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REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-51-00-991-071 **ON A/C 001-001, Fig. 521
27-51-00-991-072 Fig. 522 **ON A/C 002-049, 053-061, 101-105, 201-203,
R 27-51-00-991-072-A Fig. 522A **ON A/C 051-052, 062-099, 106-149, 151-199, 204-299, 401-499,
27-51-00-991-072-B **ON A/C 001-001, Fig. 522B
27-51-00-991-073 Fig. 523 **ON A/C 002-049, 051-061, 101-103, 201-203,
R 27-51-00-991-073-A Fig. 523A **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
R 27-51-00-991-073-B Fig. 523B **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-51-00-991-074 Fig. 524
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REFERENCE DESIGNATION
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**ON A/C 001-001,
27-51-00-991-075 Fig. 525
R **ON A/C 002-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-51-00-991-075-A Fig. 525A
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-51-00-991-076 Fig. 526
27-51-00-991-077 Fig. 527
27-51-00-991-078 Fig. 528
3. Job Set-up
__________
Subtask 27-51-00-941-079
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice on panel 114VU to tell persons not to operate the flap/slat control lever.
Subtask 27-51-00-860-074
B. Aircraft Maintenance Configuration
(1)
Make sure that:
-the fuel quantities in the wing tanks are symmetrical or that the wing tanks are empty
-two engines are installed
or
-no engines are installed.
(2)
Make sure that the aircraft weight is:
- on the landing gear (weight on wheels)
or
- on jacks (Ref. TASK 07-11-00-581-001).
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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 27-51-00-010-063
D. Get Access
**ON A/C 001-001,
(Ref. Fig. 516/TASK 27-51-00-991-067)
**ON A/C 002-049, 053-061, 101-105, 201-203,
(Ref. Fig. 516A/TASK 27-51-00-991-067-A) R **ON A/C 051-052, 062-099, 106-149, 151-199, 204-299, 401-499,
(Ref. Fig. 516B/TASK 27-51-00-991-067-B) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(1)
Put the access platform below the applicable inboard or outboard flap.
(2)
Remove the access panels for the applicable wing:
(a) For the LH wing, remove:
-573AB, 573CB (Ref. TASK 57-51-37-000-002)
-575AB (Ref. TASK 57-51-37-000-004).
(b) For the RH wing, remove:
-673AB, 673CB (Ref. TASK 57-51-37-000-002)
-675AB (Ref. TASK 57-51-37-000-004).
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Flap Rigging - General
Figure 516/TASK 27-51-00-991-067
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Flap Rigging - General
Figure 516A/TASK 27-51-00-991-067-A
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Flap Rigging - General
Figure 516B/TASK 27-51-00-991-067-B
R 1EFF : 051-052, 062-099, 106-149, 151-199, 1 27-51-00Page A511 1204-299, 401-499, 1Aug 01/05 1 1 1CES 1 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4(64)
