-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
R Refer to the MPD TASK: 574404-01
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 notices
No specific adjustable access platform 3.5 m (11 ft. 6 in.)
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
-------------------------------------------------------------------------------
27-80-00-866-004 Extending the Slats on the Ground
27-80-00-866-005 Retracting the Slats on the Ground
R NTM 57-44-04 ASRM 574000 (for corrective action) 57-44-00-991-009 Fig. 603
3. Job Set-up
__________
Subtask 57-44-00-941-055
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.
(3)
Put the adjustable access platform below the applicable wing leading edge at slat 3, zone 521(621).
Subtask 57-44-00-860-056
B. Aircraft Maintenance Configuration
(1)
Extend the slats fully (Ref. TASK 27-80-00-866-004).
(2)
Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever.
Subtask 57-44-00-865-060
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
4. Procedure
_________
(Ref. Fig. 603/TASK 57-44-00-991-009)
Subtask 57-44-00-110-058
R A. Preparation for Inspection
R R R (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the slat 3 skin connection (in the area of the lower girder at track ribs 7 and 8).
Subtask 57-44-00-280-051
B. Inspection
(1) Examine the slat 3 skin connection (Ref. NTM 57-44-04) PART 9.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 574000) for the____ correct repair procedure.
5. Close-up________
Subtask 57-44-00-865-061
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 57-44-00-860-057
B. Aircraft Configuration
(1) Retract the slats fully (Ref. TASK 27-80-00-866-005).
Subtask 57-44-00-942-061
C. Removal of Equipment
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Remove the access platform(s).
(3) Remove the safety barriers.
(4) Remove the warning notice(s).
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
1EFF : ALL 1 57-44-00Page 615 1 1 Nov 01/04R 1 1 1CES 1
Details of the Slat 3 Skin Connection in the area of the Lower Girder (Track
Ribs 7 and 8)
Figure 603/TASK 57-44-00-991-009- 12 (SHEET 1)
Details of the Slat 3 Skin Connection in the area of the Lower Girder (Track
Ribs 7 and 8)
Figure 603/TASK 57-44-00-991-009- 22 (SHEET 2)
TASK 57-44-00-200-009 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3(48)
