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2-6 P/N 13999-002 Info Manual
Section 2 Cirrus Design
Limitations SR20
Power Plant Limitations
Engine
Teledyne Continental ............................................................IO-360-ES
Power Rating ........................................................ 200 hp @ 2700 rpm
Maximum RPM .......................................................................2700 rpm
Oil:
Oil Temperature.................................... 240° F (115° C) maximum
Oil Pressure:
Minimum................................................................................ 10 psi
Maximum............................................................................. 100 psi
Approved Oils:
Engine Break-In: For first 25 hours of operation or until oil
consumption stabilizes use straight mineral oil conforming to MIL-
L-6082. If engine oil must be added to the factory installed oil, add
only MIL-L-6082 straight mineral oil.
After Engine Break-In: Use only oils conforming to Teledyne
Continental Specification MHS-24 (Ashless Dispersant Lubrication
Oil) or MHS-25 (Synthetic Lubrication Oil). Refer to Section 8 - Oil
Servicing. Oil viscosity range as follows:
All Temperatures ..............................................15W-50 or 20W-50
Above 40° F (4° C).............................................. SAE 50 or 20W50
Below 40° F (4° C) ................. SAE 30, 10W-30, 15W50, or 20W50
Fuel Grade ................Aviation Grade 100 LL (Blue) or 100 (green)
• Note •
Refer to General Limitations – Fuel Limits in this section for
operational limitations regarding fuel and fuel storage.
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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