(6)
If the APPU and FPPU angles are not within the specified limit, do these steps:
(a)
Disconnect the APPU and adjust the APPU input shaft.
(b)
Do again step (6)(a) until the APPU angles are in the specified limits in relation to the FPPU angles.
SFCC 1
PPU DATE (DEG)
DATE:XXX XX UTC:XXXX
LH APPU FPPU RH APPU
***.* ***.* ***.*
***HEX ***HEX ***HEX ***
OTHER SFCC
LH APPU FPPU RH APPU
***.* ***.* ***.* ***
***HEX ***HEX ***HEX
<RETURN PRINT>
Table 1 PPU DATA (DEG) displayed on the MCDU at the flap position FULL
R 1EFF : ALL 1 27-54-49Page 450 1 1 May 01/04 1 1 1CES 1 Subtask 27-54-49-860-059-A
H. Aircraft Maintenance Configuration
(1)
Remove the warning notice(s).
(2)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever in the cockpit.
(3)
Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 27-54-49-865-059
J. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 27-54-49-710-050 R K. Test R (1) Fully retract the flaps (Ref. TASK 27-50-00-866-009). R (2) Do an operational test of the flaps (Ref. TASK 27-54-00-710-001).
5. Close-up
________
Subtask 27-54-49-410-051
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the applicable access panels:
(a) For the LH wing, install
-193AB, 193BB
-573AB, 573BB (Ref. TASK 57-51-37-400-002).
(b) For the RH wing, install
-194AB, 194BB
-673AB, 673BB (Ref. TASK 57-51-37-400-002).
(3)
Close the applicable MLG door (Ref. TASK 32-12-00-410-001).
Subtask 27-54-49-942-051
B. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the access platform(s).
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 27-54-49Page 452 1 1 May 01/04R 1 1 1CES 1
TASK 27-54-49-000-002
Removal of the Flap Track 2 Actuator 6211CM(6261CM)
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
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)
No specific clamp
No specific safety barriers
No specific warning notice(s)
No specific access platform 2.8 m (9 ft. 2 in.)
98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
1EFF : ALL 1 27-54-49Page 453 1 1 May 01/05R 1 1 1CES 1
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 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001) 27-50-00-866-008 Extension of the Flaps on the Ground 27-54-45-000-005 Removal of the Torque Shaft 6210CM(6260CM) 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST
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