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.
FAA Form 8110-2 (8/13) Page 1
Part of the Federal A viation Regulations.
Original Product – Type Certificate Number: MDNH:
MRGHO:
Signature
Title
ST10895SC-D Associated Air Center, Inc. - c/o CT Corporation System 1999 Bryan Street, Suite 900 Dallas, TX 75201 25 A28NM Airbus A319-115 Installation of an Executive Interior in accordance with Associated Air Center (AAC) "Master Document List" Document Number 2578000000, Revision C, dated May 10, 2012, or later FAA/ODA approved revision. Airplane Flight Manual Supplement (AFMS), Document Number 2578021090, Revision IR, dated September 21, 2009, or later FAA/ODA approved revision is required.
Descriptive data about this design change can not be used to duplicate other products. This approval is limited to only the installation made in Airbus Model Number A319-115, Serial Number 3133. This STC does not permit manufacturing of parts for multiple installations 3/4/2008 9/21/2009 12/11/2017 9/22/2010 5/10/2012 Jose Mora-Vargas ODA Administrator ODA-710437-SW
FAA Form 8110-2 (8/13) Page 2
To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):
ST10895SC-D
FAA Form 8110-2 (8/13) Page 3
ST10895SC-D Limitations and Conditions (Continued):
This aircraft is not to be operated for hire or offered for common carriage. Airworthiness limitation inspections per 14 CFR Part 25, Appendix H, are contained in Chapter 3 of the “Instructions for Continued Airworthiness”, AAC Document Number 2578050090, Revision G, dated May 7, 2012, or later FAA/ODA approved revision.
Note: The FAA has reviewed the applicant's assessment showing that this modification does not impact the existing Electrical Wiring Interconnection System Instructions for Continued Airworthiness (EWS ICA) and found that no additional EWIS ICA tasks are required. Refer to Report No. 2963052091 "EWIS ICA Evaluation", Revision IR, dated January 4, 2012, or later FAA/ODA approved revision.
Certification Basis: The same as that identified on Type Certificate Data Sheet A28NM except for the election of later amendments as listed: 14 CFR 25.321(c),(d) Amdt. 25-86; 25.561(a),(b)(1)(3),(c),(d) Amdt. 25-91; 25.562
(a),(b),(c)(1)(2)(3)(4)(7)(8) Amdt. 25-64; 25.625 Amdt. 25-72; 25.783(b),(e),(j) Amdt. 25-72; 25.810(c) Amdt.76;
25.812 Amdt. 25-58; 25.813(a),(b),(c),(d),(f) Amdt. 76; 25.853(a),(c) Amdt. 25-116; 25.854(a) Amdt. 25-74;
25.856(a) Amdt. 25-111; 25.981(a)(3),(b) Amdt. 25-102; 25.1301(a)(1)(2)(3) Amdt. 25-123; 25.1316(b),(c)(6) Amdt. 25-80. This STC incorporates the use of Exemption Number 7489.
STC Amendment dated May 10, 2012, (incorporation of ERDA Model 4402 side facing divan) election of later amendments as listed: 14 CFR 25.305 Amdt. 25-86; 25.307 Amdt. 25-72; 25.341 Amdt. 25-72.
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 |
|---|---|---|
| Airbus | A319-115 | A28NM |
Every issue · 4
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| December 11, 2017 | Reissued, current | Certificate |
| May 10, 2012 | Amended, earlier issue | Certificate |
| September 22, 2010 | Amended, earlier issue | Certificate |
| September 21, 2009 | Issued, earlier issue | Certificate |