# STC ST10831SC - Type: Supplemental type certificate - Status: Current, Amended - Holder: Gore Design Completions Ltd - Description: Installation of an Executive Interior. - Status date: January 29, 2014 - Data sheets: A28NM - Certificate PDF: https://openairdocs.org/files/sha256/f0/1b/f01b85d9fa01505ecd2ce2fe201693e1de1c68421474a0dd57ac330237bbf326 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B297D4A30E6B3AB686257C770071EC07.0001 - Page: https://openairdocs.org/stc/ST10831SC ## ADs that name it None. ## Approved models (1) - Airbus A320-214 (TCDS A28NM) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. Number ST10831SC Part 25 of the Federal Aviation Regulations. Original Product – Type Certificate Number: A28NM Make: Airbus Model: A320 Model -214 Description of Type Design Change: Installation of Executive Interior (See continuation sheet 2 of 3) The installer must determine whether this design change is compatible with the previously approved modifications. (See continuation sheet 2 of 3) Date of application: December 19, 2006 Date reissued: Date of issuance: May 23, 2008 Date amended: December 22, 2008; March 6, 2009; January 29, 2014 Signature S. Frances Cox Manager, Special Certification Office, Title Southwest Region FAA Form 8110-2 (8/13) Page 1 Gore Design Completions, Ltd. 607 N. Frank Luke Drive San Antonio, TX 78226 **SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)** To (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP Code) From (Name of grantor) (Address of grantor) (Number and street) (City, State, and ZIP Code) FAA Form 8110-2 (8/13) Page 2 Number: ST10831SC Date of Issuance: May 23, 2008 Date Amended: December 22, 2008; March 6, 2009; January 29, 2014 Description of Type Design Change (Continued): Installation of Executive Interior in accordance with Gore Design Completions (GDC), Ltd., Certification Drawing List, GCD-429-03, Revision K, released September 3, 2008, or later FAA approved revision and certified in accordance with GDC Substantiation Report List, GCD-429-04, Revision C, released January 27, 2014. The aircraft is to be maintained per the “Instructions for Continued Airworthiness, Airbus A320-214 Interior Installation:, GDC Document Number GCD- 429-05, Revision G, released June 25, 2010, or later FAA accepted revision. Airplane Flight Manual Supplement (AFMS) titled “Airplane Flight manual Supplement for Airbus A320-214 with Executive Interior”, Document Number GFA-429-24, Revision A, dated December 22, 2008, or later FAA approved revision is required. 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. Parts identified in GDC document number GMT-429-70, titled “Interior Modification Parts Listing-Approved for S/N 3199 Only”, Revision A, released May 9, 2008, are not included as part of multiple STC ST10831SC and are not permitted to be reproduced or manufactured for multiple installations. Maximum seating for this aircraft (other than the pilot and co-pilot) is 8 crew (2 in the cockpit jump seats, 4 in the flight attendants seats, 1 in the hallway guard seat and 1 in the communication station seat) and 40 passengers. Other than the pilot and co-pilot, a minimum of two flight attendants are required to be on board the aircraft for compliance with this STC – one must be sitting in the forward flight attendant seat and one in the aft flight attendant seat. This aircraft is not to be operating for hire or offered for common carriage. Certification Basis: a. All regulations at the amendment levels identified in Type Certificate data Sheet (TCDS) A28NM except for the following regulations that have been complied with at a higher amendment level: 14 CFR 25.854, Amendment 74 14 CFR 25.869, Amendment 113 14 CFR 25.981, Amendment 102 14 CFR 25.1316, Amendment 80 14 CFR 25.1423, Amendment 115 14 CFR 25.1431, Amendment 113 b. This STC incorporates compliance to the following regulations by FAA Exemption 9514: 14 CFR 25.785 (h)(1), Amendment 25-51 14 CFR 25.813 (e), Amendment 25-46 c. 14 CFR 26.11 (c), Amendment 26-0 - END - FAA Form 8110-2 (8/13) Page 3 ## Every issue (3) - January 29, 2014: Amended, Current. [certificate](https://openairdocs.org/files/sha256/f0/1b/f01b85d9fa01505ecd2ce2fe201693e1de1c68421474a0dd57ac330237bbf326) - March 6, 2009: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/66/06/6606577bcaadd8367eaed24e62f25811754b4e1b4934765390e842e110a8b9c7) - May 22, 2008: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/d4/03/d4031cf55d5de3f680175dbc09a904fa425c0d2c2011cf49d83045b1f1cc0fc1) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.