EN 6057-2020 pdf download.Aerospace series – Rod-end with bearing EN 4265 in corrosion resisting steel, internal threaded shank -Dimensions and loads, Inch series.
This EN 6057 specifies the characteristics of adjustable rod-ends consisting oI
— 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.
2 Normative references
The following documents are referred to in the text in such a way that some or all of their content constitutes requirements of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies.
EN 2133, Aerospace series — Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys
EN 2424, Aerospace series — Marking of aerospace products
EN 4265, Aerospace series — Bearing sperical plain, metal-to-metal in corrosion resisting steel — Wide
series — Dimensions and loads — Inch series
EN 6099, Aerospace series Rod-end with plain bearing — Technical specification’
ISO 1132-1, Rolling bearings — Tolerances — Dejinitions
ISO 3161, Aerospace — UN] threads — General requirements and limit dimensions
ISO 8074, Aerospace — Surface treatment of austenitic stainless steel parts
MIL-PRF-23827, Grease, aircraft and instrument, gear and actuator screw, NATO Code Nummer G-354, metric2
MIL-PRF-46010, Lubricant, solid film, heat cured, corrosion-inhibiting2
MIL-PRF-8 1322, Grease, aircraft, general purpose, wide temperature range2
SAE AMS 5643, Steel, corrosion resistant, bars, wire, forgings, tubing, and rings I 6Cr-4.ONi-O.30(Cb.Ta)- 4.OCu solution heat treated, precipitation hardenable³
3 Terms, definitions and symbols
For the purposes of this document, the terms and definitions given in TR 4475 apply.
ISO and IEC maintain terininological databases for use in standardization at the following addresses:
— ISO Online browsing platform: available at http://www.iso.org/obp
— IEC Electropedia: available at http://www.electropedia.org/
Symbols of limit deviations are in accordance with definitions of ISO 1132-1.
a maximum angle of tilt of the outer ring with respect to the inner ring, with the spherical surface of the outer ring being completely in contact with the inner ring.
permissible static radial load
mp single plane mean bore diameter deviation
ds deviation of a single bore diameter
Push out load
C1 Fatigue load
4 Requirements
4.1 Configuration, dimensions, tolerances and mass
Configuration, dimensions, tolerances and mass shall be according to Figure 1 and Table 1.
Dimensions and tolerances are expressed in millimeters (inches).
Dimensions and tolerances are measured after surface treatment.
4.2 Surface roughness
Surface roughness shall be according with Figure 1.
Surface roughness is measured before surface treatment.
4.3 Material
Inner ring: see product standard EN 4265
Outer ring: see product standard EN 4265
Rod-end body: see SAE AMS 5643, hardness 35 ≤ HRC ≤ 42
4.4 Surface treatment
Rodend body:
Code T: Passivated according to ISO 8074
Code P: Cadmium plating and chromating according to EN 2133, 10 am to 20 im (400 in to 800 tin)
Bearing: See EN 4265
4.5 Loads and clearance
Loads and clearance shall be in according with Table 3 and Table 4,
4.6 Right or left hand thread
Right or left hand thread shall be according to Table 2.
4.9 Temperature range and lubricant
They shall be used in the temperature range as determined by the grease capability see below.
As they are lubricated by means of the following greases:
— code A: Grease as per MIL-PRF-23827 type 1, operating temperature range —73 °C to 121 °C.
— code B: Grease as per MIL-PRF-81322, operating temperature range —54°C to 177 °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).
NOTE lInecessary. the code 19005 shall be placed between the description block and the identity block.
6 Marking
Marking shall be according to EN 2424, style A.
7 Technical specification
Technical specification shall be according to EN 6099.
8 Quality management systems
The manufacturer’s operations shall be an approved production organisation for aerospace products and shall demonstrate that It has implemented and is able to maintain a quality management system (e.g. according to EN 9100 or an equivalent aerospace accepted and established quality management system).
The qualification procedure for aerospace standard products (e.g. according to EN 9133 or an equivalent aerospace accepted and established qualification procedure) shall be used and documented according to the specified tests if not otherwise agreed between customer and supplier.EN 6057-2020 pdf download.