Agusta AW109SP

Agusta AW109SP
Agusta AW109SP
Agusta AW109SP
Agusta AW109SP
Agusta AW109SP
Agusta AW109SP
Agusta AW109SP
Agusta AW109SP
Agusta AW109SP
Agusta AW109SP

Aircraft Information

Condition: 
New
Year: 
2017
Hours: 
20
Serial Number: 
22365
Registration Number: 
I-EASU
Price: 
Call For Price
Aircraft Description: 

Aircraft Highlights:

  • 6 Pax VIP Interior (Special Edition)
  • Delivery Time Only
  • Warranty 3 Years / 2000 hrs

Please contact Emmanuel Dupuy for more information.
 

Aircraft Information sheet: 
Airframe Information
Airframe: 

TTAF: 20

Landings: 16

Delivery Time Only

Aluminum Alloy/Composite Material & Bonded Panel Fuselage
Semi-monocoque aluminum Alloy Tail Boom
Three-Wheeled Retractable Landing Gear
Two Hinged Jettisonable Crew Doors (LH and RH)
Two Sliding Passenger Doors (LH and RH) w/ Jettisonable Windows
Acrylic Transparent Windshield & Side Windows
Acrylic Transparent Overhead Windows
Quick Removable Tail Rotor Drive Shaft Cover
Separate Baggage Compartment w/ Hinged Door
Removable Fairing & Cowlings, For Access To Controls & Drive Components
Swiveling Front Wheel w/ Tow Bar Attachment
Quick Opening Hinged Inspection Doors
Grounding Points
Jacking & Hoisting Points

Engine(s) Information
Engine(s): 

Rotors & Controls
Titanium Main Rotor Hub, Corrosion Protected
Steel Tail Rotor Hub, Corrosion Protected, Semi-Rigid Delta Hinged Type
Cyclic & Collective Controls Powered by Two (2) Hydraulic Systems
Hydraulically Powered Anti-Torque System
Adjustable Friction Devices on Cyclic & Collective System
Force Trim & Artificial Feel System
Adjustable Directional Control Pedals
Flapping & Droop Restraint Mechanism

Power Plant & Fuel System
Two (2) Independent Electronic Control Systems (FADEC)
Engine Mounted Fuel Pump & Filter Assembly
Engine Mounted Oil Pump & Filter Assembly
Engine Mounted Fuel Control & Governor
Lubrication & Cooling System
Two (2) Engine Oil Chip Detectors
Engine Control Panel
Two (2) Independent Fuel Systems w/ Cross-Feeding Valve & Control Panel
Six (6)-Cell Crash-Resistant Fuel System (575 I -152 U.S. Gal)
Submerged Fuel Boost Pump (2 each engine)
Airframe Mounted Easy Access Fuel Filter
RH Refueling Point
Ground Fuel Drains

Transmission Drive System & Hydraulic System
960 shp For Takeoff & 900 shp Continuous Operation Main Transmission
Three-Stage Transmission
Two (2) Free Wheeling Units
Dual Independent Redundant Hydraulic Systems
Two (2) Transmission Mounted Hydraulic Pumps w/ Separate Reservoir
Two (2) Ripple Dampers
Dry Sump Transmission Lubrication w/ Pressure & Scavenge Pump & Oil Tilter
Two (2) Transmission Oil Chip Detectors
Single stage, bevel gear T/R 90° Gear Box, Oil Level Sight Glass & Chip Detector
Transmission Cooling & Lubrication System
Transmission Shafts

Avionics / Radios Information
Avionics / Radios: 

Two (2) Pilot Flight/Navigation EFIS
FMS, Synthetic Vision (SYS) HTA WS
Reversionary Control Panel (RCP)
EFIS Pilot/Co-Pilot Navigation Synchronization Switch (FMS data)
Electronic Standby Instrument System (ESIS)
Second Radio Management System (RMS) RTU-4210 Collins
Second VHF/AM VHF-4000E Collins
VOR/ILS/ADF NAV-4000 Collins
DME DME-4000 Collins
Radio Altimeter AL T-4000 Collins
Second Attitude Heading Reference System (AHRS)
Second Air Data Unit (ADU)
Pilot GPS/SBAS Chelton Interfaced to EFIS/FMS
Co-pilot GPS/SBAS Chelton Interfaced to EFIS/FMS
Digital Audio Control System (DACS) COBHAM Additional Cockpit Panel
4-Axis Dual Duplex Digital AFCS w/ Integrated Flight Director
Second Electronic Clock
Second Magnetic Compass Indicator
ELT C406-N HM Artex (w/ Navigation Interface Module Embedded)
Dual Controls

Flight/Nav Instruments
Pilot Flight/nav EFIS w/ Slip Indicator & Remote Bug Panel (RBP)
Radio Management System (RMS) RTU-4210 Collins (I)
VHF/AM VHF-4000E
VOR/ILS NA V-4500 Collin
Transponder (Mode S) TDR-94 Collins
Attitude Heading Ref System (AHRS) (1) w/ One Dual AHRS Control Panel
Air Data Unit (ADU)
Digital Audio Control System (DACS) COBHAM w/ One Cockpit Panel
Electronic Clock
Magnetic Compass Indicator
Magnetic Sensor Unit
Pitot Tube Right/Left

Warning Advisory & Maintenance System
Two (2) Master Warning Lights
Two (2) Master Caution Lights
Warning, Caution & Advisory Messages (on IDS Display)
Aural Warning Generator System
Engine Fire Detection System
Exceedance Recorder System (on IDS display)
Warning Horn (Cabin)

Instrumentation (On IDS Display)
LCD Integrated Display System (IDS)
Dual Gas Generator Speed Indicator (NI%)
Dual Turbine Outlet Temperature Indicator (TOT°C)
Dual Torque Meter Indicator (TQ%)
Dual Power Turbine Speed Indicator (N2%)
Rotor Speed Indicator (NR %)
Transmission Oil Pressure (PSI) & Temperature Indicator
Two (2) Engine Oil Pressure (PSI) & Temperature Indicators
Two (2) Fuel Pressure Indicators (PSI)
Two (2) Fuel Quantity Indicators (Kg)
Two (2)  Fuel Flow Indicators (Kg/Hr)
Two (2) Flight Controls Hydraulic System Pressure Indicators (PSI)
Two (2) Utility Hydraulic System Pressure Indicators (PSI)
Outside Air Temperature Indicator  
Two (2) AC Voltmeters (VAC)
Two (2) DC Voltmeters (VDC)
Two (2) DC Ammeters (AMP)

Interior / Exterior Information
Interior: 

Interior Arrangement
Crash-Resistant Pilot Seat, Fore & Aft Adjustable, w/ Lap Belts & Head-Rest
Aluminum Alloy Honeycomb Reinforced Floor w/ Anti-Skid Finishing
Ventilation Ram Air Inlets
Anti-Reflection Instrument Panel
Air Conditioning ECS (Environment Control System)
Primer Finished Cabin Walls
Standard Color Scheme from Company Paint Selection, Solid Color

Customer Selected Configuration
Corporate Interior 6 Places
Passenger Cabin
AlI Seats Crash-Resistant Covered w/ Leather or Fabric Leather
Three (3) Fwd Facing Seats (Aft Bench) w/ Foldable Armrest & Glass holder
Three (3) Aft Facing Seats w/ See-Through Mod & w/ Foldable Armrest & Glass Holder
Forward Facing Side Armrests
4-Point Shoulder Harness w/ Inertial Reels & Safety Belts For Passenger Seats
Super Silent Soundproofing
Liners Leather/Leatherette Covered
Acoustic Screen Around Doors
Cabin Double Layer Acrylic Windows
Customized Corporate Cabin Finishing
Decoration Trim w/ Metal Inserts
Intercommunication System For Passengers
Six (6) Headset Bose ANR Type
Two (2) Cabin Loudspeakers
Reading Lights, Emergency Lights, Floor Courtesy Lights
Four (4) Passenger Hooks
Upper & Lower Air Vents
Floor Carpeting
Carpeting Protection
Seat Covers

Exterior: 

Finishing In Accordance w/ Manufacturer Specification (NTA 893 A)
Primer Exterior Painting

Additional Information
Additional Information: 

Electrical System
24 V DC 33 Ah Nickel-Cadmium Battery (19 cells) w/ Temperature Probe
Two (2) 200A Self-Cooled Starter Generators
Two (2) Voltage Regulators
Battery Relay
Two (2) Interconnecting Bus Relays
External Power Relay
Distribution Buses ( I Battery, 2 Essential, 2 Emergency, 2 Main, 2 Aux)
External Power Receptacle
Position lights (NVG Friendly - Green, Red, White)
Taxing Lights (2 RH -2 LH) & Landing (2 RH+ 2 LH) on Landing Gear Sponsons
Two (2) Anti Collision Lights (NVG friendly)
Two (2) Cockpit Utility Lights
Instrument Lights w/ Dimming Switch
Radio Master Switch w/ Ground Function

Miscellaneous/ Ground Equipment
Air Intake/Exhaust Covers
Ground Tools Kit (Including Tow Bar, Lifting Tool, Wheel Chocks)
Pitot Tubes Covers
Rotorcraft Flight Manual (RFM) & Technical Publications
Tie-Down Fittings (Main Rotor Retention Straps)

Standard Equipment
Active Noise Reduction (ANR) Headsets (Pilot & Co-Pilot)
Helicopter Terrain Awareness & Warning System
Single Pilot Dual Controls TFR Avionic Package
Two (2) Pilot Flight/Nav EFIS w/ Embedded FMS
Co-Pilot Flight/Nav EFIS w/ FMS, Synthetic Vision (SVS), HTA WS
Synthetic Vision (SYS), HTA WS Baggage Compartment Lights
Crash-Resistant Co-Pilot Seat, Fwd & Aft, w/ Lap Belts & HeadRest
Crew Open Door Actuators
First Aid Kit
Fuel Drain Electrical Valves
Internal Structural Provisions For Utility Equipment
Portable Fire Extinguisher
Shoulder Harness w/ Inertial Reels (Pilot & Co-Pilot)
Tail Boom Strake
Reversionary Control Panel (RCP)
EFIS Pilot/Co-Pilot Navigation Synchronization Switch (FMS data)
Electronic Standby Instrument System (ESIS)
 Second Radio Management System (RMS) RTU-4210 Collins
Second VHF/AM VHF-4000E Collins
VOR/ILS/ADF NAV-4000 Collins
DME DME-4000 Collins
Radio Altimeter ALT-4000 Collins
Second Attitude Heading Reference System (AHRS)
Second Air Data Unit (ADU)
Pilot GPS/SBAS Chelton Interfaced to EFIS/FMS
Co-pilot GPS/SBAS Chelton Interfaced To EFIS/FMS
Digital Audio Control System (DACS) COBHAM Additional Cockpit Panel
4-Axis Dual Duplex Digital AFCS w/ Integrated Flight Director
Second Electronic Clock
Second Magnetic Compass Indicator
ELT C406-N HM Artex (w/ Navigation Interface Module Embedded)
Dual Controls

Additional Equipment
Airframe Hourmeter
Baggage Compartment Extension (1.9 m)
Two (2) Engine Compartment Fire Extinguishers
Fuel Cap w/ Key-Lock
Pulsed Chip Detectors (In Lieu Of Quick Disconnecting Chip Detectors)
Reinforced Windshields
Retractable/Rotating Landing Light (Nose Mounted)
Rotor Brake
Windshield Wipers (Pilot & Co-Pilot) w/ Wiper Switch On Cyclic Grips

Cockpit Equipment
lnterseat Console Tray w/ 12 V Power Supply
Multipurpose Holder (w/ Space Provision For Fire Extinguisher)
Right Door Pocket
Two (2) Headset Hooks  
Cyclic & Collective Leather Gators
Curtains In Cockpit On Upper Windows

Optional Kits
Traffic Advisory System TAS-620 Avydine (Presented on EFIS)
Weather Radar RDR 2000 Bendix/King (Presented on EFIS)

Contact Information

900 Bestgate Road
Annapolis, Maryland, United States - 21401
Ph: (410) 573-1515

Email Avpro Inc.