STC ST11098SC

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), 494-SD-03, Revision P, released September 13, 2012, or later ODA approved revision. The aircraft is to be maintained per the Instructions for Continued Airworthiness GDC Document Number 494-TP-05, Revision B, released May 30, 2012, or later FAA accepted revision. Use of Airplane Flight Manual Supplement, for Boeing 737-9LBER with Executive Interior, GDC Document Number 494-TP-49, Revision IR, issued September 21, 2012, or later ODA approved revision is required.

Limitations and Conditions: You cannot use descriptive data about this design change to duplicate other products.

This approval is limited to only the installation made in Boeing Model 737-9LBER Serial No. 38890. This STC does not permit manufacturing of parts for multiple installations.

Gore Design Completions, Ltd.

607 North Frank Luke Drive San Antonio, TX 78226 A16WE Model: BOEING 737-9LBER, Serial Number 38890 Make:

Date of application: March 26, 2010

Date of issuance: September 21, 2012 Date reissued:

( Signature) Steven D. Kincaid ODA Administrator Gore Design Completions, Ltd.

(Titl )

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor ( In ink):

Maximum seating for this aircraft, other than the pilot and co-pilot, is 2 cabin crew and 33 passengers. Other than the pilot and co-pilot, 2 flight attendants are required on board the aircraft for compliance with this STC. One flight attendant must be sitting at the forward L/H entry door for taxi, takeoff, and landing. This aircraft is not to be operated for hire nor offered for common carriage.

Certification Basis:

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

o 14 CFR 25.820 amendment 114 o 14 CFR 25.853 amendment 116 o 14 CFR 25.856 amendment 111 o 14 CFR 25.981 amendment 102 o 14 CFR 25.1360 amendment 123 o 14 CFR 25.1365 amendment 123 o 14 CFR 25.1423 amendment 115 o 14 CFR 25.1431 amendment 113

This STC incorporates compliance to the following regulations by 14 CFR Part 25, Special Federal Aviation Regulations (SFAR) 109:

o 14 CFR 25.785 (j) o 14 CFR 25.785 (h)(2) o 14 CFR 25.791 (a) o 14 CFR 25.807 (d)(7) o 14 CFR 25.811 (d)(1)(2) o 14 CFR 25.812 (e)(1) o 14 CFR 25.813 (e) o 14 CFR 25.815 o 14 CFR 25.851 o 14 CFR 25.853 (d) o 14 CFR 25.858 (a)

SFAR 109 section 4(b) does not apply to this airplane since 14 CFR 25.562(c)(5)(6) is not part of the certification basis for this airplane.

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