STC SA00734LA
FAA DRS lists SA00734LA as Current · Reissued, held by Aerospace Welding Minneapolis Inc., for New Piper Aircraft PA-23-250. Recorded change: Installation of modified exhaust system. S/N 27-2505 and up. Snapshot dated June 30, 2026.
FAA-listed holder
Aircraft configurations
1
FAA revision date
FAA status
Current · Reissued
Recorded modification
What the FAA record covers
SA00734LA 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: New Piper Aircraft PA-23-250. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related engine and powerplant STCs
Installation of an Inlet Barrier Filter (IBF) System.
FAA holder: Donaldson Company Inc.
Installation of MT-Propeller Entwicklung GmbH's Model# MTV-5-1-D-C-F-R(A)/CFR210-56 5-Blade constant speed, full feathering, reversible propeller and spinner on Textron Aviation Inc. Model P210N aircraft equipped with Rolls-Royce 250-B17F/2 engine installed per FAA STC SA1003NE.
FAA holder: MT- Propeller Entwicklung GmbH
FAA record reference
- STC number
- SA00734LA
- Product
- Aircraft · Small Airplane
- Country
- United States
- Application date
- August 31, 1998
- Revision date
- November 17, 2023
- CFR references
- Not listed