STC ST04429AT

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to th e design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 1 of 3

Number: ST04429AT

This certificate issued to: Delta Flight Products, LLC.

3980 Tradeport Blvd, Bldg 1200 Atlanta, GA. 30354

Part 25 of the Federal Aviation Regulations.

T00001SE Make: Boeing Model: 777-200/-200LR Series

Description of Type Design Change: Installation of Mid-Life Reconfiguration in a Boeing 777-200/-200LR series aircraft in accordance with Delta Flight Products Master Data List 16D01MDL001, Revision G, dated June 12, 2018, or later FAA Approved revision. Delta Flight Products Airplane Flight Manual Supplement, 16D01R006, Rev -, dated June 21, 2018 and Instructions for Continued Airworthiness (ICA) 16D01R030, Rev A, dated March 1, 2018, or later FAA approved revisions, are a required part of this STC.

1) This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship betw een this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane.

2) If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

3) Boeing SB 777-24-0154 Change to Electrical Loads Management System and SB 777-25-0688 (-200 Only) to Relocate Overhead Flight Crew Rest, must be accomplished with this modification.

Date of Application: August 24, 2016 Date Reissued:

Date of Issuance: June 21, 2018 Date Amended:

Signature Title Christina M. Underwood Manager, Atlanta ACO Branch

FAA Form 8110-2 (5/14) Page 2 of 3

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST04429AT

FAA Form 8110-2 (5/14) Page 3 of 3

Limitations and Conditions: (Cont’d)

4) STC ST02657NY, Installation of Panasonic Avionics Corporation System eX2 Passenger Entertainment System, is required to be to be installed in conjunction with this modification.

5) STC ST03435NY, Installation of Bruce Aerospace Lighting, is required to be to be installed in conjunction with this modification.

6) ST02554SE, JAMCO America Lavatory and Galley Installation Delta Air Lines 777-200/200LR, is required to be to be installed in conjunction with this modification.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Boeing Model 777-200/-200LR is as follows:

a. The type certification basis for Boeing Model 777-200/-200LR series airplanes is shown on TCDS T00001SE for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, August 24, 2016, is based upon part 25 as amended by Amendment 25-100. Based on 14CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-144

25.1, 25.23(b)(2), 25.27(b), 25.301, 25.303, 25.305(a)(b)(c), 25.321(a), 25.365(g)(e), 25.561, 25.562, 25.601,

25.603, 25.605, 25.609, 25.613(a)(b)(c)(f), 25.619, 25.625, 25.785(a)(b)(c)(d) (f)(1)(3)(h)(2)(i)(j)(k),

25.789(a), 25.791, 25.793, 25.803(a), 25.811(a)(b)(c)(d)(g), 25.815, 25.853(a)(d), 25.854, 25.899(a)(1),

25.981(d), 25.1351(a)(1), 25.1415(a)(b)(c)(d), 25.1441, 25.1443(c)(2), 25.1445(b), 25.1453, 25.1455,

25.1529, 25.1541(a)(1)(b), 25.1557(a), 25.1561(b)(c).

Regulations at an intermediate amendment

25.813(e) Amdt. 25-116

Regulations at the amendment level in TCDS T00001SE

25.307(a)(d), 25.571(a)(b), 25.611, 25.787(a)(b), 25.807, 25.812(a)(1)(e)(i)(k)(l) (1)(2), 25.813(a)(b)(d),

25.831(a), 25.851(a)(1)(4)(5)(6), 25.869(a)(1)(4), 25.1301, 25.1309(a)b)(d), 25.1 353(a)(b),

25.1411(a)(b)(d)(e)(f), 25.1431(c), 25.1447(a)(c)(1)(4), 25.1450(a)(b)

14 CFR Part 26 Regulations

Based on 14 CFR 21.101(g), applicable provisions of 14 CFR Part 26 are included in the certification basis. For any future 14 CFR part 26 amendment, the holder of this STC must demonstrate compliance with the applicable sections. As of the issuance date of this STC, compliance has been found for the regulations 26.11, 26.47 (Amdt 26-0 through 26-5).

a. Exemptions: Exemption 17531 granted to Delta Flight Products (DFP) for compliance with 14 CFR §§25.813(e) to permit the installation of interior doors between passenger compartments.

---------------------------------------------------------------END---------------------------------------------------------------