What it approves
Relocation of cabin window right-side from fuselage station 217-236 to fuselage station 333-352.
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.
Number SA707EA
This Certificate issued to Lockheed Martin Aeronautics Company 36 South Cobb Drive Marietta, Georgia 30063 Part 25 of the Federal Aviation Regulations, and Part 4b of the Civil Air Regulations.
4A22 Lockheed 188C Description of Type Design Change: Relocation of Cabin Window R/H Side from F.S. 217-236 to F. S.
333-352 in accordance with Lockheed Aircraft Service Company Report #3606 dated 10/18/68, Revised 12/9/68.
Limitations and Conditions: This modification must be incorporated with STC SA708EA and can be incorporated with STC SA709EA.
This approval should not be incorporated in any aircraft of this specific model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the aircraft. 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.
Date of application : October 21, 1968
Date of issuance : December 17, 1968
Date reissued : March 20, 1974, Nov. 2, 1999, Mar. 16, 2001, Mar. 15, 2004, Apr. 26, 2004 Date amended :
( Signature)
Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title)
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 |
|---|---|---|
| Lockheed Aircraft Corporation | 188C | 4A22 |