PREN 2491 : 200P1
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
AEROSPACE SERIES - MOLYBDENUM DISULPHIDE DRY LUBRICANTS - COATING METHODS
Hardcopy , PDF
23-07-2013
English
Foreword
1 Scope
2 Purpose of process
3 Normative references
4 Terms and definitions
5 Apparatus
6 Information for the processor
7 Surface roughness of parts prior to application
8 Surface preparation
9 Coating
10 Post-treatment
11 Removal of the film
12 Characteristics, requirements and test methods
13 Quality assurance
14 Acceptance
15 Re-Treatment
Specifies the coating methods and characteristics of molybdenum disulphide dry film lubricants which may be applied to parts in titanium, titanium alloys, steel, corrosion resistant steel and nickel based alloys.
DocumentType |
Draft
|
Pages |
8
|
PublisherName |
Aerospace & Defence Industries Association of Europe
|
Status |
Withdrawn
|
Standards | Relationship |
09/30214446 DC : 0 | Identical |
PREN 2264 : 1995 | AEROSPACE SERIES - NUTS, ANCHOR, SELF-LOCKING, FLOATING, TWO LUG, INCREMENTAL COUNTERBORE, IN ALLOY STEEL, CADMIUM PLATED, MOS2 LUBRICATED - CLASSIFICATION: 900 MPA (AT AMBIENT TEMPERATURE) / 235 DEGREES C |
PREN 3538 : 200P1 | AEROSPACE SERIES - NUTS, ANCHOR, SELF-LOCKING, FIXED, TWO LUG, REDUCED SERIES, WITH COUNTERBORE, IN HEAT RESISTING STEEL, MOS[2] LUBRICATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/315 DEGREE C |
PREN 3566 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30 MINUTES IN TITANIUM ALLOY - ADAPTERS WITH LOCKING RING |
DIN EN 3740:1996-11 | AEROSPACE SERIES - BOLTS, SHOULDERED, THIN HEXAGONAL HEAD, CLOSE TOLERANCE SHANK, SHORT THREAD, IN TITANIUM ALLOY, ANODIZED, MOS[2] LUBRICATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/315 DEGREES C |
EN 2884:1996 | Aerospace series - Screws, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C |
EN 3723:1996 | Aerospace series - Nuts, hexagonal, self-locking, in heat resisting steel, FE-PA92HT (A286), MoS2 coated - Classification: 1 100 MPa (at ambient temperature)/425°C |
EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
EN 2516:1997 | Aerospace series - Passivation of corrosion resisting steels and decontamination of nickel base alloys |
TR 4070 : 1 | AEROSPACE SERIES - MOLYBDENUM DISULPHIDE COATINGS - LIST OF COMMERCIAL PRODUCTS |
ISO 1463:2003 | Metallic and oxide coatings Measurement of coating thickness Microscopical method |
EN 2133:2010 | Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys |
ISO 8080:1985 | Aerospace Anodic treatment of titanium and titanium alloys Sulfuric acid process |
ISO 2431:2011 | Paints and varnishes Determination of flow time by use of flow cups |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.