2006 a109s grand for sale

Agusta AW 109S Grand

For Sale

US$ POA

Year: 2006 | TTAF: 532

VIP Interior.

 

Aircraft Delivery Date : December 2006
Airworthiness Certificate (EASA) Date : Oct 6, 2006
Total Time: 532:30 F/H
Total Cys: 1081:00 F/C
Engines Manufacture: PRATT & WHITNEY CANADA
Model: PW207C

 

 

(Engine Lh

(S/N PCE-BH0037)

(Engine Lh

(S/N PCE-BH0034)

TimeSinceNew

532:30HRS

532:30HRS

CT

750CYS

677CYS

PT

816CYS

810CYS

IM

406CYS

396CYS

Last Overhaul

MFG DATE

MFG DATE

O/H Interval(TBO)

3500HRS

Next O/H dueatETT

3500HRS

3500HRS

TimeRemain. To next O/H

2967:30HRS

2967:30HRS

CERTIFIED OPERATIONAL WEIGHTS

Max takeOff(int./loads) 3175kg 7000lb Max takeOff(ext./loads) 3200kg 7055lb Basic Empty Weight1660kg 3660lb

OPERATIONSPECIFICATION

VFR/V;IFR/V;ILS

INTERIOR CONFIGURATION

Basic version:1-2Crew,6Passengers

BASIC HELICOPETERincluding:

•        TwPW207engines with FADEC

•        960SHPTOmain gear box

•        Aluminium allomaiframe

•        Retractabltricycle landing gear

•        Fully articulated 4 bladeT.R. Hub

•        Semi-rigid 2 bladeT.R. Hub

•        Composite Main &Tail Rotorblades

•        Pilot/Co-pilohinged doowith openinactuators

•        Pilot/Co-pilot crasresistant seats

•        Pilot/Co-pilot shoulders harness with inertireel

•        Pilot/Co-pilot heasets (2)

•        1,4mtwide passengers cabin slidindoors

•        15US Gall. Crashr esistant Fuel system

•        Pilotflight instruments, including the following instruments:

-Barometric encodinaltimeter

-Air speeindicator

 -IVSI

-Magnetic compass indicator

-Clock

•        L.C.Integratedisplay system(I.D.S.)

•        Fuedrain electrical valves

•        Quick disconnecting chidetectors

•        Firs aid kit

•        Cabin fire extinguisher

•        27Abattery

    

SINGLE PILOT IFR/FAAAVIONICS PACKAG(king-Germanseries)

ACsyste(2investors)

•        Pilonavigation instruments, includinfollowininstruments:

-LCDEADI &EHSI

-StandbyA

•        Gyrocompass

C14

Honeywell

•        Verticalgyro(No. 1)

46060-11

Flightline System

•        Verticalgyro(No. 2)

VG208

Jet Electronics

•        AFCS3 Axis Duplex

SP711

Honeywell

•        ADF

KR 87

King

•        Transponder (Mode S)

KT 73

King

•        1°VHF-COM/NAV/GPS

GNS530

Garmin

•        2°VHF-COM/NAV/GPS

GNS430

Garmin

•        ICS Pilotincluding:

   

-Pilot/Co-piloContr.Panel                             AA95-896TSO NATo    Mode

-Controller                                                          AA31-002          NATo    Audio

-CabinControl                                                  AA82-060          NAT

•       DME                                                                              KDM706A          King

•       Marker Beacon                                                            KMR675            King

 

ADDITIONAINSTALLEAVIONIEQUIPMENT

•       Co-piloflight/navigation instruments, including followininstruments:

-Barometric Altimeter

-Air Speeindicator

-VSI

-LCDEADI &EHSI

•       Flight director+ autotrim                                           FZ 702                  Honeywell

•       Radio altimeter                                                           AA300                   Honeywell

•       E.L.T.                                                                             C406-2HM           Artex

•       MovingMap                                                                  MK2Observer    Skyforce

•       EFISPilot/ Co-piloton Command Switch

•       WeatheRadar RDR200(presentedon EFIS)

•       TASSky497                                                                BF Goodrich(presented on GNS530)

ISTALLEDAUXILIARYEQUIPMENT

•       Dualcontrols

•       Rotorbrake


•       450W Rotating landing light

•       Windshielwiper (Pilot/co-Pilot)

       Engine compartmenFirextinguisher

•       Aiframhour meter

•       Baggagcompartmenextension (1.9 m)

•       Air ConditioninGarret ECU

•       VibratioAbsorber

•       Reinforced pilot/co-pilowindshield

•       Emergencyfloats kit

•       216USG. Crash-resistanfuel syste(inlieu of152USG)

•       Baggagcompartmenextension (2.3 mt)

•       Pulsechip detecto(Engines, main andtailgearboxes)

•       Fuecawith key-lock                                                                                                       

•       High-intensity strobe lights

INTERIOR

-VIInterior including.

*Paulstra sound proofing


Leatherettcovered orpainted liners

3-seataffacing centrabencwitsee-through foldable armrest

3-seatfwd facinafbench witfoldablarmrest

•    Allseat crash-resistanVImodel coverewitleatheor fabric/leather

•    4– point shoulder harness with inertial reels and safetbeltoall seats

Advisory, readinanfloor courtesy lights

Leathebellows oflight controls

• Floor carpeting

• Carpetinprotection

Seat covers

• Cabidoublglass windows

Passiveibratioabsorber

• Customizepax cabifinishing

• 6 ActivNoise Reduction (ANR headsets)

• Refrigerated cabinet

PAINTING

Customizepainting scheme, metallic color serie500

MISCELLANEOUS

                  •     Airintake/exhaust covers

•      Pilot tubes covers

•      Tie-dowfittings

•      Flight manuaandechnicapublications

•      Ground tools Kit, including:

-Towbar

-LiftingTool

-Wheelchocks

 


 SPECIFICATIONS SUBJECT TO VERIFICATION UPON INSPECTION HELICOPTER IS OFFERED SUBJECT TO PRIOR SALE OR WITHDRAWAL FROM THE MARKET AIRCRAFT WILL CONTINUE TO REMAIN IN FLIGHT SERVICE UNTIL FORMAL DEPOSIT IS PLACED.
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