NOTE : The subsequent test steps 5. thru 10. must be done in 30 seconds or
____
less.
R 7. On the circuit breaker panel 121VU:
- open the circuit breakers
HYDRAULIC/LGCIU/SYS2 2GA (Q35)
and HYDRAULIC/LGCIU/SYS1/GND
SPLY 52GA (Q34).
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-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R 8. On the circuit breaker panel 49VU:
- open the circuit breaker L/G/LGCIU/SYS1/NORM 1GA (C09).
R 9. In the cockpit, on the panel 50VU:
- push the SVCE INT OVRD pushbutton switch 15RJ.
R 10. In the cockpit, on the captains ACP 2RN1:
- set and hold the INT/RAD selector switch in the RAD position.
- speak into the cockpit boomset and the boomset in the FWD electronics compartment.
R R
- release the INT/RAD selector switch.
R 11. On the circuit breaker panel 121VU:
- close the circuit breakers HYDRAULIC/LGCIU/SYS2 2GA (Q35) and HYDRAULIC/LGCIU/SYS1/GND SPLY 52GA (Q34).
R 12. On the circuit breaker panel 49VU:
In the FWD electronics compartment andat the FWD attendant station, zone 221:
-a communication between the FWDelectronics compartment and the FWD attendant station, zone 221, is not possible.
In the cockpit, on the panel 50VU:
-
the integral light of the SVCE INTOVRD pushbutton switch comes on.
In the FWD electronics compartment andin the cockpit at the boomsets:
-
the voice and the reply is correctand clear.
-make sure that no 400Hz interference is heard.
NOTE : A small audible 400Hz
____ interference is permitted.
In the cockpit, on the panel 50VU:
-the integral light of the SVCE INTOVRD pushbutton switch goes off.
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-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
- close the circuit breaker L/G/LGCIU/SYS1/NORM 1GA (C09).
R 13. Do the test steps 3. and 4. again for all other maintenance interphone jacks.
R 14. In the cockpit, on the captains ACP 2RN1:
- push the CAB pushbutton switch.
- push the CAB rotary switch and turn it fully counterclockwise.
R 15. On the captains jack panel 61VU:
- disconnect the boomset.
R 16. At the related maintenance interphone jack:
R R R - disconnect the boomset.
5. Close-up________
Subtask 23-44-00-860-051
In the cockpit, on the captains ACP2RN1:
-
the integral light of the CABpushbutton switch goes off.
-
the integral light of the CAB rotaryswitch goes off.
In the cabin at all AIP 320 RH:
-the SERVICE INT IN USE message goes off.
A. Put the aircraft back to its initial configuration.
(1)
De-energize the CIDS (Ref. TASK 23-73-00-862-001).
(2)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 23-44-00Page 506 1 1 May 01/04 1 1 1CES 1 JACK - MAINTENANCE INTERPHONE (POWER PLANT) - REMOVAL/INSTALLATION
__________________________________________________________________
TASK 23-44-41-000-003
Removal of the Maintenance Interphone Jack (4000RJ1, 4000RJ2)
WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER
_______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
R No specific warning notice No specific access platform 2 m (6 ft. 7 in.)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
23-44-41-991-400 Fig. 401
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