2016 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
SOLD
Specification
Year: 2016
Price: Price on request
Serial Number: 22355
Registration: G-PIFZ
Condition: Excellent Pre Owned (1 Owner from New)
Total Time: 980 Hrs
Airframe Landings: 2113
Maintenance: Excellent Component Times JSSI Airframe & Engine Programs
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: 980
APU: Not Available
APU Hours: 0 Hrs
Exterior
Exterior: Exterior Gunmetal Grey / Mclaren Orange (metallic)
Interior
Interior: Corporate interior – 6 places All seats crash-resistant covered with leather 3 fwd facing seats with foldable armrest and glass holder 3 aft facing seats (central bench) with see- through modification and foldable armrest and glass holder Forward facing side armrest Single central drawer Super Silent Soundproofing Acoustic screen around doors Intercommunication system for passengers Headset BOSE ANR type (qty 6) Cabin loudspeakers (qty 2) Reading lights, emergency lights, floor courtesy lights Carpeting protection ADDITIONAL EQUIPMENT Airframe hourmeter Baggage compartment extension (2.3m) Engine compartment fire extinguisher (qty 2) Pulse chip detectors Reinforced windshields Retractable/rotating landing light Air conditioning ECS Electrically operated passenger step (RH) 213 us gal crash-resistant fuel system (in lieu of 152 US gal) Emergency floats provisions High-intensity white strobe lights on horizontal stabilizer
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/ one 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 voltimeters
Two DC voltimeters
Two DC altimeters
Specifications and details are subject to verification upon inspection. Aircraft is offered subject to prior sale or withdrawal from the market.