Conversion Process

Week 1:

The PT6 turbine engine and all firewall forward items relating to the PT6 are removed. The cockpit has all items relating PT6 engine operation removed. The aircraft firewall is thoroughly inspected prior to conversion.

Week 2:

Sheet metal work on the firewall forward fuselage is accomplished. Cockpit electrical system is installed which includes removing old circuits that relate to PT6 operation and installing a new start panel, new wiring, and new engine instruments.

Week 3:

Install engine mount assembly with new electrical junction box, battery box, wiring harnesses and a factory new engine. Re-install the OEM bleed-air heater and bleed-air vacuum system.

Weeks 4 & 5:

Install cowlings and access doors. Install and rig new engine controls. Match paint or paint entire aircraft (not included in installation cost).

Delivery:

Final inspection of entire engine installation by TTC, Inc's President Bobby Bishop and authorized installation facility. First engine test runs and first test flights by Bobby Bishop. One day of training flights with up to two pilots on Honeywell engine operation with Bobby Bishop at installation facility.