PREN 3624 : 200P1
Current
The latest, up-to-date edition.
AEROSPACE SERIES - POLYSULPHIDE SEALANTS, TWO-COMPONENT - TECHNICAL SPECIFICATION
Hardcopy , PDF
English
28-06-1996
1 Scope
2 References normative
3 Requirements
4 Definitions
5 Test fluids
6 Quality inspection
7 Identification marking and packaging
8 Storage
Annex A (normative) Acceptance test certificate for
polysulphide sealants (Example)
Technical specification for two-component polysulphide sealants used in the repair and sealing of integral and other non-flexible fuel tanks as well as pressurised cabins and other non-fuel tank areas.
| Committee |
C7
|
| DocumentType |
Draft
|
| Pages |
16
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Current
|
| Standards | Relationship |
| 91/83289 DC : DRAFT DEC 1991 | Identical |
| PREN 3101 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - SEALANTS - TEST METHOD - DETERMINATION OF RESISTANCE TO THERMAL RUPTURE |
| TR 7000-3 : 1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - RULES FOR THE DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 3: SEALANTS |
| EN 2497:1989 | Aerospace series - Dry abrasive blasting of titanium and titanium alloys |
| PREN 2599 : 200P2 | AEROSPACE SERIES - STRIP IN ALUMINIUM AND ALUMINIUM ALLOYS - THICKNESS 0,25 MM <= A <= 3,2 MM - DIMENSIONS |
| PREN 3456 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM |
| MIL-C-27725 Revision B:1969 | Coating, Corrosion Preventive, for Aircraft Integral Fuel Tanks (S/S by SAE-AMS-C-27725) |
| EN 2133:2010 | Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys |
| PREN 2590 : 200P1 | AEROSPACE SERIES - STEEL - SHEETS AND PLATES, HOT ROLLED - DIMENSIONS |
| EN 2437:2001 | Aerospace series - Chromate conversion coatings (yellow) for aluminium and aluminium alloys |
| PREN 3094 : 200P1 | AEROSPACE SERIES - SEALANTS - TEST METHOD - DETERMINATION OF APPLICATION TIME |
| ISO 2555:1989 | Plastics — Resins in the liquid state or as emulsions or dispersions — Determination of apparent viscosity by the Brookfield Test method |
| PREN 3096 : 200P1 | AEROSPACE SERIES - SEALANTS - TEST METHOD - DETERMINATION OF THE TACK-FREE TIME |
| EN 3042 : 1991 | AEROSPACE SERIES - QUALITY ASSURANCE - EN AEROSPACE PRODUCTS - QUALIFICATION PROCEDURE |
| EN 2338:2001 | Aerospace series - Sheets, hot rolled in titanium and titanium alloys - Thickness 0,8 mm < = a < = 6 mm - Dimensions |
| ISO 2768-2:1989 | GENERAL TOLERANCES - PART 2: GEOMETRICAL TOLERANCES FOR FEATURES WITHOUT INDIVIDUAL TOLERANCE INDICATIONS |
| EN 2101:1991 | Aerospace series - Chromic acid anodizing of aluminium and wrought aluminium alloys |
| EN 10204:2004 | Metallic products - Types of inspection documents |
| EN 3102:2013 | Aerospace series - Sealants - Test methods - Determination of low-temperature flexibility |
| ISO 37:2017 | Rubber, vulcanized or thermoplastic — Determination of tensile stress-strain properties |
| ISO 554:1976 | Standard atmospheres for conditioning and/or testing — Specifications |
| EN 2090:2005 | Aerospace series - Aluminium alloy AL-P2024-T3 - Clad sheet and strip 0,3 mm |
| PREN 2589 : 200P1 | AEROSPACE SERIES - STEEL - SHEET AND STRIP, COLD ROLLED - THICKNESS 0,1 MM <= A <= 3 MM - DIMENSIONS |
| ISO 868:2003 | Plastics and ebonite — Determination of indentation hardness by means of a durometer (Shore hardness) |
| ISO 1817:2015 | Rubber, vulcanized or thermoplastic — Determination of the effect of liquids |
| ISO 2781:2008 | Rubber, vulcanized or thermoplastic — Determination of density |
| PREN 3997 : 200P3 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P2024- AL CU4MG1 - T3 - SHEET AND STRIP - 0,4 MM <= A <= 6 MM |
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