Honeywell Primus Epic Avionics Suite
4-axis DAFCS (Digital Automatic Flight Control System)
Enhanced with Hovermode (HOV)
Dual PFD
Dual MFD
Single ESIS
Dual AHRS
Dual ADM
Dual Display Controllers
Dual Cursor Control Devices
Dual Modular Avionics Unit
Dual VHF Radio
Dual NAV Radio
Single Mode-S Transponder
Single ADF
Single DME
Dual pedestal mounted Multifunction Control Display Units
(MCDU)
Dual Radio Altimeter
Single ELT
Dual GPS (WAAS/SBAS)
EGPWS
TCAS II
Weather Radar

FIVE STAR Cabin Interior including:
3 VVIP / crashworthy armchairs leather covered-forward looking, (with inertial reels and
safety belt, sliding inflight direction, reclining backrest)
One Divan crashworthy seat leather covered (with inertial reels and 4 ea safety belts and
understorage compartment )
2 lateral covered armrests cabinets with metal cup holder, ICS control and multipurpose
holder installed on the divan seat )
2 additional standard crashworthy seats leather covered, including dedicated carpeting
Headsets Bose ANR type with Bluetooth capable
Multipurpose Cubby with sliding doors
Night curtain cabin separator
Passenger cabin hinged doors
Air conditioning system (Enviro)
ICS in the cabin for all passengers (ICS phone to speak with pilots)
Passenger cabin thermo acoustic double layer tinted windows
Two 115V AC power outlets in cabin and one 28V DC power outlet in cockpit
VVIP Ultrasilent soundproofing
Cockpit tinted upper windows (smoked colour)
Co-pilot hinged window
Pilot headset hooks (Qty 2)
Approach plates chart holders with lights for pilot and co-pilot

Metallic Paint (beige) with black and gold stripes.

Forced fan ventilation
Bleed air heater and defroster with air noise
suppressions
Cockpit air ventilation system
Baggage compartment cargo tie-down fittings
for increased load capacity (up to 300 kg)
Rotor brake
1st radar altimeter RT-300
2nd radar altimeter RT-300
4-axis dual Digital Automatic Flight Control
System
(DAFCS) Basic incorporated into Modular
Avionic Units
(MAUs)
Flight Director System (dual) incorporated into
the Modular Avionic Unit (MAU)
Two Honeywell GPS modules (GNSS/SBAS –
Global Navigation Satellite System/Satellite
Based Augmentation System) with Flight Plan
Management System (FPMS)
One Mode S diversity transponder with
Extended Squitter (ADSB-Out 1090 MHz)
incorporated into the Modular Radio Cabinet
(MRC)
Cockpit Voice Recorder & Flight Data Recorder
(CVR/FDR) with Underwater Locator Beacon
(ULB)
Health & Usage Monitoring System (HUMS)
Increased Gross Weight - 7000 kg

Auxilary Fuel Tanks (132 USgal)
Emergency Floats provisions, removables and Kevlar covers)
Camera on Tail Fin
Under Belly Cameras (2 ea)
Auxiliary heavy duty battery 27 Ah/28 Ah capable of paralled starting with
44Ah
battery, in lieu of 13 Ah