Cirrus DESIGN SR20 - Section 3 A Abnormal Procedures; Revision 1

P/N 11934-004 3A-1
Cirrus Design Section 3A
SR20 Abnormal Procedures
Section 3A
Abnormal Procedures
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
Revision 1