Description of the engines:
Engine 1 cycles 2,075 IMP/2,152 CT/2,493 PT
Engine 2 cycles 1,988 IMP/2,029 CT/2,489 PT
Avionics:
Moving Map Euronav V
Lightning detector system Honeywell LSZ-860
Weather radar Primus 660 Honeywell
TCAS 1 KTA-970 Honeywell Bendix/King
EGPWS
Transponder x2
DME x2
GPS x2
4 axis enhanced DAFCS with hover mode
5th central display SIRIO in cockpit
SATCOM Iridium ST3100 Aircell
PFD and MFD x2
AHRS x2
Air data modules x2
Flux valves x2
Display controllers x2
Cursor control devices x2
Reversion control panel
Display dimming control panel
SAS control panel
Remote instrument controllers x2
Modular avionic units x2
Vehicle monitoring system x2
Monitor warning system x2
Aural warning generator
Central maintenance computer
Provision for CVR/FDR data interface
Flight director system x2
Pilot and Co-pilot interphone control cyclic grip and floor
switches
VHF COMM x2
VOR/LOC/GS/MB x2
ADF
Multi control function display units
Radar altimeter RT-300 x2
Emergency Locator Transmitter (ELT)
One Flight Guidance Controller
Pilot and co-pilot digital audio panels with remote ICS audio
port for ground operation
Clock x2
Magnetic compass
Outside air temperature indicator
Master warning lights x2
Two master caution lights x2
Engine fire light x2
Baggage compartment smoke detector light
CVR/FDR with ULB
Equipment:
IBF
Camera on tail fin
Pilot and co-pilot approach plates charts holders
Pilot and co-pilot headset hooks
Emergency floats provisions
Auxiliary heavy-duty battery 27 A/H
Auxiliary transversal fuel tank 132 USG provision
Secondary swivelling landing light
Separation wall rolling curtain
Cockpit entrance/exit handle
Co-pilot storm window
Cockpit tinted upper window
Leather pocket on separation wall
Painted pockets in pilot & co-pilot doors
Passenger cabin hinged doors with specific ceiling and liners
Electrically operated passenger's steps RH and LH with boarding lights
Separation wall sliding window
Nose landing gear doors
AVCS
Passenger cabin thermo acoustic double layer tinted windows
ICS in cabin for all passengers
Air conditioning
Super silent soundproofing
New "'Silent Shell cabin interior liners leatherette covered
Other comments:
YOM 2010
Total Time 1,720 hours/2,789 landings
Configuration VIP
Engine 2x PT6C-67C
Avionics Phase 7
Flight rule Dual Pilot IFR
Crew/passengers 2 crew/6 passengers
Engine 1 TT 1,720 hours
Engine 1 cycles 2,075 IMP/2,152 CT/2,493 PT
Engine 1 TT 1,720 hours
Engine 1 cycles 1,988 IMP/2,029 CT/2,489 PT
MTOW 6,800 kgs
Highlights
Air conditioning
Super silent soundproofing
AVCS, HUMS, IBF
Electrically operated passenger's steps RH and LH
Auxiliary transversal fuel tank 132 USG provision
Emergency floats provisions
CVR/FDR with ULB, EGPWS
4 axis enhanced DAFCS with Hover mode
Moving Map Euronav V
Lightning detector system Honeywell LSZ-860
Weather radar Primus 660 Honeywell
TCAS 1 KTA-970 Honeywell Bendix/King
