What it approves
Installation of opening in fuselage right hand for emergency exit between fuselage station 226 and fuselage station 253.4. Is approved only for its structural, electrical and mechanical provisions and can be incorporated with STC SA707EA and STC SA709EA.
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 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: Installation of Opening in Fuselage R/H for Emergency Exit between F. S. 226 and F. S. 253.4 in accordance with Lockheed Aircraft Service Company Report #3607 dated 10/16/68, Revised 12/12/68.
Limitations and Conditions: This modification is approved only for its structural, electrical and mechanical provisions and can be incorporated with STC SA707EA and 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 : November 7, 1968
Date of issuance : December 17, 1968
Date reissued : Mar. 20, 1974, Nov. 2, 1999, Mar. 16, 2001, Mar. 15, 2004, Apr. 26, 2004
( 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 |