R 1EFF : 151-199, 401-499, 1 27-41-00Page 7 1 1 Aug 01/05 1 1 1CES 1
THS MECHANICAL CONTROL - ADJUSTMENT/TEST
________________________________________ TASK 27-41-00-820-001 Adjustment of the THS Zero Position 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 FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
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.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.80 m (5 ft. 11 in.)
No specific access platform 2.8 m (9 ft. 2 in.)
0U190360 1 PIN - RIGGING
98D27403500000 1 PITCH TRIM CONTROL LOCKING
R B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R 21-21-41-000-001 21-21-41-400-001 24-41-00-861-002
24-41-00-862-002
R R R R R R R 25-54-12-000-001 25-54-12-000-002 25-54-12-400-001 25-54-12-400-002 27-41-00-220-003 27-41-00-820-002 27-44-00-710-003
29-23-00-863-001
29-23-00-864-001
29-24-00-863-001
53-12-11-000-001
53-12-11-400-001
53-32-12-000-002 53-32-12-400-002 27-41-00-991-001 27-41-00-991-002 27-41-00-991-003 27-41-00-991-004
Removal of the Recirculation Filter 4012HM (4013HM) Installation of the Recirculation Filter 4012HM (4013HM)Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External Power Removal of the FWD Cargo Compartment Partition FR34 Removal of the Ceiling Panels in the FWD Cargo Compartment Installation of the FWD Cargo Compartment Partition FR34 Installation of the Ceiling Panels in the FWD Cargo CompartmentCheck of the Zero Adjustment of the THSAdjustment of the THS Control-Cables LengthOperational Test of the Trimmable Horizontal Stabilizer Actuator with both (Green and Yellow) and Individual Hydraulic SystemsPressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric PumpDepressurize the Green and Yellow Hydraulic Systems after Operation of the PTUPressurize the Yellow Hydraulic System with the Electric PumpRemoval of the Cockpit Floor Panels from FR1 Thru FR12Installation of the Cockpit Floor Panels from FR1 thru FR12Removal of the Cabin Floor PanelsInstallation of the Cabin Floor PanelsFig. 501Fig. 502Fig. 503Fig. 504
3. Job Set-up
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Subtask 27-41-00-010-054
A. Get Access R (1) Put the access platform in position at the zone 312
(2)
Open the access door 312AR.
(3)
Put the access platform in position at the zone 120.
(4)
Open the access door 811.
(5)
In the cabin, remove the floor panels 241FF, 241BF (Ref. TASK 53-32-12-000-002).
Subtask 27-41-00-860-056
B. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
Pressurize the Green and Yellow hydraulic systems.(Ref. TASK 29-23-00-863-001) (Ref. TASK 29-24-00-863-001)
(3)
On the center pedestal, make sure that the pitch-trim control-wheels are set to zero.
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