Global Jet Sales

Global Jet Sales
Aircraft Sales and Acquisitions ~ Over 45 Years of Excellence
FLORIDA
111 Second Ave NE, Ste 103
St. Petersburg, FL 33701
Office: +1 727 864 9443
[email protected]
Pat Janas / Alexander Janas
Garrett Burke / Dave Linnemeier
Brandon Carter / Jason Windle
VIRGINIA
12 Culpeper St
Warrenton, VA 20186
Office: +1 540 351 0008
Mobile: +1 540 229 4653
[email protected]
Townsend Lunsford
Asian Partner
Ste 802A, Level 8, Liberty Square Bldg
287 Silom Road, BANGKOK, 10500 THAILAND
Mobile: +66 8 1735 1500 ~ [email protected]
Trevor Merszei
Agusta A109E
s/n 11618
•One Corporate Owner
•Single Pilot IFR
•Very Well Equipped
Global Jet Sales - United States
JetSearch.com ~ [email protected]
OrientSKYs - Asia
OrientSkys.com ~ [email protected]
Asian Partner
United States
[email protected]
2004 A109E
[email protected]
S/N: 11618
$MAKE OFFER
AirFrame
Engines
CAMP
2868 Hours since New
Engine 1
Engine 2
8614 Landings
P&W 206C
2868 SNEW
2868 SNEW
Avionics
Special Features
SEE EXECUTIVE SUMMARY
FOR FEATURES/AVIONICS
Exterior 12/2004
WHITE, DRK BLUE METALLIC, JADESTONE METALLIC
Interior 2004
FIVE PASSENGER INTERIOR. 3 FWD FACING, 2 AFT FACING, CENTER CREDENZA W/NAT ICS CONTROL
PANEL & 12 VOLT POWER POINT. ENTERTAINMENT INCLUDES 5 EA BOSE AVIATION HEADSET X
UNITS FOR PAX.
Weights
MTOGW: 6,614
RAMP:
ZFW:
LANDING:
BOW:
EMPTY: 4,530
FUEL WT:
FUEL CAP:
Printed On: January 21, 2014
Last Updated On: 1/20/2014
PRELIMINARY SPECIFICATION ONLY ~ Verification Upon Inspection ~
United States
[email protected]
EXECUTIVE SUMMARY
Asian Partner
[email protected]
Last updated on 01/21/2014
AGUSTA A109E: S/N 11618
Avionics:
 4 ea Kratos/Rogerson EFIS (EADI // EHSI) p/n 160E015-3 (All interchangeable).
 2 ea Garmin GNS530A Comm/Nav/GPS, IFR approved (RFM Supplement # FM00906).
 Garmin Transponder GTX330, Mode S with Traffic Information Service, no audio.
 Garmin MX-20 Multi Function Display, with Shadin Altitude Serializer (p/n 9000M)
 Skywatch SKY497 TAS (displayed on the MX-20), consisting of Skywatch TRC 497
computer, Sensor Systems Directional Antenna (p/n 805-10890-001).
 Flight Director (autopilot) FZ-702 computer.
 2 ea HeliPilot computers (autopilot and SAS system) SP711
 Davtron clock
 DME Receiver (KDM – 706A)
 Marker Beacon Receiver (KMR – 675)
 Encoded Altimeter Indicator, Altimeter Ind., and Vertical Speed Indicator.
 Standby Altimeter Indicator, Airspeed Indicator, and Vertical Speed Indicator.
 Honeywell Radar Altimeter Trans/Receiver (RT-300)
 2 ea AMETEK Information Display Indicators
 1 ea AMETEK Data Acquisition Unit computer.
 Weather Radar ART 2000 Antenna /Transmitter
Additional Features:
 Acft. increased Max Gross Weight to 3000 kg. (STC # SR01848NY)
 Whelen wing tip position and strobe lights on LH/RH elevators.
 Recognition and boarding lights, LH/RH.
 Precise Pulselight System for sponson lights & recognition lights (STC # SH3319NM)
 LH cabin retractable boarding step.
 Supplementary Auxiliary Fuel tanks (TC optional kit.)
 Sponson Lights kit. ( TC kit )
 Pulsed Chip Detector system (TC kit)
 Reinforced, bird resistant wind screens.
 TC’d removed windshield wipers.
 Whelen LED anti-collision lights (upper & lower)
 12 VDC Power System in cockpit and cabin for crews and passengers.
 Cockpit and Cabin NAT ICS System.
 Aircell ST 3100 SAT phone System
 Airconditioned – Normalaire ECS pack and water separator system.
 Heads Up Technologies Passenger Briefing System.
 Chadwick/Honeywell VXP Vibration Monitoring System & Equipment.
 Artex C406-N HM ELT.
 Reinforced Tail Rotor Drive Shaft cover assy.
 Latitude Technologies SKYNODE Aircraft Tracking System
 Engine Fire Control System (optional)
 Composite Tail Rotor Blades (optional EP-47)
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PRELIMINARY SPECIFICATION ONLY ~ Verification Upon Inspection ~