| Standard Equipment*: Three-bladed fully articulated main rotor with elastomeric dampers; Lycoming HO-360-G1A
engine; STAR System: (Start-up Overspeed Limiter, Automatic Rotor Engagement, Low Rotor RPM Warning Device.)
70 amp alternator,; oil filler/dipstick; 32.5 gallon fuel tank; remote full flow oil filter; right-hand PIC; cushioned left &
right magneto drives; light weight/high torque starter; dual controls with cyclic retention system; offset anti-torque
pedals; night lights with strobe beacons; upstack exhaust installation; flight instruments and warning lights
including: airspeed indicator, altimeter, magnetic compass, outside air temperature (OAT), tachometer, manifold
pressure, oil temperature, oil pressure, fuel quantity, cylinder head temperature (CHT), ammeter, low fuel warning
light, running time meter, tail rotor transmission chip detector, low voltage warning light, main rotor transmission
oil temperature / pressure warning light, KY96A comm transceiver; Mode A / Mode C transponder; ACK A-30 blind
encoder; "Hot Mic" intercom system; glove box, intercom with cyclic switch; pilot's cyclic mounted radio frequency
select switch (not available with cargo hook); cabin accessory plug, modular electrical harness; splined main rotor
drive shaft and hub; tubular skid type landing gear with heavy duty skid shoes; white Glasurit urethane paint; three-
piece chin skin w/ integral side fairings; single latch doors; tinted canopy glass; ground handling wheel brackets;
lap belts and shoulder harnesses; two-place cockpit; cushioned seats and rubber floor mat (color - gray); tie down
and oil cooler winterization kit.
*Manufacturer reserves the right to modify this configuration by substituting equipment. |