Installation of ASTECH Engineered Products, Inc. Inlet Inner Barrel Assembly in accordance with Master Drawing List, A320/CFM56- 5ASeries Engine Inlet, Drawing List Number MDL030-11030 Revision C.

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

Installation of ASTECH Engineered Products fan cowl door in accordance with ASTECH’s Master Drawing List V2500 Cowl Door Assembly No. MDL030-16103, Revision “A”.

Installation of Astech/MCI tailpipe assembly

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 Engineered Products, 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 Engineered Products, Inc. Inlet Inner Barrel Assembly in accordance with ASTECH Engineered Products, Inc.

document titled, 'Master Drawing List A320 CFM56-5A Series Engine Inlet Drawing List No. MDL030-11030', Revision NC, dated December 11, 2003, or later FAA Approved revisions.

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 Engineered Products fan cowl door.

GKN Aerospace is responsible for the complete design, development, manufacture, assembly and certification of a number of fan cowl doors on both turboprop and turbofan aircraft.

We are able to provide flexible design solutions for fan cowl doors, incorporating a number of materials required dependant on the conditions that it is exposed to, ranging from complex composite sandwich construction to waffle titanium structures used in high temperature applications.

Number 2 Cockpit Windshields Addition of Layers of Polyrethane Interlayer to the Existing Qualified Design to improve In-Service Reliability.

Limitations: This approval provides for the installation of the referenced windows individually or in any combination..
Conditions: n/a

Installation of a GKN Aerospace designed Boeing 777 No 1 Windshield

PartNo. 10702 (LH) / 10703 (RH); or Part No. 10712 (LH) / 10713 (RH)

Limitations: None.

Conditions: Replacement of a Flight Compartment Window Number 1 per this STC withGKN ATS part no. 10712 (LH) / 10713 (RH) together with the relevantwiring loom modification constitutes an Alternative Method of Compliance(AMOC) to the terminating action requirements of