BS 2X 26:2001
Current
The latest, up-to-date edition.
Doping and finishing schemes for fabric covered aircraft
Hardcopy , PDF
English
15-03-2001
Foreword
1 Scope
2 Normative references
3 Definitions
4 Materials
4.1 Description
4.2 Composition of the dope and finish schemes
5 Performances
5.1 General
5.2 Tests on dopes and finishes
6 Inspection
7 Marking
Annex A (normative) Preparation of test panels
Annex B (normative) Method for the determination of
tautness properties
Annex C (normative) Method of test for resistance to
high temperatures
Annex D (normative) Method of test for resistance to
natural weathering
Annex E (normative) Method of test for freedom from
film defects
Annex F (normative) Type approval
Figure F.1 Test frame for doped fabric
Table 1 General properties
Table 2 Tests on tautening dopes
Table 3 Tests on non-tautening finishes
Describes the requirements for doping schemes of low, medium and high tautness, together with matt and glossy finishes, for aerospace purposes. Also specifies methods of producing and maintaining on aircraft fabrics taut, water-proof and air-proof surfaces and also provides methods of protecting the fabrics from the deteriorative effects of light, weather and normal service conditions.
Committee |
ACE/65
|
DevelopmentNote |
Supersedes 99/701779 DC and BS X26(1966) (07/2005) Reviewed and confirmed by BSI, November 2012. (10/2012)
|
DocumentType |
Standard
|
Pages |
16
|
PublisherName |
British Standards Institution
|
Status |
Current
|
Supersedes |
This British Standard specifies the requirements for doping schemes of low, medium and high tautness, together with matt and glossy finishes, for aerospace purposes.
These schemes provide methods of producing and maintaining on aircraft fabrics taut, water-proof and air-proof surfaces and also provides methods of protecting the fabrics from the deteriorative effects of light, weather and normal service conditions.
Annex F gives details of requirements for type approval.
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BS L 163:1978 | Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated, cold worked for flattening and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8) |
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