(1) For panel 191JB:
(a)
Remove the blanking caps from the electrical connectors.
(b)
Make sure that the electrical connectors are clean and in the correct condition.
(c)
Connect the electrical connector to the anti collision light 6LV.
EFF : ALL
53-35-13Page 426
(d) Install the bonding strap (Ref. TASK 20-28-00-912-004).
(2)
Put the panel (3) in position.
(3)
Install the washers (2) and the screws (1).
(4)
Make sure that the gap "x" between the panels 192AT/191AT and 192AB/191AB is 2.0 +1.5 -1.5 mm (0.0787 +0.0590 -0.0590 in.).
NOTE : A maximum gap of 4.0 mm (0.1574 in.) between the edges of the
____
two panels is permitted if:
-
the maximum value is for not more than 20% of the total length of the panel edges,
-
the panel edges and the gap sealant are in the correct condition.
(5) TORQUE the screws (1) to between 0.35 and 0.45 m.daN (30.97 and 39.82 lbf.in).
**ON A/C ALL
5. Close-up
________ Subtask 53-35-13-410-051
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the access platform(s).
(3)
Close the MLG doors (Ref. TASK 32-12-00-410-001).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
EFF : ALL
53-35-13Page 427
May 01/05
R
CES TASK 53-35-13-000-002 Removal of the Quick-Release Access Panels from the Belly Fairing Structure
1.
Reason for the Job
__________________
Self explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific adjustable access platform
No specific warning notice
98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C 001-049, 051-099, 101-149, 201-299,
53-35-13-991-004 Fig. 405 R **ON A/C 151-199, 401-499,
53-35-13-991-004-A Fig. 405A
**ON A/C 301-399,
53-35-13-991-004-B Fig. 405B
**ON A/C 001-049, 051-099, 101-149, 201-299,
53-35-13-991-005 Fig. 406
EFF : ALL
53-35-13Page 428
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R **ON A/C 151-199, 401-499,
53-35-13-991-005-A Fig. 406A
**ON A/C 301-399,
53-35-13-991-005-B Fig. 406B R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
53-35-13-991-006 Fig. 407
**ON A/C 301-399,
53-35-13-991-006-A Fig. 407A
**ON A/C ALL
3. Job Set-up
__________
Subtask 53-35-13-010-054
A. Get Access WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
(1)
Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever when working near the flaps/slats.
(2)
Put the warning notice on the slat/flap control lever to tell persons not to operate the slats/flaps.
(3)
Put the adjustable access platform in the required position.
EFF : ALL
53-35-13Page 429
R 4. Procedure_________ **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 53-35-13-020-052
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 FUSELAGE 机身2(126)