(5)
Make sure that the applicable wing to fuselage panels 193AB(194AB), 193BB(194BB) have been removed (Ref. TASK 53-35-11-000-001).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 431 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(6)
Make sure that the pylon aft movable fairing has been removed (Ref. TASK 54-55-00-000-001).
(7)
Make sure that the flap track No. 2 movable fairing has been removed (Ref. TASK 57-55-11-010-001).
(8)
Make sure that the flap kink seals have been removed (Ref. TASK 27-54-61-000-002).
(9)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the slat/flap control lever.
4. Procedure
_________
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.
Subtask 27-54-61-420-056
A. Install the Inboard Flap
(1)
If necessary, install the hoisting sling (Ref. TASK 27-50-00-400-002).
(Ref. Fig. 408/TASK 27-54-61-991-008)
(2)
Make sure that the flap cruise roller, at the outboard end of the flap, is set to the minimum position.
(3)
If necessary, remove the nut (123), the collar (122) and the serrated plate (124).
(4)
Turn the eccentric (125) until the minimum alignment marks are aligned.
(5)
Install the serrated plate (124), the collar (122) and the nut (123). Tighten the nut (123) by hand.
(6)
Make sure that the flap is set to its lowest position. At this position:
-
the painted (red) marks of the spherical bearing are aligned, and/or
-
the hole of the spherical bearing is at its maximum aft position.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 432 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Alignment of the Outboard Cruise-Roller of the Inboard Flap.
Figure 408/TASK 27-54-61-991-008
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 433 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(7) If necessary, repair the painted (red) marks.
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 406/TASK 27-54-61-991-007) R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
(Ref. Fig. 406A/TASK 27-54-61-991-007-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(8)
Use adhesive tape to keep the eccentric disc (114) in position on the inboard flap drive trunnion.
(Ref. Fig. 402/TASK 27-54-61-991-012)
(9)
Make sure that the interconnecting strut (10) is safetied to the outboard flap with adhesive tape.
(10) With the hoist and the hoisting sling, carefully lift the flap and put it in position over the wing.
CAUTION : MAKE SURE THAT THE FLAP DOES NOT HIT THE AIRCRAFT
_______
STRUCTURE.
(a)
Lower the flap with the hoist and engage the flap drive trunnion in the flap track carriage at the track 1 position.
(b)
Lower the outboard end of the flap and engage the flap in the flap track carriage at the track 2 position.
(11) If necessary, use a clean MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to clean the eccentric disc (114) and to remove the remaining adhesive tape.
Subtask 27-54-61-480-051
B. Installation of Support Equipment (Ref. Fig. 404/TASK 27-54-61-991-006, 405/TASK 27-54-61-991-013)
(1) Assemble the EXTRACTOR - PIN (98D27504084000) on the bolt (181).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 434 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 27-54-61-420-051
C. Continue with the Installation Procedure
(1) At the track 1 position:
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 406/TASK 27-54-61-991-007) R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
(Ref. Fig. 406A/TASK 27-54-61-991-007-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(a)
Install the eccentric bush (107) on the flap drive-trunnion. If necessary, carefully move the flap with the hoist and the sling to let you install the eccentric bush (107).
(b)
Axis align the anti-rotation spigot of the eccentric bush (107) with the hole in the outer diameter of the eccentric disc (114).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵6(24)
