Cabin Modification to VIP
Overview
Introduction
Cabin Modification to VIP
Certification Basis
The Certification Basis for the original product as amended by the following additional or alternative airworthiness requirements:- the following paragraph(s) at a later amendment:CS 25.1701 to CS 25.1729 at Amendment 11.
Your needs
Declaration of Compliance, Doc. No. DC- 10D003Z0001, Issue B dated20.03.2013;
Master Document List, Doc. No. MDL003Z0001, Issue A dated 19.03.2013;
Instructions for Continued Airworthiness, Doc. No. ICA010D259Z0001, Issue A dated 19.03.2013;
AFM Supplement (...)
Your benefits
Conditions
Aircraft Serial Number 7617 only. Prior to installation of this design change it must be determined that the interrelationship between this design change and any other previously installed design change and/or repair will introduce no adverse effect upon the airworthiness of the product.
Product Description
Cabin Modification to VIP.
Certification Basis
The Certification Basis for the original product
as amendedby thefollowing additional or
alternative airworthiness requirements:- the
following paragraph(s) at a later
amendment:CS 25.1701 to CS 25.1729 at
Amendment 11.The requirements for
environme (...)
Limitations
Declaration of Compliance, Doc. No. DC-
10D003Z0001, Issue
Bdated20.03.2013;Master Document List,
Doc. No. MDL003Z0001,Issue A dated
19.03.2013;Instructions for Continued
Airworthiness, Doc. No.
ICA010D259Z0001,Issue A dated
19.03.2013;AFM Supplement (...)
Conditions
Aircraft Serial Number 7617 only.Prior to
installation of this design change it must be
determined thatthe interrelationship between
this design change and any otherpreviously
installed design change and/ or repair will
introduce noadverseeffect upon the
airworthiness of the product.
Please contact modification supplier for further details.
STC Status: Revision Level:
STC Date: 20/03/13
Responsible Office: EASA
Your benefits
Conditions
Aircraft Serial Number 7617 only. Prior to installation of this design change it must be determined that the interrelationship between this design change and any other previously installed design change and/or repair will introduce no adverse effect upon the airworthiness of the product.