Manuel Najar

Document ID: FAA-2009-0379-0003
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: April 30 2009, at 04:53 PM Eastern Daylight Time
Date Posted: April 30 2009, at 12:00 AM Eastern Standard Time
Comment Start Date: April 29 2009, at 12:00 AM Eastern Standard Time
Comment Due Date: May 29 2009, at 11:59 PM Eastern Standard Time
Tracking Number: 8096fa5b
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This is comment on Rule

Airworthiness Directives: Airbus Model A318, A319, A320, and A321 Series Airplanes

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This AD adress all SA A/C, but only A320 airplane are affected: Current RAT SUNDSTRAND models (not concerned by this AD) is installed on A318, A319 and A321 through mod 22803, which is type design for all these models. No retrofit is possible. As such the applicability of the AD must be: AIRBUS A320-111, -211, -212, -214, -215, -231, -232 and -233 equipped with HAMILTON SUNDSTRAND (formerly DOWTY) Ram Air Turbine (RAT) Ejection Jack, Model ERPS13EJ, Part Number (P/N) 114160004A or 114160005. Aircraft having received AIRBUS modification 27189 in production or AIRBUS Service Bulletin (SB) A320-29-1100 in service, and without having received AIRBUS modification 28413 in production, are not affected by the requirements of this AD. EASA is proceeding with the revision of AD 2008-0199 accordingly. Best regards, Manuel NAJAR SA continued airworthiness (EAS - AIRBUS Central Entity) Phone : +33 (0)6 84 90 56 15 Fax : +33 (0)5 61 93 44 51 mailto : manuel.najar@airbus.com

Related Comments

Total: 2

Manuel Najar
Public Submission Posted: 04/30/2009 ID: FAA-2009-0379-0003

Comment Period Closed
May 29,2009 11:59 PM ET

Virgin America
Public Submission Posted: 05/12/2009 ID: FAA-2009-0379-0004

Comment Period Closed
May 29,2009 11:59 PM ET