CIRRUS PERSPECTIVE PLUS SYSTEM
Cirrus Aircraft has launch the new 2017 G6, the latest edition of the SR22T, SR22 and SR20 piston airplanes.
The latest model includes the just-unveiled Cirrus Perspective+ by Garmin flight deck.
At the core of the G6 is the new, next generation Cirrus Perspective+ (pronounced Perspective Plus) flight deck by Garmin.
Inspired by Garmin’s latest G1000 NXi integrated platform, Perspective+ features 10 times faster processing speed than prior Cirrus Perspective avionics, according to company officials.
Capabilities include animated datalink weather, SurfaceWatch safety protection, payload management, visual approach capabilities, wireless database uploads and more.
The keypad controller sports a QWERTY interface, allowing pilots to make a seamless transition from their smartphones, tablets or laptops.
Perspective+ also has a new HOME key — instantly bringing you back to your main navigating functions with the touch of just one button.
The Cirrus Perspective+ Integrated Avionics by Garmin presents flight instrumentation, position, navigation, communication, and identification information to the pilot through large-format displays. The Garmin Automatic Flight Control System (AFCS) provides the Flight Director (FD), Autopilot (AP), Yaw Damper (YD – optional), and manual electric trim (MET) functions. Refer to the AFCS section for more information.
THE FOLLOWING IS A LIST OF THE COMPONENTS INCLUDED IN THIS LISTING
SINCE THIS SYSTEM WILL MORE THAN LIKELY BE SOLD TO SOMEONE WHO ALREADY HAS AN AIRCRAFT WITH A STANDARD PERSPECTIVE OR POSSIBLY A G1000 SYSTEM WE HAVE REMOVED SOME OF THE COMPONENTS THAT MAY BE REDUNDANT TO YOUR NEEDS
GDU 1050A with connector
Pn 011-03470-30
Sn 49405146
GDU 1050A with connector
Pn 011-03470-20
Sn 494205156
The system features two 10 inch, high resolution LED backlit display units. The left display is configured as a Primary Flight Display (PFD). The right display is configured as an Multi Function Display (MFD). The displays communicate with each other through a High-speed Data Bus (HSDB) Ethernet connection. Each display is also paired with an Ethernet connection to the Garmin Integrated Avionics unit (GIA).
GMC 707 with connector
Pn 011-03502-20
Sn 2ZN202168
GMC 707 Provides the controls for the Garmin AFCS through an RS-232 digital interface allowing communication with the PFD and MFD.
GEA 71B with tray & connectors
Pn 011-03682-00
Sn 497005580
The GEA 71B receives and processes signals from the engine and airframe sensors. This unit communicates with both GIAs using an RS-485 digital interface.
GIA 64W with tray & connectors QTY 2
Pn 011-03711-00
Sn 4SK011300 & 4SK011127
The GIA 64W Integrated Avionics Units (IAU) function as the main communication hub, linking all LRUs with the PFD. Each GIA contains a GPS Satellite-Based Augmentation System (SBAS) receiver, VHF COM/NAV/GS receivers, a flight director and system integration microprocessors. Each GIA is paired with the on-side display via an HSDB connection.
GSU 75 with tray & connector QTY 2
Pn 011-03094-00
Sn 3KY005880 & 3KY005965
The GSU 75 ADAHRS, combining air data and altitude/heading data units.
Processes data from the pitot/static system as well as the OAT probe to provide pressure altitude, airspeed, vertical speed and OAT information to the system. This unit also provides aircraft attitude and heading information via ARINC 429 to the PFD, MFD, and GIA. The GSU 75 contains advanced sensors (including accelerometers and rate sensors) and interfaces with the GMU to obtain magnetic field information, and with the GIA to obtain GPS information.
GCU 479 (ours is damaged, see pictures) with connector
Pn 011-04048-00
Sn 4RJ001828
The GCU 479 provides the Flight Management System (FMS), navigation radio (NAV), communication radio (COM), transponder (XPDR), and course (CRS) controls for the system through an RS-232 digital interface.
GMC 707 (1) – Provides the controls for the Garmin AFCS through an RS-232 digital interface allowing communication with the PFD and MFD.
GTP 59 QTY 2 NO PN ON UNITS NO SN ON UNITS
The GTP 59 Temperature Probe provides Outside Air Temperature (OAT) data to the GSU
GMU 44 with connector QTY 2
PN 011-00870-10
SN 1CM035663 & 1CM035669
The GMU 44 magnetometer measures local magnetic field and sends the data to the GSU for processing to determine aircraft magnetic heading. This unit receives power directly from the GSU and communicates with the it, using an RS-485 digital interface.
GTA 82 with connector
PN 011-00960-00
SN 66906835
The GTA 82 pitch Trim Adapter takes input from the trim switches, GIA and GSA to control the DC motor to drive the aircraft trim system
GSA 81 with connector QTY 2
PN 011-00878-20
SN 1A1029297 & 1A1029417
The GSA 81 servos are used for the automatic control of pitch and roll.
GSM 86
PN 011-01904-00
SN 1GK031704 & 1GK031845
The GSM 86 servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo actuator to the mechanical flight-control surface linkage.
Chart unlock datacard
PN 010-00330-53
Enhanced afsc datacard
PN 010-00330-5C
Surfacewatch ebablement datacard
PN 010-00330-KA
SVS UNLOCK PFD 1 DATACARD
PN 010-00330-54
GIFD SUPPL DATA CARD
PN 010-00474-50
MISC DATA CARD
CIRRUS PN 16330-002
MISC BRACKETS
AP DISCONNECT SWITCH & GO AROUND
SWITCH
