4. Procedure
_________
Subtask 22-66-00-440-050
A. Reactivation of the FAC 2
(1) Push the circuit breaker 5CC2.
R (2) On the overhead panel 24VU, push the FLT CTL/FAC 2 pushbutton switch R (the OFF legend goes off).
(3) Do the trouble-shooting of the FAC 2. Make the necessary corrections.
5. Close-up
________
Subtask 22-66-00-862-051
A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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COMPUTER - FLIGHT AUGMENTATION (FAC) (1CC1,1CC2) - REMOVAL/INSTALLATION_______________________________________________________________________
TASK 22-66-34-000-002
Removal of the FAC (1CC1,1CC2)
1. Reason for the Job__________________
Self Explanatory
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific No specific No specific blanking capscircuit breaker(s) safety clip(s)access platform 1.6 m (5 ft. 3 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R 31-32-00-860-001 22-66-34-991-002 Procedure to Get Access to the SYSTEM REPORT/TEST Menu PageFig. 401
3. Job Set-up__________
R Subtask 22-66-34-810-050
R R R R R R R R R R R A. Trouble Shooting Data You can print the Trouble Shooting Data (TSD) as follows: - get access to the SYSTEM REPORT/TEST menu page (Ref. TASK 31-32-00-860-001), - on this page, push the line key adjacent to the AFS indication, - on the AFS MAIN MENU page, push the line key adjacent to the TROUBLE SHOOTING DATA indication to get the AFS/TROUBLE SHOOTING page, - on this page, push the line key adjacent to the BITE SELECTION (FAC1 and FAC2, COM and MON indications to get the AFS/TROUBLE SHOOTING page(s), - print the AFS/TROUBLE SHOOTING page(s).
R B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 1CC1
49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03
FOR 1CC2 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18
Subtask 22-66-34-010-051
R C. Get Access
(1)
Put the access platform in position at zone 128.
(2)
Open the access door 824.
4. Procedure
_________
(Ref. Fig. 401/TASK 22-66-34-991-002)
Subtask 22-66-34-020-051
A. Removal of the FAC
NOTE : The procedure is the same for the FACS 1CC1 and 1CC2.
____
(1)
Loosen the nuts (3) on the front of the rack (2).
(2)
Lower the nuts (3) to release the studs (4).
(3)
Pull the FAC (5) on its rack (2) to disconnect the electrical connectors (1).
(4)
Remove the FAC (5) from its rack (2).
(5)
Put blanking caps on the electrical connectors (1).
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Flight Augmentation computer (FAC)
Figure 401/TASK 22-66-34-991-002
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1 1 Feb 01/98
1 1
1CES 1
TASK 22-66-34-400-002
Installation of the FAC (1CC1,1CC2)
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
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