Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
GM to 21.A.611 Design changes
Available versions for ERULES-1963177438-3968
ED Decision 2012/020/R
found in: Initial Airworthiness and Environmental Protection (748/2012) Part-21 Part-21L (Jul 2024)
From
Initial Airworthin... (Nov 2025)
Initial Airworthin... (Jul 2024)
From section
To
Initial Airworthin... (Nov 2025)
Initial Airworthin... (Jul 2024)
To section
No visible text changes
0 removals
0 additions
View
Rich
Plain
Sync scrolling
Share
From
Show details
Hide details
To
Show details
Hide details
Version
Show side by side
GM to 21.A.611 Design changes ED Decision 2012/020/R A change to an ETSO article can either be seen: — under this [21.A.611](#_DxCrossRefBm1649097039) in the context of an ETSO authorisation, i.e., when an article as such is specifically approved under Subpart O, with dedicated rules that give specific rights and obligations to the designer of the article, irrespective of any product type design or change to the type design. For a change to such an article, irrespective of installation on any aircraft, Subpart O, and this [21.A.611](#_DxCrossRefBm1649097039) in particular, should be followed; or — when an airline or a maintenance organisation is designing a change (based on data not published in the TC holder or Original Equipment Manufacturer documentation) on an article installed on an aircraft, such a change can be considered as a change to the product in which the article is installed, not to the article taken in isolation. Therefore Subpart D can be used for the approval of this change that will be identified as ‘change to product x affecting article y’, but not ‘change to article y’.
##### GM to 21.A.611 Design changes *ED Decision 2012/020/R* A change to an ETSO article can either be seen: — under this [21.A.611](#_DxCrossRefBm485230530) in the context of an ETSO authorisation, i.e., when an article as such is specifically approved under Subpart O, with dedicated rules that give specific rights and obligations to the designer of the article, irrespective of any product type design or change to the type design. For a change to such an article, irrespective of installation on any aircraft, Subpart O, and this [21.A.611](#_DxCrossRefBm485230530) in particular, should be followed; or — when an airline or a maintenance organisation is designing a change (based on data not published in the TC holder or Original Equipment Manufacturer documentation) on an article installed on an aircraft, such a change can be considered as a change to the product in which the article is installed, not to the article taken in isolation. Therefore Subpart D can be used for the approval of this change that will be identified as ‘change to product x affecting article y’, but not ‘change to article y’.