49 Aircraft and space vehicle engineering

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New Standards

EVS-EN 6059-503:2012
Price 5.11 EUR
Aerospace series - Electrical cables, installation - Protection sleeves - Test methods - Part 503: Temperature rise due to rated current injected on the sleeve
This European Standard specifies a method of assessing the behaviour and temperature increase of EMI protection sleeves or conduits subject to permanent and/or fault currents in the shielding. It should be used together with EN 3475-100.

EVS-EN 3155-076:2012
Price 7.29 EUR
Aerospace series - Electrical contacts used in elements of connection - Part 076: Contacts, electrical, male, type A, crimp, class R - Product standard
This European Standard specifies the required characteristics, tests and tooling applicable to male contacts size 22, 20, 16, 12, 8 and 5, type A, crimp, class R, used in elements of connection according to EN 3155-002. It should be used together with EN 3155-001. The associated female contacts are defined in EN 3155-077.

EVS-EN 3155-077:2012
Price 8.63 EUR
Aerospace series - Electrical contacts used in elements of connection - Part 077: Contacts, electrical, female, type A, crimp, class R - Product standard
This European Standard specifies the required characteristics, tests and tooling applicable to female contacts size 22, 20, 16, 12, 8 and 5, type A, crimp, class R, used in elements of connection according to EN 3155-002. It should be used together with EN 3155-001. The associated male contacts are defined in EN 3155-076.

ISO 10502:2012
Price 80.62 EUR
Aerospace -- Hose assemblies in polytetrafluoroethylene (PTFE) for use up to 232 °C and 10 500 kPa -- Technical specifications and requirements

Replaced Standards

ISO 10502:1992
Aerospace -- Hose assemblies in polytetrafluoroethylene (PTFE) for use up to 232 degrees C and 10 500 kPa -- Procurement specification

Language: English

Drafts

FprEN 3682-004
Deadline 3/31/2012
Aerospace series - Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous - Part 004: Size 2 receptacle - Product standard
This standard defines the size 2 receptacle used in the family of rectangular electrical connectors for rack to panel, with interchangeable inserts. The plug corresponding to this receptacle is defined in EN 3682-005.
Language: English

FprEN 4632-004
Deadline 3/31/2012
Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 004: Homogeneous assemblies highly alloyed steels
This standard specifies the weldability and brazeability of materials or material families used in the aerospace industry. It comprises a series of sheets, by materials or material family, which: - indicate the main titles, the typical chemical composition and the main characteristics, - contain recommendations for welding and brazing, - indicate a degree of weldability or brazeability for a given process under defined conditions. - indicate a value for the welded joint mechanical resistance coefficient for each welding process when extracted from relevant bibliographical references. Joint coefficient is the ratio of stress resistance transversally to welded joint over tensile strength of parent alloy. It recommends ISO/TR 17671-3 and EN 1011-3 recommendations for pre-heating conditions specially for the welding of martensitic steels. These conditions depend on the line energy of welding, thickness, arc welding process and of hydrogen rate in filler metal. It applies unreservedly to the manufacturing of new parts or for repair.
Language: English

FprEN 2591-307
Deadline 3/31/2012
Aerospace series - Elements of electrical and optical connection - Test methods - Part 307: Salt mist
This standard specifies a method of assessing the effects of salt mist on elements of connection. It shall be used together with EN 2591-100. The test is based on EN 60068-2-11
Language: English

FprEN 2591-402
Deadline 3/31/2012
Aerospace series - Elements of electrical and optical connection - Test methods - Part 402: Shock
This standard specifies a method of assessing the ability of elements of connection to withstand mechanical shock of a specified severity. It shall be used together with EN 2591-100. This test is based on EN 60068-2-27.
Language: English

FprEN 2591-403
Deadline 3/31/2012
Aerospace series - Elements of electrical and optical connection - Test methods - Part 403: Sinusoidal and random vibration
This standard specifies a method of determining the ability of elements of connection to withstand sinusoidal or random vibrations of specified severities. It shall be used together with EN 2591-100. This test is based on EN 60068-2-6 and EN 60068-2-64.
Language: English

FprEN 3745-405
Deadline 3/31/2012
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 405: Low/High temperature bend test
This standard specifies a method of determining the attenuation variation of an optical cable during mechanical bending under load at the maximum and minimum operating temperatures.
Language: English

FprEN 3745-510
Deadline 3/31/2012
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 510: Bending test
This standard specifies a method of determining the attenuation variation of an optical cable during mechanical bending under load at the maximum and minimum operating temperatures.
Language: English

FprEN 3745-515
Deadline 3/31/2012
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 515: Buffer insertion force
This standard specifies procedures for the practical measurement of the force required to move the buffer a specified distance relative to the outer jacket.
Language: English

FprEN 3745-516
Deadline 3/31/2012
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 516: Severe cable bend test
This standard specifies a method of checking the break resistance and attenuation variation recovery of an optical cable subjected to severe bending under load.
Language: English

FprEN 3745-517
Deadline 3/31/2012
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 517: Cable tie clamping test
This standard specifies a method of determining the attenuation variation of an optical cable when clamped to a mandrel with cable ties, simulating the condition in an installed harness.
Language: English

FprEN 3456
Deadline 3/31/2012
Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled - a ≤ 6 mm
This standard specifies the requirements relating to: Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Sheet and strip, hot rolled a ≤ 6 mm for aerospace applications.
Language: English

FprEN 3464
Deadline 3/31/2012
Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Plate - 6 mm < a ≤ 100 mm
This standard specifies the requirements relating to: Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Plate 6 mm < a ≤ 100 mm for aerospace applications.
Language: English

FprEN 60952-1
Deadline 3/31/2012
Aircraft batteries - Part 1: General test requirements and performance levels
This part of IEC 60952 defines test procedures for the evaluation, comparison and qualification of batteries and states minimum performance and environmental levels for airworthiness. Where specific tests are defined with no pass/fail requirement (to establish performance capability), the manufacturer’s declared values, from qualification testing, will be used to establish minimum requirements for ongoing maintenance of approval for that design of battery. To provide representative examples, this standard utilises voltage and current values based upon an aircraft electrical system nominally rated at 28 V d.c. Additionally, the nominal values for cell voltage are assumed to be 1,2 V per cell for nickel-cadmium batteries and 2,0 V per cell for lead-acid batteries. It is important to note that when using this standard to evaluate products designed to operate on an aircraft electrical system other than the nominal 28 V d.c., or whose chemical properties are such that the individual cell voltage differs from that stated above, test values need to be adjusted accordingly. The specific topics addressed in this part of 60952 serve to establish acceptable quality standards required to qualify a battery as airworthy. In cases where the requirements for a specific application exceed those detailed in this standard the purchaser will detail said requirements in the product specification and the method of establishing compliance.
Language: English

FprEN 60952-2
Deadline 3/31/2012
Aircraft batteries - Part 2: Design and construction requirements
This part of IEC 60952 defines the physical design, construction and material requirements for nickel-cadmium and lead-acid aircraft batteries containing vented or valve-regulated cells or monoblocs. The batteries are used for both general purposes and specific aerospace applications. The specific topics addressed in this part serve to establish acceptable quality standards required to qualify a battery as airworthy as defined in Clause 3 of IEC 60952-1. A preferred range of aircraft batteries is specified in Annex A, but this part of IEC 60952 may be used for other battery sizes, arrangements and ratings. For particular applications, other design requirements may be stipulated. These will be in addition to the requirements of this part and will be covered by specific documents.
Language: English

FprEN 60952-3
Deadline 3/31/2012
Aircraft batteries - Part 3: Product specification and declaration of design and performance (DDP)
This part of IEC 60952 defines requirements for the product specification as well as procedures for a Declaration of Design and Performance (DDP) for nickel-cadmium and lead-acid aircraft batteries containing vented or valve-regulated cells or monoblocs. The batteries are used for both general purposes and specific aerospace applications. The specific topics addressed in this part serve to establish acceptable quality standards required to qualify a battery as airworthy as defined in Clause 3 of IEC 60952-1. The design construction and test requirements should conform to the requirements specified in IEC 60952-1 and IEC 60952-2.
Language: English