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Table of Contents
Introduction ........................................................................................ 1
Abnormal Procedures Guidance........................................................ 1
Circuit Breakers .............................................................................. 1
Flight Environment ............................................................................. 2
Inadvertent Icing Encounter ............................................................ 2
Inadvertent IMC Encounter............................................................. 2
Door Open In Flight ........................................................................ 2
Abnormal Landings ............................................................................ 3
Landing With Failed Brakes............................................................ 3
Landing With Flat Tire..................................................................... 3
Engine System................................................................................... 4
Low Idle Oil Pressure...................................................................... 4
Starter Engaged Annunciation........................................................ 4
Fuel System....................................................................................... 5
Left Fuel Tank Quantity .................................................................. 5
Right Fuel Tank Quantity ................................................................ 5
Fuel System (Cont) ......................................................................... 6
Fuel Filter in Bypass Mode ............................................................. 6
Electrical System ............................................................................... 6
Battery 1 Current Sensor ................................................................ 6
Integrated Avionics System ............................................................... 8
Avionics Switch Off ......................................................................... 8
Flight Displays Too Dim.................................................................. 8
PFD Cooling Fan Failure ................................................................ 8
MFD Cooling Fan Failure................................................................ 9
Pitot Static System........................................................................... 10
Pitot Static Malfunction ................................................................. 10
Pitot Heat Current Sensor Annunciation....................................... 10
Pitot Heat Required Annunciation................................................. 11
Pitot Heat Required Annunciation................................................. 11
Flight Control System....................................................................... 12
Electric Trim/Autopilot Failure....................................................... 12
Flap System Exceedance ............................................................. 12
Landing Gear System ...................................................................... 13
Brake Failure During Taxi ............................................................. 13
Left/Right Brake Over-Temperature ............................................. 13
March 2010
3A-2 Information Manual
Section 3A Cirrus Design
Abnormal Procedures SR22
Other Conditions ..............................................................................14
Aborted Takeoff ............................................................................14
Parking Brake Engaged Annunciation ..........................................15
Communications Failure ...............................................................15
March 2010
Cirrus Design Section 3A
SR22 Abnormal Procedures
Information Manual 3A-1
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.
• Caution •
If a Warning annunciation is illuminated in combination with
any of the following Abnormal annunciations, the Warning
annunciation takes precedents and shall be performed first.
Abnormal Procedures Guidance
Although this section provides procedures for handling most abnormal
system and/or flight conditions that could arise in the aircraft, 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
　
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