(43)
 At the position F, install and safety the new cotter pin (22).

 (44)
 At the position C, install and safety the new cotter pin (23).

 (45)
 TORQUE the nuts (8) to between 1.15 and 1.35 m.daN (101.76 and 119.46 lbf.in).

 (46)
 Install and safety the new cotter pins (7).

 (47)
 Apply SEALANTS (Material No. 09-013) to the parts that follow: NOTE : Make sure that the sealant does not enter the spherical

____ bearings of the eye-ends (4) and the rod-ends (29).
 -the bolts (6) and the washers (5)
 -the bolts (10), the washers (9) and the nuts (8) R - the lock nuts (11) and the eye-ends (4)
 -
the serrated plates (17)

 -
the bolts (28), the washers (25) and the nuts (24)

 -
the studs (21) and the lock nuts (30).

 (48) Install the bonding strap (18) on the screw (16) and install the nut
 (19) (Ref. TASK 20-28-00-912-004).
R  **ON A/C 051-099, 102-149, 151-199, 201-299, 401-499, Post SB 52-1100 For A/C 051-060, Subtask 32-12-14-560-050-A
 B. Preparation For a Replacement Component (Ref. Fig. 402A/TASK 32-12-14-991-002-A, 403B/TASK 32-12-14-991-001-B)
 (1)
 Remove and discard the lockwire from the lock nuts (10) and (29).

 (2)
 Loosen the lock nuts (10) and (29).

R 1EFF : 051-099, 102-149, 151-199, 201-299, 1 32-12-14Page 441 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 (3)
 Adjust the eye-ends (3) out of the spools (2) so that the dimension W is between 44.0 mm (1.7322 in.) and 46.0 mm (1.8110 in.).

 (4)
 Remove the bolts (5) and the washers (4).

 (5)
 Remove and discard the lockwire from the lock nuts (12).

 (6) Loosen the lock nuts (12) so that the studs (20) can turn. Make sure that the serrated plates (16) do not disengage. Subtask 32-12-14-420-059-A R C. Installation of a Replacement MLG Fixed Fairing Assembly
 (Ref. Fig. 403B/TASK 32-12-14-991-001-B)
 WARNING : THE WEIGHT OF THE FIXED FAIRING IS 34kg (75lb).

_______
 (1)
 Hold the fixed fairing (1) in position on the MLG.

 (2)
 At the position C, install the bush (25), the bolt (27), the washer

 (24) and the nut (23).

 (3)
 Install the RIGGING SPACER (98D32104083000) on the bolt (27), this will make sure that the dimensions Z and Y are correct. They must be between 1.3 mm (0.0511 in.) and 2.7 mm (0.1062 in.). (Ref. Fig. 402A/TASK 32-12-14-991-002-A)

 (4)
 At the position F, install the bush (26), the bolt (27), the washer

 (24) and the nut (23).

 (5)
 Install the second RIGGING SPACER (98D32104083000) on the bolt (27), this will make sure that the dimensions Z and Y are correct. They must be between 1.3 mm (0.0511 in.) and 2.7 mm (0.1062 in.).

 (6)
 Install the bolts (9), the washers (8) and the nuts (7).

 (7)
 Tighten the lock nuts (12) sufficiently to make sure that the MLG fixed fairing (1) is stable during MLG retraction.

 (8)
 Slowly retract the applicable MLG (Ref. TASK 32-30-00-867-001). During retraction of the MLG make sure that the fixed fairing (1) does not overlap the lower wing surface.

 (9)
 Remove the lock nuts (12), the locking devices (13) and (14) and the outer serrated plates (16).

 (10) Turn the studs (20) so that they are fully on the rod-ends (28).
R 1EFF : 051-099, 102-149, 151-199, 201-299, 1 32-12-14Page 442 1401-499, 1Aug 01/05 1 1 1CES 1

 (11) Turn the spools (2) to get the dimensions that follow:
 **ON A/C 051-061, 102-105, 201-203,
 Post SB  52-1100 For A/C 051-060,
 (Ref. Fig. 404/TASK 32-12-14-991-003) 
R  **ON A/C 062-099, 106-149, 151-199, 204-299, 401-499,
 (Ref. Fig. 404A/TASK 32-12-14-991-003-A) 
R  **ON A/C 051-099, 102-149, 151-199, 201-299, 401-499,
 Post SB  52-1100 For A/C 051-060,
 (a) The dimension V must be between 2.5 mm (0.0984 in.) and 9.5 mm (0.3740 in.).
 (b) At the position H, the dimension T must be between -1.5 mm (-0.0590 in.) and -4.5 mm (-0.1771 in.) (Negative Step).
 (c) At the position J, the dimension T must be between -0.5 mm (-0.0196 in.) and -4.5 mm (-0.1771 in.) (Negative Step).
 (d) The dimension S must be between 2.5 mm (0.0984 in.) and 9.5 mm (0.3740 in.).
 (e) The dimension R must be between 14.0 mm (0.5511 in.) and 31.0 mm (1.2204 in.).
 (f) The dimension P must be between -2.5 mm (-0.0984 in.) (Negative Step) and 1.5 mm (0.0590 in.).
 (g) The dimension Q must be: - between 2.5 mm (0.0984 in.) and 9.5 mm (0.3740 in.) at the inboard end of the shroud box - between 3.2 mm (0.1259 in.) and 10.2 mm (0.4015 in.) at the outboard end of the shroud box. 
　
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