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 29-10-00-863-002 Pressurize the Yellow Hydraulic System 29-10-00-864-002 Depressurize the Yellow Hydraulic System 29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
Transfer Unit (PTU)
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-23-00-860-002 31-60-00-860-001 31-60-00-860-002 Connection of the Isolation Coupling of the Power Transfer Unit (PTU)EIS Start ProcedureEIS Stop Procedure
3. Job Set-Up__________
Subtask 27-54-00-941-050
A. Safety Precautions
(1) Put the safety barriers in position.
(2) Put the warning notice(s) in position to tell persons that the flap system is in operation.
Subtask 27-54-00-860-056
B. Aircraft Maintenance Configuration
R (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2) If applicable, disconnect the Power Transfer Unit (PTU) (Ref. TASK 29-23-00-860-001).
R NOTE : The flaps travel at full speed if the Power Transfer Unit____ (PTU) is in operation. If the PTU is disconnected (electrically or hydraulically) only the yellow flap motor operates and the flaps travel at half speed.
R R NOTE : An ECAM F/CTL FLAP SYS 1 FAULT message will show when the PTU____ is isolated. This message can be ignored.
R R R (3) Pressurize the Yellow hydraulic system (Ref. TASK 29-10-00-863-002).
Subtask 27-54-00-865-050
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
Subtask 27-54-00-865-052
D. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/WTB/FLP/SYS2 12CV P20 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 122VU FLIGHT CONTROLS/WTB/FLP/SYS1 10CV S07
4. Procedure
_________
Subtask 27-54-00-710-050
A. Operational Test
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1) Do the Electronic Instrument System (EIS) start procedure (Ref. TASK 31-60-00-860-001).
1EFF : ALL 1 27-54-00Page 503 1 1 Nov 01/99R 1 1 1CES 1
(2) Do this test:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R 1. On the center pedestal on the panel 114VU:
R R - move the slat and flap control R lever to positions 1, 2, 3 and
FULL. Stop at every notch until the flaps stop at each position selected.
R 2. On the panel 114VU: R
-move the slat and flap control
R lever back to positions 3, 2, 1 and 0. Stop at every notch until the flaps stop at each position selected.
5. Close-Up
________
Subtask 27-54-00-860-057 On the aircraft:
-
the flaps move to the set position.
On the ECAM upper DU:
-
the flap position bar moves to theset position
-
the new lever position and the flaps travel direction are shown.
On the aircraft:
-
the flaps move to the set position.
On the ECAM upper DU:
-
the flap position bar moves to theset position
-
the new lever position and the flaps travel direction are shown
-no warnings related to the flap system are shown.
R A. Aircraft Maintenance Configuration R
R (1) Depressurize the Yellow hydraulic system R (Ref. TASK 29-10-00-864-002). R
(2)
If applicable, connect the PTU (Ref. TASK 29-23-00-860-002).
(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).
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