Aero Component Technologies
Holds 7 approved modifications. FAA spelling: Aero Component Technologies.
Approved modifications 7 · newest first
1994-10-19SE00054AT-D · Modification of the turbine exhaust case to provide increased wall thickness for the purpose of improved blade containment. · JT9D-7R4E, JT9D-7R4H1, JT9D-7R4E1
1994-02-14SE00049AT-D · Installation of Intermediate Compressor Case (JT8D SERIES) · JT8D Series
1994-01-05SE00048AT-D · Modification of compressor intermediate case diaphragm to permit acceptable of a 7th stage airseal ring. · JT8D-17AR, JT8D-17A, JT8D-15A
1993-10-14SE00047AT-D · Modification of turbine exhaust case to provide increased wall thickness for the purpose of improved blade containment. · JT9D-20, JT9D-20J, JT9D-3A
1993-06-22SE00046AT-D · State 1 LPC Stator: Provide a seamless one piece rubber airflow surface at the inner shroud. · JT9D-3A, JT9D-7, JT9D-20
1992-12-21SE00045AT-D · Modify -59A LPT case to reduce the thickness of four bosses to eliminate interference with the turbine case cooling... · JT9D-59A, JT9D-7Q
1992-02-24SE2888SO-D · Modify turbine exhaust case to incorporate Model -20 mount features. · JT9D-7A, JT9D-7F
Source: FAA Dynamic Regulatory System (type certificate data sheets, supplemental type certificates, technical standard order authorisations). An organisation's name is as the FAA spelled it on each record; related spellings are separate pages.