BS EN 2290-1:1998
Current
Date published:
Rod bodies, flight control in aluminium alloy, for adjustable end fittings, Dimensions and loads
| Get this standard | Prices exclude GST | |
|---|---|---|
| PDF ( Single user document) |
$257.39 NZD
|
|
| PDF ( Single user document) |
$0.00 NZD
|
|
| HardCopy |
$293.04 NZD
|
|
Related Information
49.035 Components for aerospace construction
Similar Standards
-
BS 2F 67:1980
Specification for hose for aviation fuel and engine lubricating oil for aeronautical purposes
-
BS 2HR 402:2011
Specification for nickel-chromium-cobalt-titanium-aluminium heat-resisting alloy seamless tubes (Nickel base, Cr 19.5, Co 18.0, Ti 2.5, Al 1.5)
-
BS 2HR 403:2011
Specification for nickel-chromium-titanium heat-resisting alloy seamless tubes (Nickel base, Cr 19.5, Ti 0.4)
-
BS 2HR 404:2011
Specification for nickel-cobalt-chromium-molybdenum- titanium-aluminium heat-resisting alloy seamless tubes (Nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)
BS EN 2290-1:1998
Get this standard
Prices exclude GST
PDF
( Single user document)
$257.39 NZD
PDF
( Single user document)
$0.00 NZD
HardCopy
$293.04 NZD