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.
