6017CM(6067CM)/6019CM(6069CM)
27-84-45-991-001 Fig. 401
27-84-45-991-003 Fig. 403
3. Job Set-up
__________ (Ref. Fig. 401/TASK 27-84-45-991-001, 403/TASK 27-84-45-991-003) Subtask 27-84-45-941-070
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice in position to tell persons not to operate the slat controls.
Subtask 27-84-45-860-071
B. Aircraft Maintenance Configuration
(1)
Retract the slats fully (Ref. TASK 27-80-00-866-005).
(2)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the flap/slat control lever on panel 114VU.
Subtask 27-84-45-865-099
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
Subtask 27-84-45-010-061
D. Get Access
(1)
Put the access platform in position below the applicable access panel 521EB, 621EB.
(2)
Remove the applicable access panels:
-
for 6016CM(6066CM), remove 521EB, 621EB
-
for 6020CM(6070CM), remove 521GB, 621GB.
1EFF : ALL 1 27-84-45Page 471 1 1 Feb 01/00R 1 1 1CES 1
4. Procedure
_________
(Ref. Fig. 401/TASK 27-84-45-991-001, 403/TASK 27-84-45-991-003)
Subtask 27-84-45-020-063
A. Preparation for Removal
(1)
Install a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) (Ref. TASK 27-50-00-400-003): - on the torque shaft, inboard of the applicable component - on the torque shaft, outboard of the applicable component.
(2)
Remove the applicable steady bearing (44) (Ref. TASK 27-84-44-000-002):
-
FOR 6018CM
remove the steady bearing 6017CM
-
FOR 6068CM
remove the steady bearing 6067CM.
Subtask 27-84-45-020-057
B. Removal of the Torque Shafts 6018CM(6068CM)
(1)
Hold the steady bearing (46) and remove the shaft (45).
(2)
Remove the applicable steady bearing:
-
FOR 6018CM
remove 6019CM
-
FOR 6068CM
remove 6069CM.
1EFF : ALL 1 27-84-45Page 472 1 1 Feb 01/00R 1 1 1CES 1
TASK 27-84-45-400-009
Installation of the Torque Shaft 6018CM(6068CM)
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-018
GENERAL PURPOSE ASSEMBLY PASTE (Ref. 20-31-00)
Material No. 04-022 USA MIL-PRF-81322 GRADE 2
SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1 R 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
-------------------------------------------------------------------------------
27-50-00-000-003 Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001) 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
Slats (98D27504030001)
27-80-00-866-005 Retracting the Slats on the Ground
27-84-44-000-002 Removal of the Steady Bearings FIN
6017CM(6067CM)/6019CM(6069CM) 27-84-44-400-002 Installation of the Steady Bearings FIN 6017CM(6067CM)/6019CM(6069CM) 27-84-45-991-001 Fig. 401 R 27-84-45-991-002 Fig. 402 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8(4)
