91/83289 DC : DRAFT DEC 1991
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
PREN 3624 - AEROSPACE SERIES - POLYSULPHIDE SEALANTS, TWO-COMPONENT - TECHNICAL SPECIFICATION
Published date
23-11-2012
Publisher
Withdrawn date
23-07-2013
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| Committee |
ACE/65/-/25
|
| DocumentType |
Draft
|
| PublisherName |
British Standards Institution
|
| Status |
Withdrawn
|
| Standards | Relationship |
| PREN 3624 : 200P1 | Identical |
| MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| MIL-C-27725 Revision B:1969 | Coating, Corrosion Preventive, for Aircraft Integral Fuel Tanks (S/S by SAE-AMS-C-27725) |
| DIN EN 2133:2011-05 | Aerospace series - Cadmium plating of steels with specified tensile strength <kleiner |
| EN 3456:2012 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled — a ≤ 6 mm |
| DIN EN 2120:1980-11 (Draft) | AEROSPACE; STEEL FE-PA 12, SOFTENED AND COLD DRAWN, BARS AND WIRES 0,25 MM = D = 2,5 MM |
| DIN EN 2212:1980-11 (Draft) | Aerospace; steel FE-PL 43 S, 670 MPa <kleiner |
| EN 2437:2001 | Aerospace series - Chromate conversion coatings (yellow) for aluminium and aluminium alloys |
| DIN EN 3042:1992-02 | 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 3102:2013 | Aerospace series - Sealants - Test methods - Determination of low-temperature flexibility |
| EN 4120:2004 | Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated on thread - Classification: 1 210 MPa (at ambient temperature) / 730 °C |
| EN 2589:2017 | Aerospace series - Steel - Sheet and strip, cold rolled - Thickness 0,1 mm ≤ a ≤ 3 mm - Dimensions |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| 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 |
| EN 2590:2017 | Aerospace series - Steel - Sheets and plates, hot rolled - 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 |
| EN 3094:2017 | Aerospace series - Sealants - Test method - Determination of the application time |
| ISO 2781:2008 | Rubber, vulcanized or thermoplastic — Determination of density |
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