(6)
Remove the cockpit door (Ref. TASK 52-51-11-000-001).
4. Procedure
_________ Subtask 53-16-11-020-050
A. Removal of the Mount Fitting at FR 14
(Ref. Fig. 401/TASK 53-16-11-991-001)
(1)
For the web (7)
(a)
Remove and discard the nuts (6)
(b)
Remove the washers (5) and the bolts (3)
(c)
Remove and discard the nuts (8)
(d)
Remove the bolts (14)
(e)
Remove the web (7)
(2)
For the web (13)
(a)
Remove and discard the nuts (15)
(b)
Remove the bolts (12) and the web (13)
EFF : ALL
53-16-11Page 402
Mount Fitting at FR 14
Figure 401/TASK 53-16-11-991-001
EFF : ALL 53-16-11 Page 403
Aug 01/05
CES
(3)
For the plate (4)
(a)
Remove and discard the nuts (9)
(b)
Remove the washers (10) and the bolts (23)
(c)
Remove and discard the nuts (17)
(d)
Remove the washers (16), the bolts (11) and the plate (4)
(4)
For the fitting (1)
(a)
Remove and discard the nuts (19)
(b)
Remove the washers (18) and the bolts (24)
(c)
Remove and discard the nuts (21)
(d)
Remove the washers (20) and the bolts (22)
EFF : ALL
53-16-11Page 404
TASK 53-16-11-400-001
Installation of the Mount Fitting at FR 14
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform
B. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
6 nut 53-16-01 90 -050 6 nut 53-16-01 90A-050 8 nut 53-16-01 90 -020 8 nut 53-16-01 90A-020 9 nut 53-16-01 90 -050 9 nut 53-16-01 90A-050 15 nut 53-16-01 90 -020 15 nut 53-16-01 90A-020 17 nut 53-16-01 90A-025 19 nut 53-16-01 90A-025 21 nut 53-16-01 90A-025
EFF : ALL
53-16-11Page 405
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
23-72-51-000-001 Removal of the Anti-Hijack-System Cameras
23-72-51-400-001 Installation of the Anti-Hijack-System Cameras
24-42-00-861-001 Energize the Ground Service Network from the External
Power
24-42-00-862-001 De-energize the Ground Service Network Supplied from
the External Power
25-13-41-000-001 Removal of the Ceiling Panels
25-13-41-400-001 Installation of the Ceiling Panels
25-23-42-000-001 Removal of the Ceiling Panels - Forward Utility Area
25-23-42-400-001 Installation of the Ceiling Panels - Forward Utility
Area
52-10-00-010-001 Opening of the Passenger/Crew Door
52-10-00-410-001 Closing of the Passenger/Crew Door
52-51-11-000-001 Removal of the Cockpit Door
52-51-11-400-001 Installation of the Cockpit Door
53-16-11-991-001 Fig. 401
3. Job Set-up__________
Subtask 53-16-11-860-051
A. Aircraft Maintenance Configuration
(1) Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
Subtask 53-16-11-010-051
B. Get Access
(1)
Make sure that the access platform is in position at zone 831 (841).
(2)
Make sure that the forward passenger/crew door 831 (841) is open (Ref. TASK 52-10-00-010-001).
(3)
Make sure that the Anti-Hijack-System Camera is removed (Ref. TASK 23-72-51-000-001), if installed.
(4)
Make sure that the ceiling panel 221AC is removed (Ref. TASK 25-23-42-000-001).
EFF : ALL
53-16-11Page 406
(5)
Make sure that the lining panel 211HC is removed (Ref. TASK 25-13-41-
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