What it approves
B767-300 Interior Reconfiguration
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: ST09803AC 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 A1NM Model: 767-322 Description of Type Design Change:
767-300 Interior Reconfiguration in accordance with United Airlines Master Drawing List 2500DA13 969 Revision ‘-‘, dated December 19, 2015 or later FAA approved revision.
Instructions for Continued Airworthiness, Document Number 2500R01262C Revision A, dated November 18, 2015 or later FAA approved revision must be made available to the operator at the time of installation. There is no AFM Supplement or EWIS Source Document 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: April 28, 2015 Date Reissued: March 10, 2016; July 24, 2017 Date of Issuance: December 24, 2015 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: ST09803AC 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: ST09803AC
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 A1NM.
b. The certification basis for parts changed or affected by this modification since the reference application date April 28, 2015, is based upon the type certification basis shown in TCDS A1NM with the following exceptions.
14 CFR Part Amdt 14 CFR Part Amdt
25.29 72 25.785 (f)(1)(3) 88
25.305 (a)(b) 86 25.789 (a) 46
25.307 (a)(d) 72 25.853 (a)(c)(d)(e)(h) 83
25.365 (e)(2) 54 25.854 74
25.603 46 25.856 (a) 111
25.605 (a) 46 25.869 (a)(1)(4) 72
25.613 (a)(b)(d) 72 25.1583 (c)(1)(2) 72
25.625 72 26.11 (c)(1)(2) 0
25.785 (a)(b)(c)(d)(e)(h) 51 26.47 (c) 1
c. The modification certification basis also includes Special Conditions Number 25-369-SC, dated February 7, 2008.
--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: ST09803AC
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: ST09803AC
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: ST09803AC
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 | 767-300 Series | A1NM |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| July 24, 2017 | Reissued, current | Certificate |
| December 24, 2015 | Issued, earlier issue | Certificate |