1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
98D27303001001 1 HOLDER - SIDE STICK
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-92-41-000-001 Removal of the Side Stick Assembly 19VU (18VU)
27-92-41-991-003-A Fig. 404
3. Job Set-up
__________ Subtask 27-92-41-010-051 R A. Remove the side stick assembly (Ref. TASK 27-92-41-000-001). Subtask 27-92-41-480-052
B. Install the side stick assembly on the HOLDER - SIDE STICK
(98D27303001001).
4. Procedure
_________
(Ref. Fig. 404/TASK 27-92-41-991-003-A) Subtask 27-92-41-020-051-A
A. Removal of the Side Stick Transducer-Unit
(1)
Cut and discard the cotter pins (35) from the nuts (34).
(2)
Remove the nuts (34), the washers (36).
(3)
Remove the bolts (33) and disconnect the rods (32).
(4)
Remove the nuts (38)
or remove the bolts (38) and the washers (45).
(5)
Remove the transducer unit (37).
(6)
Put blanking caps on the disconnected electrical connectors.
1EFF : ALL 1 27-92-41Page 416 1 1 May 01/03R 1 1 1CES 1
Transducer Units Figure 404/TASK 27-92-41-991-003-A
1EFF : 1 1R 1CES ALL 1 11 1 27-92-41 Page 417 May 01/03
TASK 27-92-41-400-002
Installation of the Transducer Units (4CE1,4CE2,4CE3,4CE4)
WARNING : MAKE SURE THAT THE SIDE STICK ASSEMBLY STAYS IN THE VERTICAL POSITION
_______
DURING THE MAINTENANCE PROCEDURES.
IF NOT THERE IS A RISK OF SKYDROL LEAKAGE.
SKYDROL CAN CAUSE INJURY AND/OR DAMAGE.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific warning notice
No specific access platform 1.6 m (5 ft. 3 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft) 98DNSA20206080 1 RIGGING PIN
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
No specific lockwire-corrosion resistant steel dia. 0.8 mm (0.03 in.)
Material No. 19-009 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.5MM DIA
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
cotter pin 27-92-41 01D-080
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
Power 27-92-41-000-001 Removal of the Side Stick Assembly 19VU (18VU) 27-92-41-400-001 Installation of the Side Stick Assembly 19VU (18VU) 27-92-41-991-003-A Fig. 404
3. Job Set-up
__________ Subtask 27-92-41-860-052
A. Aircraft Maintenance Configuration
(1)
Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
(2)
Make sure that the access platform is in position at the access door
822.
(3)
Make sure that the access door 822 is open.
(4)
On the battery power center 105VU:
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