P/N 13772-005
3A-1
Cirrus Design
Section 3A
SR22T
Abnormal Procedures
Introduction ........................................................................................ 3
Abnormal Procedures Guidance........................................................ 4
Circuit Breakers .............................................................................. 4
Flight Environment ............................................................................. 5
Abnormal Landings ............................................................................ 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
Fuel Imbalance ............................................................................. 11
Electrical System ............................................................................. 12
Low Voltage on Main Bus 1 .......................................................... 12
Low Voltage on Main Bus 2 .......................................................... 12
Battery 1 Current Sensor .............................................................. 12
Low Alternator 1 Output................................................................ 13
Low Alternator 2 Output................................................................ 14
Integrated Avionics System ............................................................. 15
Avionics Switch Off ....................................................................... 15
PFD Cooling Fan Failure .............................................................. 15
MFD Cooling Fan Failure.............................................................. 15
Flight Displays Too Dim................................................................ 16
Pitot Static System........................................................................... 17
Pitot Static Malfunction ................................................................. 17
Pitot Heat Current Sensor Annunciation....................................... 18
Pitot Heat Required Annunciation................................................. 18
Flight Control System....................................................................... 19
Original Issue
Section 3A: Abnormal Procedures
Table of Contents