What it approves
A319 Interior Reconfiguration and In-Seat Power System Installation
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 (5/14) Page 1 of 3
Number: ST09808AC This certificate issued to: United Airlines 600 Jefferson St.
Houston, TX 77002 Part 25 of the Federal Aviation Regulations Original Product – Type Certificate Number: Make: The Boeing Company A28NM Model: A319-132 & A319-133 Description of Type Design Change:
A319 Interior Reconfiguration and In-Seat Power System Installation in accordance with United Airlines Master Drawing List 2500DA14302, dated May 14, 2016 or later FAA approved revision.
Instructions for Continued Airworthiness, Document Number 2500R01337C, dated March 21, 2016 or later FAA approved revisions must be made available to the operator at the time of installation. There is no EWIS Source Document or AFM Supplement associated with this modification.
1) The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.
2) If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.
Date of Application: October 9, 2015 Date Reissued: October 26, 2017 Date of Issuance: May 18, 2016 Date Amended:
By Direction of the Administrator Signature Title Patrick Ashton, STC Administrator United Airlines Organization Designation Authorization
FAA Form 8110-2 (5/14) Page 2 of 3
Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: ST09808AC To (Name and address of transferee)
From (Name and address of grantor)
FAA Form 8110-2 (5/14) Page 3 of 3
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST09808AC
Certification Basis:
Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are not significant in FAA Order 8110.48, the certification basis for this modification is as follows:
a. The type certification basis for parts not changed or not affected by the change is shown in TCDS A28NM.
b. The certification basis for parts changed or affected by this modification since the reference application date October 9, 2015, is based upon the type certification basis shown in TCDS A28NM with the following exceptions.
14 CFR Part Amdt 14 CFR Part Amdt
25.571 (a) 25-86 25.853 (a)(c)(d)(e)(f)(h) 25-83
25.613 (a)(b)(d) 25-72 25.854 25-74
25.791 (a)(b)(c)(e)(e) 25-72 25.856 25-111
25.812 (i)(l)(1)(2) 25-58 25.869 (a)(1)(4) 25-72
25.851 25-74 25.1583 (c)(1)(2) 25-72
c. The modification certification basis also includes Special Conditions Number 25-403-SC, dated March 9, 2010.
--END--
FAA Form 8110-2 (5/14) Page 4 of 3
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST09808AC
FAA Form 8110-2 (5/14) Page 5 of 3
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST09808AC
FAA Form 8110-2 (5/14) Page 6 of 3
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST09808AC
ADs that name this STC · 0
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Approved models · 2
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| October 26, 2017 | Reissued, current | Certificate |
| May 18, 2016 | Issued, earlier issue | Certificate |