PREN 2314 : 1
Current
The latest, up-to-date edition.
AEROSPACE SERIES - SHOCK RESISTANT ACRYLIC SHEETS FOR AIRCRAFT GLAZING - TECHNICAL SPECIFICATION
Hardcopy , PDF
English
08-01-1984
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1 Scope and field of application
2 References
3 Materials
4 Classification
5 Physical properties
6 Optical defects
7 Optical properties
8 Resistance to weathering
9 Thermal properties
10 Mechanical properties
11 Susceptibility to crazing
12 Resistance to crack propagation
13 Dimensions
14 Qualification approval
15 Acceptance tests
16 Protection and packaging
17 Storage conditions
18 Marking
Specifies the characteristics of shock resistant transparent acrylic sheets for aircraft glazing.
| DocumentType |
Draft
|
| Pages |
13
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Current
|
| Standards | Relationship |
| DIN EN 2314:1990-10 (Draft) | Identical |
| PREN 2155-22 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZING - PART 22: DETERMINATION OF THERMAL RELAXATION OF STRETCHED ACRYLIC SHEET |
| PREN 2155-20 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZING - PART 20: DETERMINATION OF RETENTION OF STRENGTH AFTER CRAZING FOR AS-CAST ACRYLICS |
| EN 2155-19:1996 | Aerospace series - Test methods for transparent materials for aircraft materials for aircraft glazing - Part 19: Determination of craze resistance |
| PREN 2155-06 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZING - PART 6 - DETERMINATION OF OPTICAL DEFECTS |
| EN 2155-7:1997 | Aerospace series - Test methods for transparent materials for aircraft glazing - Part 7: Determination of optical deviation |
| EN 2155-9:1989 | Aerospace series - Test method for transparent materials for aircraft glazing - Part 9 : Determination of haze |
| PREN 2155-01 : 1 | AEROSPACE SERIES - TEST METHODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZING - PART 1 - DETERMINATION OF THE DENSITY AND RELATIVE DENSITY |
| PREN 2155 : 1 | AEROSPACE SERIES - TEST METHODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZING |
| PREN 2155-15 : 2 | AEROSPACE SERIES - TEST METHODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZING - PART 15 - DETERMINATION OF THERMAL STABILITY |
| EN 2155-14:1993 | Aerospace series - Test methods for tranparent materials for aircraft glazing - Part 14: Determination of the 1/10 Vicat softening temperature |
| PREN 2155-04 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR TRANSPARENT MATERIALS FOR AIRCRAFT GLAZING - PART 4 - DETERMINATION OF ULTRAVIOLET LIGHT TRANSMISSION OVER THE WAVELENGTH RANGE 280 TO 360 NM |
| EN 2155-2:1993 | Aerospace series - Test methods for transparent materials for aircraft glazing - Part 2: Determination of water absorption |
| EN 2155-12:1997 | Aerospace series - Test methods for transparent materials for aircraft glazing - Part 12: Determination of linear thermal expansion |
| EN 2155-8:1989 | Aerospace series - Test methods for transparent materials for aircraft glazing - Part 1: Determination of optical distortion |
| EN 2155-5:1989 | Aerospace series - Test methods for transparent materials for aircraft glazing - Part 5: Determination of visible light transmission |
| EN 2155-3:1993 | Aerospace series - Test methods for transparent materials for aircraft glazing - Part 3: Determination of refractive index |
| EN 2155-13:1993 | Aerospace series - Test methods for transparent materials for aircraft glazing - Part 13: Determination of temperature at deflection under load |
| EN 2155-21:1989 | Aerospace series - Test methods for transparent materials for aircraft glazing - Part 21: Determination of resistance to crack propagation (K factor) |
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