(2)
On the center pedestal, on one MCDU, get the SYSTEM REPORT/TEST/NAV page (Ref. TASK 31-32-00-860-010).
4. Procedure
_________
Subtask 34-13-00-710-054
A. Operational Test of the ALT DYNAMIC SLEW TEST NOTE : This test is for the system 1. For the other system(s), use the
____
indications between the parentheses.
NOTE : This test is an example of the altitude ramp test. Ignore the
____ warnings which are the result of a difference in altitude between the CAPT and F/O PFD.
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-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the glareshield 13VU, on the CAPT and F/O EFIS control sections of the FCU:
-pull the baro reference selector knob.
2. On the MCDU:
-
push the line key adjacent to the ADR1 (ADR2) (ADR3) indication.
-
push the line key adjacent to the OUTPUT TESTS indication.
-
push the line key adjacent to the SLEW TESTS indication.
-
push the line key adjacent to the ALT DYNAMIC SLEW indication.
- on the keyboard, enter 0/1500 and push the line key adjacent to the ALT LIMITS (FT) indication.
- on the keyboard, enter 1000 and push the line key adjacent to the ALT SLEW RATE (FT/MIN) indication.
-push the line key adjacent to the UP (START SLEW) indication.
R the baro display (above the baroreference selector knob) shows STD. the CAPT and F/O PFDs show the altitude related to the standard barometric pressure and the STD indication.
On the MCDU:
-
the ADR1 (ADR2) (ADR3) page comesinto view.
-
the ADR1 (ADR2) (ADR3) OUTPUT TESTSpage comes into view.
-
the ADR1 (ADR2) (ADR3) SLEW TESTSpage comes into view.
-
the ADR1 (ADR2) (ADR3) ALT DYNAMICSLEW page comes into view.
-
the display shows 0/1500.
-
the display shows 1000.
The test starts:
-
the CAPT (F/O) PFD shows 0 ft and the altitude increases to 1500 ft in approximately 90 seconds.
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5. Close-up
________
Subtask 34-13-00-410-058
A. Close Access
(1)
Install the protective cover on the battery power center 105VU.
(2)
Tighten the two screws.
(3)
Close the access door 822.
(4) Remove the access platform(s). R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 34-13-00-865-074
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CC1, 5CC2
**ON A/C ALL
Subtask 34-13-00-860-068
C. Put the aircraft back to its initial configuration.
(1)
On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2)
On the CAPT and F/O EFIS control sections of the FCU, push the baro reference selector knob.
(3)
Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005).
(4)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
(5)
Make sure that the work area is clean and clear of tool(s) and other items.
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TASK 34-13-00-710-005 Operational Test of the CAS DYNAMIC SLEW TEST WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
1.
Reason for the Job
__________________
This test simulates a change in airspeed.
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 safety barriers No specific access platform 1.6 m (5 ft. 3 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 31-32-00-860-010 Procedure to Get Access to the SYSTEM REPORT/TEST NAV
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