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Personnel must obey the limitations given in this chapter.
A. Airframe
A comprehensive airframe inspection is mandatory after 6,000 hours of flight.
B. Paint
It is mandatory to paint certain parts of the DA20-C1 white. This will help to keep the
temperature of the composite structure below the structural temperature limit for flight (55 C (131
F)). Paint colors, markings, and placards are subject to the following restrictions (see Figure 1):
(1) Zone I You must paint this area white. You can only paint areas of registration
marks, placards and minor trim different colors.
(2) Zone II You can paint this area any color with solar absorptivity of 0.5 or less. Or you
can paint areas of registration marks, placards and minor trim different colors on a white
background.
(3) Zone III You can paint this area any color. If you paint this area any color other than
white, you must install a structural temperature indicator (Thermindex Chemicals RTP-
55/RED). The indicator must be mounted in the area of color, close to the aircraft center
line.
Airworthiness Limitations
DA20-C1 AMM
Page 4
15 Dec 1999 04-00-00 Doc # DA201-C1
Rev. 2
Figure 1: Paint Zones
DA20-C1 AMM
Airworthiness Limitations
Doc # DA201-C1
Rev. 2 04-00-00 Page 5
15 Dec 1999
C. Engine Life Limited Components
Refer to the Teledyne Continental Form X30620 - Operator and Installation Manual - for the
engine life limited components. Replace the life Limited Components at the times indicated.
D. Aircraft Life Limited Components
Replace these components at the time shown:
Component Time Between Replacement
Rudder Control cables 3000 hours or 10 years, that which comes
first.
Engine Shock Mounts 2000 hours.
Elastomer Donuts (Nose Landing Gear) 1000 hours.
2. Component Life Tracking
To make sure that component replacement is performed at the correct time you must record the
data that follows in the Airplane Maintenance Log for each of the Life Limited Components:
− Serial numbers (where applicable).
− Flight hours and date at installation.
− Flight hours and date at removal.
Airworthiness Limitations
DA20-C1 AMM
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29 Apr 2004 04-00-00 Doc # DA201-C1
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DA20-C1 AMM
Time Limits and
Maintenance Checks
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CHAPTER 05
TIME LIMITS AND MAINTENANCE
CHECKS
Time Limits and
Maintenance Checks
DA20-C1 AMM
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Maintenance Checks
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TABLE OF CONTENTS
CHAPTER 05-00 TIME LIMITS AND MAINTENANCE CHECKS.............................................................2
1. General.......................................................................................................................2
2. Chapter Configuration ................................................................................................2
3. Words With Special Meanings....................................................................................2
CHAPTER 05-10 TIME LIMITS .............................................................................................................1
1. General.......................................................................................................................1
2. Regulatory Authorities ................................................................................................1
3. Scheduled Maintenance Time Limits .........................................................................1
4. Component Time Limits..............................................................................................2
5. Component Time Tracking .........................................................................................3
CHAPTER 05-20 SCHEDULED MAINTENANCE CHECKS ....................................................................1
1. General.......................................................................................................................1
2. Maintenance Checklist ...............................................................................................1
3. 6000 Hour Inspection .................................................................................................2
CHAPTER 05-20 Maintenance Practices Maintenance Checklist DA20-C1 ............................................5
1. General.......................................................................................................................5
　
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