NOTE : The APPU and the FPPU synchro____
angles must agree within 1.3
deg.
The LH APPU and the RH APPU
synchro angles must agree within
0.45 deg.
- write down the APPU and the
FPPU angles (deg) shown on the
display or push (in) the line
key PRINT > to get a print-out
of the screen.
NOTE : These angles, shown at____
removal, will be used as a
datum. They will let you
compare the APPU and the
FPPU angles after the
installation of the
actuator (Ref. TASK 27-54-
49-400-001).
- push the line key < RETURN
frequently until the CFDS menu
page is shown.
2. De-energize the aircraft
electrical circuits (Ref. TASK
24-41-00-862-002).
R 1EFF : ALL 1 27-54-49Page 430 1 1 May 01/04 1 1 1CES 1 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
Subtask 27-54-49-020-057
C. Preparation for Removal of the Flap Track 1 Actuator
(1)
Hold the trailing edge of the flap on supports.
(2)
Use a clamp to hold the carriage in position. NOTE : This will make sure that the carriage does not move.
____
(3)
Remove the torque shaft (1) (Ref. TASK 27-54-45-000-003). Do not remove the plunging joint (2) from the actuator.
(4)
Remove the torque shaft (4) and the universal joint (3) (Ref. TASK 27-54-45-000-002).
R **ON A/C 001-049, 051-061, 101-103, 201-203,
Subtask 27-54-49-020-064
D. Removal of the Flap Track 1 Actuator 6205CM (6255CM) CAUTION : SUPPORT THE ACTUATOR, WHICH CAN WEIGH UP TO 10.5kg (23.2lbs).
_______ THIS WILL PREVENT DAMAGE TO THE RELATED STRUCTURE AND EQUIPMENT.
(1)
Remove the nuts (10), the bolts (8) and (9) and the countersunk washers (7).
(2)
Turn the plunging joint (2) until the input bevel housing moves out of the hole in the sloping frame.
(3)
Remove the plunging joint (2).
(4)
Remove the actuator assembly from the flap drive lever and the aircraft.
(5) Prevent damage to the component interface and the adjacent area. R **ON A/C 062-099, 106-149, 151-199, 204-299, 401-499,
Subtask 27-54-49-020-064-B
D. Removal of the Flap Track 1 Actuator 6205CM (6255CM) CAUTION : SUPPORT THE ACTUATOR, WHICH CAN WEIGH UP TO 10.5kg (23.2lbs).
_______ THIS WILL PREVENT DAMAGE TO THE RELATED STRUCTURE AND EQUIPMENT.
(1)
Remove the nuts (9) the bolts (8) and the countersunk washers (7).
(2)
Turn the plunging joint (2) until the input bevel housing moves out of the hole in the sloping frame.
(3)
Remove the plunging joint (2).
(4)
Remove the actuator assembly from the flap drive lever and the aircraft.
(5) Prevent damage to the component interface and the adjacent area. **ON A/C 104-105,
Subtask 27-54-49-020-064-A
D. Removal of the Flap Track 1 Actuator 6205CM (6255CM) CAUTION : SUPPORT THE ACTUATOR, WHICH CAN WEIGH UP TO 10.5kg (23.2lbs).
_______ THIS WILL PREVENT DAMAGE TO THE RELATED STRUCTURE AND EQUIPMENT.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-49Page 432 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R (1) Remove the nuts (9) the bolts (8) and the countersunk washers (7).
R R (2) Turn the plunging joint (2) until the input bevel housing moves out of the hole in the sloping frame.
R (3) Remove the plunging joint (2).
R R (4) Remove the actuator assembly from the flap drive lever and the aircraft.
R (5) Prevent damage to the component interface and the adjacent area.
**ON A/C 301-399,
Subtask 27-54-49-020-064-C
D. Removal of the Flap Track 1 Actuator 6205CM (6255CM)
CAUTION : SUPPORT THE ACTUATOR, WHICH CAN WEIGH UP TO 10.5kg (23.2lbs)._______ THIS WILL PREVENT DAMAGE TO THE RELATED STRUCTURE AND EQUIPMENT.
(1) Remove the nuts (8) and the washers (7).
(2) Remove the bolts (5) and the countersunk washers (6)
(3) Turn the plunging joint (2) until the input bevel housing moves out of the hole in the sloping frame.
(4) Remove the plunging joint (2).
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