2012 AW109 SP
The AW109SP ‘Grand New’ is the latest incarnation of the very popular AW109 series. Building on the 109 ‘S’, the SP introduces an all new avionics suite including an integrated FMS and a 4 axis autopilot, culminating in its certification as a PBN compliant aircraft. Without doubt, the SP is one of the most capable & high-speed corporate helicopters available in its class.”
Price
Specification
Year: 2012
Price: Price on request
Serial Number: 22383
Registration: G-OATL
Condition: Pre-owned
Total Time: 820 Hrs
Airframe Landings: 2184
Maintenance: Up to Date
Performance
Crew: 1
Max Passengers: 7
Max Take-Off Weight: 3175 KG
Cruise Speed: 155 Knots
Max Range: 450 NM
Max Altitude: 19000 FT
Take-Off Distance: N/A FT
Landing Distance: N/A FT
Power
Engines: 2 x Pratt & Whitney PW207C
Engine Hours: 820
APU: Not Available
APU Hours: 0 Hrs
Exterior
Exterior: Artic White / Red & Black Decals Emergency floats provisions 213 us gal crash-resistant fuel system (in lieu of 152 US gal) Baggage compartment extension (2.3m) Engine compartment fire extinguisher (qty 2) Fuel Cap with Key-Lock Pulsed Chip Detectors Rotor Brake Retractable/Rotating Landing Light (nose mounted) Retractable/Rotating Landing Light (nose mounted) Ground Equipment Air Intake / Exhaust Covers • Tow bar and chocks Pitot covers Rotorcraft Flight Manual (RFM) and Technical Publications Tie-downs
Interior
Interior: VIP/Corporate interior – 5 places All seats crash-resistant covered with leather 4-point Shoulder Harness with Inertia reels and Safety Belts for all seats Set of 3 drawers Super Silent Soundproofing Intercommunication system for passengers Headset BOSE ANR type (qty 5) Cabin loudspeakers (qty 2) Air conditioning ECS (Environment Control System) Reading lights, emergency lights, floor courtesy lights Upper and Lower Air Vents Floor Carpeting Seat Covers
Avionics
Standard Avionic Equipment: COMM/NAV/GPS unit GARMIN 530 & 430,
Moving map display,
COMM/NAV/GPS unit,
Electronic Attitude Director Indicator (EADI),
Marker Beacon (MB) control panel,
Distance Measuring Equipment (DME) control panel and indicator,
Flight Director (FD) control panel,
Audio control panel,
Electronic Horizontal Situation Indicator (EHSI),
Electronic Display Unit (EDU),
Pilot / copilot flight navigation EFIS (4 display),
Type KT 73 Mode S transponder,
Autopilot 3 axis dual duplex AFCS, integrated Flight Director,
TRC-497 (TICAS) transceiver - receiver,
GNS 430 and 530 / VHF / VOR,
RDR-2000 Weather Radar kit,
Sky Force Moving Map,
Stormscope,
Type RT-300 radio-altimeter,
Artex C406-2HM ELT,
Additional Avionic Equipment: Dual / Single IFR package
Pilot Flight/Navigation EFIS (2 displays)w/embedded FMS,
Synthetic Vision (SVS), HTAWS, slip indicator and bug panel (rbp)
Co-pilot flight/navigation EFIS (2 displays) w/ embedded FMS,
Synthetic Vision (SVS), HTAWS, slip indicator and bug panel (rbp)
EFIS pilot / co-pilot navigation synchronization switch (FMS data)
Electronic standby instrument system (ESIS)
Second radio management system (RMS) RTU-4210 Collins
Radio manager system (RMS) RTU-4210 Collins
VHF/am VHF-4000e (2 units)
VOR/ILS Nav-4500 Collins
VOR/ILS/ADF/Nav-4000
Collins • 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 with integrated Flight Director
Second electronic clock
Second magnetic compass indicator
ELT C406-N HM Artex (w/ navigation interface module embedded)
8.4 Cockpit central Display
Enhanced Vision System (EVS) EVS-1500 Max-Viz on 8.4 display
Digital map EURONAV V Euronav Avionics interfaced to FMS on 8.4’ display
Weather Radar RDR 2000 Bendix/King (presented on EFIS)
Transponder (mode S) TRD-94 Collins
Attitude heading reference system (AHRS) w/ one dual AHRS control panel
Air data unit (ADU)
Digital audio control system (DACS) Cobham w/ additional cockpit panel
Magnetic sensor unit
LCD integrated display system (IDS)
Dual gas generator speed indicator (N1%)
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) and temperature ( ̊c) indicator
Two engine oil pressure (psii)and temperature ( ̊c) indicators
Two fuel pressure indicators (psi)
Two fuel quantity indicators (kg)
Two fuel flow indicators (kg/ hr)
Two flight controls hydraulic system pressure indicators (psi)
Outside air temperature indicator ( ̊c)
Two AC voltmeters
Two DC voltmeters
Specifications and details are subject to verification upon inspection. Aircraft is offered subject to prior sale or withdrawal from the market.