What it approves
Modification of the turbine exhaust case to provide increased wall thickness for the purpose of improved blade containment.
ADs that name this STC · 1
An AD can apply because an STC is installed, or mention one in its text.
Supplemental type certificate · Aero Component Technologies
- Holder
- Aero Component Technologies · United States
- Status
- Current · Issued
- Status date
- October 19, 1994
- Product
- Engine
- Certification basis
- Part 21
- Data sheet
- TCDSE3NE
From FAA DRS. DRS record last changed December 5, 2025.