S07TJb004 · Weather Radar RDR 2000 bendix/King (presented on EfiS) Traffic Avoidance System...

2014 AGUSTA AW109SP GRANDNEWSERiAl NUmbER 22331 – NEW AT fAcToRy

S07TJb004

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2014 agusta aw109sp grandnewS07TJb004

SERiAl NUmbER 22331 – NEW AT fAcToRy




STANDARD EQUiPmENT

Active Noise Reduction (ANR) headsets (pilot and co-pilot)Airframe hour meterbaggage compartment extension (1.9 m)baggage compartment lightscrash-resistant co-pilot seat, fore and aft adjustable, with lap belts and headrestcrew open door actuatorsfirst aid kitfuel drain electrical valvesinternal structural provisions for utility equipmentPortable fire extinguisherQuick disconnecting chip detectorsShoulder harness with inertial reels (pilot and co-pilot)Tail boom strake

ADDTioNAl EQUiPmENT

Dual controlsEngine compartment fire extinguishers (2)fuel cap with key-lockPulsed chip detectorsReinforced windshieldRetractable/rotating landing lightRotor brakeWindshield wipers (pilot and co-pilot) with wiper switch on cyclic grips

3 SiNGlE PiloT ifR (EASA) AVioNic PAcKAGE (cHElToN fliGHT SySTEmS)

Pilot flight/navigation EfiS (2 displays) with embedded fmS, Synthetic Vision (SVS),HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and Remote bug Panel (RbP)co-pilot flight/navigation EfiS (2 displays) with embedded fmS, Synthetic Vision (SVS),HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and Remote bug Panel (RbP)EfiS pilot/co-pilot navigation synchronization switchElectronic Standby instrument System (ESiS)Radio management System (RmS) RTU-4210 collins (Qty 2)VHf/Am #1 VHf-4000b collinsVHf/Am #2 VHf-4000b collinsVoR #l/ilS/ADf NAV-4000 collinsVoR #2/ilS NAV-4500 collinsDmE DmE-4000 collinsTransponder (mode S) TDR-94 collinsRadio altimeter AlT- 4000 collinsAttitude Heading Reference System (AHRS) (Qty 2) with one dual AHRS control panelAir Data Unit (ADU) (Qty 2) APilot GPS chelton (SbAS) interfaced to EfiSco-pilot GPS chelton (SbAS) interfaced to EfiSDigital lcS (two cockpit panels and Audio management Unit)4-axis dual duplex digital AfcS with integrated flight DirectorElectronic clocks (Qty 2)magnetic compass indicators (Qty 2)blT c406-N Hm Artex (with Navigation interface module embedded)




EQUiPmENT

Single central refrigerated drawerSingle drawer (qty 2)Pilot and co-pilot aft holderscurtains in cockpit (upper windows)Weather Radar RDR 2000 bendix/King (presented on EfiS)Traffic Avoidance System TAS-620 Avydine (presented on EfiS)Euroavionics Euronav V digital map interfaced to fmS (presented on 8.4” display)cockpit central monitor 8.4” display for digital mapEnhanced Vision System (EVS) maxViz 1500213 USG crash resistant fuel systems (in lieu of 152 US gall)baggage compartment extension (2.30 m)Emergency floats provisioncustomized painting scheme, metallic colours from company selection

iNTERioR

Air conditioning EcS (Environment control System)Passive vibration absorberPrimer finished cabin walls

PAiNTiNG

Standard colour scheme from company paint selection, solid colour

miScEllANEoUS / GRoUND EQUiPmENT

Air intake/exhaust coversGround tools kit (including tow bar, lifting tool, wheel chocks)Pitot tubes coversTie-down fittings provisions

ADDiTioNAl EQUiPmENT – iNTERioR comPlETioN

VIP InterIor 6 Places IncludIng

Super Silent soundproofingleatherette covered linerscabin double layer acrylic windowsAll seats crash-resistant covered with leather or fabric/leather3 aft facing seats (central bench) with see-through modification and with foldable armrest and glass holder3 fwd facing seats (aft bench) with foldable armrest and glass holder4-point shoulder harness with inertial reels and safety belts for all seatsSeats coversAdvisory, reading and floor courtesy lightsleather bellows on flight controlscabin loudspeakers6 Active Noise Reduction (ANR) headsetsfloor carpetingcarpeting protectioncustomized finishing from ViP available selections




bASic coNfiGURATioN DEScRiPTioN

aIrframe

Aluminium alloy / composite material and bonded panel fuselageSemi-monocoque aluminium alloy tail boomThree-wheeled retractable landing gearTwo hinged jettisonable crew doors (lH and RH)Two sliding passenger doors (lH and RH), 1.40 m opening, with jettisonable windowsAcrylic windshield and side windowsAcrylic overhead windowsQuick removable tail rotor drive shaft coverSeparate baggage compartment with hinged doorRemovable fairing and cowlings, for complete accessibility to the controls and drive componentsSwivelling front wheel with tow bar attachmentQuick opening hinged inspection doors, to allow Visual check of engine oil levels and maintenance inspection pointsGrounding pointsJacking and hoisting points

rotors and controls

Titanium main rotor hub, corrosion protected, fully articulated with four composite grips, four elastomeric bearings, four individually interchangeable composite material blades, swept tips, and dampersSteel tail rotor hub, corrosion protected, semi-rigid delta hinged type, with two compositeblades, individually interchangeablecyclic and collective controls powered by two hydraulic systemsHydraulically powered anti-torque systemAdjustable friction devices on cyclic and collective systemforce trim and artificial feel systemAdjustable directional control pedalsflapping and droop restraint mechanismco-Pilot brake controls (in addition to the Pilot standard ones)

Power Plant and fuel system

Two Pratt & Whitney canada PW207c turbo-shaft enginesTwo independent electronic control systems (fADEc) with normal emergency and trainingoperation modes and auto-startEngine mounted fuel pump and filter assemblyEngine mounted oil pump and filter assemblyEngine mounted fuel control and governorlubrication and cooling systemEngine oil chip detectors (2)Engine control panelTwo independent fuel systems with cross-feeding valve and control panel3-cell crash-resistant fuel system (575 l - 152 USgal)Submerged fuel boost pump (2)Airframe mounted easy access fuel filterRH refuelling pointGround fuel drains

transmIssIon drIVe system and hydraulIc system

960 shp for takeoff and 900 shp continuous operation main transmissionThree-stage transmissionfreewheeling units (2)Transmission mounted hydraulic pumps (2) with separate reservoirinternal dry sump transmission lubrication with pressure and scavenge pump and oil filterTransmission oil chip detectors (2)Single stage, bevel gear T/R 90° gear box including oil level sight glass and chip detectorTransmission cooling and lubrication systemTransmission shafts




bASic coNfiGURATioN DEScRiPTioN (coNTiNUED)

electrIcal system

24 V Dc 33 Ah nickel-cadmium battery with temperature probe200 A self-cooled starter generators (2)Voltage regulators (2)battery relaylnterconnecting bus relays (2)Extemal power relayDistribution buses (i battery, 2 essential, 2 emergency, 2 main)External power receptaclePosition lightsTaxing lights (2) and landing lights (2) on landing gear sponsonsAnti-collision lights (2)cockpit utility lights (2)instrument lights with dimming switchRadio master switch with ground function

flIght/naVIgatIon Instruments

lcD integrated Display System (iDS)Pilot flight/navigation EfiS (i PfD) with embedded fmS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and Remote bug Panel (RbP)Attitude Heading Reference System (AHRS) (i)Air Data Unit (ADU) (1)magnetic compass indicator (1)Electronic clock (1)

exterIor fInIshIng

finishing in accordance with manufacturer specification (NTA 893 A)Primer exterior painting

InstrumentatIon (on Ids dIsPlay)

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) indicatorTwo engine oil pressure (PSi) and temperature (°c) indicatorsTwo fuel pressure indicators (PSi)Two fuel quantity indicators (kg)Two fuel flow indicators (kg/hr)Two flight controls hydraulic system pressure indicators (PSi)Two utility hydraulic system pressure indicators (PSi)outside air temperature indicator (°c)Two Ac voltmeters (VAc)Two Dc voltmeters (VDc)Two Dc ammeters (Amp)

warnIng/cautIon adVIsory and maIntenance system

master warning lightsmaster caution lightsWarning, caution and advisory messages (on iDS display)Aural warning generator systemEngine fire detection systemExceedance recorder system (on iDS display)

InterIor arrangement

crash-resistant pilot seat, fore and aft adjustable, with lap belts and headrestAluminium alloy honeycomb reinforced floor with anti-skid finishingVentilation ram air inletsAnti reflection instrument panel






















Date post:	19-Jul-2018
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S07TJb004 · Weather Radar RDR 2000 bendix/King (presented on EfiS) Traffic Avoidance System...

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