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must do the inspection procedure specified for a moving propeller strike.
− Inspect the airplane for damage.
4. Engine Fire
WARNING: BEFORE YOU DO WORK ON THE AIRPLANE MAKE SURE THE FIRE
HAS BEEN EXTINGUISHED. LET THE ENGINE COOL AND
DISCONNECT THE BATTERY.
WARNING: FIRE CAN SERIOUSLY WEAKEN GFRP. IF YOU FIND ANY DAMAGE
TO GFRP, DO NOT OPERATE THE AIRCRAFT. ASK THE
MANUFACTURER FOR ADVICE
Maintenance Work References/Key Items
1 Disconnect the battery. Refer to Chapter 24-31.
2 Remove the engine cowlings. Refer to Chapter 71-10.
3 Examine the engine cowlings. Look
especially for signs of fire damage.
DA20-C1 AMM
Time Limits and
Maintenance Checks
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Rev. 9 05-50-00 Page 5
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Maintenance Work References/Key Items
4. Examine the electrical cables. Look
especially for signs of fire damage.
Replace damaged cables.
1 Examine the fuel pipes. Look especially for
signs of fire damage to the fire-protection
sleeves.
Replace damaged fuel pipes.
2 Examine the engine oil pipes. Look
especially for signs of fire damage to the fireprotection
sleeves.
Replace damaged oil pipes.
3 Examine the engine. Look especially for:
− Damage to the engine air filter.
− Damage to gaskets and seals.
− Damage to the engine mounts.
− Damage to pipes/hoses.
Replace damaged items.
4 Examine the fuselage. Look especially for:
− Blisters on the paint or burn marks.
− Disbonding of the fuselage skin from the
firewall.
If you find any damage, ask the
airplane manufacturer for advice.
WARNING: DO NOT GET FIRE EXTINGUISHER PARTICLES ON YOU.
THE CHEMICALS USED TO EXTINGUISH A FIRE CAN BE
CAUSTIC/POISONOUS. WHEN YOU CLEAN THE ENGINE
REFER TO THE FIRE EXTINGUISHER MANUFACTURERS
SAFETY INSTRUCTIONS. USE SAFETY MASKS AND
GLOVES AS RECOMMENDED.
9. Clean the engine. Make sure you clean all
the fire extinguisher particles from the engine.
Refer to the manufacturer of the fire
extinguisher.
10. Connect the battery. Refer to Chapter 24-31.
1 Troubleshoot the engine. Find the cause of
the engine fire.
− Repair the defect.
Refer to the Teledyne Continental
Motors IO-240B Maintenance Manual.
2 Do a test of the engine. Refer to the DA20-C1 Flight Manual.
Time Limits and
Maintenance Checks
DA20-C1 AMM
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DA20-C1 AMM
Dimensions And Areas
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CHAPTER 06
DIMENSIONS AND AREAS
Dimensions And Areas
DA20-C1 AMM
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TABLE OF CONTENTS
CHAPTER 06-00 DIMENSIONS AND AREAS .........................................................................................1
1. General................................................................................................................................1
A. Unit Conversions..................................................................................................................1
2. Dimensions..........................................................................................................................3
3. Adjustment Values ...............................................................................................................7
4. Control Surface Gaps...........................................................................................................7
5. Weight And Static Moments Of Control Surfaces ................................................................7
Dimensions And Areas
DA20-C1 AMM
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CHAPTER 06-00
DIMENSIONS AND AREAS
1. General
The DA 20-C1 uses the System Internationale (SI) for dimensions and areas. Imperial dimensions
are also given in brackets. For example: Wing span 10.78 m (35.4 ft).
A. Unit Conversions
Units/Abbreviations Conversion Factor
Length
Meter [m]
Millimeter [mm]
Foot [ft]
Inch [in]
[mm] / 25.4 = [in]
[cm] / 2.54 = [in]
[m] / 0.3048 = [ft]
Mass/Force
Kilogram [kg]
Pound [lb(s)]
[kg[ / 0.45359 = [lbs]
[daN] / 0.44482 = [lbs]
Moment
　
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