What it approves
Installation of a cocoon wall panel system.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Part 29 of the Federal Aviation Regulations.
Configuration 1: Applies to models SA365N, SA365N1 and AS365N2 only. Installation of a cocoon wall panel system in accordance with Advanced Flight Systems, Inc.
Installation Drawing List Report No. 8316-02, dated September 15, 1996.
1. Configuration 1: Aerospatiale Sliding L/H Door P/N 365A82.1142.0051 or P/N 365A82.1142.0053 and sliding R/H Door P/N 365A82.1142.0151 and P/N 365A82.1142.0153 is required for this modification.
Texas Aviation Services 3901 North Main Street Fort Worth, TX 76106 H10EU Make : Eurocopter France Model : SA-365N; SA-365N1; AS-365N2; EC155B; EC155B1
Date of application : August 12, 1996
Date of issuance : December 03, 1996
Date reissued : 1/28/03; 12/27/07
Date amended : 11/15/01;
4/26/05;12/12/08
( Signature) Lance T. Gant, Manager Rotorcraft Certification Office, Southwest Region
( Title) PE: MC SA3017RC-R ASW-170
FAA Form 8110-2-1(10-69) Page 2 of 3
FAA Form 8110-2-1(10-69) Page 3 of 3
Number SR00530NY Date of Issuance: December 03, 1996 Date Amended: December 12, 2008
Description of Type Design Change (Continued):
Configuration 2: Applies to models EC155B and EC155B1 only. Installation of a cocoon wall panel system in accordance with Advanced Flight Systems Inc. Installation Drawing List Report No. 913-030-001, Original revision, dated June 15, 2001.
Configuration 3: Applies to models EC155B and EC155B1 only. Installation of a cocoon wall panel system in accordance with Texas Aviation Services Installation Drawing List Report No. TAS-SR00530NY-IDL, Revision B, dated 12/11/08 (or later FAA Approved Revision). Parts to be manufactured in accordance with Texas Aviation Services Manufacturing Drawing List Report No. TAS-SR00530NY-MDL, Revision B, dated 12/11/08 (or later FAA Approved Revision).
2. Configuration 3: Eurocopter Factory installed L/H and R/H VIP Swing Doors are required for this modification.
3. Configuration 1: Advanced Flight System, Inc. Continued Airworthiness Maintenance Manual Report No. 8316-03, dated October 1, 1996.
Configuration 2: Advanced Flight System, Inc. Continued Airworthiness Maintenance Manual Document No. 913-060-001, Original revision, dated August 1, 2001.
Configuration 3: Advanced Flight System, Inc. Continued Airworthiness Maintenance Manual Document No. 913-060-001, Original revision, dated August 1, 2001.
4. The installer must determine whether this design change is compatible with previously approved modifications.
5. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.