Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
3 crushable spacer 27-54-46 04B-080 3 crushable spacer 27-54-46 22 -030 5 cotter pin 27-54-46 04B-035 5 cotter pin 27-54-46 22 -010
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 57-55-11-010-001 To Lower the Flap Track No. 2 Movable Fairing for
Access 57-55-11-410-001 To Lift the Flap Track No. 2 Movable Fairing after
Access
NTM 57-52-52 PART 7
ASRM 575200 (for corrective action)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
57-52-00-991-032 Fig. 611 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 301-399,
R 57-52-00-991-032-A Fig. 611A R **ON A/C ALL
3. Job Set-up
__________
Subtask 57-52-00-941-063
A. Safety Precautions
(1) Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(2) Put the safety barriers in position.
Subtask 57-52-00-860-101
B. Aircraft Maintenance Configuration
(1)
Fully extend the flaps (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)
Put the access platform below the applicable wing trailing edge at flap track 2, zone 531(631).
Subtask 57-52-00-865-074
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 57-52-00-010-061
D. Get Access
(1) Lower the flap track 2 fairing (Ref. TASK 57-55-11-010-001).
4. Procedure
_________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 611/TASK 57-52-00-991-032)
**ON A/C 301-399,
(Ref. Fig. 611A/TASK 57-52-00-991-032-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.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-52-00-020-052
A. Preparation for Inspection
(1) Remove these items:
-
the cotter pin (5)
-
the nut (4)
-
the crushable spacer (3)
-
the nut (6) and the washer (7)
-
the locking plate (2)
-
the splined bush (1).
Flap Track 2 Pivot Bolt - Detail
Figure 611/TASK 57-52-00-991-032
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-52-00Page 662 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R Flap Track 2 Pivot Bolt - Detail
R Figure 611A/TASK 57-52-00-991-032-A
R 1EFF : 301-399, 1 57-52-00 Page 663
1 1 May 01/04
1 1
1CES 1
(2) Discard the cotter pin (5) and the crushable spacer (3).
CAUTION : THE FLAP TO CARRIAGE BOLT ASSEMBLY HAS AN INNER AND AN_______ OUTER BOLT WHICH MAKE ONE PART. DO NOT APPLY AN END OR A TORSION FORCE TO THE INNER BOLT BECAUSE THIS WILL CAUSE DAMAGE TO THE ASSEMBLY. APPLY FORCE TO THE OUTER BOLT ONLY WHEN YOU REMOVE/INSTALL THE BOLT ASSEMBLY.
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 WINGS 机翼4(27)
