钻石40飞机维护手册 DA 40 SERIES AMM 3(77)

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(9)  Connect the bonding cable to the strut.  Install the nut and bolt near the inner mounting block. 
(10)  Install the axle, brake torque-plate and the mounting plate for the wheel fairing. Install the 6 bolts which attach the axle.  Refer to Figure 2. Torque: 6.4 Nm (4.7 ft.lb). 

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Detail Steps/Work Items  Key Items/References 
(11)  Install the brake caliper.  Refer to Section 32-40. 
(12)  Install the wheel.  Refer to Section 32-40. 
(13)  Install the back-plate to the brake caliper.  Refer to Section 32-40. 
(14)  Install the wheel fairing: S Install the outer bolt. S Install 4 screws on the inner side. 
(15)  Install the strut fairing: S Install strut fairing. S Install stub wing cover. S Install brake cover.  Optional, see O.M 40-106. Take care of padding on strut. Take care of padding on strut cover. 
(16)  Lower the airplane with jacks.  Refer to Section 07-10. 
(17)  Do a test for correct adjustment of the landing gear.  See Paragraph 3. 
(18)  Do a function test of the wheel brake system. 

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3. Test/Adjust the Main Landing Gear
Do this work at the following times: ) When required by the maintenance checklist (Chapter 05). ) After a hard landing. ) After any repair to the main landing gear strut.
A. Equipment
Item  Quantity  Part Number 
Slide sheets - 2 per side.  4  Commercial. 

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Outer Face of Wheel

Figure 3: Measure Toe-In and Camber
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B. Procedure
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Detail Steps/Work Items  Key Items/References 
(1)  Make sure that the airplane is at the empty weight.  See the Adjustment Report for the airplane. 
(2)  Remove the strut fairings, if installed: S Remove brake cover. S Remove stub wing cover. S Remove strut fairing.  Optional, see O.M 40-106. Remove bolts and washers. Remove bolts and washers. Remove bolts and washers at the rear. 
(3)  Remove the wheel fairings: S Remove the outer bolt. S Remove 4 screws from the inner side.  For each wheel. 
(4)  Move the airplane to put the main wheels on the slide sheets. 
(5)  Measure the toe-in.  Refer to Figure 3. 
(6)  Measure the camber.  Refer to Figure 3. 
WARNING: USE ONLY THE SHIMS LISTED FOR THE PURPOSE IN THE ILLUSTRATED PARTS CATALOGUE. OTHER SHIMS COULD CAUSE LANDING GEAR FAILURE. 
(7)  If necessary, adjust the toe-in and/or camber.  Refer to Chapter 06-00 for limits. Maximum 2° shim per side (camber + toe). See the Illustrated Parts Catalogue for the correct shims. Put shims between the strut and the axle. These change the angle between the axle and the airplane longitudinal or vertical axis. 
(8)  Measure the wheel track.  Across the airplane from the outermost point on one axle to the outermost point on the other axle. 
(9)  Move the airplane off the slide sheets. 

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Detail Steps/Work Items  Key Items/References 
(10)  Install the wheel fairings: S Install the outer bolt. S Install 4 screws on the inner side. 
(11)  Install the strut fairings: S Install strut fairing. S Install stub wing cover. S Install brake cover.  Optional, see O.M 40-106. Take care of padding on strut. Take care of padding on strut cover. 
　
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