REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-51-44-991-002 Fig. 601
**ON A/C 301-399,
27-51-44-991-002-A Fig. 601A
**ON A/C ALL
27-51-44-991-007 Fig. 602
__________
3. Job Set-up
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 601/TASK 27-51-44-991-002)
**ON A/C 301-399,
(Ref. Fig. 601A/TASK 27-51-44-991-002-A)
**ON A/C ALL
Subtask 27-51-44-941-058
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice in position to tell persons not to operate the flap controls.
Flap Interconnecting Strut - Inspection/Check
Figure 601/TASK 27-51-44-991-002
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-44Page 604 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R Flap Interconnecting Strut - Inspection/Check R Figure 601A/TASK 27-51-44-991-002-A
R 1EFF : 301-399, 1 27-51-44Page 605 1 1 May 01/04 1 1 1CES 1 Subtask 27-51-44-860-059-A
B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
_______ ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
(1)
Extend the flaps to position 1 (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever.
(3)
Remove the applicable upper and lower kink-seals (1) and (2) from the inboard and the outboard flaps (Ref. TASK 27-54-61-000-002).
(4)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
(5)
Fully extend the flaps (Ref. TASK 27-50-00-866-008).
(6)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever.
Subtask 27-51-44-865-068
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
Subtask 27-51-44-020-054
D. Preparation for Inspection R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 601/TASK 27-51-44-991-002)
**ON A/C 301-399,
(Ref. Fig. 601A/TASK 27-51-44-991-002-A) **ON A/C ALL
(1)
Use a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to clean the flap interconnecting strut and the flap attachment brackets (5) and (8).
(2)
Remove and discard the cotter pin (14).
(3)
Remove the nut (15), the washer (13) and the bolt (16).
(4)
Disconnect the flap interconnecting strut from the attachment bracket (8).
(5)
Pull the actuating rod out of the flap interconnecting strut until it touches the internal limit.
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 601/TASK 27-51-44-991-002)
**ON A/C 301-399,
(Ref. Fig. 601A/TASK 27-51-44-991-002-A)
**ON A/C ALL
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
EDGE:
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱4(117)
