What it approves
Installation of Hughes passenger entertainment/passenger service multiplex system.
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 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of 3
Number: SA3480WE This certificate issued to: Burrana, Inc.
743 West 1200 North, Suite 100 Springville, Utah 84663 Part 25 of the Federal Aviation Regulations Original Product Type Certificate Number:
A20WE Make: The Boeing Company
Model: Boeing 747-100, -200B, -200C, -300, Description of Type Design Change: 747SR, 747SP
Installation of Hughes Passenger Entertainment/Passenger Service Multiplex System in accordance with FAA Sealed Hughes Aircraft Company Drawing List No. 1103000-701, Revision "B", dated September 7, 1977, or later FAA Sealed revisions.
The approval of this change in type design applies only to the aforementioned aircraft. This approval should not be extended to other aircraft of these models 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 not introduce any adverse effect upon the airworthiness of that aircraft.
May 24, 1977
May 2, 1995; June 12, 1995; January 23, 1998;
May 30, 2006; August 10, 2016; March 26, 2021
Date of Issuance: November 3, 1977 Date Amended:
Title: Manager, Technical & Administrative Support Section Los Angeles ACO Branch
FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of 3
Number: SA3480WE
United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate
Certification Basis:
(Continuation Sheet) Number: SA3480WE
FAR Part 1, FAR Part 21, FAR Part 36, including Amendment 36-1 effective 1 December 1969, FAR Part 25 effective 30 June 1966, Amendments 25-1 through 25-8 plus 25-15, 25-17, 25-18 and 25-20 and special conditions summarized for recordation purposes as enclosed to FAA letter to The Boeing Company dated 20 February 1970.
Special Condition 4A, revised to apply to airplanes with the landing gear load evener system deleted, was recorded as attachment to an FAA letter to The Boeing Company dated 12 May 1971.
Exemptions from FAR Part 25.
No. 1013A dated Dec. 24, 1959 - Exemption from FAR 25.471(b) to allow lateral displacement of the C.G. from the airplane centerline.
Compliance with the following optional requirements has been established:
Ditching Provisions FAR 25.801 Ice Protection Provisions FAR 25.1219
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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.
Approved models · 6
Every issue · 3
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| March 26, 2021 | Reissued, current | Certificate |
| August 10, 2016 | Reissued, earlier issue | Certificate |
| May 30, 2006 | Reissued, earlier issue | Certificate |