1EFF : ALL 1 57-26-00Page 651 1 1 May 01/04R 1 1 1CES 1
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 27-50-00-866-009 57-55-11-000-001 57-55-11-000-004 57-55-11-400-001 Extension of the Flaps on the GroundRetraction of the Flaps on the GroundRemoval of the Flap Track Fairings Nos. 2, 3 and 4Removal of the Flap Track Fairings Nos. 2, 3 and 4Installation 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
CMM 575141 57-26-15-000-001 57-26-15-400-001 (for corrective action)Removal of the Flap-Tracks Attachment-Bracket Bearing (for corrective action)Installation of the Flap-Tracks Attachment-Bracket Bearing (for corrective action)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
57-26-00-991-009 Fig. 609
**ON A/C 301-399,
57-26-00-991-009-A Fig. 609A
R **ON A/C ALL
3. Job Set-up
__________
Subtask 57-26-00-941-058
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-26-00-866-058
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 flap/slat control lever.
Subtask 57-26-00-865-058
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 Q21R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-26-00-010-058
D. Get Access
(1)
Put the access platform below the applicable wing trailing edge at flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
(2)
Remove the applicable flap track fixed fairing access panels (Ref. TASK 57-55-11-000-001):
-
for flap track 2, remove 531AB, 531BB, 631AB, 631BB
-
for flap track 3, remove 532AB, 532BB, 632AB, 632BB
-for flap track 4, remove 533AB, 533BB, 633AB, 633BB.
**ON A/C 301-399,
Subtask 57-26-00-010-058-A
D. Get Access
(1)
Put the access platform below the applicable wing trailing edge at flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
(2)
Remove the applicable flap track fixed fairing access panels (Ref. TASK 57-55-11-000-004):
-
for flap track 2, remove 531CB, 531EB, 631CB, 631EB
-
for flap track 3, remove 532CB, 532EB, 632CB, 632EB
-for flap track 4, remove 533CB, 533EB, 633CB, 633EB.
**ON A/C ALL
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 609/TASK 57-26-00-991-009)
**ON A/C 301-399,
(Ref. Fig. 609A/TASK 57-26-00-991-009-A)
Flap Track Beams 2, 3 and 4 - Forward Spigots, Bolts and Fittings
Figure 609/TASK 57-26-00-991-009
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-26-00Page 655 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R Flap Track Beams 2, 3 and 4 - Forward Spigots, Bolts and Fittings R Figure 609A/TASK 57-26-00-991-009-A
R 1EFF : 301-399, 1 57-26-00Page 656 1 1 May 01/04 1 1 1CES 1 **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.
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(29)
