Registration: I-GIPA Year of construction: 1978 Country: Italy City/Aerodrome: Rome Ciampino


293000 

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Description

Aircraft SN: TJ-148

Airplane time state

TT: 2112 hrs
Engines, Continental TSIO-520-WB, sn 518645 and 518649
TSOH: 41 hrs
Last overhaul: 22/03/2011
TBO: 1600 hrs/12 years (24 years in Italy)
Propellers McCauley 3AF32521, sn 071550 and 071551
TSOH: 11 hrs
Last overhaul: 25/09/2014
TBO: 2000 hrs/50 years
Installed new in July 2008 Per RAM Aircraft STC

Interior

6 Seats
Light blue leather seats, white and blue side panels
Light blue curtains
Club seating arrangement

Exterior

White with red and light blue accents

Avionics

GMA340 Audio Panel, Marker Beacon
Avidyne IFD-440, 8.33 kHz, 760 channels NAV COM GPS
1 Avidyne IFD440, 8.33 kHz, 760 channels, NAV COM GPS, touchscreen, WiFi
1 Garmin Garmin GNS430, 8.33 kHz, 760 channels NAV COM GPS
King KY169A COM 3
King RDR2000 Color Radar
Garmin GTX300 Mode S Transponder
Garmin MX20 MFD with Jepp View and Radar Indicator
Sandel SN3500 HSI 1
Sandel SN32500 HSI 2
Bendix IN831A HSI 3
Bendix SG832C Compass System 1
Bendix SG832C Compass System 2
Bendix FCS810 3 Axis Autopilot/Flight Director
Altitude preselect
Sandel ST3400 TAWS/RMI
King KN63 DME
King KR87 ADF
Free Flight TRA3500/TRI40 Radar Altimeter with digital indication and altitude alerter
Revue Thommen AD323235F Air Data Computer with TAT Probe
Trans Cal SSD150-50A Altitude Encoder
Shadin Digital Fuel Computer
L3 Communication Sky-Watch 497 TCAS I
L3 Communication WX500 Stromscope
Artex 406N ELT with Satellite GPS
Davtron Clock on Pilot Control Yoke
Davtron Clock on Co-Pilot Control Yoke
PS-Engineering PAV80 DVD/FM/AM
External Camera
Avionics Innovation Audio Amplifier (4 speakers stereo)
2 Attitude Indicators
2 Altimeters
Inverter No. 1 (115/400 AC): Flytronic
Inverter No. 2 (115/400 AC): A.I.I.


Avionics description:
Information VOR/LOC GPS and Flight Plan 1 and 2 can be visualized either on HSI 1, HSI 2, RMI 1 and Multifunction Display together or separately.
TCAS information and stormscope can be visualized on MFD and HSI 1/2 and TAWS.
MX-20 has Jeppesen View capability and can display approach and airport charts.
Autopilot Heading and NAV modes can be coupled with HSI 1, 2 and 3 performing complete SID, STAR and Flight Plan.
TV camera is located in the bottom of the tail cone viewing front/down and gear and propellers too.
The stereo system is six headphone/interphone (BOSE System) and can accept signals from PAV-80 and AUX MP3 files.

Options

Surface device
Air conditioning
Courtesy table
Headset connectors for each occupant
Oxygen system
Strobe lights
Go around switch
Unfeathering accumulators
Instruments light
Control wheel map lights, mike button and ident
Double pitot system eating
Dual control yoke
Oxygen system
196 GA fuel system
Strobe 3 lights system
Tail light system
Propeller thrust detector
De-icing warning ground system
New propellers Mc Cauley low vibration

Remarks

Empty Weight: 4489.3 Lbs
Moment: .39354.45
Weighed July 2013
Airworthiness Review Certificate valid till 07/2019
Last 100 hrs / annual inspection performed 07/2019
Specifications subject to verification by purchaser

Год выпуска
1978
Страна
Italy
Налет, часов
2112
Мощность, л.с.
300х2
Скорость (макс), км/час
390