Opis:

EC145
YOM: 2008
TTSN: 3,553 Hours
Flight Rules: SP / DP IFR
Mission: Pax Transport
Status: In operation
Availability: Immediate

Airframe:
Dual Controls
Emergency Floats (FP+RP)
Bleed Air Heating System
Air Conditioning System (Aircom)
Jettisonable Cockpit Doors
42Ah Lead Acid Battery (STC Australia)
Fuzz burner for engines
Strobe light, white
8500 Analyser (FP)
Tinted Sunshades for Cockpit Windshield Roof Section
Chip detectors for tail rotor & IGB
MEGHAS Sensor Kit
Sliding Door
Search Light
Inlet Barrier Filter (AA - Australia)
Additional Electrical Unit for 400/ 200W Light
Cabin Configuration: 8 club seats
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Avionics/Radios:
Dual FCDS SMD45 (2) & SMD68 (1)
GPS/NAV/COM System Garmin 430 (2)
AudioControl System ACU 1600-2-120 (2)
High Impedance IC Amplifier Becker IC 3100-4-01
Marker Beacon receiver/lights Honeywell KR21
DME Chelton DMS-44A
Transponder Mode S Garmin GTX330
Standby Attitude Indicator AI804DC
ELT with NAV option Artex C406-NHM
Radar Altimeter Honeywell KRA405B
AFCS 3 axis
ADF Chelton DFS 43A
Weather Radar (FP)
Video Radar Unit for Weather Radar Indication
VHF FM programmable Radio NAT NPX138
SkyTrac System ISAT100
Emergency Power Supply PS-835C
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Inspection Status:
12-Months Inspection on Airframe due in June 2015
800-Months Inspection on Airframe due in April 2016