AEROSPACE SERIES - BEARINGS, SPHERICAL PLAIN, 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 - PART 3: TECHNICAL SPECIFICATION

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

02-01-2018

Publisher

Aerospace & Defence Industries Association of Europe

1 Scope
2 Normative references
3 Terms and definitions
4 Requirements, inspection and test methods
5 Quality management system
6 Packaging
7 Certificate of conformity
Annex A (normative) - Verification of permissible and
ultimate static loads (C[s], C[a])
Annex B (normative) - Verification of dynamic radial
loads (C[dyn])
Annex C (normative) - Fluids - Essential characteristics
Annex D (normative) - Peeling strength and bond integrity
Annex E (normative) - Friction coefficient
Bibliography

Describes 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.

DocumentType	Draft
Pages	41
PublisherName	Aerospace & Defence Industries Association of Europe
Status	Current

TR 4475 : 1	AEROSPACE SERIES - BEARINGS AND MECHANICAL TRANSMISSIONS FOR AIRFRAME APPLICATIONS - VOCABULARY
MIL-PRF-87257 Revision C:2017	HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE
ISO 11078:2007	Aircraft De-icing/anti-icing fluids ISO types II, III and IV
EN 10204:2004	Metallic products - Types of inspection documents