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P/N 13999-002 Info Manual 7-53
Cirrus Design Section 7
SR20 Airplane Description
Low Volts Warning Light
The airplane is equipped with a red LOW VOLTS warning light in the
annunciator panel located on the left side of the instrument panel. The
alternator control unit (ACU) located within the master control unit
(MCU), which is mounted on the engine side of the firewall, operates
the warning light.
In the event an over voltage condition occurs, the alternator control
unit (ACU) automatically removes alternator field current to shut down
the alternator. With the alternator off line, the battery supplies system
current and a discharge rate is indicated on the ammeter. Under these
conditions, depending on electrical system load, the LOW VOLTS
warning light will illuminate when system voltage drops below 25.5 ±
0.35 volts. Turning the ALT MASTER switch off and back on again may
reset the alternator control unit. If the warning light does not illuminate,
normal alternator charging has resumed. If the light illuminates again,
a malfunction has occurred.
• Note •
Illumination of the LOW VOLTS warning light and ammeter
discharge indications may occur during low RPM conditions
with an electrical load on the system, such as during a low
RPM taxi. Under these conditions, the light will go out at
higher RPM. The master switch need not be recycled since an
over voltage condition has not occurred to de activate the
alternator system.
Warning light operation can be tested by turning the landing light on
and momentarily turning off the master switch ALT portion while
leaving the BAT portion ON.
September 2011
- CIRRUS DESIGN SR20 1
- Cirrus Design Corporation 2
- 4515 Taylor Circle 2
- Duluth, MN 55811 2
- Section 1 3
- Figure 1-1 6
- Airplane Three View 6
- Figure 1-2 7
- Turning Radius 7
- The Airplane 8
- P/N 13999-002 Info Manual 1-7 9
- Cirrus Design Section 1 9
- SR20 General 9
- Meteorological Terminology 11
- Engine Power Terminology 12
- Section 1 Cirrus Design 14
- General SR20 14
- Section 2 15
- Limitations 15
- Certification Status 17
- Airspeed Limitations 18
- Airspeed Indicator Markings 19
- Power Plant Limitations 20
- Weight Limits 21
- Instrument Markings 22
- Center of Gravity Limits 23
- Maneuver Limits 24
- Flight Load Factor Limits 24
- Minimum Flight Crew 24
- Kinds of Operation 25
- Runway Surface 28
- Fuel Limits 29
- Altitude Limits 29
- Environmental Conditions 29
- Maximum Occupancy 29
- Systems and Equipment Limits 30
- Oxygen System 31
- Inflatable Restraint System 31
- Flap Limitations 31
- Other Limitations 32
- Placards 33
- EXTERNAL 34
- SR20_FM02_1222E 35
- SR20_FM02_1520B 36
- Figure 2-5 37
- Placards (Sheet 5 of 9) 37
- GRAB HERE 38
- Placards (Sheet 7 of 9) 39
- 12390-001 40
- 12390-002 40
- Placards (Sheet 9 of 9) 41
- Section 3 43
- Emergency Procedures 43
- 3-2 P/N 13999-002 Info Manual 44
- Section 3 Cirrus Design 44
- Emergency Procedures SR20 44
- 3-4 P/N 13999-002 Info Manual 46
- Emergency Procedures Guidance 47
- Memory Items 48
- Ground Emergencies 49
- Emergency Ground Egress 50
- In-Flight Emergencies 51
- Maximum Glide 52
- Engine Failure In Flight 53
- Engine Airstart 54
- Engine Partial Power Loss 55
- Low Oil Pressure 57
- Propeller Governor Failure 57
- Smoke and Fume Elimination 58
- Engine Fire In Flight 58
- Wing Fire In Flight 58
- Cabin Fire In Flight 59
- Emergency Descent 60
- Cirrus Design Section 3 61
- SR20 Emergency Procedures 61
- CAPS Deployment 62
- • WARNING • 63
- Landing Emergencies 65
- Ditching 66
- System Malfunctions 68
- Vacuum System Failure 69
- Section 3A 71
- Abnormal Procedures 71
- Abnormal Procedures Guidance 74
- Ground Procedures 75
- Landing Procedures 77
- Cirrus Design Section 3A 79
- SR20 Abnormal Procedures 79
- Communications Failure 80
- Pitot Static Malfunction 81
- Section 3A Cirrus Design 82
- Abnormal Procedures SR20 82
- Section 4 83
- Normal Procedures 83
- 4-4 P/N 13999-002 Info Manual 86
- Preflight Walk-Around 88
- P/N 13999-002 Info Manual 4-7 89
- 4-8 P/N 13999-002 Info Manual 90
- P/N 13999-002 Info Manual 4-9 91
- Before Starting Engine 92
- Starting Engine 93
- Before Taxiing 95
- Before Takeoff 96
- Normal Takeoff 99
- Short Field Takeoff 99
- Section 4 Cirrus Design 100
- Normal Procedures SR20 100
- September 2011 100
- Cirrus Design Section 4 101
- SR20 Normal Procedures 101
- Cruise Leaning 102
- Before Landing 103
- Balked Landing/Go-Around 104
- After Landing 105
- Shutdown 105
- Environmental Considerations 107
- Hot Weather Operation 109
- Fuel Conservation 110
- Section 5 111
- Performance Data 111
- 5-2 P/N 13999-002 Info Manual 112
- Section 5 Cirrus Design 112
- Performance Data SR20 112
- Introduction 113
- Flight Planning 114
- Sample Problem 114
- P/N 13999-002 Info Manual 5-5 115
- Cirrus Design Section 5 115
- SR20 Performance Data 115
- 5-6 P/N 13999-002 Info Manual 116
- P/N 13999-002 Info Manual 5-7 117
- Fuel Required 118
- P/N 13999-002 Info Manual 5-9 119
- Airspeed Calibration 120
- Altitude Correction 122
- Temperature Conversion 124
- Outside Air Temperature 125
- ISA Condition 125
- Stall Speeds 126
- Wind Components 127
- Takeoff Distance 128
- Takeoff Climb Gradient 131
- Takeoff Rate of Climb 132
- Enroute Climb Gradient 133
- Enroute Rate of Climb 134
- Figure 5-14 135
- Figure 5-15 136
- Factors: 136
- Cruise Performance 137
- Range / Endurance Profile 139
- Balked Landing Climb Gradient 141
- Balked Landing Rate of Climb 142
- Landing Distance 143
- Section 6 145
- Weight and Balance 145
- Intentionally Left Blank 146
- Figure 6-1 148
- Airplane Dimensional Data 148
- Figure 6-2 149
- Airplane Leveling 149
- Airplane Weighing Form 150
- Airplane Weighing Procedures 151
- 6-8 P/N 13999-002 Info Manual 152
- Section 6 Cirrus Design 152
- Weight & Balance SR20 152
- P/N 13999-002 Info Manual 6-9 153
- Cirrus Design Section 6 153
- SR20 Weight & Balance 153
- Weight & Balance Record 154
- Figure 6-5 155
- Airplane Interior Dimensions 155
- Loading Instructions 156
- Figure 6-6 158
- Loading Data 159
- Moment Limits 160
- Equipment List 161
- Section 7 163
- 7-2 P/N 13999-002 Info Manual 164
- Section 7 Cirrus Design 164
- Airplane Description SR20 164
- P/N 13999-002 Info Manual 7-3 165
- Airframe 168
- Empennage 169
- Flight Controls 170
- Figure 7-1 171
- Elevator Control System 171
- Aileron System 172
- Figure 7-2 173
- Aileron Control System 173
- Rudder System 174
- Figure 7-3 175
- Rudder Control System 175
- Trim Systems 176
- Yaw Trim System 177
- Flight Deck Arrangement 178
- Instrument Panel and Console 179
- Figure 7-4 179
- Flight Instruments 180
- Vertical Speed Indicator 181
- Altimeter 181
- Turn Coordinator 181
- Directional Gyro 182
- Course Deviation Indicator 183
- Magnetic Compass 185
- Wing Flaps 186
- Figure 7-5 187
- Flap Control System 187
- Landing Gear 188
- Airplane Cabin 189
- Figure 7-6 190
- Cabin General Arrangement 190
- Cirrus Design Section 7 191
- SR20 Airplane Description 191
- Windshield and Windows 192
- Cabin Safety Equipment 192
- Engine Oil System 195
- Engine Cooling 195
- Engine Fuel Injection 196
- Engine Air Induction System 196
- Engine Fuel Ignition 196
- Engine Exhaust 197
- Engine Controls 197
- Alternate Air Control 198
- Engine Indicating 198
- Figure 7-7 199
- Propeller 202
- Fuel System 203
- Figure 7-8 204
- Fuel Selector Valve 205
- Fuel Quantity Indicator 205
- Fuel Flow Indication 206
- Fuel Caution Light 206
- Boost Pump Switch 206
- Brake System 208
- Figure 7-9 209
- Electrical System 211
- Figure 7-10 212
- Power Distribution 213
- BAT & ALT Master Switches 213
- Avionics Power Switch 214
- Volt / Amp Meter 214
- Low Volts Warning Light 215
- Circuit Breakers and Fuses 216
- Ground Service Receptacle 216
- Convenience Outlet 216
- Exterior Lighting 217
- Interior Lighting 218
- Environmental System 219
- Figure 7-11 220
- Heating and Ventilation 220
- Cabin Heat Control 221
- Cabin Cooling Control 221
- Cabin Air Selector 221
- Figure 7-12 222
- Pitot-Static System 222
- Vacuum System 224
- Figure 7-13 225
- Suction Gauge 226
- Vacuum Warning Light 226
- Aux Vac Caution Light 226
- Stall Warning System 227
- Standard Avionics 228
- Multi-Function Display 230
- Autopilot 232
- GPS Navigation 234
- Navigation (Nav) Receiver 236
- Transponder 236
- Audio System 237
- Emergency Locator Transmitter 238
- Hour Meter 239
- Digital Clock 240
- System Description 242
- Activation Handle 243
- Deployment Characteristics 244
- Section 8 247
- Operator’s Publications 249
- Ordering Publications 250
- P/N 13999-002 Info Manual 8-5 251
- Cirrus Design Section 8 251
- Airworthiness Directives 252
- Airplane Inspection Periods 252
- 100-Hour Inspection 253
- 8-8 P/N 13999-002 Info Manual 254
- Section 8 Cirrus Design 254
- P/N 13999-002 Info Manual 8-9 255
- Ground Handling 256
- Leveling 260
- Servicing 262
- Tire Inflation 264
- Propeller Servicing 264
- Oil Servicing 265
- Figure 8-1 267
- Approved Oils 267
- Fuel System Servicing 268
- Draining Fuel System 270
- Battery Service 271
- Cleaning and Care 272
- Figure 8-2 273
- Cleaning Interior Surfaces 276
- Figure 8-3 277
- Section 9 281
- Supplements 281
- Log of Supplements 283
- Garmin GMA 340 Audio System 285
- Section 1 - General 286
- Audio/Transceiver Selection 288
- Speaker Output 289
- Public Address (PA) Function 289
- Personal Music Inputs 289
- Intercom 290
- P/N 11934-S01 7 of 10 291
- Cirrus Design Section 9 291
- SR20 Supplements 291
- Revision 02: 07-18-05 291
- Marker Beacon 292
- P/N 11934-S01 9 of 10 293
- 10 of 10 P/N 11934-S01 294
- Section 9 Cirrus Design 294
- Supplements SR20 294
- Dual Alternator System 295
- Section 2 - Limitations 296
- Alternator Failure 297
- 4 of 10 P/N 11934-S10 298
- Original: 09-28-99 298
- Section 5 - Performance 299
- Power Generation 300
- Low-Volts Warning Light 302
- ALT FAIL Lights 302
- 10 of 10 P/N 11934-S10 304
- L-3 Avionics Systems WX500 305
- Stormscope Sensor 305
- Section 1 General 306
- Garmin GTX 327 Transponder 309
- Section 4 - Normal Procedures 311
- Mode Selector Keys 313
- Code Selector Keys 314
- Reply Light 315
- IDENT Key 315
- FUNC Key 315
- 8 of 8 P/N 11934-S12 316
- Original: 12-26-00 316
- S-Tec System 55X Autopilot 317
- 4 of 16 P/N 11934-S13 320
- Revision 04: 08-15-07 320
- Figure - 1 321
- Autopilot Malfunction 322
- P/N 11934-S13 7 of 16 323
- In-Flight Procedures 325
- 10 of 16 P/N 11934-S13 326
- P/N 11934-S13 11 of 16 327
- 12 of 16 P/N 11934-S13 328
- 14 of 16 P/N 11934-S13 330
- P/N 11934-S13 15 of 16 331
- 16 of 16 P/N 11934-S13 332
- Traffic Advisory System 333
- Respond to Traffic Advisories 336
- 6 of 6 P/N 11934-S15 338
- Revision 01: 10-12-05 338
- Garmin GNS 430 GPS Navigator 339
- Section 2 – Limitations 341
- GNS 430 Integration 343
- 6 of 10 P/N 11934-S22 344
- Revision 02: 08-15-07 344
- GPS Navigator 346
- TERRAIN Interface* 348
- Garmin GNC 420 GPS Navigator 349
- Honeywell KGP 560 Terrain/ 357
- Awareness Warning System 357
- Activate TAWS 360
- 6 of 12 P/N 11934-S30 362
- Revision 01: 12-15-07 362
- TAWS Annunciator Panel 364
- Alert Priority 364
- Advisory Callout 364
- Figure - 2 365
- 10 of 12 P/N 11934-S30 366
- P/N 11934-S30 11 of 12 367
- Self Test 368
- Avidyne EMax™ Engine 369
- Instrumentation 369
- 4 of 4 P/N 11934-S31 372
- Avidyne CMax™ Electronic 373
- Approach Charts 373
- 4 of 4 P/N 11934-S32 376
- XM Satellite Weather System 377
- 4 of 4 P/N 11934-S33 380
- Section 10 381
- Safety Information 381
- Deployment 384
- Cirrus Design Section 10 385
- SR20 Safety Information 385
- Landing Considerations 387
- Section 10 Cirrus Design 388
- Safety Information SR20 388
- Proper Operating Practices 390
- Brake Maintenance 391
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