Diamond DA20-C1

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DA20-C1 Flight Manual

Handling

Doc # DA202-C1 April 06, 2010 Page 8 - 6

8.4.4. Jacking

The DA20-C1 can be jacked at the two jack points located on the lower side of the fuselage's

root ribs and at the tail fin. See Figure 8.3.

Figure 8.3. Jacking Point Location

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

Diamond DA20-C1 - Jacking

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