-
the MCDU shows the next page of the SFCC 1 menu.

-
the MCDU shows the SFCC 1 FLAPSYSTEM DATA menu.

-
the MCDU shows the PPU DATA page(s). Refer to Table 1.

 1EFF : ALL 1 27-54-49Page 474 1 1 May 01/04R 1 1 1CES 1

 Subtask 27-54-49-820-063
 F. Adjustment After BITE Test
 (1)
 Compare the APPU and the FPPU angles (deg) with those that were written down (or printed) before the actuator was removed (Ref. TASK 27-54-49-000-002).

 (2)
 Make sure that the FPPU angle values agree with the values recorded before the actuators were removed (+/- 0.2 deg).

 (3)
 Make sure that the APPU angle values agree with the values recorded before the actuators were removed (+/- 0.2 deg).

 (4)
 Make sure that the APPU/FPPU angles (deg) agree (+/- 1.3 deg).

 (5)
 Make sure that the LH APPU and the RH APPU angles agree (+/- 0.45 deg).

 (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
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 G. Aircraft Maintenance Configuration
 (1)
 Retract the No. 1 spoiler (Ref. TASK 27-60-00-866-002).

 (2)
 Make sure that the applicable spoiler servo-control is in the 'O' (Operation) condition.

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

 Subtask 27-54-49-865-061
 H. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
 Subtask 27-54-49-710-051
 J. Test
 (1) Do an operational test of the flaps (Ref. TASK 27-54-00-710-001).
 5. Close-up
________ Subtask 27-54-49-410-054
 A. Close Access
 (1) Install the applicable access panels:
 -
for the left wing, install 193AB, 193BB and 573AB, 573BB, 573CB, 575CB

 -
for the right wing, install 194AB, 194BB and 673AB, 673BB, 673CB, 675CB.

 Subtask 27-54-49-942-053
 B. Removal of Equipment
 (1)
 Remove the safety barriers.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the access platform(s).

R 1EFF : ALL 1 27-54-49Page 476 1 1 May 01/04 1 1 1CES 1

 (4) Remove the ground support and maintenance equipment, the special and

 standard tools and all other items.

 1EFF : ALL 1 27-54-49Page 477 1 1 May 01/04R 1 1 1CES 1

 TASK 27-54-49-000-003
 Removal of the Flap Track 3 Actuator 6221CM(6271CM)
 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.)2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT2 COLLAR-SAFETY, SPOILER
　
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