CTHIn ForceLegislation
AD/BO 105/24 - Main Rotor Pitch Link Rod Ends
Eurocopter BO 105 Series HelicoptersEurocopter BO 105 Series Helicopters
Start here
Get a plain-English read of Eurocopter BO 105 Series Helicopters
Turn the raw legal text into a practical explanation grounded in AD/BO 105/24 - Main Rotor Pitch Link Rod Ends.
Eurocopter BO 105 Series Helicopters
| AD/BO 105/24 | Main Rotor Pitch Link Rod Ends | 10/2007 |
|---|
| Applicability: | All Messerschmitt-Bolkow Blohm (MBB) Model BO 105 helicopters. |
|---|---|
| Requirement: | Action in accordance with the requirements of Transport Canada AD CF-88-07R2.Note: MBB Alert Service Bulletins BO 105LS-10-103 and BO 105-10-103 refer. |
| Compliance: | As specified in the Requirement document, with a revised effective date of27 September 2007. |
| This Airworthiness Directive becomes effective on 27 September 2007. | |
| Background: | Fatigue cracks have been found in the main rotor pitch link rod-ends. Failure of a rod-end could result in loss of control of the helicopter. |
Image unavailable in extracted text
David Villiers
Delegate of the Civil Aviation Safety Authority
13 August 2007