Michael Bruce Donahue

Document ID: FAA-2010-0223-0002
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: March 15 2010, at 12:00 AM Eastern Daylight Time
Date Posted: March 16 2010, at 12:00 AM Eastern Standard Time
Comment Start Date: March 15 2010, at 12:00 AM Eastern Standard Time
Comment Due Date: April 29 2010, at 11:59 PM Eastern Standard Time
Tracking Number: 80abde85
View Document:  View as format xml

View Comment

There are issues with paragraph (g) of the propsed rule. Paragraph (g)(1) states to remove the ramp from the door per the Bombardier Modsum. Paragraph (g)(3) states again to remove the ramp, but adds the addition of corrosion inhibiter. This can cause confusion. I recommend removing the requirement in parapraph (g)(3) and have that paragraph only address the addition of the corrosion inhibiter. Suggested wording: (3) Apply corrosion inhibitor compound, in accordance with the applicable Bombardier modification summary package specified in Table 1 of this AD. Applying corrosion inhibitor compound is a terminating action for the requirements of this AD. Mike Donahue Mesaba Airlines Chief Engineer 612-794-9418 Office 612-940-2301 Cell

Related Comments

   
Total: 4
Michael Bruce Donahue
Public Submission    Posted: 03/16/2010     ID: FAA-2010-0223-0002

Apr 29,2010 11:59 PM ET
American Eagle Airlines
Public Submission    Posted: 04/30/2010     ID: FAA-2010-0223-0005

Apr 29,2010 11:59 PM ET
American Eagle Airlines
Public Submission    Posted: 04/30/2010     ID: FAA-2010-0223-0006

Apr 29,2010 11:59 PM ET
Air Wisconsin Airlines Corp
Public Submission    Posted: 04/20/2010     ID: FAA-2010-0223-0004

Apr 29,2010 11:59 PM ET