Per TC-Holder design, the DHC-8 engine nacelles are secured with several latches.
Two of the latches (one on each side) are protected with corresponding covers. These covers tend to get damaged during operation and are replaced with new ones made of stainless steel in this modification.
To request development and/or EASA approval of a modification or repair, please contact us.
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EASA Design Organisation approval
Certified design
MAP 21 achieved an EASA Part 21 Subpart J Design Organisation Approval in 2007, EASA.21J.326, which enables us to approve modifications to the aviation industry as a delegated EASA authority.
