Bell 430

INTEGRATED INSTRUMENT DISPLAY SYSTEM (IIDS)
DUAL ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS)
PILOT EFIS (4-TUBE / GPS / FLIGHT DIRECTOR)
COPILOTS EFIS (GPS)
SINGLE AFCS (AUTOMATIC FLIGHT CONTROL SYSTEM), EFIS (4 TUBE)
NAV 1 (EFIS)
NAV 2 (EFIS)
DME (EFIS)
MODE S TRANSPONDER (AFCS)
ADF KDF 806 (SKID)
KRA-405 RADAR ALTIMETER
GPS NAVIGATION SYSTEM (ADC, 4 EFIS)
STANDBY ATTITUDE INDICATOR
VERTICAL SPEED / ALTIMETER
AIRSPEED INDICATOR
FREE AIR TEMPERATURE INDICATOR
BENDIX KING KEA 130A ENCODING ALTIMETER
COMPASS
CVFDR (COCKPIT VOICE & FLIGHT DATA RECORDER)
ELT (EMERGENCY LOCATOR TRANSMITTER)
DUAL VHF COMMUNICATION RADIOS
NAT AUDIO PANELS
NAT INTERCOM SYSTEM (ICS)
FLEXCOM II COMMUNICATIONS SYSTEM

CARGO HOOK PROVISIONS
CARGO HOOK EQUIPMENT
CARGO LIFTER – X 2 UNITS
PASSENGER SLIDING DOOR
PHOTO WINDOW
RAPPELLING FIXTURE
WIRE STRIKE PROTECTION SYSTEM (WSPS)
HEATED WINDSHIELDS
10-PLACE UTILITY SEATING CONFIGURATION
SKID GUARD KIT
LANDING LIGHT KIT
BLEED AIR HEATER
RESCUE HOIST PROVISIONS – X 2 UNITS
UPPER AUXILIARY FUEL PROVISIONS
PARTICLE SEPARATOR
DUAL CONTROLS
ECS (ENVIRONMENTAL CONTROL SYSTEM)
INTERIOR UTILITY PACKAGE
SOUNDPROOFING PACKAGE
CREW SEATS – UTILITY CONFIGURATION

CREAM LEATHER/UTILITY CONFIGURATION

RED WITH BLUE TRIM

LOW TIME
EXTENSIVE SPARES PACKAGE
GROUND SUPPORT EQUIPMENT INCLUDED
UTILITY MISSION READY

ROLLS ROYCE 250-C40B
ENGINE #1/#2
TTSN: 2,569/2,569

REMAINING:
TURBINE: 912/912
STAGE 1 WHEEL: 937/937
STAGE 2 WHEEL: 937/937
STAGE 3 WHEEL: 1,980/3,712
STAGE 4 WHEEL: 1,980/1,980

REMAINING:
TRB: 4,284
TGB: 2,430
MGB: 2,430
MRB: ON CONDITION