B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
21-52-41-000-001 Removal of the Air Conditioning Pack 10HM (11HM) 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
32-12-00-010-001 Open the Main Gear Doors for Access
27-84-45-991-001 Fig. 401
27-84-45-991-002 Fig. 402
3. Job Set-up
__________ R (Ref. Fig. 401/TASK 27-84-45-991-001, 402/TASK 27-84-45-991-002) Subtask 27-84-45-941-071
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.
(3)
Put a warning notice in position to tell persons not to operate the landing gear doors.
Subtask 27-84-45-860-064
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.
R Torque shafts - Slat Power Transmission Figure 401/TASK 27-84-45-991-001
1EFF : 1 1 1CES ALL 1 111 27-84-45 Page 403 May 01/03
Torque Shafts - Slat Power Transmission Figure 402/TASK 27-84-45-991-002
1EFF : 1 1R 1CES ALL 1 11 1 27-84-45 Page 404 May 01/00
Subtask 27-84-45-865-050
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 27-84-45-010-050
D. Get Access
(1)
Open the main gear doors (Ref. TASK 32-12-00-010-001).
(2)
Make sure that the GROUND LOCK SLEEVE is on the applicable main gear door actuator.
(3)
Remove the air conditioning pack 10HM (Ref. TASK 21-52-41-000-001).
4. Procedure
_________ (Ref. Fig. 401/TASK 27-84-45-991-001, 402/TASK 27-84-45-991-002) Subtask 27-84-45-020-050
A. Removal of the Torque Shafts 6002CM/6004CM
(1)
Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) on the torque shaft 6006CM(6056CM) (Ref. TASK 27-50-00-400-003).
(2)
Remove the nuts (2), the bolts (4) and the shaft (3).
(3)
Remove the universal joint (1).
(4)
Remove the retaining ring (6), the pin (7) and the universal joint (5).
1EFF : ALL 1 27-84-45Page 405 1 1 May 01/00R 1 1 1CES 1
TASK 27-84-45-400-002
Installation of the Torque Shaft 6002CM(6004CM)
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
__________________
R R 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
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
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
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
