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 8110-2-1(10-69) Page 1of 3
Number ST10898SC-D This Certificate issued to
Part 25 of the Federal Aviation Regulations.
Description of Type Design Change: Installation of an Executive Interior in accordance with Associated Air Center (AAC) "Master Document List" Document Number 2570000000, Revision B, dated April 28, 2010, or later FAA approved revision. Airplane Flight Manual Supplement (AFMS), Document Number 2570021090, Revision A, dated April 28, 2010, or later FAA approved revision is required.
Limitations and Conditions: 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 3260. This STC does not permit manufacturing of parts for multiple installations.
Associated Air Center, LP 8321 Lemmon Ave.
Dallas, TX 75209 A28NM Make : Airbus Model : A319-115 Date of application : July 15, 2008
Date of issuance : December 3, 2009
Date amended : April 28, 2010
( Signature) Jose Mora-Vargas ODA Administrator ODA-710437-SW
Transfer the ownership of Supplemental Type Certificate Number
to (Name of transferee)
(Address of transferee) (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)
Signature of gr antor (in ink):
FAA Form 8110-2-1(10-69) Page 3of 3
(Continuation Sheet) Number ST10898SC-D Date of Issuance: December 3, 2009
This aircraft is prohibited from conducting operations for hire or offered for common carriage. Airworthiness limitation inspections per 14 CFR Part 25, Appendix H, are contained in Chapter 3 of AAC Document Number 2570050090, Revision F, dated March 11, 2010, or later FAA approved revision, titled “Instructions for Continued Airworthiness”.
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; 25.331 Amdt. 25-86; 25.561(c) Amdt. 25-91; 25-562
(a),(b),(c)(1)(2)(3)(4)(7)(8) Amdt. 25-64; 25.625(a),(b),(c) Amdt. 25-72; 25.783(b),(e),(j) Amdt. 25-72, 25.801(a) Amdt. 25-72; 25.803(a) Amdt. 25-72; 25.807(c) Made. 25-72;25.809(a),(b),(c) Amdt. 25-72; 25.810(c) Amdt. 25-72;
25.812(e) Amdt. 25-58; 25.813(a),(b),(c),(d),(f) Amdt. 25-76, 25.853(a) Amdt. 25-116; 25.854(a) Amdt. 25-74; 25- 981(a)(3),(b) Amdt. 25-102; 25.1316(b),(c)(6) Amdt. 25-80; 25.1411 (a),(b),(e),(f),(g) Amdt. 25-72,
25.1415(a),(b),(c),(d) Amdt. 25-72. This STC incorporates the use of Exemption Number 7489.
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 · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| April 28, 2010 | Amended, current | Certificate |
| December 3, 2009 | Issued, earlier issue | Certificate |