Description of the engines:
Engine 1 cycles 7,812 N1/5,372 N2
Engine 2 cycles 5,350 N1/8,276 N2
Avionics:
KX196A COMM
KX165 COMM
ADF
Transponder
Altimeter x2
Radar altimeter
ELT
Artificial horizon x2
ICS
Gyro horizon
Emergency gyro horizon
Marker
Alticoder
Compass gyro
Slip indicator
VOR/LOC/GLIDE
HSI
RMI
GPS
Equipment:
Dual flight control
Emergency floats fixed parts
Cargo swing fixed parts
Engine fire extinguisher system
Dual sliding door
Windshield wiper provisions
Cabin heating system
Defog system
High landing gear
Crew high seats
Soundproof trimming
Additional battery for cold weather
Swiveling light
Retractable landing light
Crew and passenger internal lights
Additional battery for cold weather
Chip detector MGB and TGB
DART short step
Fire extinguisher x2
Extender rear baggage
Other comments:
YOM December 1991
Total time 9,678 hours/20,300 cycles
Configuration Corporate
Engine Arrius 1A x2
Flight rules SP VFR
Highlights:
Delivered with fresh 12 Y inspection
Engines under SBH program
Dual flight control
Emergency floats fixed parts
Cargo swing fixed parts
Dual sliding door
Cabin heating system
High landing gear
Soundproof trimming
Additional battery for cold weathe
