EN 2243-1 : 2005
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The latest, up-to-date edition.
AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 1: SINGLE LAP SHEAR
Published date
16-11-2005
Publisher
Foreword
1 Scope
2 Normative references
3 Test samples
4 Surface preparation
5 Bonding
6 Storage of test samples after bonding
7 Cutting and preparation of test pieces
8 Test conditions
9 Method of test
10 Calculation of results
11 Test report
The objective of this standard is to establish the test methods for defining the strength of suitable structural adhesives in metal to metal single lap shear, at ambient and other temperatures.
| DevelopmentNote |
Supersedes PREN 2243-01. (03/2006)
|
| DocumentType |
Test Method
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| BS EN 2243-1:2005 | Identical |
| NF EN 2243-1 : 2006 | Identical |
| PN EN 2243-1 : 2006 | Identical |
| UNE-EN 2243-1:2006 | Identical |
| UNI EN 2243-1 : 2007 | Identical |
| DIN EN 2243-1:2007-04 | Identical |
| I.S. EN 2243-1:2006 | Identical |
| NBN EN 2243-1 : 2006 | Identical |
| SN EN 2243-1 : 2006 | Identical |
| NS EN 2243-1 : 1ED 2005 | Identical |
| NEN EN 2243-1 : 2005 | Identical |
| UNE-EN 2243-1:2005 | Identical |
| DEFSTAN 00-970(PT1)SEC4/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION |
| DEFSTAN 00-970(PT1)SEC4/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
| DEFSTAN 00-970(PT1)SEC4/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION |
| DEFSTAN 00-970(PT7)SEC2/SUPP4/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D) |
| DEFSTAN 00-970(PT7)SEC4/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 4: DETAIL DESIGN AND STRENGTH OF MATERIALS |
| DEFSTAN 00-970(PT1)SEC4/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 4: DESIGN AND CONSTRUCTION |
| DEFSTAN 00-970(PT7)SEC4/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 4: DETAIL DESIGN AND STRENGTH OF MATERIALS |
| DEFSTAN 00-970(PT1)SEC4/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
| DEFSTAN 00-970(PT1)SEC4/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
| DEFSTAN 00-970(PT1)SEC4/4(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 4: DESIGN AND CONSTRUCTION |
| DEFSTAN 00-970(PT1)SEC4/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FORD SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
| DEFSTAN 00-970(PT1)SEC4/13(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
| ISO 9940:2015 | Aerospace series Fluid, hydraulic, phosphate ester-base, fire resistant Technical specification |
| DIN EN 2243-5:2006-10 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 5: AGEING TESTS |
| I.S. EN 2243-5:2005 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 5: AGEING TESTS |
| 99/701511 DC : DRAFT JAN 1999 | PREN 4106 - AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| BS EN 4106:2013 | Aerospace series. Non-metallic materials. Structural adhesive systems. Paste adhesive. Technical specification |
| UNI EN 4106 : 2014 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| DEFSTAN 00-970(PT1)SEC4/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
| DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D) |
| 12/30234431 DC : 0 | BS ISO 9940 - AEROSPACE - FIRE RESISTANT HYDRAULIC FLUIDS |
| BS ISO 9940:2015 | Aerospace series. Fluid, hydraulic, phosphate ester-base, fire resistant. Technical specification |
| 13/30290460 DC : 0 | BS ISO 9940 - AEROSPACE SERIES - FLUID, HYDRAULIC, PHOSPHATE ESTER-BASE, FIRE RESISTANT - TECHNICAL SPECIFICATION |
| 14/30302298 DC : 0 | BS ISO 9940 - AEROSPACE SERIES - FLUID, HYDRAULIC, PHOSPHATE ESTER-BASE, FIRE RESISTANT - TECHNICAL SPECIFICATION |
| PREN 2243-6 : 200P2 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 6: DETERMINATION OF SHEAR STRESS AND SHEAR STRAIN |
| BS EN 2243-5:2005 | Aerospace series. Non-metallic materials. Structural adhesives. Test method Ageing tests |
| BS EN 2243-6:2005 | Aerospace series. Non-metallic materials. Structural adhesives. Test method Determination of shear stress and shear strain |
| EN 2243-5:2005 | Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 5: Ageing tests |
| EN 2243-6 : 2005 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 6: DETERMINATION OF SHEAR STRESS AND SHEAR STRAIN |
| EN 4106:2013 | Aerospace series - Non-metallic materials - Structural adhesive systems - Paste adhesive - Technical specification |
| I.S. EN 4106:2013 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| PREN 3464 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - PLATE - 6 MM < A <= 100 MM |
| EN 2334 : 1997 | AEROSPACE SERIES - CHROMIC-SULPHURIC ACID PICKLE OF ALUMINIUM AND ALUMINIUM ALLOYS |
| PREN 2088 : 200P1 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A-T4 OR T42 - CLAD SHEETS AND STRIP - 0,4 MM <= A <= 6 MM |
| PREN 2540 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3902 (X7CRNIAL17-7) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION HARDENED - SHEET AND STRIP - A <= 6 MM - 1240 MPA <= R[M] <= 1450 MPA |
| EN 2497 : 1989 | AEROSPACE SERIES - DRY ABRASIVE BLASTING OF TITANIUM AND TITANIUM ALLOYS |
| PREN 2090 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T3 - CLAD SHEET AND STRIP - 0,3 MM <= A <= 6 MM |
| PREN 3456 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM |
| PREN 2517 : 2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P63 - ANNEALED SHEETS, STRIPS AND PLATES - A <= 100 MM |
| EN 2092:2005 | Aerospace series - Aluminium alloy AL-P7075-T6 or T62 - Clad sheet and strip - 0,4 mm |
| PREN 2087 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2014A - T6 OR T62 - CLAD SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
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