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EAD 2009-0172-E : Rotor Flight Controls – Flight Crew Pedal Position Adjustment System – Test / Modification

Number 2009-0172-E
Issued by Europe  Europe
Issue date 2009-08-05
Effective date 2009-08-07
EASA approval number
ATA Chapter 67
Approval Holder
/ Type Designation
  • AIRBUS HELICOPTERS
    • SA 330 / AS 332 / EC 225
      • SA 330 J
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Eurocopter SA 330 ASB N° 67.18 dated 03 August 2009. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. The safety assessment has requested not to implement the full consultation process and an immediate publication and notification. 3. Enquiries regarding this AD should be referred to the Airworthiness Directives, Safety Management & Research Section, Certification Directorate, EASA; E-mail: ADs@easa.europa.eu. 4. For any question concerning the technical content of the requirements in this AD, please contact: EUROCOPTER (STDI), Aéroport de Marseille Provence, 13725 Marignane Cedex, France Telephone: +33 (0) 4 42 85 97 97 - Fax +33 (0) 4 42 85 99 66 E-mail: Directive.technical-support@eurocopter.com

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