Cirrus DESIGN SR22T - Section 3 A Abnormal Procedures; Revision 1

P/N 13772-003 3A-1
Cirrus Design Section 3A
SR22T Abnormal Procedures
Section 3A
Abnormal Procedures
Table of Contents
Introduction ........................................................................................ 3
Abnormal Procedures Guidance ........................................................ 4
Circuit Breakers .............................................................................. 4
Flight Environment ............................................................................. 5
Inadvertent Icing Encounter ............................................................ 5
Inadvertent IMC Encounter............................................................. 5
Door Open In Flight ........................................................................ 5
Abnormal Landings ............................................................................ 6
Landing With Failed Brakes ............................................................ 6
Landing With Flat Tire..................................................................... 6
Engine System ................................................................................... 7
Low Idle Oil Pressure...................................................................... 7
Manifold Pressure High .................................................................. 7
Starter Engaged.............................................................................. 8
Alternate Air Door Open Annunciation............................................ 9
Fuel System ..................................................................................... 10
Low Fuel Quantity......................................................................... 10
Left Fuel Tank Quantity ................................................................ 10
Right Fuel Tank Quantity .............................................................. 10
Electrical System ............................................................................. 11
Low Voltage on Main Bus 1 .......................................................... 11
Low Voltage on Main Bus 2 .......................................................... 11
Battery 1 Current Sensor .............................................................. 11
Low Alternator 1 Output................................................................ 12
Low Alternator 2 Output................................................................ 13
Integrated Avionics System ............................................................. 14
Avionics Switch Off ....................................................................... 14
PFD Cooling Fan Failure .............................................................. 14
MFD Cooling Fan Failure.............................................................. 14
Flight Displays Too Dim................................................................ 15
Pitot Static System........................................................................... 16
Pitot Static Malfunction ................................................................. 16
Pitot Heat Current Sensor Annunciation ....................................... 17
Pitot Heat Required Annunciation................................................. 17
Flight Control System....................................................................... 18
Electric Trim/Autopilot Failure ....................................................... 18
Revision 1