What it approves
Installation of an Executive Interior
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 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), 493-SD-03, Revision S, released January 14, 2010, or later FAA approved revision. The aircraft is to be maintained per the Instructions for Continued Airworthiness GDC Document Number 493-TP-05, Revision D, released January 14, 2010, or later FAA accepted revision. Use of Airplane Flight Manual Supplement, for Boeing 737-800 with Executive Interior, GDC Document Number 493-TP-49, Revision IR, issued January 14, 2010, or later FAA 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 737-8GQ Serial No. 35792. 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 Make: The Boeing Company Model: 737-8GQ Serial No. 35792 Date of application: June 26, 2008
Date of issuance: January 15, 2010
( 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 ST10967SC Date of Issuance: January 15, 2010
Limitations and Conditions (Continued): Maximum seating for this aircraft (other than the pilot and co-pilot) is 27 passengers and 3 crew (1 in the cockpit jump seat and 2 in the flight attendant seats). Other than the pilot and co-pilot, one (1) flight attendant is required on board the aircraft for compliance with this STC. This aircraft is not to be operated for hire nor offered for common carriage.
This modification may not be installed after June 7, 2010 unless (1) previously approved Electrical Wiring Interconnection System (EWIS) instructions for continued airworthiness (ICA) have been evaluated and determined to be adequate for this installation by the FAA, or (2) revised EWIS ICA have been approved by the Federal Aviation Administration 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 regulations have been complied with at a high amendment level:
o 25.820 amendment 114
o 25.899 amendment 123
o 25.981 amendment 102
o 25.1360 amendment 123
o 25.1365 amendment 123
o 25.1423 amendment 115
o 25.1431 amendment 113
This STC incorporates compliance to the following regulations by exemption 9794:
14 CFR 25.785(h)(2)
14 CFR 25.785(j)
14 CFR 25.813(e)
14 CFR 25.853(d)
--END--
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| The Boeing Company | 737-800 Series | A16WE |