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during flight.
Section 3 - Emergency Procedures
No Change.
Section 3A - Abnormal Procedures
No Change.
Section 4 - Normal Procedures
No Change.
Section 5 - Performance
No Change.
Section 6 - Weight & Balance
Refer to Section 6 - Weight and Balance of the basic POH for current
weight and balance data.
Original Issue: 07-29-08
13772-138 3 of 4
Cirrus Design Section 9
SR22 Supplements
Section 7 - System Description
Max Viz Enhanced Vision System
The Enhanced Vision System is an electro-optical system that uses a
Long-Wave Infrared (IR) camera. Infrared is particularly effective at
night, smoke, haze, and smog in addition to a broad spectrum of rain,
snow, and radiation-type fog. However, penetration is limited during
certain environmental conditions associated with heavy rain, heavy
snow, coastal fog and most cloud formations. Therefore the EVS is not
intended for all atmospheric conditions and may only be used for
acquisition of objects normally viewed through the cockpit windows.
EVS is an aid to visual acquisitions of:
• Ground vehicles and other ground-based equipment/obstacles,
• Aircraft on taxi-ways and runways,
• Other traffic during takeoff, approach, and landing,
• Runway and taxi lights,
• 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 a 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 Perspective Integrated Avionics System Pilot’s Guide for a
general description of the system and its operating modes. 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, Ground Handling,
Servicing, and Maintenance
Original Issue: 07-29-08
4 of 4 13772-138
Section 9 Cirrus Design
Supplements SR22
Section 8 - Maintenance
Enhanced Vision System Sensor Windows
The Enhanced Vision System Sensor is located on the underside of
the LH wing. The three sensor windows are made of Germanium. In
contrast to visible light energy, infrared energy typically passes
through dirt on the window. As such, the Sensor windows requires
only occasional cleaning with mild liquid soap and water or isopropyl
alcohol, and a soft cloth.
• Caution •
If a EVS Sensor Window breaks, use gloves and masks when
handling broken germanium window material.
Do not use abrasive cleansers or cleaning pads on the
germanium window. Abrasive cleaning can damage the
sensor window coating.
Do not use any cleansers containing ammonia. Ammonia will
remove the sensor window coating.
Original Issue: 07-29-08
Information Manual 10-1
Cirrus Design Section 10
SR22 Safety Information
Section 10
Safety Information
Table of Contents
Introduction ........................................................................................ 3
Cirrus Airframe Parachute System (CAPS) ....................................... 4
Deployment Scenarios.................................................................... 4
General Deployment Information.................................................... 6
Landing Considerations .................................................................. 7
Taxiing, Steering, and Braking Practices ......................................... 10
Operating Practices ...................................................................... 10
Brake Maintenance....................................................................... 11
March 2010
10-2 Information Manual
Section 10 Cirrus Design
Safety Information SR22
March 2010
Intentionally Left Blank
Cirrus Design Section 10
SR22 Safety Information
Information Manual 10-3
Introduction
This aircraft is designed to operate safely and efficiently in a flight
environment. However, like any other aircraft, pilots must maintain
proficiency to achieve maximum safety, utility, and economy.
As the pilot you must be thoroughly familiar with the contents of this
　
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