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stabilizer (ST) mode if available. If optional electric HSI is installed,
use HDG mode to help maintain wings level - set HDG bug to the
current airplane heading before engaging autopilot.
• WARNING •
Do not use HDG mode if airplane is equipped with a vacuum
powered directional gyro or vacuum powered HSI.
2. Rely upon “partial panel” techniques while in instrument
conditions. Cover inoperative instruments if possible.
3. Endeavor to fly to visual conditions as soon as possible.
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3-28 Information Manual
Section 3 Cirrus Design
Emergency Procedures SR20
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Information Manual 3A-1
Cirrus Design Section 3A
SR20 Abnormal Procedures
Section 3A
Abnormal Procedures
Table of Contents
Introduction .................................................................................. 3A-3
Abnormal Procedures Guidance.................................................. 3A-4
Ground Procedures...................................................................... 3A-5
Brake Failure During Taxi ......................................................... 3A-5
Aborted Takeoff ........................................................................ 3A-5
In-Flight Procedures..................................................................... 3A-6
Inadvertent Icing Encounter ...................................................... 3A-6
Inadvertent IMC Encounter....................................................... 3A-6
Door Open In Flight .................................................................. 3A-6
Landing Procedures..................................................................... 3A-7
Landing With Failed Brakes...................................................... 3A-7
Landing With Flat Tire............................................................... 3A-7
System Malfunctions.................................................................... 3A-8
Alternator Failure ...................................................................... 3A-8
LOW VOLTS Warning Light Illuminated ................................... 3A-9
Communications Failure ......................................................... 3A-10
Pitot Static Malfunction ........................................................... 3A-11
Electric Trim/Autopilot Failure................................................. 3A-12
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3A-2 Information Manual
Section 3A Cirrus Design
Abnormal Procedures SR20
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Information Manual 3A-3
Cirrus Design Section 3A
SR20 Abnormal Procedures
Introduction
This section provides procedures for handling abnormal system and/or
flight conditions which, if followed, will maintain an acceptable level of
airworthiness or reduce operational risk. The guidelines described in
this section are to be used when an abnormal condition exists and
should be considered and applied as necessary.
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3A-4 Information Manual
Section 3A Cirrus Design
Abnormal Procedures SR20
Abnormal Procedures Guidance
Although this section provides procedures for handling most abnormal
system and/or flight conditions that could arise in the SR20, it is not a
substitute for thorough knowledge of the airplane and general aviation
techniques. A thorough study of the information in this handbook while
on the ground will help you prepare for time-critical situations in the air.
Sound judgement as well as thorough knowledge of the aircraft, its
characteristics, and the flight manual procedures are essential in the
handling of any abnormal system and/or flight condition. In addition to
the outlined items in the Abnormal Procedures, the following steps are
considered part of all abnormal situations:
• Maintain Aircraft Control
• Analyze the Situation
• Take Appropriate Action
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Information Manual 3A-5
Cirrus Design Section 3A
SR20 Abnormal Procedures
Ground Procedures
Brake Failure During Taxi
Ground steering is accomplished by differential braking. However,
increasing power may allow some rudder control due to increased
groundspeed and airflow over the rudder.
1. Engine Power......................................................... AS REQUIRED
• To stop airplane - REDUCE
• If necessary for steering - INCREASE
2. Directional Control ...............................MAINTAIN WITH RUDDER
3. Brake Pedal(s) ......................................................................PUMP
If directional control can not be maintained:
4. Mixture ..............................................................................CUTOFF
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 1148-126(20)
