Installation of Kannad 406 AF ELT

Certification Basis


Limitations
-Engineering Order 2022014 - EO - 02.-AFM
Supplement, Doc. No 2022014 - AM - 02.-
Continued Airworthiness Report Doc.
No2022014 - CA - 02.

Conditions
1. This STC is approved only for the product
configuration as defined in the approved
design data referred to in the paragraph
Description". Compatibility with other
aircraft/engine configurations shall be
determined by the installer.

Please contact modification supplier for further details.

STC Status: Revision Level: REV. 1
STC Date: 07/04/05
Responsible Office: EASA