49.035 - Components for aerospace construction
ICS 49.035 Details
Components for aerospace construction
Bauteile und Komponenten der Luft- und Raumfahrttechnik
Composants pour la construction aeronautique
Sestavni deli za letalsko in vesoljsko gradnjo
General Information
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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 for1 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 cover:
- 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 to 960 MHz frequency range.
- Standard25 pagesEnglish languagesale 10% offe-Library read for1 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 for1 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 for1 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 for1 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 for1 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 for1 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 for1 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 for1 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 for1 day
This European standard 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 for1 day
This European standard specifies the dimensions, mass, 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 for1 day
The intended users of the “Mechanical shock design and verification handbook” are engineers involved in design, analysis and verification in relation to shock environment in spacecraft. The current know-how relevant to mechanical shock design and verification is documented in this handbook in order to make this expertise available to all European spacecraft and payload developers.
The handbook provides adequate guidelines for shock design and verification; therefore it includes advisory information, recommendations and good practices, rather than requirements.
The handbook covers the shock in its globally, from the derivation of shock input to equipment and sub-systems inside a satellite structure, until its verification to ensure a successful qualification, and including its consequences on equipment and sub-systems. However the following aspects are not treated herein:
- No internal launcher shock is treated in the frame of this handbook even if some aspects are common to those presented hereafter. They are just considered as a shock source (after propagation in the launcher structure) at launcher/spacecraft interface.
- Shocks due to fall of structure or equipment are not taken into account as they are not in the frame of normal development of a spacecraft.
- Technical report540 pagesEnglish languagesale 10% offe-Library read for1 day
This document recommends engineering practices for European programs and projects. It may be cited in contracts and program documents as a reference for guidance to meet specific program/project needs and constraints.
The target users of this handbook are engineers involved in design, analysis and verification of launchers and spacecraft in relation to structural stability issues. The current know‐how is documented in this handbook in order to make this expertise available to all European developers of space systems.
It is a guidelines document; therefore it includes advisory information rather than requirements.
- Technical report462 pagesEnglish languagesale 10% offe-Library read for1 day
This document recommends engineering practices for European programs and projects. It may be cited in contracts and program documents as a reference for guidance to meet specific program/project needs and constraints.
The target users of this handbook are engineers involved in design, analysis and verification of spacecraft and payloads in relation to general structural loads analysis issues. The current know‐how is documented in this handbook in order to make this expertise available to all European developers of space systems.
It is a guidelines document; therefore it includes advisory information rather than requirements.
- Technical report502 pagesEnglish languagesale 10% offe-Library read for1 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 for1 day
This document specifies the characteristics of a bearing, spherical plain in corrosion resisting steel with self-lubricating liner, wide series for aerospace applications.
These bearings are not intended for use of moving parts especially for control mechanism and operating system. They shall be used in the temperature range -55 °C to 163 °C.
- Standard14 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of a bearing, spherical plain in corrosion resisting steel with self-lubricating liner, narrow series for aerospace applications.
These bearings are not intended for use of moving parts especially for control mechanisms and operating systems. They shall be used in the temperature range -55 °C to 163 °C.
- Standard14 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for 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 standard applies whenever referenced.
- Standard43 pagesEnglish languagesale 10% offe-Library read for1 day
This standard specifies the characteristics of bearing, spherical plain in corrosion resisting steel with self-lubricating liner, narrow series for aerospace applications.
These tie rods are not intended for use of moving parts especially for control mechanism and operating system. They shall be used in the temperature range −55 °C to 163 °C.
- Standard14 pagesEnglish languagesale 10% offe-Library read for1 day
This standard specifies the characteristics of bearing, spherical plain with self lubricating liner in corrosion resisting steel with self-lubricating liner, wide series for aerospace applications.
These tie rods are not intended for use of moving parts especially for control mechanism and operating system. They shall be used in the temperature range −55 °C to 163 °C.
- Standard14 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the required characteristics, inspections and tests, quality assurance, conditions for qualification, acceptance and delivery of rod-ends with self-aligning bearings metal to metal designed to withstand slight swivelling under load. They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
This document applies to all rod-ends with self-aligning bearings metal to metal. It may be applied when referred to in a product standard or in a design specification.
- Standard22 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing with reduced internal radial clearance and threaded shank in corrosion resisting steel, designed to withstand only slow rotations and oscillations under load.
They consist of:
- a rod end comprising:
- circumferential groove to identify location;
- 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.
They are intended to be used in the temperature range: −54 °C to 150 °C.
However, being lubricated with the following greases:
- very high pressure grease, ester type (code A), operational range −73 °C to 121 °C; or
- very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range −54 °C to 177 °C (see EN 2067);
their field of application when lubricated with code A grease is limited to 121 °C.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing in corrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy, designed to withstand only slow rotations and oscillations under load.
They consist of:
- a rod end comprising:
- circumferential groove to confirm that the assembled rod-end is "in safety" emphasized with the application of red paint;
- 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.
They are intended to be used in the temperature range: −54 °C to 150 °C.
However, being lubricated with the following greases:
- very high pressure grease, ester type (code A), operational range −73 °C to 121 °C; or
- very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range −54 °C to 177 °C (see EN 2067);
their field of application when lubricated with code A grease is limited to 121 °C.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of adjustable rod-ends consisting of:
- a spherical plain bearing, metal to metal, in corrosion resisting steel, wide series (EN 4265)
- a rod end with internal threaded shank
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the required characteristics, inspections and tests, quality assurance, conditions for qualification, acceptance and delivery of rod-ends with self-aligning bearings metal to metal designed to withstand slight swivelling under load. They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
This document applies to all rod-ends with self-aligning bearings metal to metal. It may be applied when referred to in a product standard or in a design specification.
- Standard22 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing in corrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy, designed to withstand only slow rotations and oscillations under load.
They consist of:
- a rod end comprising:
- circumferential groove to confirm that the assembled rod-end is "in safety" emphasized with the application of red paint;
- 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.
They are intended to be used in the temperature range: −54 °C to 150 °C.
However, being lubricated with the following greases:
- very high pressure grease, ester type (code A), operational range −73 °C to 121 °C; or
- very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range −54 °C to 177 °C (see EN 2067);
their field of application when lubricated with code A grease is limited to 121 °C.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing with reduced internal radial clearance and threaded shank in corrosion resisting steel, designed to withstand only slow rotations and oscillations under load.
They consist of:
- a rod end comprising:
- circumferential groove to identify location;
- 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.
They are intended to be used in the temperature range: −54 °C to 150 °C.
However, being lubricated with the following greases:
- very high pressure grease, ester type (code A), operational range −73 °C to 121 °C; or
- very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range −54 °C to 177 °C (see EN 2067);
their field of application when lubricated with code A grease is limited to 121 °C.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of adjustable rod-ends consisting of:
- a spherical plain bearing, metal to metal, in corrosion resisting steel, wide series (EN 4265)
- a rod end with internal threaded shank
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of inch based spherical plain bearing, metal to metal, in corrosion resisting steel, narrow series.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
They shall be used in the temperature range as determined by the grease capability as below:
- code A: grease as per MIL PRF 23827 Type I, operating temperature range −73 °C to 121 °C;
- code B: grease as per MIL PRF 81322, operating temperature range −54 °C to 177 °C.
The range of application for bearings lubricated with grease per code A is limited to 121 °C.
In both cases the spherical surface of the outer or inner ring have to be provided with a dry film lubricant as per MIL PRF 46010 or equivalent (anti seizing protection).
- Standard17 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of spherical plain bearings in corrosion resisting steel with self-lubricating liner, low starting torque and low friction coefficient, elevated duty cycles under low oscillations at different operating conditions, narrow series for aerospace applications.
These self-lubricating spherical plain bearings are intended for use in fixed or moving parts of the aircraft structure especially for control mechanism and operating systems. The bearings are designed to be subjected under low dynamic radial loads and slow rotations in the temperature range of −55°C to 120 °C (−67°F to 248 °F).
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the characteristics of spherical plain bearings in corrosion resisting steel with self-lubricating liner, low starting torque and low friction coefficient, elevated duty cycles under low oscillations at different operating conditions, wide series for aerospace applications.
These self-lubricating spherical plain bearings are intended for use in fixed or moving parts of the aircraft structure especially for control mechanism and operating systems. The bearings are designed to be subjected under low dynamic radial loads and slow rotations in the temperature range of −55°C to 120 °C (−67 °F to 248 °F).
- Standard14 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for spherical plain bearings in corrosion resisting steel with self-lubricating liner, low starting torque and low friction coefficient, elevated duty cycles under low oscillations at different operating conditions.
This standard applies whenever referenced.
These self-lubricating spherical plain bearings are intended for use in fixed or moving parts of the aircraft structure especially for control mechanism and operating systems. The bearings are designed subjected under low dynamic radial loads and slow rotations in the temperature range of −55 °C to 120 °C (−67 °F to 248 °F).
The liner may be of a fabric or composite material bonded to the inside diameter of the outer ring or in a composite material moulded into a pre-formed cavity between the inner and outer rings.
- Standard42 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of spherical plain bearing in corrosion resistant steel, with self-lubricating liner, wide series, elevated load under low oscillations applications.
They shall be used in the temperature range −55 °C to 163 °C.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of inch based spherical plain bearing, metal to
metal, in corrosion resisting steel, narrow series.
They are intended for use in fixed or moving parts of the aircraft structure and their control
mechanisms.
They shall be used in the temperature range as determined by the grease capability as below:
— code A: grease as per MIL-PRF-23827 Type I, operating temperature range −73 °C to 121 °C;
— code B: grease as per MIL-PRF-81322, operating temperature range −54 °C to 177 °C.
The range of application for bearings lubricated with grease per code A is limited to 121 °C.
In both cases the spherical surface of the outer or inner ring have to be provided with a dry-film
lubricant as per MIL-PRF-46010 or equivalent (anti-seizing protection).
- Standard17 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of adjustable rod-ends consisting of:
- a self aligning ball bearing with self lubricating liner (EN 4614);
- a rod end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of adjustable rod-ends consisting of:
- a spherical plain bearing, metal to metal, in corrosion resisting steel, wide series (EN 4265);
- a rod-end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of inch based spherical plain bearings, metal to metal, in corrosion resisting steel, extra wide inner ring inch series.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
The slide hole treatment either at the outer ring or inner ring.
- Standard17 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of adjustable rod ends consisting of:
- a spherical plain bearing, metal to metal, in corrosion resisting steel, extra wide series (EN 6097);
- a rod–end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of adjustable rod-ends consisting of:
- a self-aligning spherical plain bearing with self-lubricating liner per EN 6096;
- a rod-end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies general characteristics of spherical plain bearings in corrosion resisting steel with self-lubricating liner, extra wide inner ring, inch series.
They are intended for use in fixed or moving parts of the aircraft structure and control mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of spherical plain bearings in corrosion resisting steel with self-lubricating liner, low starting torque and low friction coefficient, elevated duty cycles under low oscillations at different operating conditions, wide series for aerospace applications. These self-lubricating spherical plain bearings are intended for use in fixed or moving parts of the aircraft structure especially for control mechanism and operating systems. The bearings are designed to be subjected under low dynamic radial loads and slow rotations in the temperature range of -55°C to 120 °C (-67 °F to 248 °F).
- Standard14 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of spherical plain bearings in corrosion resisting steel with self-lubricating liner, low starting torque and low friction coefficient, elevated duty cycles under low oscillations at different operating conditions, narrow series for aerospace applications. These self-lubricating spherical plain bearings are intended for use in fixed or moving parts of the aircraft structure especially for control mechanism and operating systems. The bearings are designed to be subjected under low dynamic radial loads and slow rotations in the temperature range of -55°C to 120 °C (-67°F to 248 °F).
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of spherical plain bearing in corrosion resistant steel, with self-lubricating liner, wide series, elevated load under low oscillations applications. They shall be used in the temperature range -55 °C to 163 °C.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of spherical plain bearings in corrosion resisting steel, with self lubricating liner, narrow series, for elevated load. at ambient temperature, with or without swaging groove, intended for use in the fixed or moving parts of the aircraft structure and control mechanisms.
They shall be used in the temperature range −55 °C to +163 °C.
- Standard12 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of spherical plain bearings in corrosion resisting steel, with self- lubricating liner, wide series, for elevated load at ambient temperature, with or without swaging groove, intended for use in the fixed or moving parts of the aircraft structure and control mechanisms.
They shall be used in the temperature range -55° C to +163° C.
- Standard12 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies preferred test fluids for evaluating the resistance of non-metallic and related materials to the action of fluids.
The aim of this document is to rationalise the choice of fluids used for qualification and batch testing of materials.
In some cases, the test fluid and conditioning temperatures may closely simulate in-service conditions. However, no direct behaviour with service conditions shall be implied.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of adjustable rod-ends consisting of:
— a self-aligning spherical plain bearing with self-lubricating liner per EN 6096;
— a rod-end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control
mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of adjustable rod-ends consisting of:
a spherical plain bearing, metal to metal, in corrosion resisting steel, wide series (EN 4265);
a rod-end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control
mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the characteristics of adjustable rod ends consisting of:
a spherical plain bearing, metal to metal, in corrosion resisting steel, extra wide series (EN 6097);
a rod–end with threaded shank with an optional longitudinal groove for locking purposes.
They are intended for use in fixed or moving parts of the aircraft structure and their control
mechanisms.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day