STC ST10936SC

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Project Number ST8934SC-T JM

Part 25 of the Federal Aviation Regulations.

Description of Type Design Change: Installation of an Executive Interior in accordance with Gore Design Completions (GDC), Ltd., Certification Drawing List (CDL), 459-SC-03, Revision M, released March 6, 2009, or later FAA approved revision. The aircraft is to be maintained per the “Instructions for Continued Airworthiness”, GDC Document Number 459-TP-05, Revision B, released March 5, 2009, or later FAA accepted revision. Airplane Flight Manual Supplement (AFMS) titled “Airplane Flight Manual Supplement for Airbus A340-313with Executive Interior”, Document Number 456-TP-49, Revision IR, issued March 09, 2009, or later FAA approved revision is required.

Limitations and Conditions: The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Gore Design Completions, Ltd.

607 North Frank Luke Drive San Antonio, TX 78226 A43NM Make : Airbus Model : A340 Model -313 Date of application : June 06, 2008

Date of issuance : March 10, 2009

( Signature) S. Frances Cox, Manager Special Certification Office Southwest Region

( Title)

FAA Form 8110-2-1(10-69) Page 2 of 3

FAA Form 8110-2-1(10-69) Page 3 of 3

Number ST10936SC Date of Issuance: March 10, 2009

Parts identified in GDC document number 459-SD-71, titled “Interior Modification Parts Listing – Approved for S/N 528 Only” are not included as part of the multiple STC and can not be used to permit manufacturing of parts for multiple installations.

Maximum seating for this aircraft (other than the pilot and co-pilot) is 12 crew (flight attendants) and 110 passengers.

Other than the pilot and co-pilot, 8 flight attendants are required on board the aircraft for compliance with this STC.

One flight attendant must be sitting at each emergency exit for taxi, takeoff, and landing. This aircraft is not to be operated for hire or offered for common carriage.

This modification may not be installed after June 7, 2010 unless (1) previously approved Electrical Wiring Interconnection System (EWIS) Instruction for Continued Airworthiness (ICA) have been evaluated and determined to be adequate for this installation by the FAA, or (2) revised EWIS ICCA have been approved by the FAA Oversight Office. (Refer to §26.11)

Certification Basis: All regulations at the amendment levels identified in Type Certificate Data Sheet (TCDS) A16WE except for the following regulation that have been complied with at a higher amendment level:

o 25.820 amendment 114 o 25.856 amendment 111 o 25.981 amendment 102 o 25.1316 amendment 80 o 25.1423 amendment 115 o 25.1431 amendment 113

This STC incorporate compliance to the following regulation by exemption 9822:

14 CFR 25.562(c)(5) 14 CFR 25.785(d) 14 CFR 25.785(h)(1) 14CFR25.813(e) 14 CFR 25.853(a-1)