S
ECTION
7: A
IRPLANE
AND
S
YSTEMS
C
IRRUS
D
ESIGN
A
VIONICS
SR20
7-84
P/N 11934-005
•
Runway and terrain features during climb, descent, and low altitude
maneuvering.
The EVS sensor, located on the underside of the LH wing, contains a
long-wave infrared camera that produces an infrared image and a lowlight
CMOS camera that produces a visible image. The two images are then
combined to produce a single fused image and transmitted directly to the
MFD. Upon power-up, the sensor requires approximately 90 seconds to
produce a usable image. The image generated is a monochrome image. The
hotter an object is the whiter it appears on the display.
28 VDC Enhanced Vision System operation is supplied through the 5-amp
EVS CAMERA circuit breaker on MAIN BUS 3. Refer to the Max Viz
Enhanced Vision System Pilot’s Guide for a detailed discussion of the
system. For maintenance information and special precautions to be
followed, refer to Section 8,
Enhanced Vision System Sensor Windows
.
SurfaceWatch
The SurfaceWatch feature displays visual annunciations and runway and
taxiway information on the PFD to improve pilot situational awareness
during ground operations and air operations in the airport environment.
Refer to the Cirrus Pers Integrated Flight Deck Pilot’s Guide for a
detailed discussion of the SurfaceWatch feature.
Flight Stream 510 Wireless Avionics Interface
The Flight Stream 510 Wireless Avionics Interface allows the connection of
a compatible mobile electronic device to the avionics. The Flight Stream
510 utilizes a Bluetooth™ connection for pairing up to 4 devices as well as a
Wi-Fi connection for wireless database transfer. The Flight Stream 510 is
installed in the bottom MFD card slot.
• CAUTION •
AHRS information transmitted by Flight Stream 510 is not to be
used as a primary source of aircraft attitude information.
Data output from the Flight Stream 510 can be used to provide additional
situational awareness for the pilot and passengers. Flight plans can be
transferred between compatible mobile devices and the integrated avionics
system using supported mobile applications. The Flight Stream 510 also
serves as a wireless GDL 69 controller through which the aircraft crew or
passengers can select Sirius/XM audio channels and control volume.
Power for Flight Stream 510 operation is supplied through the MFD which
is powered by the 5-amp MFD A circuit breaker on Main Bus 3 and the
5-amp MFD B circuit breaker on Main Bus 1.
For a complete description of the Flight Stream 510 system, its operating
modes, and additional detailed operating procedures, refer to the Perspec-
tive Integrated Avionics System Pilot's Guide.
Reissue A
