Supplemental type certificate · Aero Component Technologies

Holder
Aero Component Technologies · United States
Status
Current · Issued
Status date
December 21, 1992
Product
Engine
Certification basis
Part 21
Data sheet
TCDSE3NE

From FAA DRS. DRS record last changed December 6, 2025.

What it approves

Modify -59A LPT case to reduce the thickness of four bosses to eliminate interference with the turbine case cooling manifold installed on -7Q engines. This modification permits use of the -59A LPT case on-7Q engines.

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 2

MakeModelData sheet
Pratt & Whitney DivisionJT9D-59AE3NE
Pratt & Whitney DivisionJT9D-7QE3NE