(2)
Remove the screw (16) and release the bonding lead (17).
(3)
Remove the cotter pin (7) and discard it.
(4)
Remove the nut (6) and the bolt (1). NOTE : The axle head is rectangular and thus it can touch the fairing
____ panel. Turn the axle head to help removal of the bolt.
(5) Remove the nut (5), the bolt (2) and the bush (4). NOTE : The axle head is rectangular and thus it can touch the fairing
____ panel. Turn the axle head to help removal of the bolt.
(6)
Remove the cotter pins (12) and discard them.
(7)
Remove the nuts (13) and the bolts (10).
(8)
Remove the nuts (14), the hollow pins (11) and the bushes (15).
Movable Fairing Assembly
Figure 401/TASK 54-55-00-991-001
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 54-55-00Page 404 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R Movable Fairing Assembly
R Figure 401A/TASK 54-55-00-991-001-A
R 1EFF : 301-399, 1 54-55-00 Page 405
1 1 May 01/04
1 1
1CES 1
(9) Remove the movable fairing (19).
1EFF : ALL 1 54-55-00Page 406 1 1 May 01/04R 1 1 1CES 1
TASK 54-55-00-400-001
Installation of the Aft Movable Fairing
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
B. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
R 7 cotter pin 54-55-11 01A-010 7 cotter pin 54-55-11 01C-010
R 12 cotter pins 54-55-11 01A-010 12 cotter pins 54-55-11 01C-010
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
27-50-00-866-008 Extension of the Flaps on the Ground
78-30-00-081-041 Make the Thrust Reverser Serviceable after
Maintenance
78-30-00-481-041 Make the Thrust Reverser Unserviceable for
Maintenance
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
54-55-00-991-001 Fig. 401
**ON A/C 301-399,
54-55-00-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 54-55-00-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform and the warning notices are in position.
(2)
Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-00-481-041).
(3)
Make sure that the flap/slat control lever is in position 2 (Ref. TASK 27-50-00-866-008).
4. Procedure
_________
Subtask 54-55-00-420-050
A. Installation of the Aft Movable Fairing R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 401/TASK 54-55-00-991-001)
**ON A/C 301-399,
(Ref. Fig. 401A/TASK 54-55-00-991-001-A)
**ON A/C ALL
(1)
Put the movable fairing (19) in position
(2)
Install the bushes (15), the hollow pins (11) and the nuts (14).
(3)
Torque the nuts (14) to between 1.5 and 1.8 m.daN (11.06 and 13.27 lbf.ft)
(4)
Install the bolts (10), the nuts (13) and tighten them.
(5)
Safety the nuts (13) with the cotter pins (12)
(6)
Install the bush (4), the bolt (2) and the nut (5).
(7)
Torque the nut (5) to between 1.5 and 1.8 m.daN (11.06 and 13.27 lbf.ft)
