(4)
Put the stop plate (4) in position on the end of the flap track beam (7).
(5)
Install the bolts (1) and (2) together with the washers (3) and (9) in the nuts (6) and (8).
R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
Subtask 27-54-46-420-054-A
A. Preparation for Installation
(1)
Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Make sure that the carriage No.1 (1) is in the correct condition.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Do an inspection of the component interface and/or the adjacent area. Subtask 27-54-46-420-059-A
B. Installation of the No.1 Flap Carriage WARNING : SUPPORT THE UNIT/ASSEMBLY OR IT WILL FALL AND BECOME DAMAGED OR
_______ INJURE PERSONNEL. THE UNIT/ASSEMBLY IS HEAVY.
(1)
Apply LUBRICANTS (Material No. 06-011) to the smooth part of the bolts (2) and (4).
(2)
Carefully put the carriage No.1 (1) on the flap track beam (3).
(3)
Install the bolts (2) and (4) together with the bush (5) on the flap track beam (3).
(4)
TORQUE the bolts (2) and (4) to between 1.4 and 2.6 m.daN (10.32 and
19.17 lbf.ft).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-46Page 415 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R **ON A/C 301-399,
R Subtask 27-54-46-420-054-B
R A. Preparation for Installation
R (1) Clean the component interface and/or the adjacent area with a
R MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS
R (Material No. 11-026).
R (2) Make sure that the carriage No.1 (4) is in the correct condition.
R (3) Make sure that the parts retained from the removed component are
R clean and in the correct condition.
R (4) Do an inspection of the component interface and/or the adjacent area.
R Subtask 27-54-46-420-059-B
R B. Installation of the No.1 Flap Carriage
R WARNING : SUPPORT THE UNIT/ASSEMBLY OR IT WILL FALL AND BECOME DAMAGED OR_______
R INJURE PERSONNEL. THE UNIT/ASSEMBLY IS HEAVY.
R (1) Carefully put the carriage No.1 (4) on the flap track beam (7).
R (2) Apply SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-
R 019) to the interface of the stop plate (3) and the smooth part of
R the bolts (1).
R (3) Put the stop plate (3) in position on the end of the flap track beam
R (7).
R (4) Install the bolts (1) together with the washers (2).
R (5) Install the washers (5) and the nuts (6).
R (6) TORQUE the nuts (6) to between 0.7 and 0.8 m.daN (61.94 and 70.79
R lbf.in).
R 1EFF : 301-399, 1 27-54-46Page 416 1 1 May 01/04 1 1 1CES 1 **ON A/C ALL
5. Close-up
________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-46-410-052
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the flap track beam No. 1 (Ref. TASK 57-51-33-400-001).
(3)
Install the inboard flap (Ref. TASK 27-54-61-400-001).
(4)
Remove the GROUND LOCK SLEEVE from the MLG door actuating cylinder.
(5) Close the MLG doors (Ref. TASK 32-12-00-410-001).
**ON A/C 301-399,
Subtask 27-54-46-410-052-A
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the flap track beam No.1 (Ref. TASK 57-51-33-400-001).
(3)
Install the inboard flap (Ref. TASK 27-54-61-400-003).
(4)
Remove the GROUND LOCK SLEEVE from the MLG door actuating cylinder.
(5)
Close the MLG doors (Ref. TASK 32-12-00-410-001).
R **ON A/C ALL
Subtask 27-54-46-865-057
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV, 10CV, 12CV.
Subtask 27-54-46-860-063
C. Aircraft Maintenance Configuration
(1) Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control lever in the cockpit.
(2) Install the safety collar on the circuit breakers 10CV and 12CV. Subtask 27-54-46-942-056
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5(67)
