EN 2348:1988
(Main)Aerospace series - Control cable assemblies - Technical specification
Aerospace series - Control cable assemblies - Technical specification
This standard specifies the characteristics of control cable assemblies in accordance with EN 2641 for aeronautical applications.
Luft- und Raumfahrt - Seilzüge für Flugzeugsteuerungen - Technische Lieferbedingungen
Série aérospatiale - Câbles de commandes équipés - Spécification technique
Aerospace series - Control cable assemblies - Technical specification
General Information
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Control cable assemblies - Technical specificationLuft- und Raumfahrt - Seilzüge für Flugzeugsteuerungen - Technische LieferbedingungenSérie aérospatiale - Câbles de commandes équipés - Spécification techniqueAerospace series - Control cable assemblies - Technical specification49.035Sestavni deli za letal
...
This May Also Interest You
This document specifies the characteristics of spherical plain bearings in corrosion resisting steel, with assembly slots, metric series, with or without lubrication holes and groove, intended for use in fixed or moving parts of aircraft structure and control mechanisms, within the temperature range from −54 °C to 150 °C.
It also applies to the following temperature ranges when lubricated with the following greases (see EN 2337):
- ester type very high pressure grease (code letter A), operating range from −73 °C to 121 °C;
- synthetic hydrocarbon type very high pressure grease general purpose (code letter B), operating range from −54 °C to 177 °C.
Their field of application when lubricated with grease code letter A is limited to 121 °C.
- Standard10 pagesEnglish languagesale 10% offe-Library read for×1 day
This document specifies the characteristics of adjustable rod-ends with self-aligning double row ball bearing and threaded shank in steel.
They consist of:
- a rod-end comprising:
- either seals or shields;
- an optional longitudinal groove for locking purpose;
- an inner ring with balls.
These rod-ends are intended for use with flight control rods or rods for aerospace structures.
- Standard13 pagesEnglish languagesale 10% offe-Library read for×1 day
This document is applicable to new manufactured tags after publication of this document.
This document aims to:
- provide specification for RFID tag manufacturers to design and manufacture passive UHF RFID tags for the aeronautical industry;
- identify required performances for UHF RFID tags in order to be read/written during ground operations only, while being subject to the global flight environment;
- identify functional and environmental validation tests to be performed on passive UHF RFID tags with associated pass/fail criteria as well as associated test methods;
- check functionalities and resistance to environment for airborne passive UHF RFID tags.
This document does not apply to:
- the reader (interrogator – readers). It will be addressed appropriately by individual applicants;
- active RFID devices or battery assisted passive (BAP) RFID devices;
- RFID tags designed to operate outside the 860 MHz to 960 MHz frequency range.
- Standard25 pagesEnglish languagesale 10% offe-Library read for×1 day
This document is applicable in the aeronautical domain to on-board parts and to equipment intended to be embedded or positioned on any civil or military airborne vehicle with a type certificate.
The purpose of this document is to guide design, manufacturing, maintenance and operations organizations in the installation, removal and replacement of RFID tags (UHF and HF) and Contact Memory Buttons (CMB), according to the environments defined in RTCA DO-160/EUROCAE ED-14 and according to the type of support and the expected fixation performances. This guide will provide help in the specification of the tag installation/removal functions and/or will enable the solutions on offer from tag suppliers to be enhanced.
The term "tag" used in this document covers all the tags used to store electronic data, including RFID tags and CMB tags. As a reminder, the tags can also contain information that can be read by devices other than RFID or CMB readers (e.g. bar codes - Data Matrix, QR codes, etc., and/or alphanumerical characters) and information that can be read by the naked eye without any tools (human-readable).
- Standard33 pagesEnglish languagesale 10% offe-Library read for×1 day
This document specifies the minimum requirements for the qualification, acceptance, delivery and
inspection of standard parts by the aerospace industry and its manufacturers.
This document is valid for standard parts and their assemblies as described in a product standard, if
mentioned therein. This specification can also be applied to other parts when specifically invoked by
the terms of delivery.
Parts/sections of this document are not applicable in cases where the product standard stipulates
requirements that differ from this specification.
- Standard9 pagesEnglish languagesale 10% offe-Library read for×1 day
This document specifies the required characteristics for heat-shrinkable polyolefin identification
sleeving for use in aircraft electrical systems at operating temperatures between −55 °C and 135 °C.
This specification is for the characterisation of identification sleeves only.
This sleeving is flexible and flame retarded, and is available with 2:1 and 3:1 shrink ratios.
The product is normally supplied with internal diameters up to 57 mm.
The standard colours are white or yellow.
Sizes or colours other than those specifically listed in this standard may be available. These items are
considered to comply with this document if they comply with the property requirements listed in tables 3
and 4 except for dimensions and mass.
As the sleeving to be tested is a printed article the complete system is to be recorded as part of the
evaluation. The sleeve will only be considered as meeting the requirements of this document if printed
with the printer, ribbon, inks, and settings referenced within the test report.
Mark adherence and print permanence are determined in this document using method EN 6059-407.
- Standard13 pagesEnglish languagesale 10% offe-Library read for×1 day
This document specifies the required characteristics for heat-shrinkable semi rigid polyvinylidene identification sleeves for use in aircraft electrical systems at operating temperatures between -55 °C and 225 °C.
This specification is for the characterisation of Identification sleeves only.
This sleeving is a semi rigid tough product and is suitable for use where high temperatures and extreme fluid resistance properties are required.
It is available with a shrink ratio of 2:1.
The product is normally supplied with internal diameters up to 38 mm
The standard colours are white, black or yellow
For use at temperatures above 200 °C black with white or silver ink is recommended
Sizes or colours other than those specifically listed in this standard may be available. These items shall be considered to comply with this document if they comply with the property requirements listed in tables 2 and 3 except for dimensions and mass.
As the sleeving to be tested is a printed article the complete system is to be recorded as part of the evaluation. The sleeve will only be considered as meeting the requirements of this specification if printed with the printer, ribbon/inks and settings referenced within the test report.
Mark adherence and print permanence are determined in this document using method EN 6059-407.
- Standard11 pagesEnglish languagesale 10% offe-Library read for×1 day
This document specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for shock mounts with bushes, designed to withstand static and dynamic loads possible for aerospace interior applications in the temperature range from -55 °C to 85 °C.
- Standard20 pagesEnglish languagesale 10% offe-Library read for×1 day
This document specifies the dimensions, masses, the tolerances and the required characteristics of shock mounts with bushes for aerospace interior application and without contamination by phosphate-ester hydraulic fluids.
- Standard19 pagesEnglish languagesale 10% offe-Library read for×1 day
This document specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for a spherical plain bearing in corrosion resisting steel, with self-lubricating liner, for elevated loads at ambient temperature intended for use in fixed or moving parts of the aircraft structure and control mechanisms.
This document applies whenever referenced.
- Standard43 pagesEnglish languagesale 10% offe-Library read for×1 day
Questions, Comments and Discussion
Ask us and Technical Secretary will try to provide an answer. You can facilitate discussion about the standard in here.