STC SA708EA
FAA DRS lists SA708EA as Current · Reissued, held by Lockheed Martin Aeronautics Company, for Lockheed Aircraft 188C. Recorded change: 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. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA708EA identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.
Applicability
Aircraft named in FAA DRS
Named aircraft: Lockheed Aircraft 188C. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related electrical systems STCs
Installation of Teledyne Battery Products Gill LT Valve-Regulated Lead-Acid.
FAA holder: Teledyne Battery Products
FAA record reference
- STC number
- SA708EA
- Product
- Aircraft · Large Multi-Engine
- Country
- United States
- Application date
- November 7, 1968
- Revision date
- April 26, 2004
- CFR references
- Part 21, Part 25