Airworthiness Directives; Eurocopter Deutschland GmbH (ECD) Helicopters
airworthiness · Rule · Final rule. · Published 2013-11-08 · Effective 2013-12-13 · 78 FR 67020
Document
Document number
2013-26562
Federal Register citation
78 FR 67020
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Eurocopter Deutschland GmbH (ECD)
Publication date
2013-11-08
Effective date
2013-12-13
FAA docket
Docket No. FAA-2013-0519
Abstract
We are adopting a new airworthiness directive (AD) for ECD Model BO105C (C-2 and CB-2 Variants) and BO105S (CS-2 and CBS-2 Variants) helicopters with a certain third stage turbine wheel installed. This AD requires installing a placard on the instrument panel and revising the limitations section of the rotorcraft flight manual (RFM). This AD is prompted by several incidents of third stage engine turbine wheel failures, which were caused by excessive vibrations at certain engine speeds during steady-state operations. These actions are intended to alert pilots to avoid certain engine speeds during steady-state operations, prevent failure of the third stage engine turbine, engine power loss, and subsequent loss of control of the helicopter.