EASA validation of FAA originally approved
STC SA02789CE "Installationof a
Bendix/King CAS-81 TCAS System".

Certification Basis
The Certification Basis for the original product
remains applicable tothis certificate/
approval.The requirements for environmental
protection and the associatedcertificated
noiseand/ or emissions levels of the original
product areunchanged and remain applicable
to this certificate/ approval.

Limitations
See original FAA approved STC SA02789CE
documents:-,,Jet Aviation Certification
Drawing List No. AD910011, Revision Fdated
March 11th, 2011 and-,,Jet Aviation Report
No 13-328M001, Revision F, FAA Flight
ManualSupplement dated May 13th, 2011
and-,,I (...)

Conditions
Aeroplanes modified in accordance with this
STC must be maintained inaccordance with
Approved Instructions for Continued
Airworthiness, JetAviation Report No. 13-
027E054, SectionO - Airworthiness
Limitations,Revision NC dated June 03rd
2011 or late (...)

Please contact modification supplier for further details.

STC Status: Revision Level:
STC Date: 06/12/12
Responsible Office: EASA