Installation of Turbomach Gemini Model T-20G-10C1 auxiliary power unit.

Installation of Turbomach/Gemini Model T-20G-10C1 auxiliary power unit.

Installation of Meggitt Avionics Engine Instrument Display System.

Installation of Williams/Rolls FJ44-2A engine. Installation of STC SA732NW required for this mod.

Installation of forward lounge toilet.

Installation of Kannad 406 AF ELT Certification Basis Limitations -Engineering Order 2022014 - EO - 02.-AFM Supplement, Doc. No 2022014 - AM - 02.- Continued Airworthiness Report Doc. No2022014 - CA - 02. Conditions 1. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph Description". Compatibility with other aircraft/engine configurations shall be determined by the installer.

Installation of a Shadin Company Digital Fuel Flow Meter.

Replacement of existing engine indicators (ITT. c/o FAN RPM, c/o TURBINE RPM, FUEL FLOW, FUEL QUANTITY, OIL TEMP & OIL PRESS) with Howell Instruments indicators.

Installation of bar, header, dividers, folding table and modification of toilet.

Replacement of existing engine indicators (ITT, percent fan RPM, percent turbine RPM, fuel flow, fuel quantity, oil pressure) with Howell Instruments indicators.