• There are no items in your cart

DEFSTAN 80-221/1(2009) : 2009

Current

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)

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

16-01-2009

Free

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

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.