Installation of emergency power supply system.

Waste Receptacle Fire Containment Substantiation in accordance with Data List Report No. F00-01016 Revision R dated 11-Oct-2011, or later FAA approved revision.Instructions for Continued Airworthiness, Report ICA-F00-01016-501, revision A, dated 21-July-2011 or later FAA approved revision is required.

Installation of Pratt & Whitney Engine Services, Inc. Data Transmission Unit (DTU).

Installation of GDS Aero Tail Cone APU Firewall Assembly, P/N GF2APU-FW1.

EASA Validation of FAA STC ST00261BO:Installation of Pratt <(>&<)> Whitney Engine Services, Inc DataTransmission Unit (DTU) in accordance with Pratt <(>&<)> Whitney EngineServices, Inc, Master Document List DTU-T-100-6, Revision F dated 23rdJuly 2009, or later revisions approved by EASA in accordanc... EASA.IM.A.S.03229 FAA STC ST00261BO

Replacement or the inner aluminum barrel of the engine inlet cowl<(>,<)>with an inlet barrel of carbon graphite sandwich construction<(>,<)> toprovide a solution for in-service corrosion. FAA STC ST04413AT