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Table 1 PPU DATA (DEG) displayed on the MCDU at the flap position FULL
Subtask 27-54-49-860-060-A
H. Aircraft Maintenance Configuration
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Retract the No. 2 and the No. 3 spoilers (Ref. TASK 27-60-00-866-002).
(3)
Remove the warning notice(s).
(4)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever in the cockpit.
(5) Retract the flaps fully (Ref. TASK 27-50-00-866-009). Subtask 27-54-49-865-063
J. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 27-54-49-710-052
K. Test
(1) Do an operational test of the flaps (Ref. TASK 27-54-00-710-001).
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5. Close-up
________ Subtask 27-54-49-410-057
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:
-for the left wing, install 573BB, 575AB, 575BB, 575CB, 575DB
-for the right wing, install 673BB, 675AB, 675BB, 675CB, 675DB. Subtask 27-54-49-942-055
B. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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TASK 27-54-49-000-004
Removal of the Flap Track 4 Actuator 6233CM(6283CM)
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__________________
R R Self Explanatory
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R No specific No specific No specific No specific No specific 98D27504030001 98D27604000000 circuit breaker(s) safety clip(s) clampsafety barrierswarning notice(s) access platform 2.8 m (9 ft. 2 in.)1 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT2 COLLAR-SAFETY, SPOILER
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 27-51-18-000-001 Removal of the Asymmetry-Position Pick-Off Unit 29CV
(30CV) 27-54-45-000-013 Removal of the Torque Shaft 6232CM(6282CM) 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
F/CTL Page
27-54-49-400-004 Installation of the Flap Track 4 Actuator
6233CM(6283CM) (for corrective action)
**ON A/C 001-049, 051-061, 101-103, 201-203, 301-399,
27-54-49-991-005 Fig. 403
R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
27-54-49-991-005-A Fig. 403A
**ON A/C 001-049, 051-061, 101-105, 201-203,
27-54-49-991-004 Fig. 406
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
27-54-49-991-004-A Fig. 406A **ON A/C ALL
3. Job Set-up
__________
**ON A/C 001-049, 051-061, 101-103, 201-203, 301-399,
(Ref. Fig. 403/TASK 27-54-49-991-005) R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
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