- 2,045 FH
- Delivered May 2007
- Pratt & Whitney PT6A-66B Engines
- Collins Pro Line 21 Avionics Suite
- RVSM, Mach 0.7, Category II Landings and Steep Approach
- JAR OPS1
- Fresh from A-Check and 5-Year Inspection
2007 Piaggio Avanti II
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Technical Specifications
Headlines
Main Features
- 2,045 FH
- Delivered May 2007
- Pratt & Whitney PT6A-66B Engines
- Collins Pro Line 21 Avionics Suite
- IFIS 5000 Upgrade with Electronic Charts and Maps Overlay
- RVSM, Mach 0.7, Category II Landings and Steep Approach
- JAR OPS1
- Fresh from A-Check and 5-Year Inspection
Engines
Pratt & Whitney PT6A-66B Engines
- 2045/2045 FH since new
- 200 FH since HSI
- 3600 FH TBO
Avionics
Rockwell-Collins ProLine 21 Avionic Package
.Radio Management System – Collins RTU-4200, CDU-3000
.Dual VHF COM - Collins VHF-4000 Transceiver with Antenna with 8.33 kHz spacing
.VHF NAV 1 + ADF - Collins NAV-4000 VOR/ILS/MKR/ADF Receiver with Antennae
.VHF NAV 2 - Collins NAV-4500 VOR/ILS/MKR Receiver with Antennae
.Single DME - Collins DME-4000 (3 channel) with Antenna
.Dual Mode S Flight ID Diversity Transponder - Collins TDR-94D
.Radio Altimeter - Collins ALT-4000 (Operation to 2500 ft) with Antennae
.Turbulence Detection Weather Radar - Collins RTA-852 Colour Radar with 12" Antenna
.TCAS I – L-3 Communications SkyWatch HP model SKY899
.TAWS Class B with Worldwide Database – L-3 Landmark TAWS 8000
.Dual Audio Panel - Baker B1045
.Dual Cockpit Speaker
.Dual hand-held Microphone
.Dual Boom/Microphone/Headset
.EFIS with EIS – Three Collins displays AFD-3010, two DCP-3030, CCP-3000
.Flight Guidance System - Collins Dual FGC-3003 (A/P,YD and dual Flight Director included),three SVO-3000 Servos, single FGP-3000 Flight Guidance Panel Single FMS - Collins FMC-3000 (NAV to NAV and VNAV), CDU-3000 (used also for radiotuning),
.DBU-4100
.GPS Sensor Unit - Collins GPS-4000
.Dual ADS - Collins ADC-3000
.Dual AHRS - Collins AHC-3000 and FDU-3000
.Maintenance Diagnostic System - Collins MDC-3110
.Four Data Concentrator Unit - Collins DCU-3001
.Stand-by Cluster Instrument – L-3 Communications GH-3100
.Emergency Locator Transmitter – Techtest Model 503 (3 frequency)
.Dual Clock (Flight Hour Meter included)
.Dual Master Annunciator
.Dual Turn&Slip Indicator (shown on the displays)
.Reversionary/Miscellaneous Panel
Additional equipment
. Satellite Phone Air Cell ST3100 with dual handset
. Engine Fire Extinguisher
. Air Ambulance Provisions
. Max Take Off Weight Increase (12,100 lbs)
Exterior
Overall white with red, gold and blue accents
Interior
VIP Corporate Interiors - Option 1 floorplan (7-Place + 1)
. Four single passenger seats in club arrangement
. One single passenger side-facing seats.
. Two-seat divan
. Aft fully enclosed lavatory with flushing potty and belted aft auxiliary passenger seat,
. Dual executive tables
. Refreshment center with ice chest and miscellaneous storage
Download
2007 Avanti II - Nov. '17.pdf
SPECIFICATIONS AND/OR DESCRIPTIONS ARE PROVIDED FOR INTRODUCTORY PURPOSES ONLY AND DO NOT CONSTITUTE REPRESENTATIONS OR WARRANTIES BY ORIONFLY. VERIFICATION OF SPECIFICATIONS, FLIGHT HOURS, INSTALLED EQUIPMENT, AND AIRCRAFT CONDITIONS IS THE SOLE RESPONSIBILITY OF THE PURCHASER. SOME PHOTOS MAY HAVE BEEN CHANGED OR NOT CURRENT. INFORMATION HAS BEEN PROVIDED BY THE SELLER AND HAS NOT BEEN INDEPENDENTLY VERIFIED BY ORIONFLY. AIRCRAFT SUBJECT TO PRIOR SALE AND WITHDRAWAL FROM THE MARKET. PRICES ARE NET OF VAT, IF APPLICABLE.
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