(2)
Tighten the two screws.
(3)
Close the access door 822.
(4)
Remove the access platform(s).
1EFF : ALL 1 27-64-00Page 507 1 1 May 01/05R 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-149, 201-299,
TASK 27-64-00-820-001-A
Adjustment of the Spoilers
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY
_______ OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
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 circuit breaker(s) safety clip(s) No specific feeler gauge No specific warning notice No specific warning notices No specific access platform 1.6 m (5 ft. 3 in.) No specific access platform 3.5 m (11 ft. 6 in.) No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft) 98D27603000001 1 SPOILER POSITION CHECK TOOL 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 27-64-00Page 508 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
98D27903500000 2 PIN-SIDE STICK LOCKING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
27-50-00-866-008 Extension of the Flaps on the Ground
27-50-00-866-009 Retraction of the Flaps on the Ground
27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance
27-64-00-710-001 Operational Test of the Spoiler Hydraulic Actuation
29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply
29-10-00-864-003 Depressurize the Blue Hydraulic System
29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
Hydraulic System through the PTU with the Electric
Pump
29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems
after Operation of the PTU
29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump
29-24-00-864-001 Depressurize the Yellow Hydraulic System
27-64-00-991-001 Fig. 501
27-64-00-991-006 Fig. 502
27-64-00-991-002 Fig. 503
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 27-64-00Page 509 1 1 May 01/05 1 1 1CES 1
3. Job Set-up
__________ Subtask 27-64-00-860-060
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Make sure that the flaps are in the fully retracted position (Ref. TASK 27-50-00-866-009).
(3)
On the center pedestal, make sure that the SPEED BRAKE control lever is set to RET.
(4)
Install the PIN-SIDE STICK LOCKING (98D27903500000) on each side stick controller.
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