-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job
__________________
Refer to the MPD TASK: 572610-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
No specific warning notice
No specific access platform 2.5 m (8 ft. 2 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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. 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 57-55-11-000-001 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-000-004 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-001 Installation of the Flap Track Fairings Nos. 2, 3 and
4 57-55-11-400-004 Installation of the Flap Track Fairings Nos. 2, 3 and 4 ASRM 572600 (for corrective action) R CMM 57-51-41 (for corrective action) 57-26-00-991-011 Fig. 611
3. Job Set-up
__________
Subtask 57-26-00-941-066
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put warning notice in the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-26-00-866-062
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 on the control lever.
Subtask 57-26-00-865-062
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
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-26-00-010-067
D. Get Access
(1)
Put the access platform below the applicable wing trailing edge at the flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
(2)
Remove the applicable flap track fairing access panels (Ref. TASK 57-55-11-000-001):
(a)
For the flap track 2,:
-
for the left wing, remove 531CB
-
for the right wing, remove 631CB.
(b)
For the flap track 3,:
-
for the left wing, remove 532CB
-
for the right wing, remove 632CB.
(c)
For the flap track 4,:
-
for the left wing, remove 533CB
-
for the right wing, remove 633CB.
**ON A/C 301-399,
Subtask 57-26-00-010-067-A
D. Get Access
(1)
Put the access platform below the applicable wing trailing edge at the flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
(2)
Remove the applicable flap track fairing access panels (Ref. TASK 57-55-11-000-004):
(a)
For the flap track 2,:
-
for the left wing, remove 531CB
-
for the right wing, remove 631CB.
(b)
For the flap track 3,:
-
for the left wing, remove 532CB
-
for the right wing, remove 632CB.
(c)
For the flap track 4,:
-
for the left wing, remove 533CB
-
for the right wing, remove 633CB.
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2(33)
