What it approves
Installation of Bin Lift Assist in a Boeing 777-200/-200LR series aircraft
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.
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: ST04426AT
This certificate issued to: Delta Flight Products, LLC.
3980 Tradeport Blvd, Bldg 1200 Atlanta, GA. 30354
Part 25 of the Federal Aviation Regulations.
Original Product – Type Certificate Number: Make: Boeing T00001SE Model: 777-200/-200LR Series
Installation of Bin Lift Assist in a Boeing 777-200/-200LR series aircraft in accordance with Delta Flight Products Master Data List 16D07MDL001, Revision C, dated 16 May-2018, or later FAA Approved revision.
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 between 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 shal l give the other person written evidence of that permission.
3) Delta Flight Products Instructions for Continued Airworthiness (ICA) 16D0 7R003, Revision A, dated 03-APR-2018, or later FAA approved revision, is a required part of this STC.
Date of Application: April 17, 2017 Date Reissued:
Date of Issuance: June 4, 2018 Date Amended:
Signature
Title Christina M. Underwood Manager, ACO Branch
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 the design data nor to alter an aircra ft, aircraft engine, or propeller.
FAA Form 8110-2 (5/14) Page 2 of 3
Transfer the ownership of Supplemental Type Certificate Number: ST04426AT
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: ST04426AT
Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircra ft, aircraft engine, or propeller.
FAA Form 8110-2 (5/14) Page 3 of 3
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, April 17, 2017, is based upon part 25 as amended by Amendment 25-144. 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, 25.601, 25.603(a)(b)(c), 25.605(a)(b), 25.609(a)(b),
25.613(a)(b)(c)(f), 25.619(a)(b)(c), 25.789(a), 25.853(a)(d), 25.899(a)(1), 25.981(d), 25.1529,
25.1541(a)(1)(b), 25.1561(b)(c).
Regulations at an intermediate amendment
None
Regulations at the amendment level in TCDS T00001SE
25.21(a)(1), 25.305(a)(b)(c), 25.307(a), 25.321(a), 25.561(a)(b)(3)(d), 25.611, 25.625(a)(b)(c), 25.787(a)(b),
25.853(a)(d)(1)(2)(4), 25.869(a)(1)(4), 25.1301(a)(b)(c)(d), 25.1309(a)(b), 25.1351(a)(1), 25.1353(a)(b),
25.1411(a)(b)(d)(e)(f), 25.1431(c), 25.1557(a).
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 (Amdt 26-0 through 26-5): 26.11.
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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.