About this document
EASA AD 2006-0216-E for ATR Aircraft by Kaung MyatToe is a document available to read on EtoBox.
This emergency airworthiness directive from EASA requires operators to inspect the locking bolt on the main landing gear shock absorber attachment pin within 15 days for all applicable ATR 42 and ATR 72 aircraft. The inspection is needed to check that the locking bolt is correctly installed after an incident where the pin migrated and ruptured due to the absence of the locking bolt. Operators must also refer to the Messier Dowty service bulletin for inspection instructions and corrective actions depending o
- Author
- Kaung MyatToe
- Language
- EN