Install 5-section outside wings – Great Plains 8560 FCF Assembly Manual User Manual

Page 18

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14

8323-8560FCC

Great Plains Manufacturing, Inc.

560-483Q-ENG

02/10/2014

Install 5-Section Outside Wings

Refer to Figure 14
75. Align holes in outside wing hinge

with hole in LH

and RH outside wing

, secure with 1 x 5 1/2 hex

bolt

, 5/8 lock washers, 5/8 nuts and two 5/8 x 3 1/

32 x 5 u-bolts

, 5/8 lock nuts. Fasten the front out-

side wing hinge

to wing brace the same way.

76. Carefully align holes in wing hinges

with holes in

fold brackets. Secure with 1 1/4 x 7 Gr. 8 hex bolt
and 1 1/4 top lock nut.

77. Attach outside wing brace

to front side of wing

frame with 3/4 x 2 hex bolts

, 3/4 lock washers, 3/4

hex nuts.

78. Attach bolt-on stub

to side of wing brace and front

of wing frame with 5/8 x 4 1/32 x 4 1/4 u-bolts

, 5/8

lock washers and 5/8 nuts

79. Attach holes in wheel arm L

, to wing frame

,

secure with 1 1/4 x 6 pin

, 3/8 x 2 1/4 hex bolts and

3/8 top lock nuts.

80. Attach base end of 3.25 x 8 x 1.25 lift cylinder (mod-

els 8539-8548) or 3.50 x 8 x 1.325lift cylinder (mod-
els 8551-8560)

to front hole of cylinder mount

plate with 1 x 3 1/8 pin

, 1.5 x 1.0 x.075 machine

washer and 3/16 x 2 cotter pin. Attach rod end of cyl-
inder

to torque tube lever with 1 x 3 1/8 pin

, 1.5

x 1.0 x.075 machine washer and 3/16 x 2 cotter pin.

81. Mount bottom of 180 fold rocker

to wing hinge

with 1 x 3 1/8 clevis pin

, 1.5 x 1.0 x.075 machine

washer and 3/16 x 2 cotter pin.

82. Attach base end of 4 x 16 x 1.25 cylinders

to cen-

ter fold bracket with 1 x 3 1/8 pin

, 1.5 x 1.0 x.075

machine washer and 3/16 x 2 cotter pin.

83. Do not attach rod end of fold cylinders until fold sys-

tem has been purged, See “Purging Hydraulic Sys-
tem
” on page 22.

84. Attach T bracket

to wing frame with 1/2 x 3 1/32 x

5 u-bolts

, 1/2 lock washers and 1/2 nuts.

Note: See layout section in “Operator’s Manual” for proper

placement of lock mount

.

85. Tighten all bolts to specs, See “Torque Values

Chart” on page 25.

Figure 14

5-Section Outside Wing Assembly

41896

3

18

5

U

D

F

B

L

R

4

2

9

9

13

12

1

16

14

17

15

6

8

1

7

11

19

14

10

1

2

4

5

1

1

6

3

7

8

9

10

2

11

12

13

14

12

14

15

1

16

17

14

18

19

18

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