Repair Design & 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:


FAA – Bilateral effective from 5 May 2011

Overview: Bilateral Agreements


TCCA – Bilateral effective from 20 September 2011

Overview: Bilateral Agreements

BASA EU US Product Certification (pdf)