Description
Cirrus SR20 All-Electric Airplane Information Manual (P/N 13999-003, Jan 2005)
This is the full Cirrus SR20 All-Electric Airplane Information Manual, document P/N 13999-003, dated January 2005, covering the Cirrus Design SR20 on Aircraft Serials 1268 and Subsequent. Structured exactly like the SR20 Pilot’s Operating Handbook it was harmonized with, this Airplane Information Manual walks through every operating section a pilot or owner needs for reference: general airplane data, limitations, emergency procedures, normal procedures, performance, weight and balance, and a complete systems description of the all-electric SR20 airframe.
File Details
- Manual type: Airplane Information Manual (POH-format reference)
- Aircraft: Cirrus Design SR20, All-Electric variant
- Applicability: Aircraft Serials 1268 and Subsequent
- Document Number: P/N 13999-003
- Date: January 2005
- Language: English
- Page Count: 402 pages
- File Format: PDF
Chapters Covered
- Section 1 – General: airplane data, engine and propeller specs, fuel and oil capacities, certificated weights, cabin dimensions, symbols and terminology
- Section 2 – Limitations: airspeed limitations, power plant limits, instrument markings, weight and CG limits, CAPS and system limits, kinds of operation, placards
- Section 3 – Emergency Procedures: ground emergencies, in-flight emergencies, engine failure and airstart, fire procedures, CAPS deployment, landing emergencies
- Section 4 – Normal Procedures: preflight walk-around, engine start, taxi, takeoff, climb, cruise, descent, landing, environmental considerations, noise and fuel conservation
- Section 5 – Performance Data: flight planning, sample problems, airspeed and altitude calibration, stall speeds, takeoff and landing distance, climb and cruise performance, range/endurance profiles
- Section 6 – Weight and Balance: airplane weighing procedures, weight and balance record, loading instructions, CG limits, equipment list
- Section 7 – Airplane and Systems Description: airframe, flight controls, trim systems, flight deck arrangement, cabin, landing gear, engine, propeller, fuel system, electrical system, lighting, environmental system, stall warning, pitot-static system
- Section 8 – Handling, Servicing, Maintenance: airplane records, airworthiness directives, inspection periods, ground handling, servicing, battery service, cleaning and care
- Section 9 – Supplements: log of FAA-approved supplements for optional avionics, autopilot, oxygen, and traffic/weather systems
Together these nine sections give a Cirrus SR20 owner or pilot the same organizational structure as the factory-issued Airplane Information Manual – a single reference for how the all-electric SR20 is built, limited, operated, and maintained.
Complete PDF Bookmark Tree
Complete Bookmarks
The complete bookmarks in the “Cirrus SR20 All-Electric Airplane Information Manual – Serials 1268 and Up (P/N 13999-003, Jan 2005) PDF Download” are as follows:
+SR20 Information Manual (Electric)p. 1
+Section 1 – Generalp. 3
The Airplanep. 8
Symbols, Abbreviations and Terminologyp. 10
+Section 2 – Limitationsp. 15
Certification Statusp. 17
Airspeed Limitationsp. 18
Airspeed Indicator Markingsp. 19
Power Plant Limitationsp. 20
Instrument Markingsp. 22
General Limitationsp. 23
System Limitsp. 27
Kinds of Operationp. 28
Placardsp. 32
+Section 3 – Emergency Proceduresp. 39
Airspeeds for Emergency Operationsp. 42
Emergency Procedures Guidancep. 43
Ground Emergenciesp. 45
In-Flight Emergenciesp. 47
Maximum Glidep. 48
Landing Emergenciesp. 61
System Malfunctionsp. 65
+Section 4 – Normal Proceduresp. 71
Airspeeds for Normal Operationp. 74
Normal Proceduresp. 75
Environmental Considerationsp. 93
Noise Characteristics/Abatementp. 96
Fuel Conservationp. 97
+Section 5 – Performance Datap. 99
Flight Planningp. 102
Sample Problemp. 102
Airspeed Calibrationp. 108
Airspeed Calibrationp. 109
Altitude Correctionp. 110
Altitude Correctionp. 111
Temperature Conversionp. 112
Outside Air Temperature for ISA Conditionp. 113
Stall Speedsp. 114
Wind Componentsp. 115
Takeoff Distancep. 116
Takeoff Distancep. 117
Takeoff Distancep. 118
Takeoff Climb Gradientp. 119
Takeoff Rate of Climbp. 120
Enroute Climb Gradientp. 121
Enroute Rate of Climbp. 122
Time, Fuel and Distance to Climbp. 123
Cruise Performancep. 124
Cruise Performancep. 125
Range / Endurance Profilep. 126
Range / Endurance Profilep. 127
Balked Landing Climb Gradientp. 128
Balked Landing Rate of Climbp. 129
Landing Distancep. 130
Landing Distancep. 131
+Section 6 – Weight and Balancep. 133
Airplane Weighing Formp. 138
Airplane Weighing Proceduresp. 139
Weight & Balance Recordp. 142
Loading Instructionsp. 144
Center of Gravity Limitsp. 146
Weight & Balance Loading Formp. 147
Loading Datap. 148
Moment Limitsp. 149
Equipment Listp. 150
+Section 7 – Airplane and Systems Descriptionp. 151
Airframep. 156
Wing Flapsp. 158
Primary Flight Controlsp. 160
Trim Systemsp. 166
Flight Deck Arrangementp. 168
Airplane Cabinp. 172
Landing Gearp. 178
Enginep. 181
Propellerp. 188
Fuel Systemp. 189
Electrical Systemp. 193
Exterior Lightingp. 201
Interior Lightingp. 202
Environmental Systemp. 203
Stall Warning Systemp. 206
Pitot-Static Systemp. 208
Avionics and Navigationp. 211
Cirrus Airplane Parachute Systemp. 232
+Section 8 – Handling, Servicing, Maintenancep. 237
Operator’s Publicationsp. 239
Airplane Records and Certificatesp. 241
Airworthiness Directivesp. 242
Airplane Inspection Periodsp. 243
Ground Handlingp. 246
Servicingp. 252
Battery Servicep. 260
Cleaning and Carep. 261
+Section 9 – Supplementsp. 273
+Garmin GMA 340 Audio Systemp. 275
Section 1 – Generalp. 276
Section 2 – Limitationsp. 277
Section 3 – Emergency Proceduresp. 277
Section 4 – Normal Proceduresp. 277
Section 5 – Performancep. 277
Section 6 – Weight & Balancep. 277
Section 7 – System Descriptionp. 277
+Garmin GTX 327 Transponderp. 285
Section 1 – Generalp. 286
Section 2 – Limitationsp. 287
Section 3 – Emergency Proceduresp. 287
Section 4 – Normal Proceduresp. 287
Section 5 – Performancep. 288
Section 6 – Weight & Balancep. 288
Section 7 – Systems Descriptionp. 288
+S-Tec System Thirty Autopilot with GPSSp. 293
Section 1 – Generalp. 295
Section 2 – Limitationsp. 296
Section 3 – Emergency Proceduresp. 297
Section 4 – Normal Proceduresp. 298
Section 5 – Performancep. 303
Section 6 – Weight & Balancep. 303
Section 7 – Systems Descriptionp. 304
+S-Tec System 55X Autopilot w/ Altitude Selector/Alerterp. 307
Section 1 – Generalp. 308
Section 2 – Limitationsp. 309
Section 3 – Emergency Proceduresp. 312
Section 4 – Normal Proceduresp. 314
Section 5 – Performancep. 323
Section 6 – Weight & Balancep. 323
Section 7 – Systems Descriptionp. 323
Altitude Selector / Alerterp. 327
+Avidyne EX-Series Multifunction Flight Displayp. 331
Section 1 – Generalp. 332
Section 2 – Limitationsp. 334
Section 3 – Emergency Proceduresp. 335
Section 4 – Normal Proceduresp. 335
Section 5 – Performancep. 335
Section 6 – Weight & Balancep. 336
Section 7 – Systems Descriptionp. 336
+Garmin GNS 430 GPS Navigatorp. 343
Section 1 – Generalp. 344
Section 2 – Limitationsp. 345
Section 3 – Emergency Proceduresp. 346
Section 4 – Normal Proceduresp. 346
Section 5 – Performancep. 349
Section 6 – Weight & Balancep. 349
Section 7 – Systems Descriptionp. 349
+Garmin GNC 420 GPS Navigatorp. 353
Section 1 – Generalp. 354
Section 2 – Limitationsp. 355
Section 3 – Emergency Proceduresp. 356
Section 4 – Normal Proceduresp. 356
Section 5 – Performancep. 357
Section 6 – Weight & Balancep. 357
Section 7 – Systems Descriptionp. 357
+Avidyne Entegra-Series Primary Flight Displayp. 361
Section 2 – Limitationsp. 364
Section 3 – Emergency Proceduresp. 367
Section 4 – Normal Proceduresp. 369
Section 5 – Performancep. 369
Section 6 – Weight & Balancep. 369
Section 7 – System Descriptionp. 370
+S-Tec System 55SR Autopilotp. 377
Section 1 – Generalp. 378
Section 2 – Limitationsp. 379
Section 3 – Emergency Proceduresp. 382
Section 4 – Normal Proceduresp. 384
Section 5 – Performancep. 389
Section 6 – Weight & Balancep. 389
Section 7 – Systems Descriptionp. 389
+Section 10 – Safety Informationp. 393
Cirrus Airframe Parachute System (CAPS) Deploymentp. 396
Specifications Referenced Inside
- Engine: Teledyne Continental IO-360-ES, 6-cylinder, air-cooled, horizontally opposed, direct drive, 200 hp @ 2700 rpm
- Propeller: Hartzell constant-speed, two-blade and three-blade options listed with model numbers and diameters
- Fuel: 60.5 U.S. gallon total capacity, 56 U.S. gallon usable, 100LL / 100 grade aviation fuel
- Weights: 3000 lb max gross takeoff, 2900 lb max landing, 950 lb max useful load
Why Pilots and Owners Use This Manual
The Cirrus SR20 All-Electric Airplane Information Manual lays out the airspeed limitations, emergency checklists, normal operating flows, and performance charts a pilot references before and during flight, plus the weight and balance and systems descriptions an owner needs to understand how the all-electric SR20’s electrical, fuel, and flight control systems work together. Having the correct figures and procedures on hand – rather than relying on memory or a mismatched revision – matters for safe, informed operation of this specific serial range.
This Cirrus SR20 Information Manual downloads instantly as a PDF after checkout – no shipping, no waiting. Read it on a laptop, tablet, or phone, or print any section you want in the hangar or cockpit bag.
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