Specifications

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

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

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