Baseline (Green) Configuration

Propulsion

  • Two Pratt & Whitney Canada PT6A-65B turboprop engines rated at 1,100 SHP each
  • Two Hartzell Propeller Inc. HC-B5MP-3D 5-bladed constant-speed propellers with feathering and reverse
  • Displayed on engine instruments
    ITT – Interturbine Temperature
    Tq – Engine Torque
    Np – Propeller Speed
    Ng – Gas Generator Speed
    Oil Temperature Indicator
    Oil Pressure Indicator
    Fuel Flow Indicator
  • Engine Fire Protection System with cockpit annunciators, three sets of flame detectors, and two-shot extinguishers in each engine nacelle
  • Inertial Separators, bleed air deiced engine inlets, and electrically deiced propellers
  • Control Surfaces
  • Wing is a semi-monocoque, two-spar, all-metal split structure consists of the center section and two outboard wing sections
  • Each outer wing is fitted with a flap, an aileron, a two-section slat, and two spoilers
  • Empennage is a cantilever, all-metal, semi-monocoque with twin vertical fins and rudders
  • Horizontal stabilizer leading edge is fitted with a fixed slat which serves to eliminate air flow separation
  • Both elevator halves fitted with trim tabs
  • Both rudders fitted with trim tabs

Flight Instruments

  • Pilot and co-pilot EFIS systems, each includes EADI, EHSI and mode control panel
  • Airspeed – refer to Avionics Package
  • Altimeter – refer to Avionics Package
  • VSI – refer to Avionics Package
  • Pitot-Static system, dual
  • Digital electric clock, AstroTech LC-2 Quartz Chronometer
  • Standby magnetic compass
  • Master Warning/Annunciator Panel, mounted in low profile Glareshield, Pilot and co-pilot
  • Cockpit, Flight & Ground Controls
  • Primary flight – longitudinal, lateral, and directional controls provided at Pilot and Copilot stations.
  • Conventional yoke type control sand rudder pedal type controls.
  • Center console throttle quadrant and rudder pedal type controls.
  • Electric elevator, aileron and rudder trim controls
  • Dual hydraulic systems, powered by engine-driven pumps, with hydroaccumulator to supply hydraulic pressure in case of pump failure
  • Hydraulic driven flaps, spoilers, main wheel brakes and nose wheel steering
  • Battery – Dual 26 Ah Acid batteries provide up to 30 minutes of backup power as well as engine start capability
  • DC Generators – two 28 VDC engine-driven generators
  • Battery – Dual 26 Ah Acid Nickel-Cadmium batteries provide up to 30 minutes of backup power as well as engine start capability
  • AC Power – two 115 VAC converters
  • Ground Power Receptacle – 28 VDC

Electrical System

  • Battery – Dual 26 Ah Acid batteries provide up to 30 minutes of backup power as well as engine start capability
  • DC Generators – two 28 VDC engine-driven generators
  • AC Power – two 115 VAC converters
  • Ground Power Receptacle – 28 VDC

Fuel System

  • Six fuel tanks (one main and two auxiliary in each wing) with gravity fuel fillers and central-point pressure refueling, 602 US gallon capacity
  • Cross-feed system allows fuel transfer between wings
  • Fuel supplied to engine via electric pumps in each tank
  • Sensors in each tank display on analog and digital cockpit instruments
  • Dual fuel flow gauges display each engine’s consumption Ice & Rain Protection

Ice & Rain Protection

  • Bleed air heated leading edges on wings, horizontal stabilizer, vertical stabilizers
  • Engine inertial separators and bleed air heated inlets
  • Deiced pitot-static sensors – electrically heated
  • Deiced pilot and co-pilot windshield – electrically heated
  • Deiced propellers – electrically heated mats on each blade
  • Windshield wiper system - two speed

Lighting

  • Cockpit lighting includes Instrument panel, pilot and copilot Control Panels, and Cockpit ceiling lights
  • Cabin lighting includes Exit lights, Fasten seat belt lights, ceiling lights, and Entry stairs ceiling light
  • External lights include Nose-mounted taxi lights, Main gear support-mounted landing lights, Navigation lights, and Strobe lights

Cabin Comfort System

  • Cockpit and cabin bleed air heating w/windshield defogging system
  • Heating and ventilation control panel
  • Ram air ventilation system
  • Electric ventilation blower

Paint & Corrosion Protection

  • Refer to Paints and Finishes section
  • Black instrument panel paint finish

Cockpit/Cabin Appointments

  • Pilot/co-pilot seats - vertically adjusting, 4 point restraint/harness, fabric upholstery
  • Pilot/co-pilot light filters mounted above cockpit dome windows
  • Cockpit

Manual fire extinguisher

  • Crash axe for emergency egress
  • Emergency locator transmitter
  • Right side emergency exit
  • Left and right side cabin emergency exits

Avionics

  • Avionics master switch
  • Garmin GTN 650 (16W) #1 WAAS-certified GPS, ILS/VOR with localizer and glideslope
  • Garmin GTN 650 (16W) #2 WAAS-certified GPS, ILS/VOR with localizer and glideslope
  • Honeywell Bendix/King KR 22 marker beacon receiver control and annunciator panel
  • Space, wiring and structural provisions for Honeywell Bendix/King KFC 325 Auto Flight Control Systems
  • Dual Honeywell Bendix/King EFS 50 Electronic Flight Instrument System
  • Dual Litef LCR 100 – Attitude Heading Reference System.
  • Honeywell Bendix/King MST67A Mode S Transponder, fully compatible with mode A and C, S (ELS, EHS) transponder formats, compatible with TCAS II
  • Space, wiring and structural provisions for Honeywell Bendix/King KDM706A DME
  • Honeywell Bendix/King KDC481T Air Data Computer (ADC), King KRA-405B Radar Altimeter with Decision Height alerting displayed on EFIS, 0-2,500 ft.
  • Honeywell Bendix/King RDR2000 Digital Color Radar with Vertical Profile. Avoidance range > 200 NM. Displayed on X600 Multifunction Display.
  • Electric Inverter, Supply 115 V/400 HZ, 36 V/400 HZ and 26 V/400 HZ AC electric power
  • Dual Airspeed indicators are located on the pilot and co-pilot instrument panels
  • Dual Altimeters are located on the pilot and co-pilot instrument panels.
  • CAS 100B TCAS II 7.1 with dual Honeywell Bendix/King IVA 81D
  • Mid Continent LifeSaver Backup Attitude Indicator with own battery
  • Kannad 406AF Emergency Locator Transmitter
  • Two KMA 24H-70 - Audio Selector/Amplifier/ICS Panels. ICS with volume control included in KMA 24H-70 Audio Panels with Voice Operated Intercom (VOX)
  • Honeywell Mk VI Enhanced Ground Proximity Warning System (TAWS A).
  • AstroTech LC-2 Quartz Chronometer
  • Cabin loudspeaker allows crew to transmit messages to passengers
  • Avionics Master rocker switch in Overhead Switch Panel
  • Space, wiring and structural provisions for ADF #1
  • Provides basic provisions for installation of the Honeywell Bendix/King KHF 1050 Radio
  • IPS FIKI - structural and wiring provisions,
  • AUTOPILOT - structural and wiring provisions.