22.
Release the rudder pedals.
23.
Engage the AP2 again.
24.
On the First Officer's side stick controller:
-Apply a usual load in one direction
The AP1 disengages.
This pushbutton switch comes on.
You must get the same results as step
12.
On the First Officer's PFD:
-
The 1FD2 indication replaces the 1FD1indication.
On the Captain's PFD:
-
The 2FD2 indication replaces the 1FD2 indication.
This pushbutton switch comes on.
Make sure that the load threshold ofthe rudder pedals is more than that of step 3 (the load you apply to the pedals must be below the new load threshold per step 21).
The AP2 disengages.
This pushbutton switch comes on.
The side stick controller is locked.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-Apply a higher load until it moves freely
25.
Release the First Officer's side stick controller.
26.
Engage the AP2 again.
27.
Do the step 24 with the Captain's side stick controller.
28.
Release the Captain's side stick controller.
29.
Close the circuit breaker 10CA1 and after the safety test, make sure that the FD1 engages.
30.
Cancel the AP warnings:
-Engage the AP1 or AP2
-
Push and release the takeover and priority pushbutton switch on Captain's or First Officer's side stick controller.
or
-
Push the MASTER WARN light on the glareshield
-
Push the CLEAR key on the ECP (ECAM Control Panel).
5. Close-up
________
Subtask 22-10-00-860-053
The AP2 disengages.
This pushbutton switch comes on.
You must get the same results as thoseof step 24.
On the Captain's PFD:
-The 1FD2 indication replaces the 2FD2indication.
A. Aircraft Maintenance Configuration
(1)
Depressurize the aircraft hydraulic system (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-10-00-864-003).
(2)
On the overhead panel , on the ADIRS CDU, set the OFF/NAV /ATT selector switches to OFF.
(3)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(4)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-
002).
TASK 22-10-00-710-003
Operational Test of the Vertical Speed and Heading Hold Modes
WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
1. Reason for the Job
__________________
To do a check of a longitudinal mode and a lateral mode.
2. Job Set-up Information
______________________
A. 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
R 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
R Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 34-10-00-860-004 IR Alignment Procedure
1EFF : ALL 1 22-10-00Page 513 1 1 Feb 01/01 1 1 1CES 1
3. Job Set-up__________
Subtask 22-10-00-860-054
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
Make sure that the aircraft is in the ground condition with the engines shut down.
(3)
Align the ADIRS (two ADIRS are necessary for this test)
(Ref. TASK 34-10-00-860-004).
(4)
On the overhead panel, on the FLT CTL panels (23VU and 24VU):
-make sure that the ELAC 1 and 2, SEC 1, 2 and 3, FAC 1 and 2 pushbutton switches are pushed (the FAULT and OFF legends are off).
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