EN 2243-4:2005
Current
Current
The latest, up-to-date edition.
Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 4: Metal-honeycomb core flatwise tensile test
Published date
26-10-2005
Publisher
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Foreword
Introduction
1 Scope
2 Normative references
3 Definitions, symbols and
abbreviations
4 Health and safety
5 Principle/Technique
6 Resources
7 Test samples/Test pieces
8 Testing procedure
9 Expression of results
10 Designation
11 Test report
This standard defines the general requirements for the determination of strength of structural adhesives by testing in tension metal to honeycomb core joints, at ambient or other temperatures.Two types of test pieces are defined:Type A: direct bonding of honeycomb to facing blocks;Type B: bonding of honeycomb between the two facing sheets, then bonding of the whole to the facing blocks.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 2243-4. (01/2006) Supersedes UNE EN 2243-4:1993. (08/2006)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| NF EN 2243-4 : A2006 | Identical |
| I.S. EN 2243-4:2005 | Identical |
| SNV DIN EN 2243-4 : 1991 | Identical |
| NBN EN 2243-4 : 2006 | Identical |
| SN EN 2243-4 : 2006 | Identical |
| PN EN 2243-4 : 2006 | Identical |
| UNI EN 2243-4 : 2007 | Identical |
| NS EN 2243-4 : 2ED 2006 | Identical |
| UNE-EN 2243-4:2006 | Identical |
| BS EN 2243-4:2005 | Identical |
| NEN EN 2243-4 : 2005 | Identical |
| DIN EN 2243-4:2006-10 | Identical |
| UNE-EN 2243-4:2005 | Identical |
| 93/706616 DC : 0 | PREN 2833-1 - AEROSPACE SERIES - TECHNICAL SPECIFICATION - GLASS FIBER THERMOSETTING PREIMPREGNATES - PART 1: GENERAL |
| PREN 2642 : 200P1 | AEROSPACE SERIES - STRUCTURAL ADHESIVE SYSTEMS - ADHESIVE FILM - TECHNICAL SPECIFICATION |
| 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 |
| 99/701511 DC : DRAFT JAN 1999 | PREN 4106 - AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION |
| PREN 2833-1 : 200P2 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS |
| 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) |
| 97/708408 DC : DRAFT APR 1997 | PREN 7000-9 - AEROSPACE - NON-METALLIC MATERIALS - RULES FOR THE DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 9: PAINTS AND VARNISHES |
| 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 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 3487 : 200P2 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - BAR FOR MACHINING - A OR D <= 250 MM - 500 MPA <= R[M] <= 700 MPA |
| PREN 4385 : 200P2 | AEROSPACE SERIES - NON-METALLIC MATERIALS - GENERAL ORGANISATION OF STANDARDISATION - LINKS BETWEEN TYPES OF STANDARDS |
| PREN 2419 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024-T351 - PLATE - 6 MM < A <= 80 MM |
| ISO 7500-1:2015 | Metallic materials Calibration and verification of static uniaxial testing machines Part 1: Tension/compression testing machines Calibration and verification of the force-measuring system |
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