Letectví a kosmonautika

Oblast zaměření: Letectví a kosmonautika
Komise : ASD-STAN (Aerospace)
Původce: CEN
K připomínkám do: 4.07.2022
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This document specifies the characteristics, qualification and acceptance requirements for helical coil screw thread inserts.

It is applicable whenever referenced.

Oblast zaměření: Letectví a kosmonautika
Komise : ASD-STAN (Aerospace)
Původce: CEN
K připomínkám do: 4.07.2022
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This document specifies the general conditions for test methods applicable to circuit breakers.

Oblast zaměření: Letectví a kosmonautika
Komise : ASD-STAN (Aerospace)
Původce: CEN
K připomínkám do: 1.08.2022
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This document defines the requirements for the effective control of non-deliverable software. This document can be used during the development, test, production, release, use, maintenance, and retirement of non-deliverable software. This can include non-deliverable software procured from outside manufacturers and incorporated in the production, evaluation, test, acceptance, or calibration of a deliverable product. When an organization outsources one or more of the processes involved in the creation of non-deliverable software, this document applies.

This document focuses solely on the unique requirements of the operational processes that pertain to non-deliverable software as defined by section 1.2. Operational processes not covered in this document are addressed by the organization’s Quality Management System (QMS), based on EN 9100 and/or ISO 9001.

Oblast zaměření: Letectví a kosmonautika
Komise : ASD-STAN (Aerospace)
Původce: CEN
K připomínkám do: 1.08.2022
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This document establishes the requirements for performing and documenting FAI. It is emphasized that the requirements specified in this document are complementary (not alternative) to customer and applicable statutory and regulatory requirements.

If there is a conflict between the requirements of this document, and customer or applicable statutory/regulatory requirements, the latter takes precedence.

In this document, the following verbal forms are used:

•      “shall” indicates a requirement;

•      “should” indicates a recommendation;

•      “may” indicates a permission;

•      “can” indicates a possibility or a capability.

Information marked as “NOTE” is for guidance in understanding or clarifying the associated requirement.

Oblast zaměření: Letectví a kosmonautika
Komise : ASD-STAN (Aerospace)
Původce: CEN
K připomínkám do: 8.08.2022
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This document specifies the requirements relating to:

Heat resisting nickel base alloy Ni‑Cr20Co3Fe3

Rm ≥ 650 MPa

Sheets and strips, cold rolled

0,25 mm < a ≤ 3 mm

for aerospace applications.

Oblast zaměření: Letectví a kosmonautika
Komise : ASD-STAN (Aerospace)
Původce: CEN
K připomínkám do: 8.08.2022
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This document specifies the characteristics of electrical wires DZA family for use in the on board:

—   115 V (phase to neutral) or 200 V (phase to phase) electrical network of aircraft;

—   230 V (phase to neutral) or 400 V (phase to phase) electrical network of aircraft and particularly use in non-pressurized areas.

This cable family is used at operating temperature between -65 °C and 260 °C. These cables are demonstrated to be arc resistant for both networks (115 V and 230 V).

Oblast zaměření: Letectví a kosmonautika
Komise : ASD-STAN (Aerospace)
Původce: CEN
K připomínkám do: 8.08.2022
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This document specifies the characteristics of UV laser printable electrical wires DZ family for use in the on board:

—   115 V (phase to neutral) or 200 V (phase to phase) electrical network of aircraft;

—   230 V (phase to neutral) or 400 V (phase to phase) electrical network of aircraft and particularly use in non-pressurized areas.

This cable family is used at operating temperature between -65 °C and 260 °C. These cables are demonstrated to be arc resistant for both networks (115 V and 230 V).

Oblast zaměření: Letectví a kosmonautika
Komise : ASD-STAN (Aerospace)
Původce: CEN
K připomínkám do: 8.08.2022
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This document specifies the characteristics of a UV laser printable coaxial cable, 50 Ω, type WZ, for use in aircraft electrical systems at operating temperatures between -65 °C and 200 °C and especially for high frequency up to 6 GHz.

The document encloses also a regular and reinforced cable version (code R) which is used for sensitive systems with controlled VSWR.