What it approves
Installation of a DC-8-51 landing gear on DC-8-52 airplane.
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.
This Certificate issued to United Air Lines, Inc.
600 Jefferson Street Houston, Texas 77002
Part 25 of the Federal Aviation Regulations. (For certification basis, see Type Certificate Data Sheet 4A25).
4A25
Boeing
DC-8-52 Description of Type Design Change: Installation of DC-8-51 landing gear on DC-8-52 airplanes.
Limitations and Conditions: The DC-8-51 and DC-8-52 are aerodynamically identical.
Therefore, no higher loads will be induced into the airframe nor will th e airframe induce higher loads into the landing gear. 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.
This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.
Date of application: May 13, 1980
Date of issuance: June 9, 1980
Date reissued: November 30, 2011
( Signature) Haifa Haj-Eid Supervisor, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title)
NOTE:
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THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.
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 | DC-8-52 | 4A25 |