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Adjustment Report. The value must be as shown in the
Control Surfaces Adjustment Report.
(17) If the pre-load is not correct, adjust the control rod
between the bellcrank in the wing and the flap
horn. Do items 16 & 17 again as necessary.
Refer to Section 27-00.
(18) Do items 16 & 17 for the right flap.
(19) Do a test of the flap system. Refer to Paragraph 3.
(20) Do an inspection of all the controls that you have
adjusted.
S If necessary for your airworthiness authority,
do a second inspection of the controls.
(21) Install these items:
S The passenger seat.
S The flap bellcrank access panels.
Refer to Section 25-10.
Refer to Section 53-40.
AIRCRAFT
Flight Controls DA 40 Series
AMM
Page 208
20 Sep 2007 27-50-00 Doc # 6.02.01
Rev. 5
5. Flap Push-Rod Access
Flap Push-Rod Remove/Install Access References
Between the idler lever at the rear
main bulkhead and the wing root rib.
Passenger seat.
Center section access panels.
Refer to Section 25-10.
Refer to Section 52-40.
Between the wing root rib and the
bellcrank in the left/right wing.
Center section access panels.
Flap bellcrank access panels
under each wing.
Refer to Section 52-40.
Between the bellcrank in the left/right
wing and the flap.
Flap bellcrank access panels
under each wing.
Refer to Section 52-40.
6. Flap Bellcrank and Lever Access
Flap Bellcrank/Lever Remove/Install Access References
Idler lever at the rear main bulkhead. Passenger seat. Refer to Section 25-10.
Bellcrank in the wing. Flap bellcrank access panels
under each wing.
Refer to Section 52-40.
AIRCRAFT
DA 40 Series
AMM
Fuel System
Doc # 6.02.01
Rev. 5 28-TITLE Page 1
20 Sep 2007
CHAPTER 28
FUEL SYSTEM
AIRCRAFT
Fuel System
DA 40 Series
AMM
Page 2
20 Sep 2007 28-TITLE Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Fuel System
Doc # 6.02.01
Rev. 5 28-CONTENTS Page 1
20 Sep 2007
TABLE OF CONTENTS
CHAPTER 28
FUEL SYSTEM
Section 28-00
Fuel System - Lycoming Engine
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
% 2. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
% 3. Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
Section 28-01
Fuel System - TAE 125 Diesel Engine
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
3. Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
Section 28-10
Fuel Storage System - Lycoming Engine
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
Trouble-Shooting
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 101
AIRCRAFT
Fuel System
DA 40 Series
AMM
Page 2
20 Sep 2007 28-CONTENTS Doc # 6.02.01
Rev. 5
Maintenance Practices
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
2. Remove/Disassemble the Fuel Tank Assembly . . . . . . . . . . . . . . 201
3. Assemble/Install the Fuel Tank Assembly . . . . . . . . . . . . . . . . . . 206
4. Test the Fuel Storage and Distribution System . . . . . . . . . . . . . . 210
Section 28-11
Fuel Storage System - TAE 125 Diesel Engine
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Fuel Tank Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
3. Fuel Filler Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
Trouble-Shooting
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 101
Maintenance Practices
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
2. Remove/Disassemble the Fuel Tank Assembly . . . . . . . . . . . . . . 201
3. Assemble/Install the Fuel Tank Assembly . . . . . . . . . . . . . . . . . . 205
AIRCRAFT
DA 40 Series
AMM
Fuel System
　
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