N967ML - 2003 EAGLE R & D HELICYCLE

2003

EAGLE R & D

HELICYCLE

N967ML

HC17ML

VFR

New

52.0

1

See http://home.bellsouth.net/personalpages/pwp-967ml for pictures and build details. West Atlanta. Modified Solar T62 turbine 160 derated to 105 HP Single Seat – 220 lb max pilot Gross Weight – 860 lbs Empty Weight – 551 lbs Fuel Capacity – 21 (16+5 reserve) US gal Jet-A Range with Reserve – 180 miles Rate of Climb – 900 fpm Hover IGE – 9,500 feet Service Ceiling – 10,500 feet Normal Cruise (half doors) – 95 to 100 mph Max Airspeed, Sea Level/Std Conditions – 110 mph Helicyle completed Dec. 2003, flying 2004, 52 TT, night equiped, single place turbine, factory inspected. Flying regularly.

4130, All welding done at factory. White Dupont Imron. Internal airframe treated for corrosion and sealed. Current weight & balance set for 150 lb pilot.

52

SNEW

Eagle R&D modified Solar T62T-32 Turbine (160 derated to 105 HP) Jet-A burn rate ~11.5 gal per hour.

Eagle R&D Main rotor and tail rotor system, dynamic balanced by factory during preflight checkout.

Factory supplied aux fuel tank installed.

Microair 760 VHF, Microair T2000 mode C transponder, Davtron 655 (OAT, volts, density alt), panel lights, hobbs, EGT, Trans temp, turbine oil press., rotor tach, turbine tach, connection and mount for Garmin GPSMAP 196.

Landing lights with wig-wag function, nav lights, flashing beacon (meets VFR night requirement). Blad hangers, blade storage box, tail boom support stand, aux battery connector.

2003 Paint White Dupont Imron, half door kit installed, door frame accented with red/blue strips

2003 interior Seat navy blue simulated leather covering temperfoam seat bottom and back pad. Covered by a professional aircraft interior shop.

Factory preflight inspection completed in February 2004, by B.J. Schramm (the designer and original owner or Rotorway). Electronic balance completed during checkout. Phase I flight restrictions complete and now past 40 hour mark.