What it approves
Convert straight mount engine to dynafocal mount configuration
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 (5/14) Page 1 of 2
Number: SE1051SW
Part 13 of the Civil Air Regulations.
Original Product – Type Certificate Number: E-274 Make: Lycoming Engines Model: O-320-B1A; O-320-A2B Description of Type Design Change:
Convert straight mount engine to dynafocal mount configuration according to Drawing 69C5019, Revision A and 69C5020, Revision B, dated July 10, 1069.
1. Engine data plate must be marked to add “CPI-D”.
2. Eligible for installation per STC SA1046SW.
3. The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.
Date of Application: May 26, 1969 Date Reissued: 6/23/72; 1/11/83/ 4/2/08; 7/20/15; 1/25/16;
10/31/16 Date of Issuance: July 8, 1969 Date Amended:
Signature
Title James A. Grigg Acting Manager, Fort Worth Aircraft Certification Office, Southwest Region Continental Motors Inc.
2039 S. Broad St.
Mobile, AL 36615
FAA Form 8110-2 (5/14) Page 2 of 2
Transfer the ownership of Supplemental Type Certificate Number: SE1051SW
To (Name and address of transferee)
From (Name and address of grantor)
FAA Form 8110-2 (5/14) Page 3 of 3
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.