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To lock elevator movement.
(4) Measure the distance between the trailing edge
of each aileron and the trailing edge of the wing
tip.
Record these measurements.
The left aileron must align with the right
aileron.
(5) Remove the rigging pins from the following:
S The bottom of each control stick.
S The left stick mounting bracket.
WARNING: WHEN YOU DO WORK ON THE AIRPLANE CONTROLS, YOU MUST
MAKE SURE THE AREAS AROUND THE CONTROLS/CONTROL
SURFACES ARE CLEAR OF PERSONS/EQUIPMENT. IF YOU DO
NOT DO THIS, INJURY TO PERSONNEL AND DAMAGE TO
CONTROL SURFACES CAN OCCUR.
(6) Move the control stick fully to the left and hold it
against the stop.
(7) Measure the distance between the trailing edge
of the left aileron and the trailing edge of the wing
tip.
Record the measurement.
The distance must be as shown in the
Control Surfaces Adjustment Report.
(8) Measure the distance between the trailing edge
of the right aileron and the trailing edge of the
wing tip.
Record the measurement.
The distance must be as shown in the
Control Surfaces Adjustment Report.
(9) Move the control stick fully to the right and hold it
against the stop.
(10) Measure the angle between the trailing edge of
the right aileron and the trailing edge of the wing
tip.
Record the measurement.
The distance must be as shown in the
Control Surfaces Adjustment Report.
(11) Measure the angle between the trailing edge of
the left aileron and the trailing edge of the wing
tip.
Record the measurement.
The distance must be as shown in the
Control Surfaces Adjustment Report.
(12) Install the right pilot’s seat. Refer to Section 25-10.
AIRCRAFT
DA 40 Series
AMM
Flight Controls
Doc # 6.02.01
Rev. 5 27-10-00 Page 203
20 Sep 2007
3. Aileron Control System Adjustments
If you cannot get the correct range of movement of the aileron control system, use this procedure to
adjust the system. Gust travel refers to the amount of travel remaining at the control surface with the
control stick held against the cockpit stop.
WARNING: IF YOU DO AN ADJUSTMENT OF A PUSH-ROD, YOU MUST MAKE
SURE THAT THE PUSH-ROD IS STILL IN SAFETY. IF YOU DO NOT DO
THIS, THE PUSH-ROD CAN DISCONNECT. THIS CAN CAUSE DEATH
OR INJURY TO PERSONS.
Item Quantity Part Number
Rigging pins. 3 -
Ruler. 1 Commercial.
A. Aileron Adjustment Procedure
Detail Steps/Work Items Key Items/References
(1) Remove these items for access:
S Pilots’ seats.
S Passenger seat.
S Push-rod access panels under the center
section.
S Aileron bellcrank access panels under each
wing.
Refer to Sections:
25-10
52-40
(2) Install rigging pins in the following:
S The bottom of each control stick.
S The left stick mounting bracket.
S The front bellcrank.
S The idler lever.
S The rear bellcrank.
S The left aileron bellcrank.
S The right aileron bellcrank.
Refer to Figures 1 & 2.
To lock the stick to the torque tube.
To lock the elevator movement.
On the control bulkhead.
On the front main bulkhead.
On the rear main bulkhead.
In the wing.
In the wing.
AIRCRAFT
Flight Controls DA 40 Series
AMM
Detail Steps/Work Items Key Items/References
Page 204
20 Sep 2007 27-10-00 Doc # 6.02.01
Rev. 5
Note: Keep the aileron rigging pins in position until you have completed the
adjustments. You can do the procedure with 3 rigging pins. Lock each lever or
bellcrank in sequence.
(3) If you cannot put a rigging pin into a lever or
bellcrank, adjust the push-rods as necessary.
Refer to Section 27-00 for the push-rod
adjustment procedure.
(4) Measure the distance between the trailing edge
of each aileron and the trailing edge of the wing
tip.
Record these measurements.
The left aileron must align with the right
aileron.
(5) Remove the rigging pins from the following:
S The bottom of each control stick.
S The left stick mounting bracket.
S The front bellcrank.
S The idler lever.
S The rear bellcrank.
S The left aileron bellcrank.
S The right aileron bellcrank.
Refer to Figures 1 & 2.
On the control bulkhead.
On the front main bulkhead.
On the rear main bulkhead.
In the wing.
In the wing.
(6) Do the Aileron Control Test Procedure. Refer to Paragraph 2.
(7) If necessary, adjust the push-rods between the
aileron bellcranks in the wing and the ailerons.
Refer to Section 27-00.
Adjust the rods to give the
　
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