For Sale
The A109S Grand is a lightweight twin-engine helicopter, known for its speed, elegant appearance and ease of control. This specific model is a popular choice for VIP/corporate customers.
YEAR
2009
TTAF
1020
LOCATION
Europe
AVAILABILITY
Immediate
PRICE
PRICE ON REQUEST
Features
Notes/highlights
- Very Low Time
- Air Conditioning, Weather Radar, TCAS
- Fixed Part For Floats
- Hoist and Hook
- Engines are on P&W ESP Gold Program
Avionics
- Copilot flight/navigation instruments (LCD EADI and EHSI, barometric altimeter, airspeed indicator, VSI)
- Gyrocompass C14 Honeywell
- Vertical gyro #1 46060-11 Flightline System
- Vertical gyro #2 VG-208 JET Electronics
- 3-axis duplex AFCS SP711 Honeywell
- ADF KR 87 Bendix/King
- Transponder (mode S) KT 73 Bendix/King
- VHF#1 COM/NAV/GPS GNS 530 Garmin
- VHF#2 COM/NAV/GPS GNS 430 Garmin
- DME KDM 706A Bendix/King
- Marker beacon KMR 675 Bendix/King
- Pilot ICS (including pilot/copilot control panel. mode controller. audio cabin control)
- AC power supply system (two inverters)
- Copilot flight/navigation instruments (LCD EADI and EHSI. barometric altimeter airspeed indicator. VSI)
- Flight director FZ 702 Honeywell with autotrim
- Radio altimeter AA 300 Honeywell
- ELT C406-2HM Artex
- Moving map KMD 550 Bendix/King
- Radio master switch with ground function
- EFIS pilot/copilot in command switch
- Moving Map MKII Observer (Sky Force)
- TCAS SKY 791 (BF Goodrich)
- Weather Radar presented on pilot/copilot EHSI RDR 2000 Bendix/King.
- Two (2) independent electronic control systems (FADEC) w/ emergency & training operation modes & auto start
- Airspeed indicator
- Instantaneous vertical speed indicator
- Barometric encoding altimeter
- Magnetic compass indicator
- Clock. 8 days and elapsed time
- LC Integrated Display System (IDS)
- Master Warning & Caution lights
- Engine fire detection system
- Aural Warning Generator system
- Exceedance recorder system (on IDS display)
Interior and exterior
- Interior: Soundproofing PAULSTRA VIP Interior (5 places) including leatherette covered or painted liners. 3 seats aft facing central bench and see-through with foldable armrest and 2 seats aft bench fwd facing with central cabinet/bar. Additional amenities include advisory, reading and floor courtesy light, Floor carpeting, Cabin double glass windows, Two individual crash-resistant pilot seats fore and aft adjustable with lap belts, Aluminum alloy honeycomb reinforced floor with anti-skid finishing, Ventilation ram air inlets, passive vibration absorber
- Exterior: Beige paint scheme with dark stripes
Optional equipment
- Air conditioning ECU Garret
- Emergency floats provision
- Structural provision for utility equipment (emergency floats, rescue hoist, cargo hook)
- Reinforced windshield
- 213 US gall. Fuel system
- Baggage compartment extension (to 1.9 m)
- Engine compartment fire extinguishers
- Baggage compartment extension (2,3 mt)
- Baggage compartment light
- Pilot and copilot shoulder harness with inertia reel
- Crew open door actuators
- Quick disconnecting chip detectors
- Pulsed chip detector
- Fuel drain electrical valves
- Tail boom strake
- Airframe hour meter provision
- Dual control
- Rotor brake
- 450 W Retractable/Rotating landing light
- Pilot and copilot windshield wipers
- Wiper switch on pilot cyclic grip
- Rotorcraft Flight Manual and technical publications
- Hook for Jacket (nr. 2) right and left in pax cabin
- Locking fuel cap & Ground fuel drains
- Airframe mounted easy access fuel filter
- Engine oil chip detectors (one per engine)
- Two independent fuel systems with cross-feeding valve and control panel
- 3-cell crash-resistant fuel system (460 kg – 152 USG)
- Submerged fuel boost pump (one per system)
- RH refueling point
- High-intensity strobe lights on horizontal stabilizer
- Ground tools kit (including tow bar. lifting tool. wheel chocks)
- Air intake/exhaust covers
- Pitot tubes covers
- Tie-down fittings
- Portable fire extinguisher
- First aid kit
- Fuel cup with key-lock
- Six (6) Active Noise Reduction (ANR) headsets
Reference number: P-L1EwJYUdLD
The aircraft is operating, why the condition and component times will be subject to changes depending upon such operations. Verification of the condition of the aircraft and its component times shall be the responsibility of the purchaser.
