Diamond DA20-C1 - Viscosity Table

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DA20-C1 Flight Manual

General

Doc # DA202-C1 April 06, 2010 Page 1 - 7

Table 2

The viscosity should be selected according to the various climatic conditions using Table 2.

Use only the oils specified TCM specification MHS 24

Oil Capacity: Maximum : 6.0 US qt (5.68 liters)

Minimum : 4.0 US qt (3.78 liters)

Revision 25

Main Page

Default Chapter5
- Table of Contents5
- List of Effective Pages7
- Record of Revisions11
- Revision Log17
- Revision Highlights19
- General Information23
- Certification Basis24
Chapter 1 General24
- Introduction24
- Warnings, Cautions, and Notes24
Operating Limitations37
- Airspeed Limitations38
- Airspeed Indicator Markings38
Chapter 238
- Introduction38
- Power Plant Limitations39
- Engine39
- Additional for Aircraft Equipped with Altitude Compensating Fuel System40
- Propeller40
- Powerplant Instrument Markings41
Chapter 359
- Engine Failures59
Chapter 474
- Introduction74
- Structural Temperature Indicator75
- Normal Operation Checklist77
- Preflight Inspection77
Normal Operating Procedures74
Chapter 594
- Introduction94
- Nose Data105
Weight and Balance / Equipment List107
Chapter 6108
- Introduction108
- Description of the Airplane and Its Systems125
Chapter 7127
- Empennage127
- Fuselage127
Introduction127
- Wings127
- Flaps128
Airframe127
Flight Controls128
- Trim System128
- Flap Position Indicator129
- Pedal Adjustment129
- Flight Control Lock130
- INSTRUMENT PANEL (See Figure 7.2)131
- Cabin Air132
- Cabin Heat132
- Flight Instruments132
Landing Gear System133
- Parking Brake133
- Wheel Brakes133
- Brake System Schematic Diagram134
Seats and Safety Belts135
Baggage Compartment135
Canopy136
- Canopy View137
Powerplant138
- Engine Controls138
- Mixture Control139
  - Wood Propeller139
  - Lubricating140
- Oil System Schematic Diagram140
Fuel System141
- Fuel System Schematic Diagram142
- Fuel Dipstick143
- Fuel Filter Bowl Drain143
- Fuel Shut-Off Valve143
- Tank Drain143
- Electric Fuel Pump (Priming Pump) Operation144
  - Fuel Prime144
  - Fuel Pump144
Electrical System145
- To Check the Fuel Level144
- Electical System Simplified Schematic145
- Ignition System145
- Power Supply145
- Ammeter146
- Electrical Powered Equipment146
- Generator Warning Light146
- Instruments146
- Voltmeter146
- Illumination Pattern and Adjustment Diagrams147
- Internal Lighting147
Pitot and Static Pressure Systems148
Stall Warning System148
- Handling, Preventive and Corrective Maintenance149
- Airplane Alterations or Repairs150
- Airplane Inspection Period150
Avionics148
Chapter 8150
- Introduction150
- Ground Handling151
- Supplements159
External Power Operation161
Chapter 9162
- General162
Winterization Kit171
- Winterization Kit: Operating Limitations172
Supplement 2172
- General172
Description of the Airplane and Its Systems174
- Handling, Preventive and Corrective Maintenance174
Recognition Lights175
- The Winterization Kit Components174
- Winterization Kit: Handling, Preventative and Corrective Maintenance174
- Recognition Lights: Airplane Performance176
- Recognition Lights: Normal Procedures176
- Recognition Lights: Operating Limitatios176
- Recognition Lights: Weight and Balance176
- April 16, 2009177
  - The Recognition Light System Description177
  - The Recognition Light System Handling, Preventative and Corrective Maintenance178
Gross Weight Increase (800 Kg)179
- Doc # DA202-C1 Revision179
- Operating Limitations Data180
Supplement 4180
- General180
- Revision182
S-Tec Autopilot195
- S-Tec Autopilot Operating Limitations196
- S-Tec Autopilot Placards196
Supplement196
- General196
Auxiliary Fuel System213
- Auxiliary Fuel System: Emergency Procedures214
- Auxiliary Fuel System: Operating Limitations214
- Auxiliary Fuel System: Normal Procedures215
- Auxiliary Fuel Moment Chart216
- Auxiliary Fuel System: Weight and Balance216
- Auxiliary Tank Fuel Transfer216
- Auxiliary Fuel System: Description of the Airplane and Its Systems217
- Auxiliary Fuel System: Handling, Preventative and Corrective Maintenance218
Stick Mounted Trim Switches219
- Control Stick Grip (Left Hand Shown) View221
- Stick Mounted Trim Switches: Description of the Airplane and Its Systems221
- Stick Mounted Trim Switches: Handling, Preventative and Corrective Maintenance221
- 20 US Gallon Fuel Tank223
- 20 US Gallon Fuel Tank: Operating Limitations224
- 20 US Gallon Fuel Tank: Performance224
- 20 US Gallon Fuel Tank: Weight and Balance224
- 20 US Gallon Fuel Tank: Description of the Airplane and Its Systems225
Reversed Instrument Panel227
- Reversed Instrument Panel: Description of the Airplane and Its Systems229
Pitot Heat Operation231
- Reversed Instrument Panel: Operating Limitations233
- Reversed Instrument Panel: Emergency Procedures234
- Reversed Instrument Panel: Normal Procedures234
- Reversed Instrument Panel: Normal Operation Checklist235
- Airplane and Its Systems236
- Pitot Heat Description236
Brazilian Placards and Markings237
Garmin G500 Integrated Display System245
- Cockpit Reference Guide247
- G500 System Software Requirements247
- Aerobatic Maneuvers248
- AHRS Operational Area248
- G500: Kinds of Operation248
- Navigation Angle248
- Garmin G500: Placards249
- G500: Emergency Procedures253
- Abnormal Indications254
- AHRS Failure254
- Air Data Computer (ADC) Failure254
- Loss of Electrical Power254
- Warnings, Cautions and Advisories255
- G500: Normal Operation Procedures257
- PFD Bezel Keys258
- PFD Knob and Soft Keys258
- MFD Knobs and MFD Soft Keys259
- PFD Soft Keys259
- AHRS Normal Operating Mode260
- MFD Bezel Keys260
- MFD Knobs260
- MFD Soft Keys260
- Autopilot Operations261
- Course Pointer Auto Slewing261
- Mass and Balance261
- Performance261
  - Synthetic Vision Technology (SVT)261
  - Terrain Display261
  - G500: Description of the Airplane and Its Systems262
  - Major Instruments and Controls263
  - Avionics – General (G500)264
  - Gdc 74A Adc264
  - GDU 620 Display264
  - Grs 77 Ahrs264
  - GMU 44 Magnetometer265
  - Gns 430W Gps265
  - G500 System Overview with Optional and Required Equipment266
  - Airplane Handling, Care and Maintenance267

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