Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
GM 21.A.708(d) Control of aircraft configuration
Available versions for ERULES-1963177438-3995
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 21.A.708(d) Control of aircraft configuration ED Decision 2012/020/R The applicant should establish a method for the control of any change or repair made to the aircraft, for changes and repairs that do not invalidate the conditions established for the permit to fly. All other changes should be approved in accordance with [21.A.713](#_DxCrossRefBm1649097475) and when necessary a new permit to fly should be issued in accordance with [21.A.711](#_DxCrossRefBm1649097268).
##### GM 21.A.708(d) Control of aircraft configuration *ED Decision 2012/020/R* The applicant should establish a method for the control of any change or repair made to the aircraft, for changes and repairs that do not invalidate the conditions established for the permit to fly. All other changes should be approved in accordance with [21.A.713](#_DxCrossRefBm485230968) and when necessary a new permit to fly should be issued in accordance with [21.A.711](#_DxCrossRefBm485230759).