2011 AIRBUS H135
Aircraft Summary
General
Year
2011
Manufacturer
AIRBUS
Model
H135
Condition
Used
Description
Beautiful H135 available for sale and ready for inspection in China.
Make your offer if interested.
Airframe
Total Time
100
Airframe Notes
Basic Equipment
-Dual Controls
-Bleed Air Heating System
-Skid Gear with LH and RH Long Boarding Steps
-Reinforced Rear Landing Gear Cross Tube
-LH and RH Sliding Doors
-7’’ Copilot Instrument Panel with Glare Shield
-Slant Panel
-Center Console
-Avionics Compartment
-Engine Fire Detectors
-Engine Fire Extinguishing System
-Electronic Engine Control (FADEC-Box)
-Chip Detectors with Quick-Disconnect Plugs
-Overspeed Protection System
-Yaw-SAS (Stability Augmentation System)
-SAFT Battery, ULM, 40 Ah, 24V
-AC System (50VA)
-Starter Generator (2x 200A, 28V DC)
-Map Case in Copilot Door
-Map Cases on Instrument Panel Glare Shield
-Illuminated Chart Holder for Pilot Side
-Lighting :
oAnti-Collison Warning Light (Red Flashing)
oFixed Nose-Mounted Landing Light (250 W)
oThree Position Lights (Red, Green and White)
oAdjustable Instrument Lighting
oOne Utility Light in the Cockpit
o5 Spot-Lights in the Cabin
oOne Light in Cargo Compartment RH Side
-Flashlight Copilot Side
-Landing and Search Light, 450 W
-First Aid Kit
-Portable Fire Extinguisher
-Ground Handling Kit (Includes : Two Ground Handling Wheels, Basic Aircraft Covers (Short Time), Main Rotor Blade Tie Down Lash Bags, Oil Drain Hoses, Fuel Tank Drain Device, Keys for Cockpit, Cabin and Baggage Compartment Doors and Tank Flap (One-Key System), Battery Key, Lifting Points)
Engine 1
Engine 1 Manufacturer
PRATT & WHITNEY
Engine 1 Time
100
Engine 1 Notes
Pratt & Whitney PW206B2
Engine 2
Engine 2 Manufacturer
PRATT & WHITNEY
Engine 2 Time
100
Engine 2 Notes
Pratt & Whitney PW206B2
Avionics
Avionics/Radios
Basic Avionics / Instruments
-Central Panel Display System (CPDS) consisting of :
oCaution Advisory Display (CAD) with Indication of :
Caution and Advisory Information
Fuel Quantity Indication
oVehicle and Engine Multifunction Display (VEMD) with Indication of :
Torque
Engine Parameters
FLI (First Limit Indicator) for TQ, TOT, N1 as Analog Display
Main Transmission Parameters (Oil Pressure and Oil Temperature)
Dual Ammeter (Generator)
Ammeter (Battery)
Dual Voltmeter
Outside Air Temperature (OAT)
Automatic In Flight Power Check
Parameters of Optional Equipment (e.g. Internal Long Ranger Fuel Tank)
oClock (2”)
oMagnetic Compass
oEngine Cycle Counter (On Flight Report Page)
oTriple (Rotor and Engines) RPM-Indicator (2”)
oStandard Instruments : (Single Pilot)
Altimeter (2”)
Airspeed Indicator (2”)
oWarning Unit :
Engine Fire Warning with Fuel Emergency Shut-Off
Warning Lights
Aural Warning
oMain Switch Panel :
DC Power Control
Digital Engine Control (FADEC)
oPitot / Static System with Electrical Heated Pitot Tube, Pilot Side
oStatic Pressure Crossover System
oAir Data Computer
Avionics / Instruments
-AV Pack Dual Pilot IFR GC FL Interconnection / Wiring
-FliteLine CVC-151 (Chelton) VHF AM/COM System, Pilot
-FliteLine CVC-151 (Chelton) VHF AM/COM System, Copilot
-FliteLine CCN-955 (Chelton) VHF AM/COM and NAV Control Unit, NVG Compatible, Pilot
-NAT ACP-53 Digital Audio Control System, incl. AMU50, Pilot and Copilot
-Honeywell KRA-405B Radar Altimeter
-Honeywell MST-67A Transponder, Mode S
-Chelton CDM-451 DME Distance Measuring Equipment
-FliteLine CVN-251 (Chelton) VOR/ILS/MKR Navigation System, Pilot
-FliteLine CVN-251 (Chelton) VOR/ILS/MKR Navigation System, Copilot
-Special Eurocopter Avionics/Radio Master Switches
-CMC Electronics CMA-5024 GPS Sensor for CMA-9000
-CMC Electronics CMA-9000 Flight/Navigation Management System
-Goodrich AI-804 DC 2” Standby Horizon with Emergency Battery
-MEGHAS Dual Flight Control Display System (FCDS) (2x SMD 45 / 1x SMD 68)
-MEGHAS Sensor Kit
-Copilot / Pilot Static System (Electrically Heated)
-Video Radar Unit (VRU)
-Digital Automatic Flight Control System (DAFCS)
-Provisions for ANR
-Provisions for GSM Phone (Antenna, 28V DC, Interfacing to ICS)
-Avidyne TAS-620 Traffic Advisory System
-Avidyne TAS-620 Indicator 3” MHD
-Avidyne TAS-620 Interface with EURONAV
-Targa CMA-9000 Data Transfer Unit (DTU) for FMS/NMS
-EuroAvionics RN-6 Digital Moving Map EURONAV IV+, Interfaced with FCDS
-Artex C406-N HM ELT, including NAV Opt.
Additional Equipment
Additional Equipment
Optional Equipment
-Multifunction Handle on the Main Gearbox Cowling (LH and RH)
-Fuzz Burners for Engines
-Engine Outlet Heat Protection
-Engine Compressor Wash Kit
-Tinted Sun Shades for Cockpit Windshield Roof Section
-Tinted Window for Cockpit Doors
-Tinted Windows for Passenger Cabin, including Sliding Windows for Sliding Doors
-IFR Training Screen
-Windshield Wiper System
-Air Conditioning System (New Generation, Mechanically Driven)
-Rotor Brake System
-Fuel Management System (Fuel Flow Meters)
-Settling Protectors
-Snow Skids, Provisions Only
-Strobe Lights, White
-Boarding Step Illumination
-Executive Covers for Controls (Collective and Cyclic)
-Bose AHX34-04 ANR LEMO 28 VDC Headsets, Low Impedance
-Glenair/Lemo ANR Headset Adapter Cable
Interior
Interior Notes
Interior
-Executive Configuration :
oCabin : 2 Front Passenger Seats
2 Rear Passenger Seats
1 Fifth Seat
Armrest in Rear Window Niche, LH and RH
Rear Cabinet
Front Cabinet with Executive Ice Box
Passenger Service Unit (Air Outlets & Reading Lights)
Headsets Holders
Bleed Air Heating Adjustment Knob
Placards Special Plating
LH and RH Cabin Handles
Retractable Coat Hooks (2 each) in Rear Cabin
Variable Tie-Down Net
oCockpit : 2 Pilot Seats in Brown Leather
5-Point Seat Belts
oSeats : Brown Leather
oCarpet : Light Brown (Cabin, Cockpit and Cargo Compartment)
-Enhanced Soundproofing Kit
-Separation Wall for Cabin / Cargo Compartment
-Special Painted Interior
-Door Catch System for Cockpit Doors and the Sliding Doors
-One Hand Latching System for Clam-Shell Doors
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