49.100 - Ground service and maintenance equipment
ICS 49.100 Details
Ground service and maintenance equipment
Bodenversorgung. Wartungsgerate
Matériel d'entretien et pour les services au sol
Oprema za servis in vzdrževanje na tleh
General Information
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This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, the operation and the maintenance of baggage and equipment tractors when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This document applies to self-propelled baggage and equipment tractors with driver accommodation.
This document does not apply to pedestrian controlled equipment.
This document deals with vibrations which are considered as significant. Vibration measurements are dealt with in EN 1915-3.
No extra requirements on noise are provided other than those given in EN 1915-4.
NOTE EN 1915-4 provides the general GSE noise requirements.
This part of EN 12312 is not applicable to baggage and equipment tractors manufactured before the date of its publication.
This part of EN 12312 when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4 provides the requirements for baggage and equipment tractors.
- Standard31 pagesEnglish languagesale 10% offe-Library read for1 day
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 CCAR 25, 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 CCAR 25, 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, 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. NOTE The requirements for cargo covers are not defined in this document, except insofar as net restraint is incorporated therein.
- Standard51 pagesEnglish languagesale 15% off
This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, the operation and the maintenance of baggage and equipment tractors when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This document applies to self-propelled baggage and equipment tractors with driver accommodation.
This document does not apply to pedestrian controlled equipment.
This document deals with vibrations which are considered as significant. Vibration measurements are dealt with in EN 1915-3.
No extra requirements on noise are provided other than those given in EN 1915-4.
NOTE EN 1915-4 provides the general GSE noise requirements.
This part of EN 12312 is not applicable to baggage and equipment tractors manufactured before the date of its publication.
This part of EN 12312 when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4 provides the requirements for baggage and equipment tractors.
- Standard31 pagesEnglish languagesale 10% offe-Library read for1 day
This document defines the terms related to air cargo and aircraft ground equipment. The terms and definitions of this document are primarily intended to provide uniform understanding. It is intended that they be used in any other documents, manuals and standards in the areas of air cargo and airport ground equipment.
- Standard20 pagesEnglish languagesale 15% off
- Standard21 pagesFrench languagesale 15% off
This document specifies minimum requirements for dimensions and unobstructed space around main deck passenger doors on the outer skin of civil transport aircraft, applicable when these doors are designed to accept the connection of existing passenger boarding bridges or transfer vehicles. This document is not applicable to existing models of civil transport aircraft, or derivative models with entry into service up to the 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.
- Standard4 pagesEnglish languagesale 15% off
This document specifies minimum requirements for dimensions and unobstructed space around upper deck passenger doors on the outer skin of civil transport aircraft, applicable when these doors are designed to accept the connection of existing passenger boarding bridges or transfer vehicles. This document is not applicable to existing models of civil transport aircraft, or derivative models with entry into service up to the 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.
- Standard4 pagesEnglish languagesale 15% off
This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of AFE when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some performance requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines, airports and fuelling companies.
This document applies to all types of aircraft fuelling equipment:
a) aircraft refuellers,
b) hydrant dispensers,
c) defuellers,
d) hydrant pit servicing vehicles,
e) pit cleaner vehicles, and
f) stationary dispensing units
intended to service aircraft with aviation fuels and to be operated on airfields, heliports and other aircraft refuelling related areas such as maintenance bases.
This document does not apply to:
g) AFE whose only power source for aircraft refuelling is directly applied manual effort,
h) hydrant systems, tank farms, pipework and underground tanks,
i) specific hazards due to the operation of the AFE in a potentially explosive atmosphere, and
j) built-in fire extinguisher systems.
No extra requirements on noise and vibration are provided other than those in EN 1915-3:2004+A1:2009 and EN 1915- 4:2004+A1:2009.
NOTE EN 1915-3:2004+A1:2009 and EN 1915-4:2004+A1:2009 provide the general GSE vibration and noise requirements.
This document does not deal with hazards in respect to a standard automotive chassis and from other vehicles on the apron.
This document is not applicable to AFE which are manufactured before the date of publication of this document by CEN.
This part of the EN 12312 series when used in conjunction with EN 1915-1:2023, EN 1915-2:2001+A1:2009, EN 1915-3:2004+A1:2009 (for vehicles) and EN 1915-4:2004+A1:2009 provides the requirements for AFE.
- Standard53 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of AFE when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some performance requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines, airports and fuelling companies.
This document applies to all types of aircraft fuelling equipment:
a) aircraft refuellers,
b) hydrant dispensers,
c) defuellers,
d) hydrant pit servicing vehicles,
e) pit cleaner vehicles, and
f) stationary dispensing units
intended to service aircraft with aviation fuels and to be operated on airfields, heliports and other aircraft refuelling related areas such as maintenance bases.
This document does not apply to:
g) AFE whose only power source for aircraft refuelling is directly applied manual effort,
h) hydrant systems, tank farms, pipework and underground tanks,
i) specific hazards due to the operation of the AFE in a potentially explosive atmosphere, and
j) built-in fire extinguisher systems.
No extra requirements on noise and vibration are provided other than those in EN 1915-3:2004+A1:2009 and EN 1915- 4:2004+A1:2009.
NOTE EN 1915-3:2004+A1:2009 and EN 1915-4:2004+A1:2009 provide the general GSE vibration and noise requirements.
This document does not deal with hazards in respect to a standard automotive chassis and from other vehicles on the apron.
This document is not applicable to AFE which are manufactured before the date of publication of this document by CEN.
This part of the EN 12312 series when used in conjunction with EN 1915-1:2023, EN 1915-2:2001+A1:2009, EN 1915-3:2004+A1:2009 (for vehicles) and EN 1915-4:2004+A1:2009 provides the requirements for AFE.
- Standard53 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of passenger boarding bridges (PBBs) when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or their authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This document applies to:
a) apron-drive bridges;
b) fixed-head bridges (also referred to as nose-loaders) or pedestal bridges;
c) suspended bridges
for embarking/disembarking of passengers. It is applicable from the interface with the terminal building, which can be movable, e.g. on two levels to separate arrival and departure level to the connection with the aircraft including fixed tunnels.
This document does not apply to:
d) elevating lounges;
e) passenger stairs;
f) other form of aircraft access equipment;
g) autonomous PBB positioning.
No extra requirements on noise are provided other than those in EN 1915 4:2004+A1:2009.
NOTE EN 1915 4:2004+A1:2009 provides the general noise requirements.
This part of EN 12312 is not applicable to PBBs which were manufactured before the date of publication of this document by CEN.
This part of EN 12312 when used in conjunction with EN 1915-1:2023 and EN 1915 2:2001+A1:2009 provides the requirements for PBBs.
- Standard37 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of passenger boarding bridges (PBBs) when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or their authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This document applies to:
a) apron-drive bridges;
b) fixed-head bridges (also referred to as nose-loaders) or pedestal bridges;
c) suspended bridges
for embarking/disembarking of passengers. It is applicable from the interface with the terminal building, which can be movable, e.g. on two levels to separate arrival and departure level to the connection with the aircraft including fixed tunnels.
This document does not apply to:
d) elevating lounges;
e) passenger stairs;
f) other form of aircraft access equipment;
g) autonomous PBB positioning.
No extra requirements on noise are provided other than those in EN 1915 4:2004+A1:2009.
NOTE EN 1915 4:2004+A1:2009 provides the general noise requirements.
This part of EN 12312 is not applicable to PBBs which were manufactured before the date of publication of this document by CEN.
This part of EN 12312 when used in conjunction with EN 1915-1:2023 and EN 1915 2:2001+A1:2009 provides the requirements for PBBs.
- Standard37 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, the operation and the maintenance of passenger stairs when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and ground handling agencies.
This document applies to:
a) self-propelled passenger stairs with seated or standing driver with top speed above 6 km/h (Category A);
b) towable passenger stairs, with self-propelled function at docking with top speed up to 6 km/h with drive controls from ground, remote control or standing driver position (Category B);
c) towable stairs, with manual positioning, equipped with powered means, e.g. for height adjustment, stabilizers (Category C);
d) automatic levelling systems of stairs for embarking/disembarking of passengers.
This document does not apply to stairs to be moved on public roadways.
"Powered" is also understood as manual effort stored in springs or hydraulic accumulators, etc., the dangerous action of which can be produced or can continue after the manual effort has ceased or directly applied manual effort for lifting or lowering loads.
Those clauses of this document that can apply can also be used as a guideline for the design of towable stairs without powered means.
This document does not establish additional requirements for the following:
e) persons falling out of an aircraft with the passenger stairs not in position;
f) hazards resulting from a moving stairway (escalator);
g) aircraft upper deck door access.
No extra requirements on noise and vibration are provided other than those in EN 1915-3:2004+A1:2009 and EN 1915-4:2004+A1:2009.
NOTE EN 1915-3:2004+A1:2009 and EN 1915-4:2004+A1:2009 provide the general GSE vibration and noise requirements.
This document is not applicable to passenger stairs which are manufactured before the date of its publication.
This part of EN 12312, when used in conjunction with EN 1915-1:2023, EN 1915-2:2001+A1:2009, EN 1915-3:2004+A1:2009 and EN 1915-4:2004+A1:2009, provides the requirements for passenger stairs.
- Standard28 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, the operation and the maintenance of passenger stairs when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and ground handling agencies.
This document applies to:
a) self-propelled passenger stairs with seated or standing driver with top speed above 6 km/h (Category A);
b) towable passenger stairs, with self-propelled function at docking with top speed up to 6 km/h with drive controls from ground, remote control or standing driver position (Category B);
c) towable stairs, with manual positioning, equipped with powered means, e.g. for height adjustment, stabilizers (Category C);
d) automatic levelling systems of stairs for embarking/disembarking of passengers.
This document does not apply to stairs to be moved on public roadways.
"Powered" is also understood as manual effort stored in springs or hydraulic accumulators, etc., the dangerous action of which can be produced or can continue after the manual effort has ceased or directly applied manual effort for lifting or lowering loads.
Those clauses of this document that can apply can also be used as a guideline for the design of towable stairs without powered means.
This document does not establish additional requirements for the following:
e) persons falling out of an aircraft with the passenger stairs not in position;
f) hazards resulting from a moving stairway (escalator);
g) aircraft upper deck door access.
No extra requirements on noise and vibration are provided other than those in EN 1915-3:2004+A1:2009 and EN 1915-4:2004+A1:2009.
NOTE EN 1915-3:2004+A1:2009 and EN 1915-4:2004+A1:2009 provide the general GSE vibration and noise requirements.
This document is not applicable to passenger stairs which are manufactured before the date of its publication.
This part of EN 12312, when used in conjunction with EN 1915-1:2023, EN 1915-2:2001+A1:2009, EN 1915-3:2004+A1:2009 and EN 1915-4:2004+A1:2009, provides the requirements for passenger stairs.
- Standard28 pagesEnglish languagesale 10% offe-Library read for1 day
IEC 61820-1-2:2024 describes requirements for AGL systems including power supplies, transformation of energy, cables, and any electrical component utilized to produce the light intended to be used as a visual aid for air and ground navigation based on IEC 61820-1, complemented with series circuit specific topics.
- Standard37 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the technical requirements to minimise the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of container/pallet dollies and loose load trailers when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some performance requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies. This document applies to container/pallet dollies using ball-mat, inverted cargo castors, or rollers and loose load trailers intended to be used for the transportation of baggage and cargo on airports (examples, see Annex A). This document does not apply to trailers of similar design as used on public roads, e.g., truck type trailers. This document does not establish requirements for noise and vibration. Noise and vibration are dealt with respectively in EN 1915-4 and EN 1915-3. This document is not applicable to container/pallet dollies and loose load trailers which are manufactured before the date of publication by ISO of this document. NOTE Certain measurements have been given in imperial units (in parentheses), following the metric measurements, since the containers/pallets to be handled are based mainly on the imperial system.
- Standard21 pagesEnglish languagesale 15% off
- Standard21 pagesFrench languagesale 15% off
This document specifies the requirements of baggage handling 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, safety handling and routing of the baggage (containers and bulk baggage, departure and arrival circuits, at terminal and at aircraft, excluding passenger check-in process). 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 aircraft loading system.
- Standard14 pagesEnglish languagesale 15% off
IEC 61820-3-2:2023 specifies the requirements for power electronic converter systems (PECS) dedicated to powering aeronautical ground lighting (AGL) circuits with series circuit topology. An example of a traditional implementation is an AGL circuit with 6,6 A RMS nominal current, powered by a constant current regulator (CCR). In addition to revising the requirements for 6,6 A CCR setups, this document introduces requirements for general PECS for new AGL systems including systems specifically designed for LED based luminaires.
This first edition cancels and replaces IEC 61822 published in 2009. This edition constitutes a technical revision.
This edition includes the following significant technical changes with respect to IEC 61822:2009:
a) introduction of power electronic converter systems (PECS) to be used in the aeronautical ground lighting systems other than the 6,6 A aeronautical ground lighting systems;
b) introduction of classification for different device types;
c) introduction of IEC 62477-1:2022 and IEC 62477-2:2018 as the basis for safety related requirements.
- Standard37 pagesEnglish languagesale 10% offe-Library read for1 day
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. 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 can 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 with a maximum ramp mass of ≤ 50 000 kg (110 000 lb). It does not apply to: — aircraft airworthiness certified as commuter category aeroplanes; — aircraft airworthiness certified as main line aircraft with a maximum ramp mass of > 50 000 kg (110 000 lb), which are covered by ISO 8267-1.
- Standard5 pagesEnglish languagesale 15% off
IEC 61820-3-4:2023 specifies protective provisions for the operation of lamp systems powered by series circuits in aeronautical ground lighting.
The protective provisions described here refer only to secondary supply systems for loads that are electrically separated from the series circuit.
This document specifies the level of SELV, and alternatively PELV, under consideration of additional personnel protection during work on live secondary circuits by electrically skilled persons. This document also covers the special operational features of aeronautical ground lighting and addresses the level of training and the requirements for maintenance procedures detailed in IEC 61821 and other national or regional regulation.
The requirements and tests are intended to set a specification framework for system designers, system installers, users, and maintenance personnel to ensure a safe and economic use of electrical systems in installations for the beaconing of aerodromes.
This document complements existing IEC aeronautical ground lighting (AGL) standards and can be used as a design specification.
- Standard49 pagesEnglish languagesale 10% offe-Library read for1 day
This document applies to GSE when used in civil air transport as intended by the manufacturer and contains safety requirements relating to the equipment in general.
This document specifies the technical requirements to minimise the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of GSE when used as intended including any reasonably foreseeable misuse by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This part of EN 1915 is intended to be used in conjunction with EN 1915-2:2001+A1:2009, EN 1915-3:2004+A1:2009 (for self-propelled GSE) and EN 1915-4:2004+A1:2009, and with the relevant part of EN 12312 to give the requirements for the types of GSE within the scope of EN 12312.
When EN 12312 does not contain a relevant part for a GSE, EN 1915 (all parts) gives general requirements that may apply, although additional machine specific requirements, to be determined by the manufacturer, are likely to be required.
This part of EN 1915 does not apply to automotive parts approved for public vehicles in the EU and EFTA, when used on GSE for the purpose for which they are designed.
This part of EN 1915 does not establish additional requirements for the following:
a) operation elsewhere than in an airport environment;
b) operation in severe conditions, e.g. ambient temperature below -20 °C or over 50 °C, tropical or saturated salty atmospheric environment, strong magnetic or radiation field;
c) operation subject to special rules, e.g. potentially explosive atmosphere except as regards operation in the vicinity of an aircraft fuel tank during fuelling operation;
d) hazards caused by power supply other than from electrical networks;
e) hazards occurring during construction, transportation, decommissioning and disassembly of the GSE;
f) hazards caused by wind velocity in excess of the figures given in this document;
g) direct contact with food stuffs;
h) earthquake, flood, landslide, lightning and more generally any exceptional natural event;
i) electromagnetic compatibility (EMC);
j) hazards caused by noise and vibration, see EN 1915-3:2004+A1:2009 and EN 1915-4:2004+A1:2009.
While this standard gives some basic requirements for wireless remote controls, additional requirements will be necessary.
This part of EN 1915 is not applicable to GSE which are manufactured before the date of publication by CEN of this document.
- Standard68 pagesEnglish languagesale 10% offe-Library read for1 day
This document applies to GSE when used in civil air transport as intended by the manufacturer and contains safety requirements relating to the equipment in general.
This document specifies the technical requirements to minimise the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of GSE when used as intended including any reasonably foreseeable misuse by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This part of EN 1915 is intended to be used in conjunction with EN 1915-2:2001+A1:2009, EN 1915-3:2004+A1:2009 (for self-propelled GSE) and EN 1915-4:2004+A1:2009, and with the relevant part of EN 12312 to give the requirements for the types of GSE within the scope of EN 12312.
When EN 12312 does not contain a relevant part for a GSE, EN 1915 (all parts) gives general requirements that may apply, although additional machine specific requirements, to be determined by the manufacturer, are likely to be required.
This part of EN 1915 does not apply to automotive parts approved for public vehicles in the EU and EFTA, when used on GSE for the purpose for which they are designed.
This part of EN 1915 does not establish additional requirements for the following:
a) operation elsewhere than in an airport environment;
b) operation in severe conditions, e.g. ambient temperature below -20 °C or over 50 °C, tropical or saturated salty atmospheric environment, strong magnetic or radiation field;
c) operation subject to special rules, e.g. potentially explosive atmosphere except as regards operation in the vicinity of an aircraft fuel tank during fuelling operation;
d) hazards caused by power supply other than from electrical networks;
e) hazards occurring during construction, transportation, decommissioning and disassembly of the GSE;
f) hazards caused by wind velocity in excess of the figures given in this document;
g) direct contact with food stuffs;
h) earthquake, flood, landslide, lightning and more generally any exceptional natural event;
i) electromagnetic compatibility (EMC);
j) hazards caused by noise and vibration, see EN 1915-3:2004+A1:2009 and EN 1915-4:2004+A1:2009.
While this standard gives some basic requirements for wireless remote controls, additional requirements will be necessary.
This part of EN 1915 is not applicable to GSE which are manufactured before the date of publication by CEN of this document.
- Standard68 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard26 pagesEnglish languagesale 15% off
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.
- Standard11 pagesEnglish languagesale 15% off
- Standard12 pagesFrench languagesale 15% off
This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of aircraft movement equipment when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some performance requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This document applies to:
- aircraft tractors with driver accommodation,
- remote controlled aircraft movement equipment, and
- attachment devices
used for all operations utilizing aircraft movement equipment, e.g.:
- push back, and
- maintenance towing.
This document does not apply to:
- ground power installations on aircraft tractors,
- fixed ramp integrated systems,
- special towing equipment (e.g. for recovery),
- dispatch towing tractors, or
- tractors with a standing driver.
This document deals with vibrations and noise which are considered as significant hazards. Vibration measurements are dealt with in EN 1915 3:2004+A1:2009. Noise measurements and reduction are dealt with in EN 1915 4:2004+A1:2009.
This document does not deal with hazards in respect to a standard automotive chassis or from hazards arising from potential interaction with other vehicles on the apron.
This part of EN 12312 is not applicable to aircraft movement equipment manufactured before the date of its publication.
This part of EN 12312 is intended to be used in conjunction with EN 1915 1:2013, EN 1915 2:2001+A1:2009, EN 1915 3:2004+A1:2009 (for vehicles) and EN 1915 4:2004+A1:2009.
This part of EN 12312 when used in conjunction with EN 1915 1:2013, EN 1915 2:2001+A1:2009, EN 1915 3:2004+A1:2009 and EN 1915 4:2004+A1:2009 provides the requirements for aircraft movement equipment.
- Standard29 pagesEnglish languagesale 10% offe-Library read for1 day
- Standard1 pageEnglish languagesale 15% off
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.
- Standard44 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of aircraft movement equipment when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some performance requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This document applies to:
- aircraft tractors with driver accommodation,
- remote controlled aircraft movement equipment, and
- attachment devices
used for all operations utilizing aircraft movement equipment, e.g.:
- push back, and
- maintenance towing.
This document does not apply to:
- ground power installations on aircraft tractors,
- fixed ramp integrated systems,
- special towing equipment (e.g. for recovery),
- dispatch towing tractors, or
- tractors with a standing driver.
This document deals with vibrations and noise which are considered as significant hazards. Vibration measurements are dealt with in EN 1915 3:2004+A1:2009. Noise measurements and reduction are dealt with in EN 1915 4:2004+A1:2009.
This document does not deal with hazards in respect to a standard automotive chassis or from hazards arising from potential interaction with other vehicles on the apron.
This part of EN 12312 is not applicable to aircraft movement equipment manufactured before the date of its publication.
This part of EN 12312 is intended to be used in conjunction with EN 1915 1:2013, EN 1915 2:2001+A1:2009, EN 1915 3:2004+A1:2009 (for vehicles) and EN 1915 4:2004+A1:2009.
This part of EN 12312 when used in conjunction with EN 1915 1:2013, EN 1915 2:2001+A1:2009, EN 1915 3:2004+A1:2009 and EN 1915 4:2004+A1:2009 provides the requirements for aircraft movement equipment.
- Standard29 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the technical requirements to minimise the hazards listed in Clause 4 which can arise during the commissioning, the operation and the maintenance of conveyor belt vehicles when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This European Standard applies to
a) self-propelled conveyor belt vehicles with or without driver's accommodation,
b) self-propelled conveyor belt vehicles equipped with a van body,
c) towed conveyor belt vehicles,
intended to be used for manual loading/unloading of aircraft.
This European Standard does not apply to any extensions or appurtenances of conveyor belt vehicles entering the aircraft cargo compartment in order to facilitate loading and unloading therein ("Aircraft Bulk Loading Systems", ABLS).
This European Standard does not apply to pneumatic systems and to cable-less remote controls.
This part of EN 12312 is not applicable to conveyor belt vehicles which were manufactured before the date of publication of this European Standard by CEN.
This part of EN 12312 when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4 provides the requirements for conveyor belt vehicles.
- Standard30 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the technical requirements to minimise the hazards listed in Clause 4 which can arise during the commissioning, the operation and the maintenance of conveyor belt vehicles when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This European Standard applies to
a) self-propelled conveyor belt vehicles with or without driver's accommodation,
b) self-propelled conveyor belt vehicles equipped with a van body,
c) towed conveyor belt vehicles,
intended to be used for manual loading/unloading of aircraft.
This European Standard does not apply to any extensions or appurtenances of conveyor belt vehicles entering the aircraft cargo compartment in order to facilitate loading and unloading therein ("Aircraft Bulk Loading Systems", ABLS).
This European Standard does not apply to pneumatic systems and to cable-less remote controls.
This part of EN 12312 is not applicable to conveyor belt vehicles which were manufactured before the date of publication of this European Standard by CEN.
This part of EN 12312 when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4 provides the requirements for conveyor belt vehicles.
- Standard30 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard46 pagesEnglish languagesale 15% off
This document specifies the dimensions of connections for starting aircraft engines by air, which are necessary to ensure international interchangeability of connectors with adaptors. lt also gives the minimum clearances required on the aircraft to provide adequate access for the ground adaptor.
- Standard5 pagesEnglish languagesale 15% off
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.
- Standard44 pagesEnglish languagesale 10% offe-Library read for1 day
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.
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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.
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IEC 61820-1:2019 covers principles of design and installation requirements for AGL systems including control, monitoring and transformation of energy, the cables and any electrical component utilized to produce the light intended to be used as a visual aid for air and ground navigation. This document defines in general the fundamental principles to provide safe, reliable and efficient operation of AGL systems independent of the particular system design. Where certain aspects of design are specific to a particular type of system (e.g. series-circuit), these are supplemented in the applicable part.
- Standard19 pagesEnglish languagesale 10% offe-Library read for1 day
1.1 General
This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, the operation and the maintenance of maintenance or service stairs and platforms when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
These machines are designed to be used as aircraft ground support equipment with the intended use to serve aircraft in outdoor conditions on the apron. They can also be used indoors at hangars. The use of such equipment for operations not in conjunction with aircraft is not defined as intended use therein. Due to the good operational conditions on the apron, deviations from some clauses of EN 280 were deemed acceptable.
This European Standard applies to:
a) self-propelled fixed or adjustable maintenance or service stairs and elevating platforms;
b) towable maintenance or service stairs and platforms equipped with powered means, e.g. for height adjustment, stabilizers;
designed for aircraft maintenance or service purposes including access to the aircraft.
NOTE 1 Powered will be also understood as manual effort stored in springs or hydraulic accumulators, etc., the dangerous action of which can be produced or can continue after the manual effort has ceased or directly applied manual effort for lifting or lowering loads.
NOTE 2 Those clauses of this standard that can apply can also be used as a guideline for the design of towable maintenance or service stairs and platforms without powered means.
This European Standard does not apply to:
c) maintenance docks either fixed to the ground or moveable only for docking procedure;
d) ground support equipment specifically intended, built and equipped with a fluid system for aircraft de-icing and anti-icing (see EN 12312 6);
NOTE 3 This does not prevent aircraft de-icers meeting the requirements of EN 12312 6 from being used as a means of access for aircraft maintenance, e.g. windshield cleaning, etc.
e) mobile elevating work platforms (MEWP) used at the airports for purposes other than aircraft maintenance, e.g. buildings and facilities (see EN 280).
No extra requirements on noise and vibration are provided other than those given in EN 1915 3 and EN 1915 4.
NOTE 4 EN 1915 3 and EN 1915 4 provide the general GSE vibration and noise requirements.
This European Standard does not deal with hazards in respect to a standard automotive chassis and from other vehicles on the apron.
This part of EN 12312 is not applicable to maintenance or service stairs and platforms which are manufactured before the date of publication of this standard by CEN.
This part of EN 12312 when used in conjunction with EN 1915 1, EN 1915 2, EN 1915 3 and EN 1915 4 provides the requirements for maintenance or service stairs and platforms.
1.2 Classification
For the purposes of this document, mobile elevating work platforms (MEWPs) used for aircraft maintenance access are divided into two main groups A and B. In addition, group C is considered as described in c) hereafter:
a) Group A: MEWPs where the vertical projection of the centre of the platform area is always inside the tipping lines.
NOTE 1 See 5.2 hereafter for the specific requirements applying to Group A MEWPs.
b) Group B: MEWPs where the vertical projection of the centre of the platform area may be outside the tipping lines.
NOTE 2 See 5.3 hereafter for the specific requirements applying to Group B MEWPs.
c) Group C consists of maintenance or service access stairs, where persons are not elevated by the machine but climb a flight of steps.
(...)
- Standard28 pagesEnglish languagesale 10% offe-Library read for1 day
1.1 General
This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, the operation and the maintenance of maintenance or service stairs and platforms when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
These machines are designed to be used as aircraft ground support equipment with the intended use to serve aircraft in outdoor conditions on the apron. They can also be used indoors at hangars. The use of such equipment for operations not in conjunction with aircraft is not defined as intended use therein. Due to the good operational conditions on the apron, deviations from some clauses of EN 280 were deemed acceptable.
This European Standard applies to:
a) self-propelled fixed or adjustable maintenance or service stairs and elevating platforms;
b) towable maintenance or service stairs and platforms equipped with powered means, e.g. for height adjustment, stabilizers;
designed for aircraft maintenance or service purposes including access to the aircraft.
NOTE 1 Powered will be also understood as manual effort stored in springs or hydraulic accumulators, etc., the dangerous action of which can be produced or can continue after the manual effort has ceased or directly applied manual effort for lifting or lowering loads.
NOTE 2 Those clauses of this standard that can apply can also be used as a guideline for the design of towable maintenance or service stairs and platforms without powered means.
This European Standard does not apply to:
c) maintenance docks either fixed to the ground or moveable only for docking procedure;
d) ground support equipment specifically intended, built and equipped with a fluid system for aircraft de-icing and anti-icing (see EN 12312 6);
NOTE 3 This does not prevent aircraft de-icers meeting the requirements of EN 12312 6 from being used as a means of access for aircraft maintenance, e.g. windshield cleaning, etc.
e) mobile elevating work platforms (MEWP) used at the airports for purposes other than aircraft maintenance, e.g. buildings and facilities (see EN 280).
No extra requirements on noise and vibration are provided other than those given in EN 1915 3 and EN 1915 4.
NOTE 4 EN 1915 3 and EN 1915 4 provide the general GSE vibration and noise requirements.
This European Standard does not deal with hazards in respect to a standard automotive chassis and from other vehicles on the apron.
This part of EN 12312 is not applicable to maintenance or service stairs and platforms which are manufactured before the date of publication of this standard by CEN.
This part of EN 12312 when used in conjunction with EN 1915 1, EN 1915 2, EN 1915 3 and EN 1915 4 provides the requirements for maintenance or service stairs and platforms.
1.2 Classification
For the purposes of this document, mobile elevating work platforms (MEWPs) used for aircraft maintenance access are divided into two main groups A and B. In addition, group C is considered as described in c) hereafter:
a) Group A: MEWPs where the vertical projection of the centre of the platform area is always inside the tipping lines.
NOTE 1 See 5.2 hereafter for the specific requirements applying to Group A MEWPs.
b) Group B: MEWPs where the vertical projection of the centre of the platform area may be outside the tipping lines.
NOTE 2 See 5.3 hereafter for the specific requirements applying to Group B MEWPs.
c) Group C consists of maintenance or service access stairs, where persons are not elevated by the machine but climb a flight of steps.
(...)
- Standard28 pagesEnglish languagesale 10% offe-Library read for1 day
ISO 1825:2017 specifies the dimensions and construction of, and requirements for, four types of hose and hose assembly for use in all operations associated with the ground fuelling and defuelling of aircraft.
All four types are designed for:
a) use with petroleum fuels having an aromatic-hydrocarbon content not exceeding 30 % by volume;
b) operation within the temperature range of −30 °C to +65 °C and such that they will be undamaged by climatic conditions of −40 °C to +70 °C when stored in static conditions;
c) operation at up to 2,0 MPa (20 bar) maximum working pressure, including surges of pressure which the hose can be subjected to in service.
NOTE 1 Type C hoses are intended for general pressure applications on all vehicles used for plane fuelling. They can also be used for vehicle/rail car loading and discharge where excessive vacuum does not occur.
NOTE 2 Type F hoses can be used for plane delivery applications on vehicles that are also used for defuelling at high flow rates where type C hoses are not suitable.
NOTE 3 Type E and F hoses can also be used for vehicle/rail car loading and discharge, for trailer to fueller transfer and for elevation platform supply (riser) to provide greater kink resistance.
- Standard35 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard36 pagesEnglish languagesale 15% off
- Standard36 pagesFrench languagesale 15% off
ISO 1464:2018 specifies the minimum clear space to be provided beneath the aircraft main jacking points, in order to accommodate tripod jacks and thus ensure adequate clearance between the jacks and the adjacent aircraft structure. ISO 1464:2018 is not intended to define fully all jack clearance dimensions. In situations where clearances are critical, it is used as a design aid only. Final critical clearances are established by using actual jack dimensions.
- Standard4 pagesEnglish languagesale 15% off
ISO 1825:2017 specifies the dimensions and construction of, and requirements for, four types of hose and hose assembly for use in all operations associated with the ground fuelling and defuelling of aircraft.
All four types are designed for:
a) use with petroleum fuels having an aromatic-hydrocarbon content not exceeding 30 % by volume;
b) operation within the temperature range of −30 °C to +65 °C and such that they will be undamaged by climatic conditions of −40 °C to +70 °C when stored in static conditions;
c) operation at up to 2,0 MPa (20 bar) maximum working pressure, including surges of pressure which the hose can be subjected to in service.
NOTE 1 Type C hoses are intended for general pressure applications on all vehicles used for plane fuelling. They can also be used for vehicle/rail car loading and discharge where excessive vacuum does not occur.
NOTE 2 Type F hoses can be used for plane delivery applications on vehicles that are also used for defuelling at high flow rates where type C hoses are not suitable.
NOTE 3 Type E and F hoses can also be used for vehicle/rail car loading and discharge, for trailer to fueller transfer and for elevation platform supply (riser) to provide greater kink resistance.
- Standard35 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard35 pagesEnglish languagesale 15% off
This European Standard specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of lavatory service equipment when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This European Standard applies to:
a) self-propelled lavatory vehicles;
b) towable lavatory vehicles;
c) moveable parts of ramp integrated systems,
designed for servicing aircraft and intended to be used under the conditions given in EN 1915-1:2013, Clause 1.
No extra requirements on noise and vibration are provided other than those in EN 1915-3 and EN 1915-4.
NOTE EN 1915-3 and EN 1915-4 provide the general GSE vibration and noise requirements.
This part of EN 12312 is not applicable to lavatory service equipment which is manufactured before the date of publication of this standard by CEN.
This part of EN 12312, when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4, provides the requirements for lavatory service equipment.
- Standard18 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of potable water service equipment when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This European Standard applies to:
a) self-propelled potable water vehicles;
b) towable potable water vehicles;
c) moveable parts of ramp integrated systems,
designed for servicing aircraft and intended to be used under the conditions given in EN 1915-1:2013, 1.
No extra requirements on noise and vibration are provided other than those in EN 1915-3 and EN 1915-4.
NOTE EN 1915-3 and EN 1915-4 provide the general GSE vibration and noise requirements.
This part of EN 12312 is not applicable to potable water service equipment which is manufactured before the date of publication of this standard by CEN.
This part of EN 12312, when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4, provides the requirements for potable water service equipment.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day
ISO 1825:2017 specifies the dimensions and construction of, and requirements for, four types of hose and hose assembly for use in all operations associated with the ground fuelling and defuelling of aircraft. All four types are designed for: a) use with petroleum fuels having an aromatic-hydrocarbon content not exceeding 30 % by volume; b) operation within the temperature range of −30 °C to +65 °C and such that they will be undamaged by climatic conditions of −40 °C to +70 °C when stored in static conditions; c) operation at up to 2,0 MPa (20 bar) maximum working pressure, including surges of pressure which the hose can be subjected to in service. NOTE 1 Type C hoses are intended for general pressure applications on all vehicles used for plane fuelling. They can also be used for vehicle/rail car loading and discharge where excessive vacuum does not occur. NOTE 2 Type F hoses can be used for plane delivery applications on vehicles that are also used for defuelling at high flow rates where type C hoses are not suitable. NOTE 3 Type E and F hoses can also be used for vehicle/rail car loading and discharge, for trailer to fueller transfer and for elevation platform supply (riser) to provide greater kink resistance.
- Standard27 pagesEnglish languagesale 15% off
- Standard29 pagesFrench languagesale 15% off
This European Standard specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, the operation and the maintenance of deicers and equipment designed exclusively for deicing and washing of aircraft with deicing/antiicing/washing liquids when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
NOTE 1 Safety of aircraft in connection with deicing/antiicing operations is not dealt with in this European Standard. Any, even minor, aircraft deicing or antiicing operation directly affects flight safety on take-off. Prevention of aeronautical accidents resulting from in-flight icing principally concerns the fluids and methods used, but it may in certain cases also concern deicing or antiicing equipment design or operation. These aeronautical aspects are controlled by the applicable Civil Aviation regulations ICAO 9640-AN/940, Manual of aircraft ground de-icing/anti-icing operations and EASA EU-OPS Subpart D 1.345 and its Acceptable Means of Compliance (AMC) and covered in ISO 11076:2012 (AEA Recommendations). They are not covered in this European Standard.
This European Standard applies to:
a) self-propelled deicers with fixed or mobile platform or hinged boom;
b) towable deicers with fixed or mobile platform or hinged boom;
c) stationary deicing/antiicing equipment (e.g. fixed boom, gantry or tower cranes equipped with aircraft deicing/antiicing fluid systems).
This European Standard does not apply to:
d) fixed installations, such as separate storage tanks or heating and filling stations, which are not an integrated part of the stationary deicing equipment;
e) hydraulic control systems;
f) pneumatic systems;
g) flow generating systems as such.
No extra requirements on noise and vibration are provided other than those in EN 1915-3 and EN 1915-4.
NOTE 2 EN 1915-3 and EN 1915-4 provide the general GSE vibration and noise requirements.
This European Standard is not dealing with hazards in respect to a standard automotive chassis and the traffic on the apron.
This part of EN 12312 is not applicable to deicers and deicing/antiicing equipment which are manufactured before the date of publication of this standard by CEN.
This part of EN 12312 when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4 provides the requirements for deicers and deicing/antiicing equipment.
- Standard42 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard11 pagesEnglish languagesale 15% off
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.
- Standard8 pagesEnglish languagesale 15% off
This European Standard specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of potable water service equipment when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This European Standard applies to:
a) self-propelled potable water vehicles;
b) towable potable water vehicles;
c) moveable parts of ramp integrated systems,
designed for servicing aircraft and intended to be used under the conditions given in EN 1915-1:2013, 1.
No extra requirements on noise and vibration are provided other than those in EN 1915-3 and EN 1915-4.
NOTE EN 1915-3 and EN 1915-4 provide the general GSE vibration and noise requirements.
This part of EN 12312 is not applicable to potable water service equipment which is manufactured before the date of publication of this standard by CEN.
This part of EN 12312, when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4, provides the requirements for potable water service equipment.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of lavatory service equipment when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This European Standard applies to:
a) self-propelled lavatory vehicles;
b) towable lavatory vehicles;
c) moveable parts of ramp integrated systems,
designed for servicing aircraft and intended to be used under the conditions given in EN 1915-1:2013, Clause 1.
No extra requirements on noise and vibration are provided other than those in EN 1915-3 and EN 1915-4.
NOTE EN 1915-3 and EN 1915-4 provide the general GSE vibration and noise requirements.
This part of EN 12312 is not applicable to lavatory service equipment which is manufactured before the date of publication of this standard by CEN.
This part of EN 12312, when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4, provides the requirements for lavatory service equipment.
- Standard18 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, the operation and the maintenance of deicers and equipment designed exclusively for deicing and washing of aircraft with deicing/antiicing/washing liquids when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
NOTE 1 Safety of aircraft in connection with deicing/antiicing operations is not dealt with in this European Standard. Any, even minor, aircraft deicing or antiicing operation directly affects flight safety on take-off. Prevention of aeronautical accidents resulting from in-flight icing principally concerns the fluids and methods used, but it may in certain cases also concern deicing or antiicing equipment design or operation. These aeronautical aspects are controlled by the applicable Civil Aviation regulations ICAO 9640-AN/940, Manual of aircraft ground de-icing/anti-icing operations and EASA EU-OPS Subpart D 1.345 and its Acceptable Means of Compliance (AMC) and covered in ISO 11076:2012 (AEA Recommendations). They are not covered in this European Standard.
This European Standard applies to:
a) self-propelled deicers with fixed or mobile platform or hinged boom;
b) towable deicers with fixed or mobile platform or hinged boom;
c) stationary deicing/antiicing equipment (e.g. fixed boom, gantry or tower cranes equipped with aircraft deicing/antiicing fluid systems).
This European Standard does not apply to:
d) fixed installations, such as separate storage tanks or heating and filling stations, which are not an integrated part of the stationary deicing equipment;
e) hydraulic control systems;
f) pneumatic systems;
g) flow generating systems as such.
No extra requirements on noise and vibration are provided other than those in EN 1915-3 and EN 1915-4.
NOTE 2 EN 1915-3 and EN 1915-4 provide the general GSE vibration and noise requirements.
This European Standard is not dealing with hazards in respect to a standard automotive chassis and the traffic on the apron.
This part of EN 12312 is not applicable to deicers and deicing/antiicing equipment which are manufactured before the date of publication of this standard by CEN.
This part of EN 12312 when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4 provides the requirements for deicers and deicing/antiicing equipment.
- Standard42 pagesEnglish languagesale 10% offe-Library read for1 day