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P/N 13999-002 Info Manual 7-43
Cirrus Design Section 7
SR20 Airplane Description
The airplane may be serviced to a reduced capacity to permit heavier
cabin loadings. This is accomplished by filling each tank to a tab
visible below the fuel filler, giving a reduced fuel load of 13 gallons
usable in each tank (26 gallons total usable in all flight conditions).
Drain valves at the system low points allow draining the system for
maintenance and for examination of fuel in the system for
contamination and grade. The fuel must be sampled prior to each
flight. A sampler cup is provided to drain a small amount of fuel from
the wing tank drains, the collector tank drains, and the gascolator
drain. If takeoff weight limitations for the next flight permit, the fuel
tanks should be filled after each flight to prevent condensation.
Fuel Selector Valve
A fuel selector valve, located at the rear of the center console,
provides the following functions:
• LEFT...................................Allows fuel to flow from the left tank
• RIGHT .............................Allows fuel to flow from the right tank
• OFF ........................................Cuts off fuel flow from both tanks
The valve is arranged so that to feed off a particular tank the valve
should be pointed to the fuel indicator for that tank. To select RIGHT or
LEFT, rotate the selector to the desired position. To select Off, first
raise the fuel selector knob release and then rotate the knob to OFF.
Fuel Quantity Indicator
A dual reading 2¼” fuel quantity indicator is installed on the console
immediately forward of the fuel selector valve. The LEFT pointer
indicates left tank fuel quantity and sweeps a scale marked from 0 to
28 U.S. gallons in 2½-gallon increments. The RIGHT pointer sweeps
an identical scale for the right tank. Each scale is marked with a yellow
arc from 0 to 8.2 gallon. The indicators are calibrated to read ‘0’ when
no usable fuel remains. Each indicator also provides an output signal
to illuminate the FUEL caution light when the fuel quantity goes below
approximately 8-9 gallons in each tank. The indicator is internally
lighted. 28 VDC for fuel quantity system operation is supplied through
the 5-amp ENGINE INST circuit breaker on the Essential Bus.
• Note •
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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