Cirrus SR20 Specifications Page 104
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3A-12 P/N 11934-004
Section 3A Cirrus Design
Abnormal Procedures SR20
Flight Control System
Electric Trim/Autopilot Failure
Any failure or malfunction of the electric trim or autopilot can be over-
ridden by use of the control yoke. If runaway trim is the problem, de-
energize the circuit by pulling the appropriate circuit breakers and land
as soon as conditions permit.
1. Airplane Control ......................................... MAINTAIN MANUALLY
2. Autopilot (if engaged) .................................................DISENGAGE
If Problem Is Not Corrected:
3. Circuit Breakers............................................ PULL AS REQUIRED
• PITCH TRIM
• ROLL TRIM
• YAW SERVO
• AP SERVOS
4. Power Lever ........................................................... AS REQUIRED
5. Control Yoke................................. MANUALLY HOLD PRESSURE
6. Land as soon as practical.
Flap System Exceedance
FLAPS Caution
Flaps are extended beyond airspeed limitations.
Flaps at 100%, airspeed greater than 109 KIAS for 5 seconds or more,
OR
Flaps at 50%, airspeed greater than 124 KIAS for 5 seconds or more.
1. Airspeed...........................................................................REDUCE
or
1. Flaps .............................................................................. RETRACT
FLAPS
Original Issue
- CIRRUS DESIGN SR20 1
- Cirrus Design Corporation 2
- 4515 Taylor Circle 2
- Duluth, MN 55811 2
- List of Effective Pages 3
- B P/N 11934-004 4
- SR20 List of Effective Pages 4
- P/N 11934-004 C 5
- Foreword 7
- The Handbook 8
- Revising the Handbook 9
- Identifying Revised Material 9
- Revision Service 10
- Supplements 10
- Retention of Data 11
- Warnings, Cautions, and Notes 11
- Section 1 13
- Figure 1-1 16
- Airplane Three View 16
- Figure 1-2 17
- Airplane Interior Dimensions 17
- Figure 1-3 18
- Turning Radius 18
- The Airplane 19
- 1-8 P/N 11934-004 20
- Section 1 Cirrus Design 20
- General SR20 20
- Meteorological Terminology 22
- Engine Power Terminology 23
- 1-12 P/N 11934-004 24
- Cirrus Design Section 1 25
- SR20 General 25
- P/N 11934-004 1-13 25
- Section 2 27
- Limitations 27
- 2-2 P/N 11934-004 28
- Section 2 Cirrus Design 28
- Limitations SR20 28
- Certification Status 29
- Airspeed Limitations 30
- Airspeed Indicator Markings 31
- Powerplant Limitations 32
- Weight Limits 33
- PowerPlant 34
- Electrical 35
- Center of Gravity Limits 36
- Maneuver Limits 37
- Flight Load Factor Limits 37
- Minimum Flight Crew 37
- Kinds of Operation 38
- Runway Surface 42
- Fuel Limits 43
- Altitude Limits 43
- Environmental Conditions 43
- Maximum Occupancy 43
- Systems and Equipment Limits 44
- Cirrus Design Section 2 45
- SR20 Limitations 45
- P/N 11934-004 2-19 45
- Enhanced Vision System 46
- Other Limitations 47
- Placards 48
- EXTERNAL 49
- Figure 2-4 50
- (Sheet 3 of 6) 50
- DAY - NIGHT - VFR - IFR 51
- FOLLOWING FLIGHT OPERATIONS: 51
- GRAB HERE 52
- IN INJURY OR DEATH 53
- Section 3 55
- Emergency Procedures 55
- 3-2 P/N 11934-004 56
- Section 3 Cirrus Design 56
- Emergency Procedures SR20 56
- Emergency Procedures Guidance 58
- Circuit Breakers 59
- Memory Items 59
- 3-6 P/N 11934-004 60
- Engine Failures 61
- Engine Failure In Flight 62
- Airstart 63
- Smoke and Fire 64
- Cirrus Design Section 3 65
- SR20 Emergency Procedures 65
- P/N 11934-004 3-11 65
- Wing Fire In Flight 66
- Engine Fire During Start 66
- Smoke and Fume Elimination 67
- Emergency Descent 68
- Forced Landings 69
- Ditching 70
- Engine System Emergencies 71
- Oil Temperature High 72
- Engine Speed High 72
- P/N 11934-004 3-19 73
- Engine Partial Power Loss 74
- P/N 11934-004 3-21 75
- Propeller System Emergencies 76
- Fuel System Emergencies 77
- Electrical System Emergencies 78
- Low Voltage on Essential Bus 79
- Low Alternator 1 Output 80
- Low Alternator 2 Output 80
- PFD Display Failure 81
- Emergency Exit 82
- Unusual Attitude Emergencies 83
- 3-30 P/N 11934-004 84
- Other Emergencies 85
- Starter Engaged Annunciation 86
- CAPS Deployment 87
- 3-34 P/N 11934-004 88
- P/N 11934-004 3-35 89
- Section 3A 91
- Abnormal Procedures 91
- 3A-2 P/N 11934-004 92
- Section 3A Cirrus Design 92
- Abnormal Procedures SR20 92
- Abnormal Procedures Guidance 93
- Flight Environment 94
- Abnormal Landings 95
- Engine System 96
- Fuel System (Cont) 98
- Figure 3A-1 99
- Circuit Breaker Panel 99
- Integrated Avionics System 100
- MFD Cooling Fan Failure 101
- Pitot Static System 102
- Flight Control System 104
- Landing Gear System 105
- Other Conditions 106
- Communications Failure 107
- Intentionally Left Blank 108
- Section 4 109
- Normal Procedures 109
- Introduction 111
- SR22_FM04_1454 112
- Cirrus Design Section 4 113
- SR20 Normal Procedures 113
- P/N 11934-004 4-5 113
- Revision 1 113
- 4-6 P/N 11934-004 114
- Section 4 Cirrus Design 114
- Normal Procedures SR20 114
- Original Issue 114
- P/N 11934-004 4-7 115
- 4-8 P/N 11934-004 116
- Before Starting Engine 117
- Starting Engine 118
- P/N 11934-004 4-11 119
- Before Taxiing 120
- Before Takeoff 121
- 4-14 P/N 11934-004 122
- P/N 11934-004 4-15 123
- Normal Takeoff 124
- Short Field Takeoff 124
- P/N 11934-004 4-17 125
- 4-18 P/N 11934-004 126
- Cruise Leaning 127
- Before Landing 128
- P/N 11934-004 4-21 129
- Balked Landing/Go-Around 130
- After Landing 130
- Shutdown 131
- Environmental Considerations 132
- P/N 11934-004 4-25 133
- Fuel Conservation 134
- Section 5 135
- Performance Data 135
- Temperature Conversion 142
- Stall Speeds 144
- Wind Components 145
- Takeoff Distance 146
- Takeoff Distance - 3050 LB 147
- Takeoff Distance - 2500 LB 148
- Takeoff Climb Gradient 149
- Takeoff Rate of Climb 150
- Enroute Climb Gradient 151
- Enroute Rate of Climb 152
- Cruise Performance 155
- Range / Endurance Profile 157
- Balked Landing Climb Gradient 159
- Balked Landing Rate of Climb 160
- Landing Distance 161
- Section 6 163
- Weight and Balance Data 163
- Airplane Weighing Form 166
- Airplane Weighing Procedures 167
- 6-6 P/N 11934-004 168
- Section 6 Cirrus Design 168
- Weight and Balance Data SR20 168
- SR22_FM06_1440A 169
- Loading Instructions 170
- Loading Data 172
- Moment Limits 173
- Weight & Balance Record 174
- Equipment List 175
- Section 7 177
- 7-2 P/N 11934-004 178
- Section 7 Cirrus Design 178
- Airframe 180
- Empennage 181
- Flight Controls 182
- Figure 7-1 183
- Elevator System 183
- Aileron System 184
- Figure 7-2 185
- Rudder System 186
- Control Locks 186
- Figure 7-3 187
- Instrument Panel 188
- SR20_FM07_3010 189
- Flight Instruments 190
- SR20_FM07_3009 191
- Attitude Indicator 192
- Airspeed Indicator 193
- Altimeter 194
- Vertical Speed Indicator 195
- Magnetic Compass 195
- Wing Flaps 196
- Figure 7-6 197
- Landing Gear 198
- Cirrus Design Section 7 199
- P/N 11934-004 7-25 199
- Baggage Compartment 200
- P/N 11934-004 7-27 201
- 7-28 P/N 11934-004 202
- Cabin Doors 203
- Engine Controls 204
- P/N 11934-004 7-31 205
- Engine Indicating 206
- Density Alt 8000 Ft 207
- 7-34 P/N 11934-004 208
- P/N 11934-004 7-35 209
- Engine Lubrication System 210
- Ignition and Starter System 210
- Air Induction System 210
- Engine Exhaust 211
- Engine Fuel Injection 211
- Engine Cooling 211
- Propeller 212
- Fuel System 213
- Fuel Selector Valve 214
- Fuel Pump Operation 214
- Figure 7-8 215
- Fuel System Schematic 215
- Fuel Indicating 216
- 7-44 P/N 11934-004 218
- P/N 11934-004 7-45 219
- Electrical System 220
- Figure 7-10 221
- Electrical System Schematic 221
- Power Distribution 222
- Electrical System Protection 223
- 7-50 P/N 11934-004 224
- Electrical System Control 225
- Ground Service Receptacle 226
- Electrical Indicating 227
- Lighting Systems 229
- Interior Lighting 230
- Environmental System 231
- Figure 7-12 232
- Distribution 233
- 7-60 P/N 11934-004 234
- Stall Warning System 235
- Pitot-Static System 236
- Figure 7-13 237
- Avionics 238
- Figure 7-14 239
- 7-66 P/N 11934-004 240
- P/N 11934-004 7-67 241
- SR20_FM07_2807 242
- SR20_FM07_2820 243
- 7-70 P/N 11934-004 244
- P/N 11934-004 7-71 245
- Optional Avionics 246
- P/N 11934-004 7-73 247
- 7-74 P/N 11934-004 248
- P/N 11934-004 7-75 249
- SR20_FM07_3011 250
- Avionics Support Equipment 251
- 7-78 P/N 11934-004 252
- Cabin Features 253
- Fire Extinguisher 254
- Hour Meters 255
- Emergency Egress Hammer 255
- Convenience Outlet 255
- System Description 256
- Activation Handle 257
- 7-84 P/N 11934-004 258
- Deployment Characteristics 259
- Section 8 261
- Operator’s Publications 263
- Ordering Publications 264
- Airworthiness Directives 266
- Airplane Inspection Periods 266
- 100-Hour Inspection 267
- 8-8 P/N 11934-004 268
- Section 8 Cirrus Design 268
- Cirrus Design Section 8 269
- P/N 11934-004 8-9 269
- Ground Handling 270
- P/N 11934-004 8-11 271
- 8-12 P/N 11934-004 272
- P/N 11934-004 8-13 273
- Leveling 274
- P/N 11934-004 8-15 275
- Servicing 276
- P/N 11934-004 8-17 277
- Tire Inflation 278
- Propeller Servicing 278
- Oil Servicing 278
- Figure 8-1 280
- Approved Oils 280
- Fuel System Servicing 281
- 8-22 P/N 11934-004 282
- Draining Fuel System 283
- Battery Service 284
- Cleaning and Care 285
- Figure 8-2 286
- P/N 11934-004 8-27 287
- 8-28 P/N 11934-004 288
- Cleaning Interior Surfaces 289
- Figure 8-3 290
- P/N 11934-004 8-31 291
- 8-32 P/N 11934-004 292
- Section 9 293
- Log of Supplements 295
- P/N 11934-S36 1 of 8 297
- Cirrus Design Section 9 297
- SR20 Supplements 297
- Revision 01: 12-18-08 297
- Section 1 - General 298
- Section 2 - Limitations 299
- Section 4 - Normal Procedures 300
- Section 5 - Performance 300
- P/N 11934-S36 5 of 8 301
- Inspection / Test 302
- P/N 11934-S36 7 of 8 303
- Control System 305
- Autopilot Malfunction 307
- Autopilot Miscompare 308
- P/N 11934-S41 7 of 16 311
- Revision 01: 08-26-09 311
- Figure - 1 312
- GFC 705 AFCS Mode Controller 313
- Altitude Hold (ALT) 10 Feet 314
- P/N 11934-S41 11 of 16 315
- SR20_FM09_2920 316
- Roll and Pitch Servo 317
- Integrated Avionics Units 317
- Autopilot Disconnect Switch 318
- Take Off / Go Around Button 318
- Pitch Trim Adapter 318
- Annunciation System 319
- No Change 320
- P/N 11934-S42 1 of 6 321
- Original Issue: 12-18-08 321
- Response To TAWS Warnings 323
- Response To TAWS Cautions 323
- System Constraints 325
- Section 10 327
- Safety Information 327
- Deployment Scenarios 330
- Cirrus Design Section 10 331
- SR20 Safety Information 331
- P/N 11934-004 10-5 331
- Landing Considerations 333
- P/N 11934-004 10-9 335
- Operating Practices 336
- Brake Maintenance 337
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