Repair Design and Bilateral Acceptability
Repair Design and Bilateral Acceptability
In accordance with the bilateral arrangements all repair designs approved by the MTU Aero Engines AG Part-21 Design Organisation EASA.21J.248 or MTU Maintenance Hannover GmbH Part 21 Design Organisation EASA.21J.572 are acceptable to the following authorities without further approvals:
USA
FAA – Bilateral effective from 5 May 2011
Canada
TCCA – Bilateral effective from 20 September 2011