 50 000 kg (110,000 lb). It does not apply to
— aircraft airworthiness certified under FAR/EASA-CS Parts 23 as commuter category aeroplanes, and
— aircraft airworthiness certified under FAR/EASA-CS Parts 25 but with a maximum ramp mass of > 50 000 kg (110,000 lb), which are covered by ISO 8267‑1.
Where a family of existing or contemplated aircraft types bridges two mass categories, use a single tow bar attachment fitting interface for all of them, and consider the use of the standard dimensions for the higher mass category, be it part of this document or ISO 8267‑1, throughout the family.
NOTE As far as practical, this document was defined in order to be compatible with as many existing aircraft types as possible in the mass category concerned.
|
Published |
2019-09 |
Edition : 3 |
Number of pages : 5 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO/DIS 8267-2 |
Aircraft — Tow bar attachment fittings interface requirements — Part 2: Regional aircraft |
|
Under development |
|
Edition : 4 |
Number of pages : 5 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 8267:1985 |
Aircraft — Tow bar attachment fittings — Interface requirements |
|
Withdrawn |
1985-06 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 8267:1997 |
Aircraft — Tow bar attachment fittings for transport aircraft with a maximum ramp mass over 50 000 kg (110 000 lb) — Interface requirements |
Gives the requirements for tow bar attachment fittings in tricycle type landing gears of civil aircraft with a ramp mass greater than 50 000 kg (110 000 lb). Replaces the first edition.
|
Withdrawn |
1997-02 |
Edition : 2 |
Number of pages : 4 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 8775:1988 |
Aerospace — Gaseous oxygen replenishment connection for use in fluid systems (new type) — Dimensions (Inch series) |
Lays down the mating dimensions and access clearance for a replenishment coupling. Describes the requirements for the coupling mating dimensions, the thread and access clearance, which shall be in accordance with those given in figures and tables.
|
Published |
1988-02 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 9666:1993 |
Aircraft — Self-propelled lavatory-servicing vehicle — Functional requirements |
Applies to all self-propelled lavatory-servicing vehicles suitable for all aircraft types commonly in service in civil air transport. Shall be applied with due reference to national regulations on sanitation that are applicable in the area in which it is proposed that the vehicle is to be used. Does not specify equipment design but highlights certain criteria that are known to be essential for efficient operation in the airline environment.
|
Published |
1993-12 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
43.160
Special purpose vehicles
;
49.100
Ground service and maintenance equipment
|
| ISO 9667:1998 |
Aircraft ground support equipment — Tow bars |
|
Withdrawn |
1998-12 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 9667:2016 |
Aircraft ground support equipment — Tow bars |
ISO 9667:2016 specifies dimensional and physical requirements of tow bar connections to tractor and aircraft (see Figure 1). It is applicable to any new type of commercial-transport-category aircraft tow bar designed or built after publication of this International Standard.
|
Withdrawn |
2016-01 |
Edition : 2 |
Number of pages : 5 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 9678:1991 |
Aircraft — Self-propelled potable-water vehicle |
Specifies the functional requirements. Is not intended to specify equipment design. Gives certain criteria that are known to be essential for efficient operation. Should be applied with due reference to national regulations. To avoid any accidental contamination, the unit should only be used to supply aircraft with potable water. The informative annex A gives a bibliography.
|
Published |
1991-04 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 9939:1994 |
Aerospace — Pressure re-oiling connection (new type) |
Specifies the basic dimensions of a pressure re-oiling connection for use with all oils for aircraft engines, and the clearance envelope to be provided.
|
Published |
1994-01 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance 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 10841:1996 |
Aircraft — Catering vehicle for large capacity aircraft — Functional requirements |
Specifies the functional, performance and safety requirements for a vehicle equipped with a liftable van body used for loading and unloading of catering equipment and supplies on all large capacity aircraft types in service in international civil air transport.
|
Published |
1996-06 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 10842:2006 |
Aircraft — Ground service connections — Locations and types |
ISO 10842:2006 specifies the locations and types of aircraft ground service connections in order to optimize ground services, both fixed and mobile, for the following seven services:
400 Hz electrical power;preconditioned air for cabin conditioning;pneumatic power for jet engine start;potable water;lavatory service (draining, flushing);aircraft refuelling;interphone (headset) connections.
It focuses on these aircraft services because
these connections are those most frequently used during aircraft airport turnaround operations;in terms of economic benefit, they have the greatest impact through improved efficiency.
ISO 10842:2006 applies to any new type of main line commercial transport category aircraft designed or built after its publication.
In addition, it applies to any substantially modified new derivative aircraft type in the same category (derived from a previously existing type), insofar as technically and economically practical, if specified in the aircraft type specification established between customer airline(s) and manufacturer.
|
Withdrawn |
2006-11 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 3004-5:1988 |
Light gauge metal containers — Capacities and related cross-sections — Part 5: Open-top cans for fish and other fishery products |
|
Withdrawn |
1988-06 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
55.120
Cans. Tins. Tubes
|
| ISO 10842:2017 |
Aircraft — Ground service connections — Locations and types |
ISO 10842:2017 specifies the locations and types of aircraft ground service connections in order to optimize ground services both fixed and mobile, for the seven different services hereafter:
- 400 Hz electrical power;
- preconditioned air for cabin conditioning;
- pneumatic power for jet engine start;
- potable water;
- lavatory service (draining, flushing);
- aircraft refuelling;
- interphone (headset) connections.
It focuses on these aircraft services because:
- these connections are those most frequently used during aircraft airport turnaround operations;
- in terms of economic benefit, they have the greatest impact through improved efficiency.
ISO 10842:2017 is intended to apply to any new type of main line commercial transport category aircraft designed or built after its publication.
In addition, it is expected that any substantially modified new derivative aircraft type in the same category (derived from a previously existing type) will, insofar as technically and economically practical, meet the requirements of this document, if specified in the aircraft type specification established between customer airline(s) and manufacturer.
It is not the intent of this document to restrict in any way the basic design of any future types of civil passenger transport aircraft. It aims, however, at clarifying for aircraft design engineers the design characteristics which would make it difficult or impossible for a new type of aircraft to be adequately serviced from existing airport facilities. Should basic aircraft design requirements impose on a future model certain characteristics not complying with the present document:
- either alternative methods of servicing the aircraft will have to be implemented; or
- existing facilities in the airports where such a new type of aircraft is to operate will require some degree of modification/rework; or
- additional interface devices/equipment will be required in order to service such a new type of aircraft;
in either case resulting in increased aircraft servicing constraints and operating cost.
|
Published |
2017-07 |
Edition : 2 |
Number of pages : 11 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11075:1993 |
Aerospace — Aircraft de-icing/anti-icing Newtonian fluids, ISO type I |
Establishes the minimum requirements for Newtonian fluids (composition, properties, materials compatibility, environmental protection, anti-icing performance, quality assurance provisions) used in the removal and prevention of ice, snow or frost on exterior surface of parked aircraft.
|
Withdrawn |
1993-07 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11075:2007 |
Aircraft — De-icing/anti-icing fluids — ISO type I |
ISO 11075:2007 defines the requirements for ISO type I fluids used in the removal and prevention of ice, snow, or frost on exterior surfaces of main line and regional civil transport airplanes on the ground.
ISO 11075:2007 is applicable to de-icing/anti-icing fluids for use on airplanes in general. However, the applicability may have limitations for particular airplane types. It is the airplane operator's responsibility to consult the aircraft operations manual, the aircraft maintenance manual and the service letters of the airplane manufacturer, to determine any limitations/restrictions relating to the use of de-icing/anti-icing fluids that conform to ISO 11075:2007 for the type and model of airplane to be treated.
|
Published |
2007-04 |
Edition : 2 |
Number of pages : 3 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11076:1993 |
Aerospace — Aircraft de-icing/anti-icing methods with fluids |
|
Withdrawn |
1993-07 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11076:2000 |
Aerospace — Aircraft de-icing/anti-icing methods with fluids |
|
Withdrawn |
2000-03 |
Edition : 2 |
Number of pages : 20 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11076:2000 |
Aerospace — Aircraft de-icing/anti-icing methods with fluids |
|
Withdrawn |
2000-12 |
Edition : 3 |
Number of pages : 20 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11076:2006 |
Aircraft — Ground-based de-icing/anti-icing methods with fluids |
ISO 11076:2006 establishes the minimum requirements for aircraft de-icing/anti-icing methods on the ground, in accordance with the ICAO Manual of aircraft ground de-icing/anti-icing operations and relevant national regulations, to facilitate the safe operation of transport aircraft during icing conditions. This International Standard does not specify requirements for specific aircraft model types.
Frost, ice or snow deposits, which can seriously affect the aerodynamic performance and/or controllability of an aircraft, are effectively removed by the application of the procedures specified in ISO 11076:2006.
De-icing/anti-icing by mechanical means is not covered by this International Standard.
|
Withdrawn |
2006-11 |
Edition : 4 |
Number of pages : 32 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11076:2012 |
Aircraft — De-icing/anti-icing methods on the ground |
ISO 11076:2012 establishes the minimum requirements for aircraft de-icing/anti-icing methods on the ground, in accordance with the ICAO Manual of aircraft ground de-icing/anti-icing operations (Doc. 9640-AN/940) and relevant national regulations, to facilitate the safe operation of main-line and regional civil transport airplanes during icing conditions. ISO 11076:2012 does not specify requirements for specific aircraft model types.
|
Withdrawn |
2012-11 |
Edition : 5 |
Number of pages : 4 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 6968:1983 |
Aircraft — Wide body aircraft lower 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 12173:2003 |
Space data and information transfer systems — Telecommand — Command operation procedures |
ISO 12173:2003 specifies the logic required to carry out Command Operation Procedure-1 (COP-1) of the transfer layer. It is applicable only to projects which are compatible with the transfer layer as defined in ISO 12172.
|
Withdrawn |
2003-02 |
Edition : 2 |
Number of pages : 73 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11076:2020 |
Aircraft — Deicing/anti-icing methods on the ground |
This document establishes the minimum requirements for deicing/anti-icing methods on the ground of main line and regional airplanes, in accordance with ICAO, Document 9640-AN/9401) and the relevant civil aviation requirements, to facilitate the safe operation of main line and regional civil transport airplanes during icing conditions. This document does not specify requirements for specific aircraft model types.
Airlines' published manuals, procedures or methods supplement the information contained in this document.
Frost, ice or snow deposits, which can seriously affect the aerodynamic performance and/or controllability of an aircraft, are effectively removed by the application of the procedures specified in this document.
It is the airplane operator's responsibility to consult airplane manufacturer's aircraft operations manual, aircraft maintenance manual and service letters to determine any limitations/restrictions relating to the use of deicing/anti-icing methods meeting this document for the type and model of airplane to be treated.
|
Published |
2020-01 |
Edition : 6 |
Number of pages : 3 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11077:1993 |
Aerospace — Self-propelled de-icing/anti-icing vehicles — Functional requirements |
Specifies the general functional and performance requirements for a self-propelled, boom type aerial device, equipped with an aircraft de-icing/anti-icing fluid spraying system.
|
Withdrawn |
1993-07 |
Edition : 1 |
Number of pages : 5 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11077:2014 |
Aircraft ground equipment — De-icers — Functional requirements |
ISO 11077:2014 specifies the general functional, performance, and safety requirements for a self-propelled vehicle equipped with a boom type aerial device and aircraft de-icing/anti-icing fluid (ADF) spraying systems, hereinafter designated as "de-icer".
ISO 11077:2014 does not specify a comprehensive set of technical design criteria for aircraft de-icing/anti-icing vehicles, but only those relating to the main functional, safety, and performance requirements.
ISO 11077:2014 is not applicable to stationary equipment, e.g. gantries, cranes, used to perform de-icing/anti-icing operations on aircraft.
|
Published |
2014-06 |
Edition : 2 |
Number of pages : 21 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11078:1994 |
Aerospace — Aircraft de-icing/anti-icing non-Newtonian fluids, ISO type II |
Establishes the requirements for non-Newtonian fluids used in the removal and prevention of frozen deposits of frost, ice and snow on exterior surfaces of parked aircraft and the minimum requirements for an environmental test chamber and test procedure to carry out anti-icing performance tests according to the current materials specification for ISO type II aircraft de-icing/anti-icing non-Newtonian fluids.
|
Withdrawn |
1994-10 |
Edition : 1 |
Number of pages : 29 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11078:2007 |
Aircraft — De-icing/anti-icing fluids — ISO types II, III and IV |
ISO 11078:2007 defines the requirements for non Newtonian ISO types II, III and IV fluids used in the removal and prevention of ice, snow, or frost on exterior surfaces of main line and regional civil transport airplanes on the ground.
ISO 11078:2007 is applicable to de-icing/anti-icing fluids for use on airplanes in general. However, the applicability may have limitations for particular airplane types. It is the airplane operator's responsibility to consult the aircraft operations manual, the aircraft maintenance manual and the service letters of the airplane manufacturer, to determine any limitations/restrictions relating to the use of de-icing/anti-icing fluids that conform to ISO 11078:2007 for the type and model of airplane to be treated.
|
Published |
2007-04 |
Edition : 2 |
Number of pages : 3 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11217:1993 |
Aerospace — Hydraulic system fluid contamination — Location of sampling points and criteria for sampling |
Specifies location and criteria for hydraulic system fluid particulate contamination in aeroplanes, helicopters and space vehicles, and provides indirectly related references. Requirements are specified in SAE ARP 4268 which is adopted as a de facto ISO international Standard. For the purposes of international standardization, the outlined modification shall apply to clause 2 of AS4059A.
|
Withdrawn |
1993-05 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 11241:1994 |
Aircraft — Aircraft engine transport devices |
Specifies functional, dimensional, structural and environmental requirements for the design of aircraft engine transport devices, used to transport aircraft engines in wide-body aircraft. These devices are intended to be used in conjunction with pallets compatible with ISO 8097 Class II restraint requirements. Specifies minimum air and ground handling features and is intended to ensure interchangeability and compatibility with present and future air transport and ground handling system.
|
Published |
1994-08 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 11532:2012 |
Aircraft ground equipment — Graphical symbols |
ISO 11532:2012 establishes common graphical symbols for use on all types of aircraft ground support equipment. They have been compiled for the benefit of those who deal with such equipment, such as airlines, airport handling agencies, airport authorities, manufacturers, etc., in order to facilitate fast and accurate identification of controls, indicators and decals of powered and unpowered equipment.
|
Withdrawn |
2012-11 |
Edition : 1 |
Number of pages : 39 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
01.080.20
Graphical symbols for use on specific equipment
|
| ISO 11532:2018 |
Aircraft ground equipment — Graphical symbols |
ISO 11532:2018 establishes common graphical symbols for use on all types of aircraft ground support equipment.
They have been compiled for the benefit of those who deal with such equipment, such as airlines, airport handling agencies, airport authorities, manufacturers, etc., in order to facilitate fast and accurate identification of controls, indicators and decals of powered and unpowered equipment.
The presentation of this document is based on the recommendations of ISO/TC 145, Graphical symbols.
ISO 11532:2018 is also intended to promote standardization of terms for controls, indicators, etc. for aircraft ground support equipment and alleviate language problems.
These graphical symbols are intended to be placed on all new equipment and retrofitted on all existing equipment as far as possible.
NOTE This document is intended to be read with the documents listed in the bibliography.
|
Published |
2018-02 |
Edition : 2 |
Number of pages : 36 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
01.080.20
Graphical symbols for use on specific equipment
|
| 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 12056:1996 |
Aircraft — Self-propelled passenger stairs for large capacity aircraft — Functional requirements |
Gives the functional, performance and safety requirements for self-propelled passenger boarding stairs intended for access to the cabin of all aircraft types commonly in service in international civil air transport with a cabin door sill height equal to or exceeding 2,54 m.
|
Published |
1996-08 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 12604-1:2017 |
Aircraft ground handling — Checked baggage — Part 1: Mass and dimensions |
ISO 12640-1:2017 specifies mass and dimensions requirements for individual pieces of baggage checked in by airline passengers at airports to be carried in aircraft cargo compartments.
ISO 12640-1:2017 does not apply to cabin baggage carried on board by passengers.
|
Published |
2017-02 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO/CD 12604-2.2 |
Aircraft ground handling — Checked-in baggage — Part 2: Handling guidelines |
|
Under development |
|
Edition : 1 |
|
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 12604-3:2022 |
Aircraft ground handling — Checked baggage — Part 3: Workstation ergonomics |
This document specifies the requirements for workstation ergonomic design of baggage handling agents for individual pieces of baggage checked-in by airline passengers at airports to be carried into aircraft cargo holds.
This document applies to all manual handling workplaces in the processing chain for sorting, safe handling and routing of the baggage (containers and bulk baggage, departure and arrival circuits, at terminal and at aircraft, excluding passenger check-in process and loading into aircraft cargo holds). This document doesn't apply to manual handling of odd-sized baggage.
This document does not specify the baggage handling systems in and out of airport terminals, except the baggage weights and dimensions to be handled and the critical characteristics of manual workstations.
This document does not specify the baggage handling systems in the aircraft.
|
Published |
2022-11 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
13.180
Ergonomics
;
49.100
Ground service and maintenance equipment
|
| ISO 14625:1999 |
Space systems — Ground support equipment for use at launch, landing, or retrieval sites— General requirements |
|
Withdrawn |
1999-03 |
Edition : 1 |
Number of pages : 22 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.140
Space systems and operations
|
| ISO 14625:2007 |
Space systems — Ground support equipment for use at launch, landing or retrieval sites — General requirements |
ISO 14625:2007 specifies the general characteristics, performance, design, test, safety, reliability, maintainability and quality requirements for ground support equipment (GSE) and systems intended for use at launch, landing or retrieval-site installations, or other locations that are the responsibility of the launch, landing and retrieval site. ISO 14625:2007 does not specify how to design GSE, but establishes the minimum requirements to provide simple, robust, safe, reliable, maintainable and cost-effective GSE.
ISO 14625:2007 is applicable to the design of non-flight hardware and software used to support the operations of transporting, receiving, handling, assembly, inspection, test, checkout, service, launch and recovery of space vehicles and payloads at the launch, landing or retrieval sites. As such, the requirements of ISO 14625:2007 are optional for hardware used only at the manufacturing, development or test sites prior to arrival at the launch, landing or retrieval sites. However, if such GSE is temporarily used at a launch, landing or retrieval site, for whatever reason, conformity with all the safety-related requirements of ISO 14625:2007 is a minimum requirement for the GSE.
|
Withdrawn |
2007-11 |
Edition : 2 |
Number of pages : 24 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.140
Space systems and operations
|
| ISO 14625:2023 |
Space systems — Ground support equipment for use at launch, landing or retrieval sites — General requirements |
This document specifies the general characteristics, performance, design, test, checkout, maintenance, safety, reliability, maintainability and quality requirements for ground support equipment (GSE) and systems intended for use at launch, landing or retrieval-site installations, or other locations that are the responsibility of the launch, landing and retrieval site. This document does not specify how to design, checkout and maintain GSE, but establishes the minimum requirements to provide simple, robust, safe, reliable, maintainable and cost-effective GSE.
This document is applicable to the design, checkout and maintenance of non-flight hardware and software used to support the operations of transporting, receiving, handling, assembly, inspection, test, checkout, service, launch and recovery of space vehicles and payloads at the launch, landing or retrieval sites. As such, the requirements of this document are optional for hardware used only at the manufacturing, development or test sites prior to arrival at the launch, landing or retrieval sites. However, if such GSE is dual use equipment to be also at a launch, landing or retrieval site, for whatever reason, all the safety-related requirements of this document apply to the GSE.
|
Published |
2023-01 |
Edition : 3 |
Number of pages : 26 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.140
Space systems and operations
|
| ISO/PAS 15594:2004 |
Airport hydrogen fuelling facility operations |
ISO/PAS 15594:2004 specifies the fuelling procedures, hydrogen boil-off management procedures, hydrogen storage requirements, and characteristics of the ground support equipment required to operate an airport hydrogen fuelling facility.
|
Withdrawn |
2004-10 |
Edition : 1 |
Number of pages : 17 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 15845:2014 |
Aircraft ground equipment - Boarding vehicle for persons with reduced mobility - Functional and safety requirements |
ISO 15845:2014 specifies the minimum functional and safety requirements for enclosed self-propelled boarding vehicles designed for transporting and boarding/de-boarding persons with reduced mobility onto/from the main deck or upper deck of main line civil transport aircraft on which they are travelling as a passenger.
The intent of ISO 15845:2014 is not to specify equipment design, but rather to define minimum functional and safety requirements and highlight those criteria which are known to be essential to an efficient and safe operation on civil transport aircraft in the environment of international airports.
ISO 15845:2014 specifies the worldwide requirements recognized by aircraft and vehicle manufacturers as well as airlines and airport authorities. In addition, it shall be applied with due reference to the national governmental regulations of the country where the vehicle is to be operated. The main though not exclusive areas in which such national regulations can apply are:
? general requirements applicable to road vehicles, or similar local airport regulations;
? sanitary requirements regarding design, cleaning, disinfection and equipment of vehicles that can be used to carry diseased persons with or without medical attendance;
? safety requirements applicable to elevating equipment carrying persons in the elevated position.
Nothing in this International Standard, however, shall be deemed to supersede any locally applicable law or regulation, unless a specific exemption has been obtained for this purpose from the appropriate Authority. See NOTE of 4.1.1 hereafter as regards legal requirements applicable in the European Union and EFTA.
ISO 15845:2014 assumes that a disabled or incapacitated passenger can be accompanied by at least one attendant, and can be seated in a wheelchair or reclining on a stretcher trolley. Major factors in the design of the vehicle, with relevance to safety, are the consideration of psychological aspects, i.e. feelings of well-being and security, and the physical comfort of the passenger and the avoidance of panic.
ISO 15845:2014 also assumes that any type of wheelchair, e.g. standard type with or without occupant self-restraint system, aircraft aisle width wheelchairs without armrests, non-occupant propelled wheelchairs, battery powered wheelchairs, etc., or any type of stretcher transport trolley, can be employed.
NOTE It is assumed that battery powered wheelchairs will not be taken into the cabin of an aircraft.
ISO 15845:2014 does not apply to other forms of aircraft loading equipment which can be used but is not specifically designed for boarding of incapacitated or disabled persons, e.g. mobile lounges, passenger boarding bridges, or externally mounted pods such as used on medical evacuation helicopters.
ISO 15845:2014 does not apply to unmodified automotive parts approved for public vehicles, e.g. chassis, when used on a boarding vehicle for the purpose for which they were designed.
Certain requirements of this International Standard are specifically dictated by overwing access to doors of certain aircraft types, and might not apply to other aircraft types. However, the intent of this International Standard is that any vehicle capable of reaching the upper deck of very large capacity aircraft (VLCA) shall be able to safely handle this specific situation.
|
Published |
2014-12 |
Edition : 1 |
Number of pages : 21 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 16004:2005 |
Aircraft ground equipment — Passenger boarding bridge or transfer vehicle — Requirements for interface with aircraft doors |
ISO 16004:2005 specifies dimensional interface and unobstructed space requirements applicable to the aircraft mating section of either passenger boarding bridges or passenger transfer vehicles used at airports for boarding and disembarkation of passengers on the types of civil transport aircraft listed below. These types of aircraft have a door sill height greater than 2,0 m (80 in) above the ground. Lower aircraft usually do not require such means of access, and have not been taken into account.
Data was compiled and checked as to the exact location of such items on the most frequently used civil transport aircraft types (i.e. families of aircraft sub-types with the same fuselage design and the same general type designator, which potentially includes any future derivative aircraft with the same fuselage). These types include the following:
AIRBUS INDUSTRIE: A300 / A310 / A318 / A319 / A320 / A321 / A330 / A340BOEING COMMERCIAL AIRPLANE: B717 / B727 / B737 / B747 / B757 / B767 / B777LOCKHEED AIRCRAFT: L1011McDONNELL DOUGLAS: DC9 / DC10 / MD11 / MD80 / MD90
It is not the intent of ISO 16004:2005 to specify any requirements applicable to aircraft design. Future aircraft types with a new fuselage should meet the main deck passenger doors requirements for interface with passenger boarding bridges or passenger transfer vehicles of ISO 7718, which would ensure their compatibility with the aircraft mating section of passenger boarding bridges or passenger transfer vehicles meeting the requirements of ISO 16004:2005.
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Withdrawn |
2005-04 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 16004:2017 |
Aircraft ground equipment — Passenger boarding bridge or transfer vehicle — Interface requirements with aircraft doors |
ISO 16004:2017 specifies dimensional interface and unobstructed space requirements applicable to the aircraft mating section of either
a) passenger boarding bridges, or
b) passenger transfer vehicles
used at airports for boarding and disembarkation of passengers on the types of civil transport aircraft which have been listed hereafter. These types of aircraft have a door sill height greater than 2,0 m (80 in) over the ground. Lower aircraft usually do not require such means of access, and have not been taken into account.
|
Published |
2017-01 |
Edition : 2 |
Number of pages : 6 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 17775:2006 |
Aircraft — Ground-service connections — Potable water, toilet-flush water and toilet drain |
ISO 17775:2006 specifies the detail dimensions of the male connector interfaces, fitted to an aircraft, used for servicing of the potable water systems, the toilet-flush water systems, and the toilet drain systems currently in common use. ISO 17775:2006 is applicable to all commercial aircraft with water and toilet systems and is recommended for military and private aircraft that use water and toilet systems.
ISO 17775:2006 does not include requirements for the ground half (female) couplings or protective caps, but provides sufficient interface details for such items to be designed. It does not include any specified dimensions for the clearance required around the connector on the aircraft body itself for either any protective caps or ground half couplings, although general recommendations are made.
|
Published |
2006-12 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 10537:2010 |
Space data and information transfer systems — Encapsulation service |
ISO 10537:2010 specifies the encapsulation service which is used by space missions to transfer data units that are not directly transferred by the space data link protocols over a ground-to-space or space-to-space communications link.
|
Withdrawn |
2010-09 |
Edition : 1 |
Number of pages : 28 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 20683-1:2005 |
Aircraft ground equipment — Design, test and maintenance for towbarless towing vehicles (TLTV) interfaced with nose-landing gear — Part 1: Main-line aircraft |
ISO 20683-1:2005 is applicable to towbarless towing vehicles (TLTVs) interfacing with the nose landing gear of main line civil transport aircraft with a maximum ramp mass over 50 000 kg (110 000 lb). The requirements for regional transport aircraft with a lower maximum ramp mass are specified in ISO 20683-2. It is not applicable to TLTVs which were manufactured before its date of publication.
ISO 20683-1:2005 specifies general design requirements, testing and evaluation requirements, maintenance, calibration, documentation, records, tracing and accountability requirements in order to ensure that the loads induced by the tow vehicle will not exceed the design loads of the nose gear or its steering system, or reduce the certified safe life limit of the nose gear, or induce a stability problem during aircraft pushback and/or gate relocation or maintenance towing operations.
ISO 20683-1:2005 specifies requirements and procedures for towbarless towing vehicles (TLTVs) intended for aircraft push-back and gate relocation or maintenance towing only. It is not intended to allow for dispatch (operational) towing (see Clause 3, Terms and definitions). Dispatch towing imposes greater loads on nose gears and aircraft structure due to the combination of speed and additional passenger, cargo and fuel loads.
ISO 20683-1:2005 does not apply to towbarless towing vehicles interfacing with aircraft main landing gear.
|
Withdrawn |
2005-03 |
Edition : 1 |
Number of pages : 21 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 20683-1:2016 |
Aircraft ground equipment — Nose gear towbarless towing vehicle (TLTV) — Design, testing and maintenance requirements — Part 1: Main line aircraft |
ISO 20683-1:2016 is applicable to towbarless aircraft towing vehicles (TLTVs) interfacing with the nose landing gear of main line civil transport aircraft with a maximum ramp mass over 50 000 kg (110 000 lb). The requirements for regional transport aircraft with a lower maximum ramp mass are specified in ISO 20683‑2. It is not applicable to TLTVs which were manufactured before its date of publication.
It specifies general design requirements, testing and evaluation requirements, maintenance, calibration, documentation, records, tracing and accountability requirements in order to ensure that the loads induced by the tow vehicle will not exceed the design loads of the nose gear or its steering system, or reduce the certified safe life limit of the nose gear, or induce a stability problem during aircraft pushback and/or gate relocation or maintenance towing operations.
This document specifies requirements and procedures for towbarless tow vehicles (TLTVs) intended for aircraft pushback and gate relocation or maintenance towing only. It is not intended to allow for dispatch (operational) towing (see Clause 3). Dispatch towing imposes greater loads on nose gears and aircraft structure due to the combination of speed and additional passenger, cargo, and fuel loads.
This document does not apply to towbarless towing vehicles interfacing with aircraft main landing gear.
|
Published |
2016-08 |
Edition : 2 |
Number of pages : 24 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 20683-2:2004 |
Aircraft ground equipment — Design, test and maintenance for towbarless towing vehicles (TLTV) interfaced with nose-landing gear — Part 2: Regional aircraft |
ISO 20683-2:2004 is applicable to towbarless aircraft towing vehicles (TLTVs) interfacing with the nose-landing gear of civil transport aircraft with a maximum ramp mass comprised between 10 000 kg and 50 000 kg (22 000 lb and 110 000 lb), commonly designated as "regional aircraft". The requirements for main line transport aircraft with a higher maximum ramp mass are specified in ISO 20683-1, which is not applicable to TLTVs which were manufactured before its date of publication.
ISO 20683-2:2004 specifies general design requirements, testing and evaluation requirements, maintenance, calibration, documentation, records, tracing and accountability requirements in order to ensure that the loads induced by the tow vehicle not exceed the design loads of the nose gear or its steering system, or reduce the certified safe life limit of the nose gear, or induce a stability problem during aircraft push back and/or maintenance towing operations.
ISO 20683-2:2004 specifies requirements and procedures for towbarless tow vehicles (TLTVs) intended for aircraft push-back and gate relocation or maintenance towing only. It is not intended to allow for dispatch (operational) towing. Dispatch towing imposes greater loads on nose gears and aircraft structure due to the combination of speed and additional passenger, cargo, and fuel loads.
ISO 20683-2:2004 does not apply to towbarless towing vehicles interfacing with aircraft main landing gear.
|
Withdrawn |
2004-10 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 20683-2:2016 |
Aircraft ground equipment — Design, testing and maintenance requirements for nose gear towbarless towing vehicle (TLTV) — Part 2: Regional aircraft |
ISO 20683-2:2016 is applicable to towbarless aircraft towing vehicles (TLTVs) interfacing with the nose landing gear of civil transport aircraft with a maximum ramp mass comprised between 10 000 and 50 000 kg (22 000 and 110 000 lb), commonly designated as "regional aircraft." The requirements for main line transport aircraft with a higher maximum ramp mass are specified in ISO 20683‑1. It is not applicable to TLTVs which were manufactured before its date of publication.
It specifies general design requirements, testing and evaluation requirements, maintenance, calibration, documentation, records, tracing and accountability requirements in order to ensure that the loads induced by the tow vehicle will not exceed the design loads of the nose gear or its steering system, or reduce the certified safe life limit of the nose gear, or induce a stability problem during aircraft push back and/or maintenance towing operations.
It specifies requirements and procedures for towbarless tow vehicles (TLTVs) intended for aircraft pushback and gate relocation or maintenance towing only. It is not intended to allow for dispatch (operational) towing (see Clause 3). Dispatch towing imposes greater loads on nose gears and aircraft structure due to the combination of speed and additional passenger, cargo, and fuel loads.
It does not apply to towbarless towing vehicles interfacing with aircraft main landing gear.
|
Published |
2016-08 |
Edition : 2 |
Number of pages : 15 |
Technical Committee |
49.100
Ground service and maintenance 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 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 23748:2016 |
Aerospace series — O-ring grooves — Dimensions |
ISO 23748:2016 specifies the dimensions of grooves for use with O-rings for aerospace in static sealing applications:
- radial sealing: rod or bore mounted O-rings;
- axial sealing: internal or external pressure source.
|
Published |
2016-10 |
Edition : 1 |
Number of pages : 30 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 23748:2016/Amd 1:2021 |
Aerospace series — O-ring grooves — Dimensions — Amendment 1 |
|
Published |
2021-02 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.100
Ground service and maintenance equipment
|
| ISO 27470:2011 |
Aircraft ground equipment — Upper deck catering vehicle — Functional requirements |
ISO 27470:2011 specifies the minimum functional, performance and safety requirements for a catering vehicle capable of transporting and loading/unloading in-flight service (catering) equipment and supplies into or from the upper deck of very large capacity aircraft, as well as the main deck of these or other aircraft types.
The intent of ISO 27470:2011 is not to specify equipment design, but rather to define minimum functional and performance requirements and highlight those criteria which are known to be essential to an efficient and safe operation on civil transport aircraft in the environment of international airports.
ISO 27470:2011 specifies the worldwide requirements recognized by aircraft and vehicle manufacturers as well as airlines and catering agencies. In addition, it shall be applied with due reference to the national governmental regulations of the country where the vehicle is to be operated. The main though not exclusive areas in which such national regulations may apply are: a) general requirements applicable to road vehicles; b) sanitary requirements regarding design, cleaning and disinfection of vehicles used to carry food for human consumption; c) stability and other safety requirements applicable to elevating equipment carrying personnel in the elevated position.
Nothing in ISO 27470:2011, however, shall be deemed to supersede any locally applicable law or regulation, unless a specific exemption has been obtained for this purpose from the appropriate Authority.
Certain requirements of ISO 27470:2011 are specifically dictated by overwing access to doors of certain aircraft types, and may not apply to other aircraft types. However, the intent of ISO 27470:2011 is that any upper deck catering vehicle shall be capable of safely handling this specific situation.
|
Published |
2011-03 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
49.100
Ground service and maintenance equipment
|
| ISO 27471:2012 |
Aircraft ground equipment — Upper deck loader — Functional requirements |
|
Published |
2012-06 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.100
Ground service and maintenance 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 4116:1980 |
Ground equipment requirements for compatibility with aircraft unit load devices |
|
Withdrawn |
1980-10 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 4116:1986 |
Air cargo equipment — Ground equipment requirements for compatibility with aircraft unit load devices |
Specifies requirements for those portions of ground and terminal handling equipment that will have a direct bearing on the life of the device for the purpose of preventing on due wear on the device. Covers requirements for conveyor systems, guides, stops and restraint hardware that are used on trucks, transporters, dollies, storage provisions, pallet build-up hoists, or other device-handling equipment. The devices can be containers, galley modules and pallets for aircraft galley and cargo systems.
|
Published |
1986-07 |
Edition : 2 |
Number of pages : 4 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.120
Cargo equipment
|
| ISO 6702-1:1991 |
Aircraft — Requirements for on-board weight and balance systems — Part 1: General |
Specifies requirements for the function, characteristics, and installation of an on-board weight and balance system for use on civil transport aircraft. This first edition cancels and replaces the first edition ISO 6702:1984.
|
Published |
1991-11 |
Edition : 1 |
Number of pages : 14 |
Technical Committee |
49.090
On-board equipment and instruments
;
49.120
Cargo equipment
|
| ISO 6702-2:1991 |
Aircraft — Requirements for on-board weight and balance systems — Part 2: Design, performance and interface characteristics |
Requirements are specified in ARINC 737:1985 together with its Supplement 1 (1988), which are adopted as a de facto ISO International Standard.
|
Published |
1991-11 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.090
On-board equipment and instruments
;
49.120
Cargo equipment
|
| ISO 6702:1984 |
Aircraft — Requirements for on board weight and balance control systems |
|
Withdrawn |
1984-12 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.090
On-board equipment and instruments
;
49.120
Cargo equipment
|