(4)
Install the center mount clamp (25), as follows:
(a)
Remove the bolt (10), the washer (15) and the nut (20) from the band on the center mount clamp (25).
(b)
Open the band on the center mount clamp (25) and put the lower case drain hose (5) into the hole in the insert.
(c)
Put the band on the insert and install the bolt (10), the washer
(15) and the nut (20).
(d)
Make sure that the center mount clamp is installed at a distance of 338 mm (13.3070 in.) below the flange of the suction hose/tube.
(e)
TORQUE the nut (20) to between 0.23 and 0.28 m.daN (20.35 and
24.77 lbf.in).
(5)
Make sure that the lower case drain hose (5) is in the correct position.
NOTE : Use a second wrench to hold the fittings when you TORQUE the
____ coupling nuts. This prevents damage to the hose.
(6)
TORQUE the coupling nuts of the lower case drain hose (5) to between
2.43 and 2.77 m.daN (17.92 and 20.42 lbf.ft).
(7)
Remove the container.
1EFF : ALL 1 29-11-49Page 442 1 1 Feb 01/03R 1 1 1CES 1
Subtask 29-11-49-710-061
B. Operational Test
(1) Do the operational test of the Green hydraulic system (Ref. TASK 29-11-00-710-001).
(2) During the dry motoring of the engine 1, make sure that there are no R leaks from the case drain hose/tube.
(3) Make sure that the level of the hydraulic fluid in the Green reservoir is correct. If necessary, fill the reservoir (Ref. TASK 12-12-29-611-001) or (Ref. TASK 12-12-29-611-002).
5. Close-up
________
Subtask 29-11-49-860-094
A. Aircraft Maintenance Configuration
(1)
Remove the access platform(s).
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 29-11-49-410-062
B. Close Access
R (1) Close the left fan cowl door: FOR 1000EM1 R - close the door 437AL (Ref. TASK 71-13-00-410-040).
(2)
Close the door 195BB.
Subtask 29-11-49-942-063
C.
Safety Precautions
(1) Remove the warning notice(s).
TASK 29-11-49-000-005
Removal of the Hydraulic Low-Pressure Switch Tube
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS FOR A SHORT TIME AFTER
_______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY.
CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC
_______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
R No specific container No specific protective covers No specific warning notice(s) No specific wrench No specific container 5 l (1.3208 USgal) FOR FIN 1000EM1 No specific access platform 0.8 m (2 ft. 7 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 29-11-49-991-910 Fig. 407
R 29-11-49-991-922 Fig. 408 FOR FIN 1000EM1 71-13-00-010-040 Opening of the Fan Cowl Doors
3. Job Set-up
__________
Subtask 29-11-49-860-085
A. Aircraft Maintenance Configuration
(1)
Depressurize the Green hydraulic system (Ref. TASK 29-23-00-864-001).
(2)
Depressurize the Green hydraulic reservoir (Ref. TASK 29-14-00-614-001).
(3)
Put warning notice(s) in position to tell persons not to pressurize the Green hydraulic system: - on the ground service panel 197CB.
(4)
Put warning notice(s) in position on the access door 195BB to tell persons not to pressurize the Green hydraulic reservoir.
Subtask 29-11-49-941-071
B. Safety Precautions
(1)
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