曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

to the full open position. The air is then distributed by either ram air or
by an optional blower fan to the distribution manifold mounted to the
center, aft side of the firewall
Vent Selection
Conditioned air from the distribution manifold can be proportioned and
directed to passengers and/or the windshield by manipulating the
cabin vent selector. The selector is mechanically linked to butterfly
valves at the entrances to the windshield diffuser and the cabin floor
ducting. There is continuous airflow to the panel and armrest eyeball
outlets. Each occupant can control the flow rate from 'off' to maximum
by rotating the nozzle.
When the selector is in the far left position, both butterfly valves are
closed providing maximum airflow to the panel and armrest eyeball
outlets. Rotating the selector a quarter-turn clockwise opens the cabin
floor butterfly valve allowing airflow to the rear seat foot warmer
diffusers and the front seat outlets mounted to the underside of each
kickplate. Rotating the selector another quarter-turn clockwise opens
the windshield diffuser butterfly valve which permits shared airflow to
the defrosting mechanism and cabin floor outlets. When the selector is
in the far right position, the cabin floor butterfly valve is closed
providing maximum airflow to the windshield diffuser.
Temperature Selection
The temperature selector is mechanically linked to the hot and cold air
valves. Rotating the selector simultaneously opens and closes the two
valves, permitting hot and cold air to mix and enter the distribution
system. Rotating the selector clockwise, permits warmer air to enter
the system - counterclockwise, cooler air.
Original: 03-27-07
13772-130 57 of 58
Cirrus Design Section 9
SR22 Supplements
Section 8 - Handling, Servicing &
Maintenance
Servicing
Filling Fuel Tanks
Observe all safety precautions required when handling gasoline. Fuel
fillers are located on the forward slope of the wing. Each wing holds a
maximum of 46.0 U.S. gallons. When using less than the standard
92.0 U.S. gallon capacity, fuel should be distributed equally between
each side.
Original: 03-27-07
58 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Original: 03-27-07
Intentionally Left Blank
Information Manual 10-1
Cirrus Design Section 10
SR22 Safety Information
Section 10
Safety Information
Table of Contents
Introduction ...................................................................................10-3
Cirrus Airframe Parachute System (CAPS) Deployment ..............10-4
Deployment Scenarios...............................................................10-4
Mid-Air Collision......................................................................10-4
Structural Failure ....................................................................10-4
Loss of Control .......................................................................10-5
Landing Required in Terrain not Permitting a Safe Landing...10-5
Pilot Incapacitation .................................................................10-5
General Deployment Information...............................................10-5
Deployment Speed .................................................................10-5
Deployment Altitude ...............................................................10-6
Deployment Attitude ...............................................................10-6
Landing Considerations .............................................................10-7
Emergency Landing Body Position.........................................10-7
Door Position ..........................................................................10-7
Water Landings ......................................................................10-8
Post Impact Fire .....................................................................10-9
Ground Gusts .........................................................................10-9
Taxiing, Steering, and Braking Practices ....................................10-10
Proper Operating Practices .....................................................10-10
Brake Maintenance..................................................................10-11
June 2007
10-2 Information Manual
Section 10 Cirrus Design
Safety Information SR22
June 2007
Intentionally Left Blank
Information Manual 10-3
Cirrus Design Section 10
SR22 Safety Information
Introduction
The Cirrus Design SR22 is a modern, advanced technology airplane
designed to operate safely and efficiently in a flight environment.
However, like any other aircraft, pilots must maintain proficiency to
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(153)