manufacturer
Bell
configuration
VIP
condition
Used
year
2017
time
1000
helicopter location
Chile
serial number
12456
listing ID
HT21651
Description
Designed to offer the best performance in its category, the Bell 505 Jet Ranger X is equipped with a Turbomeca Arrius 2R engine and dual-channel FADEC system, which provide the aircraft with 504 shp of takeoff power and speeds above 120 knots.
The model has numerous features that increase operational safety, including HTAWS (terrain warning system), digital aeronautical charts and synthetic vision (optional), as well as anti-crash seats.
From the outside, the model draws attention with well-defined lines and curves. Inside, the large main window is impressive, providing excellent visibility for pilots and passengers.
A completely flat floor and wide doors facilitate access for cargo and passengers, and the seats are easily removed or folded to adapt the aircraft to any mission. With the Bell 505 Jet Ranger X, the possibilities are truly extensive.
avionics
INTEGRATED AVIONICS SYSTEM with GARMIN G1000H™ SUITE
Two 10.4-inch (26.4 cm) high-resolution displays, providing Primary Flight Display (PFD) and MultiFunction Display (MFD) functionality
Integrated Avionics Unit, consisting of a 16-watt VHF communications transceiver with 8.33 kHz pitch, VHF navigation, WAAS GPS navigation and glideslope receiver
An audio control panel with Automatic Speech Recognition (ASR) feature logging
An Air Data Attitude Heading Reference Unit (ADAHRS) with outside air temperature (OAT) probe and magnetometer
An S Mode transponder with extended squitter, including Traffic Information Service (TIS), with ADS-B output capability
An engine and airframe interface unit
Engine Integrated Indication and Crew Alerting System (EICAS), including the Power Status Indicator (PSI) that provides an integrated display presentation of all critical engine parameters in a single gauge to present the Remaining power “margin”
Fuel flow indication with range ring display capability
Flight data logging of standard aircraft and engines Parameters
ELECTRICAL SYSTEM:
Auxiliary power outlet (28 VDC system)
Battery, 17 amp-hour lithium-ion
External power and grounding receptacle
Starter generator (165 amps)
Solid-state voltage regulator
Heated pitot tube
Static doors, unheated
LED lighting (interior/exterior)
Single LED landing light and two LED taxi lights
Illuminated baggage compartment
AVIONICS AND INSTALLED EQUIPMENT:
Garmin G1000H Integrated Avionics
GIA 63H GPS/WAAS/VHF COM/VHF NAV
GEA 71H Engine and Airframe unit
GMA 350H Audio panel
GTX 33H Extended Squitter (ES) Mode S
transponder
GSU 75 Air Data Attitude Heading
Reference Unit (ADAHRS)
GMU 44 Magnetometer
Standby Attitude Module (SAM)
