Proposed Deviation on Thrust Reverser inner wall structure - Applicable to Boeing 777 aircraft, (powered with Rolls Royce engines).

Starting date of initial consultation

20 May 2010

Comments are invited on this Deviation and should be sent by mail or electronic mail (preferred means), before the 20^th of May 2010, to:

Consultation / Publication type

Consultation status

Consultation closed

Affected primary technical domain

Validity

Not superseded

Closing date of consultation

20/05/2010

[pdf]

EASA Project Certification Manager (PCM) — Continuing Airworthiness Large Aeroplanes

CT.1 — Large Aeroplanes Department

Phone

+49 221 89990 4148

E-mail

Alexandre.Peytouraux [at] easa.europa.eu

Stay informed when this page is updated, or when we publish new content like this. You can always unsubscribe or update these settings later on.