HELITALIA SpA

Document ID: FAA-2008-0490-0002
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: May 09 2008, at 11:07 AM Eastern Daylight Time
Date Posted: May 28 2008, at 12:00 AM Eastern Standard Time
Comment Start Date: May 28 2008, at 12:00 AM Eastern Standard Time
Comment Due Date: June 7 2008, at 11:59 PM Eastern Standard Time
Tracking Number: 80603569
View Document:

This is comment on Rule

Airworthiness Directives: Bell Helicopter Textron Model 204B, 205A, 205A-1, 205B, 210, 212, 412, 412CF, and 412EP Helicopters

View Comment

With reference to the Airworthiness Directive No. 2008-10-03, regarding Bell 412, we have the following questions: 1) if, during the accomplishment of paragraph (b), we find any damage (within the maximum repair limits) on tail rotor blades, what is the required corrective action? 2) Is it required to accomplish paragraph (c) together with paragraph (b), every 25 hours/30 days? 3) Is paragraph (c) a "not-repetitive" task? or is it required to accomplish it before each flight, during preflight inspection? Best Regards Luca Fioretti Helitalia SpA - Technical department

Related Comments

Total: 3

HELITALIA SpA
Public Submission Posted: 05/28/2008 ID: FAA-2008-0490-0002

Comment Period Closed
Jun 07,2008 11:59 PM ET

Australian Helicopters
Public Submission Posted: 05/28/2008 ID: FAA-2008-0490-0003

Comment Period Closed
Jun 07,2008 11:59 PM ET

Robert Fisher
Public Submission Posted: 06/09/2008 ID: FAA-2008-0490-0008

Comment Period Closed
Jun 07,2008 11:59 PM ET