Installation of a Smiths Industries Flat Plate Engine and Systems Panel with Honeywell Thrust Rating Computer.

Installation of ASTEC Manufacturing inlet assembly per ASTECH Manufacturing, Inc.

Document no. MDL-030-06009 titled Master Drawing List - MD-80 Series Inlet, Revision A00, dtd 6/20/01 or later FAA approved revision.

GKN Aerospace is responsible for the complete design, development, manufacture, assembly and certification of Inlets for turbofan and turboprop applications

Installation of ASTECH Manufacturing, Inc. inlet assembly

GKN Aerospace is responsible for the complete design, development, manufacture, assembly and certification of Inlets for turbofan and turboprop applications.

Installation of ASTECH/MCI tailpipe assembly.

Installation of the APU EGT and Tach indicators.

Installation of P&W JT8D-200 Series Engines incorporating the improved forward Fan Case as described in the P&W SB JT8D6478, Rev.1, dated 1 August 2007. EASA.IM.A.S.01925 FAA STC ST00228BO

Installation of Nose Cowl Anti-Icing Elbow Assembly

Installation of a JET Engineering, Ltd. Advanced Jet Nozzles on the above airplane model(s) when powered by Pratt & Whitney JT8D-21JT8D-217, 7A, -217C, 219 engines EASA.IM.A.S.02331 FAA STC ST01943LA

Installation of modified Pratt & Whitney JT8D-217, or JT8D-217A, or JT8D-217C, or JT8D-219 engines.

Supplemental Operating Configurations MD-80.Addition of engine and part intermix. EASA.IM.A.S.01180 FAA STC ST01649SE