钻石40飞机维护手册 DA 40 SERIES AMM 3(24)

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(1)  Make a copy of the Control Surfaces Adjustment Report.  Refer to Section 06-00. Use it to record the measurements. 
(2)  Make sure that the flaps are fully UP: S Set the ALT/BAT switch (Lycoming version) or ELECTRIC MASTER key switch (TAE version) to ON. S Set the flaps to T/O. S When the flaps stop moving, set the flaps to UP. S When the flaps stop moving, set the ALT/BAT switch (Lycoming version) or ELECTRIC MASTER key switch (TAE version) to OFF. 
(3)  Do a test for the correct pre-load in the flap UP position: S Put a loop of adhesive tape on the trailing edge of the left flap opposite the up-stop. S Pull down on the loop of tape with the spring balance until the flap just moves from the up-stop. S Record the value in the Control Surfaces Adjustment Report.  The value must be as shown in the Control Surfaces Adjustment Report. 
(4)  If the pre-load is not correct, adjust the control rod between the bellcrank in the wing and the flap horn. Do items 3 & 4 again as necessary.  Refer to Section 27-00. 

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Detail Steps/Work Items  Key Items/References 
(5)  Do items 3 & 4 for the right flap. 
(6)  Zero the inclinometer to the left flap: S Put the inclinometer on the left flap close to the flap horn. S Zero the inclinometer. S Remove the inclinometer. 
(7)  Set the flaps to T/O: S Set the ALT/BAT switch (Lycoming version) or ELECTRIC MASTER key switch (TAE version) to ON. S Set the flaps to T/O. S When the flaps stop moving, set the ALT/BAT switch (Lycoming version) or ELECTRIC MASTER key switch (TAE version) to OFF. 
(8)  Measure the angle of the left flap. S Record the value in the Control Surfaces Adjustment Report.  Use the inclinometer. The value must be as shown in the Control Surfaces Adjustment Report. 
(9)  Do item 8 for the right flap. 
(10)  Set the flaps to LDG: S Set the ALT/BAT switch (Lycoming version) or ELECTRIC MASTER key switch (TAE version) to ON. S Set the flaps to LDG. S When the flaps stop moving, set the ALT/BAT switch (Lycoming version) or ELECTRIC MASTER key switch (TAE version) to OFF. 
(11)  Measure the angle of the left flap. S Record the value in the Control Surfaces Adjustment Report.  Use the inclinometer. The value must be as shown in the Control Surfaces Adjustment Report. 
(12)  Do item 11 for the right flap. 
(13)  Set the flaps to UP. 

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4. Adjust the Flap Control System
If you cannot get the correct range of movement of the flap control system, use this procedure to adjust the system.
A. Equipment
Item  Quantity  Part Number 
Rigging pins.  3  -
Inclinometer.  1  Commercial. 

B. Adjust The Flap Control System Procedure
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Detail Steps/Work Items  Key Items/References 
(1)  Make a copy of the Control Surfaces Adjustment Report.  Refer to Section 06-00. Use it to record the measurements. 
(2)  Remove these items for access: S The passenger seat. S The flap bellcrank access panels.  Refer to Section 25-10. Refer to Section 53-40. 
(3)  Disconnect the airplane main battery.  Refer to Section 24-31 (Lycoming version) or 24-34 (TAE version). 
(4)  Remove the bolt, spacer, washer and nut which attach the actuator push-rod to the idler lever.  At the rear main bulkhead. Hold the flaps. 
(5)  Put a rigging pin in the idler lever.  Refer to Figure 3. At the rear main bulkhead. 
　
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