Description of the engines:
Engine 1 cycles 5,003 IMP/3,489 CT/4,095 PT
Engine 2 cycles 4,602 IMP/2,999 CT/4,090 PT
Avionics:
Autopilot 4-axis software FDR enhanced
EGPWS Honeywell Mark 22
Weather radar Primus 660
TCAS I Honeywell KTA-970 model
Kit auxiliary battery 27 AH
HF Antenna
PFD and MFD x2
ESIS (attitude, airspeed, altitude, vertical speed, compass and ILS data)
AHRS x2
Air data module x2
Flux valve x2
Display controller x2
Cursor control device x2
Reversion control panel
Display dimming control panel
Stability augmentation system control panel
Remote instrument controller x2
Vehicle monitoring system x2
Monitoring 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/HF Comm x2
Mode S diversity transponder
VOR/LOC/GS/MB x2
ADF
DME
MCDU x2
Radar altimeter RT 300 x2
ELT 121.5/243/406 MHz
Flight guidance controller
Honeywell GPS module with FPMS
Pilot and co-pilot digital audio panels remote ICS audio port for ground operation
Digital clock x2
One magnetic compass
Master Warning Lights x2
Master Caution Lights x2
Engine 1 & 2 Fire Light x2
Baggage compartment smoke detector light
Dual electrical power connection for CVR/FDR
CVR/FDR with ULB
Equipment:
LH and RH electrically operated passengers steps with light
Standard passenger cabin ceiling liners
Composite liners leather/leatherette covered
Dome lights
Moquette finishing on cabin floor
Cabin handles
Cabin loudspeakers
Passenger cabin thermo acustic double layer windows
Ripple damper
Vibration absorber (3rd mass)
Nose landing gear door
Super silent soundproofing
ICS in cabin for all passengers
Air conditioning system
Coat hangers x3
Emergency floats provision
Crew crashworthy seats with inertial reels and safety belts
Cockpit dome/storm light
Cockpit utility lights x2
28 V DC cockpit/cabin power outlet
Cockpit panel sun-glare shields
Overhead cockpit windows sun shades
Floor provisions for 15 seat configuration
Fluorescent lighted emergency exit signs
Cockpit map and data case in central console
Two flash lights for pilot and co-pilot
Map and data cases in pilot and co-pilot doors
ICS panel with plug for one headset
Air ventilation system
First aid kit
Other comments:
YOM 31/1/2007
Configuration VIP
Flight rule IFR
Empty weight 4,643 kgs
MTOW 6,800 kgs
Avionics phase 4
Highlights
LH and RH electrically operated passengers steps
Super silent soundproofing
Vibration absorber (3rd mass)
Emergency floats provision
Air conditioning system
Ripple damper
Moquette finishing on cabin floor
TCAS I, EGPWS, HF Antenna
Autopilot 4-axis software FDR enhanced
