Proposed Special Condition on CS25.901(c) at Amdt 11 - Fan blade loss - effects at aircraft level - Applicable to Airbus A-320 Neo (equipped with CFN LEAP-1A engines)

28 Jul 2015

Consultation closed

Consultation Type

Deadline for comments

18/08/2015

Applicable to Manufacturers

Affected Primary Technical Domain

[pdf]

EASA Project Certification Manager

Phone

+49 221 89990 4148

E-mail

alexandre.peytouraux [at] easa.europa.eu

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