Subtask 27-54-61-916-052
 N. Application of Special Materials
 (Ref. Fig. 403/TASK 27-54-61-991-005, 404/TASK 27-54-61-991-006)

 **ON A/C 001-049, 051-061, 101-103, 201-203,
 (Ref. Fig. 406/TASK 27-54-61-991-007)
 **ON A/C 062-099, 104-105, 151-158, 204-210,
 (Ref. Fig. 406A/TASK 27-54-61-991-007-A)
 **ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
 (Ref. Fig. 408/TASK 27-54-61-991-008)
 (1) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
 -
the bolt (111)

 -
the nut (174), the cotter pin (175), the nut (177), the washer

 (178) and the bolt (181)
 -
the bolts (76), the washers (77), the shear bolt (80), the washer (81), the nut (83) and the cotter pin (82)

 -
the bolt (86), the washer (87), the nut (88) and the cotter pin

 (89)
 -the nut (123).
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 27-54-61Page 445 1201-210, 1Aug 01/05 1 1 1CES 1R **ON A/C 106-149, 159-199, 211-299, 401-499,

 Subtask 27-54-61-916-052-A
 N. Application of Special Materials (Ref. Fig. 403A/TASK 27-54-61-991-005-B, 404/TASK 27-54-61-991-006, 406A/TASK 27-54-61-991-007-A, 408/TASK 27-54-61-991-008)
 (1) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
 -
the bolt (111)

 -
the nut (174), the cotter pin (175), the nut (177), the washer

 (178) and the bolt (181)
 -the bolt (79), the washer (78), the nut (76) and the cotter pin
 (77)
 -the bolt (80), the washer (81), the nut (82) and the cotter pin
 (83)
 -the nut (123).
 **ON A/C 001-049, 051-061, 101-103, 201-203,
 Subtask 27-54-61-420-053
 P. Installation of the Bonding Straps (Ref. Fig. 403/TASK 27-54-61-991-005, 404/TASK 27-54-61-991-006, 406/TASK 27-54-61-991-007)
 (1)
 Attach the bonding strap (115) from the flap carriage at track 1 to the flap drive trunnion with the bolt (116), the washer (117) and the nut (118) (Ref. TASK 20-28-00-912-004).

 (2)
 Attach the bonding strap from the flap carriage at track 2 to the flap bracket with the bolt (182) and the nut (183) (Ref. TASK 20-28-00-912-004).

 (3)
 Attach the bonding strap (74) between the inboard flap and the outboard flap with the bolt (75) and the nut (73) (Ref. TASK 20-28-00-912-004).

 (4)
 Attach the bonding strap (71) with the bolt (72) and the nut (70) (Ref. TASK 20-28-00-912-004).

R 1EFF : 001-049, 051-061, 101-103, 106-149, 1 27-54-61Page 446 1159-199, 201-203, 211-299, 401-499, 1Aug 01/05 1 1 1CES 1

R  **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
 Subtask 27-54-61-420-053-A
 P. Installation of the Bonding Straps **ON A/C 062-099, 104-105, 151-158, 204-210,
R  (Ref. Fig. 403/TASK 27-54-61-991-005) **ON A/C 106-149, 159-199, 211-299, 401-499,
R  (Ref. Fig. 403A/TASK 27-54-61-991-005-B) **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
R  (Ref. Fig. 404/TASK 27-54-61-991-006, 406A/TASK 27-54-61-991-007-A) (1) Attach the bonding strap from the flap carriage at track 2 to the flap bracket with the bolt (182) and the nut (183) (Ref. TASK 20-28-00-912-004). (2) Attach the bonding strap (74) between the inboard flap and the outboard flap with the bolt (75) and the nut (73) (Ref. TASK 20-28-00-912-004). (3) Attach the bonding strap (71) with the bolt (72) and the nut (70) (Ref. TASK 20-28-00-912-004). **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 27-54-61-860-057
 Q. Aircraft Configuration (1) Install the interconnecting strut (Ref. TASK 27-51-44-400-001). (2) Manually retract the flaps (Ref. TASK 27-50-00-866-012) (3) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000). (4) Extend the flaps to position 1 (Ref. TASK 27-50-00-866-008). 

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 447 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 (5) Install the flap kink seals (Ref. TASK 27-54-61-400-006). **ON A/C 001-001, 051-052,
 Subtask 27-54-61-410-051-A
 R. Close Access
 (Ref. Fig. 401/TASK 27-54-61-991-001)

 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Lift the flap track No. 2 movable fairing (Ref. TASK 57-55-11-410-001).

 (3)
 Install the pylon aft moveable fairing (Ref. TASK 54-55-00-400-001).

 (4)
 Install the fairing panels 193AB(194AB) and 193BB(194BB) as follows:

 (a) For the fairing panel 193AB(194AB): 1 Put the fairing panel in position on the aircraft.
　
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