DEFSTAN 80-221/1(2009) : 2009
Current
The latest, up-to-date edition.
PAINT REMOVER FOR AIR DRYING PAINT SCHEME FOR AEROSPACE PURPOSES - TYPE 1: HIGH VISCOSITY (BRUSHING) - TYPE 2: LOW VISCOSITY (SPRAYING)
Hardcopy , PDF
English
01-16-2009
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Foreword
0 Introduction
1 Scope
2 Warning
3 Normative References
4 Description
5 Information to be Supplied by the Purchaser
6 Keeping Qualities
7 Quality Assurance
8 Product Conformity Certification
9 Containers and Marking of Containers
10 Composition
11 Testing
Annex A - Determination of Viscosity
Annex B - Determination of Rate of Evaporation
Annex C - Determination of Freedom from Corrosive Action
Annex D - Determination of Paint Removing Power
Annex E - Determination of Water Rinsability
Annex F - Determination of Stress Corrosion Cracking
Annex G - Determination of Resistance to Hydrogen
Embrittlement
Describes the requirements for the performance of a paint remover for use in the removal of the more resistant paint coatings such as polyurethanes from the metallic surfaces of aircraft and electronic equipment.
| DocumentType |
Standard
|
| Pages |
18
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Current
|
| BS EN ISO 1514:2004 | Paints and varnishes. Standard panels for testing |
| BS EN ISO 1513:1995 | Paints and varnishes. Examination and preparation of samples for testing |
| BS EN ISO 3696:1995 | Water for analytical laboratory use. Specification and test methods |
| BS 2X 34:1998 | Specification for two component polyurethane finish for aerospace purposes |
| BS EN 23270:1991 | Specification for temperatures and humidities for conditioning and testing paints, varnishes and their raw materials |
| BS EN ISO 7539-5:1995 | Corrosion of metals and alloys. Stress corrosion testing Method for the preparation and use of C-ring specimens |
| BS EN 2832:1993 | Hydrogen embrittlement of steels. Notched specimen test |
| BS 2L 97:1971 | Specification for plate of aluminium-copper-magnesium-manganese alloy (solution treated, controlled stretched and aged at room temperature) (Cu 4.4, Mg 1.5, Mn 0.6) |
| BS EN 10130:2006 | Cold rolled low carbon steel flat products for cold forming. Technical delivery conditions |
| BS ISO 3116:2007 | Magnesium and magnesium alloys. Wrought magnesium alloys |
| BS EN 1652:1998 | Copper and copper alloys. Plate, sheet, strip and circles for general purposes |
| BS EN 2395:2005 | Aerospace series. Aluminium alloy AL-P2014A-T4 or T42. Sheet and strip. 0,4 mm ≤a ≤6 mm |
| BS L 168:1978 | Specification for bars and extruded sections of aluminium-copper-magnesium-silicon-manganese alloy (solution treated and artificially aged) (not exceeding 200 mm diameter or minor sectional dimension) (Cu 4.4, Mg 0.5, Si 0.7, Mn 0.8) |
| BS EN ISO/IEC 17050-1:2010 | Conformity assessment. Suppliers declaration of conformity General requirements |
| BS EN 2334:1997 | Chromic-sulphuric acid pickle of aluminium and aluminium alloys |
| BS 2X 33:1998 | Specification for two component epoxy primer for aerospace purposes |
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