STC SA1064SO
FAA DRS lists SA1064SO as Current · Surrendered, held by Aeronautical Engineers, Inc, for Lockheed Aircraft 188A. Recorded change: Increase in zero fuel weight from 82,500 lbs. to 90,800 lbs. Snapshot dated June 30, 2026.
FAA-listed holder
Aircraft configurations
1
FAA revision date
FAA status
Current · Surrendered
Recorded modification
What the FAA record covers
SA1064SO 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 188A. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
Related fuel systems STCs
Note A. Installation of ACT, Inc. FPTFW0000 High Strength Fuel Cells; Note B. Installation of ACT, Inc. FPTFW00001 High Strength Self Sealing Fuel Cells; Note C. Installation of ACT, Inc. FPTFW00003 High Strength Self Sealing Fuel Cells with interfaces for left side single point refueling and auxiliary tank 14-54 (at station 241.0).
FAA holder: GKN Aerospace Transparency Systems Fort Worth
Installation of 18 gallon nylon auxiliary fuel tanks on airplanes equipped with standard range 64 gallon capacity bladder tank or 62 gallon fiberglass fuel tanks. (A185F thru S/N 18503683 and later airplanes originally equipped w/bladder fuel tanks).
FAA holder: Hartwig Aircraft Fuel Cell Repair