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replacement date in the airplane log-book.
(12) Do a functional test of the ELT. Refer to Paragraph 3.
DA20-C1 AMM
Equipment/Furnishings
Doc # DA201-C1
Rev. 15 25-60-01 Page 205
30 Apr 2009
5. ELT Periodic Inspection
The ELT installation must be inspected at least once every 12 months to maintain serviceability.
Detail Steps/Work Items Key Items
(1) Examine the ELT and the ELT mounting
tray, look specially for:
• Security of the fasteners.
• Security of all mechanical assemblies
(2) Examine the cable which connects the ELT.
Look specially for:
• Cuts or abrasions to the outer sheath
of the cable.
(3) Read the expiry date of the system battery
and replace the battery if necessary
Refer to Paragraph 4.
Equipment/Furnishings
DA20-C1 AMM
Page 206
30 Apr 2009 25-60-01 Doc # DA201-C1
Rev. 15
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DA20-C1 AMM
Fire Protection
Doc # DA 201-C1
Rev. 0 26-TITLE Page 1
19 Dec 1997
CHAPTER 26
FIRE PROTECTION
Fire Protection
DA20-C1 AMM
Page 2
19 Dec 1997 26-TITLE Doc # DA 201-C1
Rev. 0
Intentionally left blank
DA20-C1 AMM
Fire Protection
Doc # DA 201-C1
Rev. 0 26-CONTENTS Page 1
19 Dec 1997
TABLE OF CONTENTS
CHAPTER 26-00 FIRE PROTECTION - GENERAL ......................................................................1
1. General .............................................................................................................................1
2. Description ........................................................................................................................1
Fire Protection
DA20-C1 AMM
Page 2
19 Dec 1997 26-CONTENTS Doc # DA 201-C1
Rev. 0
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DA20-C1 AMM
Fire Protection
Doc # DA 201-C1
Rev. 0 26-00-00 Page 1
19 Dec 1997
CHAPTER 26-00
FIRE PROTECTION - GENERAL
1. General
This Chapter tells you only about the fire extinguisher installed in the airplane. See the
manufacturers manual for more data about the fire extinguisher.
2. Description
Figure 1 shows the installation of the fire extinguisher in the airplane. The fire extinguisher is
located behind the right seat in the baggage compartment. Bolts attach the mounting bracket for
the fire extinguisher to the baggage compartment floor. The extinguisher uses a dry powder which
is non-toxic. The powder does not leave a residue.
The only on-airplane maintenance is:
− Monitor the pressure indicator. It must show in the green sector.
− Make sure that the seal wire is not broken.
− Make sure that the extinguisher is correctly held in the mounting.
If the seal wire is broken, remove the extinguisher for weighing. Weight data is given on the
extinguisher body.
You must replace the extinguisher (or return it to the manufacturer for repair):
− When the weight is incorrect.
− When the pressure is too low.
− When the extinguisher has been used.
Fire Protection
DA20-C1 AMM
Page 2
19 Dec 1997 26-00-00 Doc # DA 201-C1
Rev. 0
Figure 1: Fire Extinguisher Installation
DA20-C1 AMM
Flight Controls
Doc # DA201-C1
Rev. 0 27-TITLE Page 1
19 Dec 1997
CHAPTER 27
FLIGHT CONTROLS
Flight Controls
DA20-C1 AMM
Page 2
19 Dec 1997 27-TITLE Doc # DA201-C1
Rev. 0
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DA20-C1 AMM
Flight Controls
Doc # DA201-C1
Rev. 0 27-CONTENTS Page 1
19 Dec 1997
TABLE OF CONTENTS
CHAPTER 27-00 FLIGHT CONTROLS....................................................................................................1
1. General.......................................................................................................................1
2. Description..................................................................................................................1
3. Control Rods...............................................................................................................1
MAINTENANCE PRACTICES ....................................................................................................201
1. General...................................................................................................................201
2. Remove/Install The Control Stick ...........................................................................201
CHAPTER 27-10 FLIGHT CONTROLS - AILERONS AND TABS .................................................1
1. General.......................................................................................................................1
 
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