(b)
 Close the cargo door carefully with the crane and put the door locking handle in the LOCKED position.

 (c)
 Make sure that the lateral gaps 'A' thru 'D' are correct.

 (d)
 Measure the gaps 'G' between the piano hinge halves of the cargo door and the fuselage.

 (e)
 Pull out the hinge pins (24) about 150 mm (5.9055 in.) and install the washers (25), (26), (27), (28) in accordance with the subsequent table between FR26A and FR26.

 Table for Selection of Washers (Item 25 thru Item 28)
 GAP 'G' IN mm (in.) | ITEM 25 | ITEM 26 | ITEM 27 | ITEM 28 | THICKNESS --------------------------|---------|---------|---------|---------|------------
0.0 (0.000) - 0.3 (0.011) | -| -| -| _ | _
 0.3 (0.011) - 0.4 (0.015) | 1 | -| -| _ | 0.3 (0.011)
 0.4 (0.015) - 0.5 (0.020) | -| 1 | -| _ | 0.4 (0.015)
 0.5 (0.020) - 0.6 (0.024) | -| -| 1 | _ | 0.5 (0.020)
 0.6 (0.024) - 0.7 (0.028) | 2 | -| -| _ | 0.6 (0.024)
 0.7 (0.028) - 0.8 (0.031) | 1 | 1 | -| _ | 0.7 (0.028)
 0.8 (0.031) - 0.9 (0.035) | -| 2 | -| _ | 0.8 (0.031)
 0.9
 (0.035) - 1.0 (0.039) | -| 1 | 1 | _ | 0.9 (0.035)

 1.0
 (0.039) - 1.1 (0.043) | -| -| 2 | _ | 1.0 (0.039)

 1.1 (0.043) - 1.2 (0.047) | 1 | 2 | -| _ | 1.1 (0.043)
 1.2 (0.047) - 1.3 (0.051) | 1 | 1 | 1 | _ | 1.2 (0.047)
 1.3 (0.051) - 1.4 (0.055) | 1 | -| 2 | _ | 1.3 (0.051)
 1.4 (0.055) - 1.5 (0.059) | -| 1 | 2 | _ | 1.4 (0.055)
 1.5 (0.059) - 1.6 (0.063) | -| -| 3 | _ | 1.5 (0.059)
R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-31-11Page 416 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 GAP 'G' IN mm (in.) | ITEM 25 | ITEM 26 | ITEM 27 | ITEM 28 | THICKNESS --------------------------|---------|---------|---------|---------|------------
1.6 (0.063) - 1.7 (0.067) | 2 | -| 2 | _ | 1.6 (0.063)
 1.7 (0.067) - 1.8 (0.071) | 1 | 1 | 2 | _ | 1.7 (0.067)
 1.8 (0.071) - 1.9 (0.075) | -| 2 | 2 | _ | 1.8 (0.071)
 1.9
 (0.075) - 2.0 (0.079) | -| 1 | 3 | _ | 1.9 (0.075)

 2.0
 (0.079) - 2.1 (0.083) | -| -| -| 1 | 2.0 (0.079)

 2.1 (0.083) - 2.2 (0.087) | 2 | -| 3 | -| 2.1 (0.083)
 2.2 (0.087) - 2.3 (0.091) | 1 | 1 | 3 | -| 2.2 (0.087)
 2.3 (0.091) - 2.4 (0.095) | 1 | -| -| 1 | 2.3 (0.091)
 2.4 (0.095) - 2.5 (0.098) | -| 1 | -| 1 | 2.4 (0.095)
 2.5 (0.098) - 2.6 (0.102) | -| -| 1 | 1 | 2.5 (0.098)
 2.6 (0.102) - 2.7 (0.106) | 2 | -| -| 1 | 2.6 (0.102)
 2.7 (0.106) - 2.8 (0.110) | 1 | 1 | -| 1 | 2.7 (0.106)
 2.8 (0.110) - 2.9 (0.114) | -| 2 | -| 1 | 2.8 (0.110)
 2.9 (0.114) - 3.0 (0.118) | -| 1 | 1 | 1 | 2.9 (0.114)
 NOTE : The THICKNESS column refers the total thickness of the
____ applicable washers in mm (in.) .
 (4)
 Install the hinge pins (24) again and make sure that the lateral gaps 'A' thru 'D' are correct.

 (5)
 Open the cargo door with the crane until the door opening angle is between 135 and 136 degrees.

 (6)
 Install the SUPPORT STRUT - CARGO DOORS (98D52307524000) to safety the opened cargo door.

 (7)
 Remove the sling (5) from the cargo door.

 (8)
 Attach the end-fittings (30) and the shims (29) with the screws (31) to the fuselage structure.

 (9)
 Connect the piston eye end (18) to the actuator attachment fittings

 (13)
 of the cargo door as follows:

 (a)
 If removed, install the bushes (22) and (23) into the actuator attachment fitting (13).

 (b)
 Put the piston eye end (18) to the actuator attachment fitting

 (13) and install the bolt (14) with the washer (15).
 NOTE : If you can not install the bolt (14) adjust the length of
____ the door actuator (Ref. TASK 52-31-11-820-004).
 (c) Install the washer (15) and the nut (16) to the bolt (14).
R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-31-11Page 417 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 (d)
 TORQUE the nut (14) to between 1.0 and 1.35 m.daN (88.49 and

 119.46 lbf.in) and loosen it to the next cotter pin hole.

 (e)
 Safety the nut (14) with the cotter pin (17).

 (f)
 Install the bonding jumpers (10) with the bolts (12), the washers

 (11) and the nuts (9) to the actuator attachment fitting (13) (Ref. TASK 20-28-00-912-004).
 (10) Install the wire harness 4611VB (21) to the ceiling lining of the actuator area and connect the connector (20) to the receptacle (19) (Ref. TASK 52-31-24-400-001).
　
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