I08 - Imaginarni 08

This document provides a visual identity to be displayed by European tourist organizations in accordance with CWA 5643-1 and establishes requirements and guidance on the use of the visual identity.
This document also includes informative annexes relating to implementation (checklist), references to national standards and protocols and information addressed to the user of the service offered by the tourist organizations.

This document establishes requirements and recommendations for tourist organizations to prevent the spread of coronavirus SARS-CoV-2 in order to protect their employees’ health from COVID-19 and to provide safer tourist services and products to tourists and residents.
NOTE   This document does not address after-work practices of employees.
This document applies to the whole tourism value chain, including the following 20 subsectors:
accommodation
adventure tourism and ecotourism
beaches
catering services
golf services
medical and wellness spas
MICE tourism
museums and heritage sites
natural protected areas (NPAs)
night leisure
scuba diving
ski areas
theme and leisure parks
NOTE   This includes water parks, animal parks (zoos, aquariums, wildlife refuges) and family entertainment centres.
tourist transport
tourist guides
tourist visits
tourist information offices
travel agencies
unique public spaces
yacht harbours and nautical activities
Each tourist organization is expected to conform only to those measures that apply to the services that it offers, including the core requirements established in Clause 4, the relevant applicable subclause in Clause 5 and the relevant applicable ancillary services and facilities in Clause 6.
NOTE   The term tourist organization applies for all 20 subsectors.

This standard specifies the characteristics of elbows 45°, welded ends, for pipe couplings 8°30', in titanium alloy, for
aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range:   55  C to 135  C

This standard specifies the requirements relating to:
Steel FE-WM1001 (X13Cr12)
Filler metal for welding
Wire and rod
for aerospace applications.

This standard specifies the characteristics of tees, with thrust wire nut on run, for pipe couplings 8°30', in titanium alloy, for
aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range:   55  C to 135  C

This standard specifies the requirements relating to:
Steel FE-WA2602 (X4NiCrTiMoV26-15)
Filler metal for welding
Wire and rod
for aerospace applications.

This standard specifies the characteristics of straight swivel nuts for pipe couplings, 60°, spherical, in TI-P64001, for aerospace applications.
NOTE Assembly in accordance with TR 4052.

This standard specifies a method of measuring the characteristic impedance of:
-   a permanent bus terminator;
-   a removable bus or stub terminator.
It shall be used together with EN 2591-100.

This standard specifies the standard procedures for conditioning prior to testing unaged fibre reinforced plastic materials including reinforcing fibres and cured resin systems for aerospace applications.
NOTE   In the case of uncured preimpregnate materials, requirements for conditioning before testing are specified in the relevant technical specification or test method.

This standard specifies a method of verifying the effectiveness of non-removable fixing of the hermetically sealed connector shell to the equipment shell.
It shall be used together with EN 2591.

This standard defines the dimensions and tolerances for the port connection of inch series pipe couplings, 37°, for aerospace applications.
Matched fluid system component shall have a port end in accordance with EN 4550-2.

This standard specifies a method of verifying the ability of an element of connection to withstand shock when submitted to repeated falls.
It shall be used together with EN 2591-100.

This standard specifies a method of verifying the ability of optical connection elements, with a hermetic sealing element to sustain thermal shock.
It shall be used together with EN 2591-100.

This standard specifies a method of testing the resistance of an optical cable to the kink test, for aerospace applications.

This standard specifies a method for measuring the capacitance variation in a cable (multipair cables).
It shall be used together with EN 3475-100.

This standard specifies a method of checking the ability of elements of electrical and optical connection to withstand the use of the tools for insertion and extraction of contacts.
It shall be used together with EN 2591-100.

This standard specifies the characteristics of unions, bulkhead, welded end, for pipe couplings 8°30', in titanium alloy, for aerospace applications.
Nominal pressure: 28 000 kPa
Temperature range: - 55 °C to 135 °C

TC - Minor editorial modifications

This standard specifies the characteristics of welded ferrules for inch series pipe couplings, 37°, in heat resisting steel, for aerospace applications.
Nominal pressure: Class D in accordance with ISO 6771

TC - Minor editorial modifications

This standard specifies a method of verifying that the relative magnetic permeability of a test item is below a specified value.
The method is suitable for low permeability values : i.e. relative magnetic permeability of 2,5 or less.
It shall be used together with EN 2591-100.

This standard specifies the characteristics of tees, reduced, with thrust wire nut on run, for pipe couplings 8 30', in titanium
alloy, for aerospace applications.
Nominal pressure:   up to 28 000 kPa
Temperature range:    55  C to 135  C

This standard specifies a method of measuring the mass of conductors and cables.
It shall be used together with EN 3475-100.

This standard specifies the characteristics of thrust wires for titanium alloy pipe couplings, 60°, spherical, in FE-PA 13, for aerospace applications.
NOTE Use with EN 3856.

This standard specifies a method of measuring the forward and backward crosstalk of light between multi-channel optical connection elements.
It shall be used together with EN 2591-100.

This standard specifies the characteristics of elbows 90°, bulkhead, welded end, long, for pipe couplings 8°30', in titanium
alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range:   55 °C to 135 °C

This standard specifies the characteristics for blanking plugs with lockring for pipe couplings 8°30', in titanium alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range: - 55 °C to  + 135 °C

TC - Minor editorial modifications

This standard specifies the characteristics of tees, reduced, for pipe couplings 8 30', in titanium alloy, for aerospace
applications.
Nominal pressure: up to 28 000 kPa
Temperature range:   55  C to 135  C

This standard specifies a method of measuring signal distortion of couplers.
It shall be used together with EN 2591-100.

This standard specifies a method of measuring open circuit impedance of couplers.
It shall be used together with EN 2591-100.

This standard specifies a method of determining the ability of optical connection elements (including permanent connections) and fibre optic couplers to withstand continuous acceleration.
It shall be used together with EN 2591-100.

This standard specifies the characteristics of unions, welded end, threaded for pipe couplings 8°30', in titanium alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range: - 55 °C to 135 °C

This standard specifies a method of determining the effects of accelerated ageing on a finished cable.
It shall be used together with EN 3475-100.

This standard specifies a method of verifying the effectiveness of the protection of contacts (scoop-proof) used in elements of electrical and optical connection.
It shall be used together with EN 2591-100.

This standard specifies the characteristics of spring tension clips for the support of electrical harnesses, in FE-PA3903 for aerospace applications.
Maximum operating temperature: 250 °C

ISO 16091:2002 describes the set of management requirements needed to identify and provide logistic support, so the customer can operate and maintain a product in its operational environment for the expected lifetime.
These requirements also aim, throughout the product life cycle, at implementing everything pertinent to the control of the risks considered as critical regarding the operational objectives.
The management requirements are applicable to those activities necessary to design, develop, deliver, deploy and manage an organized and structured set of materials and software, services, processes and information dedicated to support the system throughout its life cycle.
ISO 16091:2002 specifies management, studies, production activities, information management processes and tasks to meet the customer's need for logistic support.
When viewed from the perspective of a specific programme or project context, the requirements defined in ISO 16091:2002 should be tailored to match the genuine requirements of a particular profile and circumstances of a programme or project.

This standard specifies the dimensions and tolerances of:
Sheets
in aluminium and aluminium alloys
Thickness 0,25 mm < a < 6 mm
for aerospace applications.

This standard specifies a method of checking the resistance to damage under torsion of insulated conductors or finished cables.
It shall be used together with EN 3475-100.

This standard specifies the characteristics of welded ferrules for pipe couplings, 60°, spherical, in TI-P64001, for aerospace applications.
NOTE  Assembly in accordance with TR 4052

This standard defines the dimensions and tolerances for the port end of inch series pipe couplings, 37°, for aerospace applications.
Matched fluid system component shall have a port connection in accordance with EN 4550-3.

This standard specifies the characteristics for bulkhead unions for pipe couplings 8°30', in titanium alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range: - 55 °C to  + 135 °C

This standard specifies a method of assessing the capability of a cable to resist different hot and humid environments.
It shall be used together with EN 3475-100.

This standard specifies a method of determining the stability in insert of male contacts used in elements of electrical and optical connection.
It shall be used together with EN 2591-100.

This standard specifies the requirements relating to:
Steel FE-WM1501 (X13CrNiMoCo12-3-2-2)
Filler metal for welding
for aerospace applications.

This standard specifies the requirements relating to:
Magnesium alloy MG-W68001
Filler metal for welding
Wire and rod
for aerospace applications.

This standard specifies a method of checking the sealing of optical connection elements (including permanent connections) and fibre optic couplers exposed to low pressure.
It shall be used together with EN 2591-100.

TC - Minor editorial modifications

AECMA - Correction in table

This standard specifies the characteristics of threaded straight unions for pipe couplings, 60° spherical, in TI-P64001, for aerospace applications.
NOTE  Assembly in accordance with TR 4052, port connection prEN 4051