STC ST09822DS

ST09822DS United Airlines 4933 Wright Rd.

Houston, TX 77032 25 Federal Aviation Regulations A1NM The Boeing Company 767-300 Series 767-300 Interior Reconfiguration in accordance with United Airlines Master Drawing List 2500DA15136 Revision ‘L‘, dated May 12, 2022 or later FAA approved revision.

Instructions for Continued Airworthiness, Document Number 2500R01508C Revision ‘A‘, dated October 22, 2021, or later FAA accepted revision is required for this installation. No AFM Supplement or EWIS ICA is required for 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. (continued on page 3) May 18, 2018 March 3, 2019 April 10, 2020; November 19, 2021; June 10, 2022

Raju Tumarada, STC Administrator United Airlines Organization Designation Authorization 4

ST09822DS 4

ST09822DS Limitations and Conditions (continued):

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.

3) Prior or concurrent installation of the following modifications is required with this STC (aircraft applicability is identified within the following documentation):

- Boeing Service Bulletin 767-53-0292, Version 02, dated January 29, 2019, or later FAA approved revision

- Boeing Service Bulletin 767-53-0291, Version 01, dated November 19, 2018, or later FAA approved revision

- Boeing Service Bulletin 767-52-0102, Version 01, dated October 10, 2018, or later FAA approved revision

- Boeing Service Bulletin 767-25-0568, Version 01, dated November 2, 2018, or later FAA approved revision

- Delta Engineering Corporation FAA STC ST03205NY, amended June 27, 2017, or later amendment 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.

ST09822DS

b. The certification basis for parts changed or affected by this modification since the reference application date May 18, 2018, is based upon the type certification basis shown in TCDS A1NM with no exceptions.

14 CFR Part Amdt 14 CFR Part Amdt

25.365(g) 54 25.813(c) 76

25.613(a)(b)(d) 72 25.851(a)(1)(2)(4)(5)(6)(7) 74

25.785(h) 51 25.853 83

25.787(a)(b) 51 25.854 74

25.793 51 25.856(a) 111

25.807(a)(7)(iv)(v)(vi)(vii)(c)(7) 67 25.869(a)(4) 72

25.812 (a)(c)(d)(e)(f)(i)(l)(k) 58 25.981(d) 125

c. The modification certification basis also includes Special Conditions Number 25-369-SC, dated February 7, 2008.

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