Cirrus SR20 - Section 3 A Abnormal Procedures

P/N 13999-004 Info Manual 3A-1
Cirrus Design Section 3A
SR20 Abnormal Procedures
Section 3A
Abnormal Procedures
Table of Contents
Introduction ........................................................................................ 3
Abnormal Procedures Guidance........................................................ 3
Circuit Breakers .............................................................................. 3
Flight Environment ............................................................................. 4
Inadvertent Icing Encounter............................................................ 4
Inadvertent IMC Encounter............................................................. 4
Door Open In Flight ........................................................................ 4
Abnormal Landings ............................................................................ 5
Landing With Failed Brakes............................................................ 5
Landing With Flat Tire..................................................................... 5
Engine System ................................................................................... 6
Low Idle Oil Pressure...................................................................... 6
Starter Engaged Annunciation........................................................ 7
Fuel System ....................................................................................... 8
Low Fuel Quantity........................................................................... 8
Left Fuel Tank Quantity .................................................................. 8
Right Fuel Tank Quantity ................................................................ 9
Fuel Filter in Bypass Mode Airplane Serials 2016 thru 2031.......... 9
Electrical System ............................................................................. 10
Low Voltage on Main Bus 1 .......................................................... 10
Low Voltage on Main Bus 2 .......................................................... 10
Battery 1 Current Sensor .............................................................. 10
Low Alternator 1 Output................................................................ 11
Low Alternator 2 Output................................................................ 12
Integrated Avionics System ............................................................. 13
Avionics Switch Off ....................................................................... 13
PFD Cooling Fan Failure .............................................................. 13
MFD Cooling Fan Failure.............................................................. 13
Flight Displays Too Dim ................................................................ 14
Pitot Static System........................................................................... 15
Pitot Static Malfunction ................................................................. 15
Pitot Heat Current Sensor Annunciation....................................... 16
Pitot Heat Required Annunciation................................................. 16
Flight Control System....................................................................... 17
Electric Trim/Autopilot Failure....................................................... 17
Flap System Exceedance ............................................................. 17
September 2011