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时间:2011-03-22 06:40来源:蓝天飞行翻译 作者:admin
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1 cotter pin 27-92-41 01D-080 18 cotter pins 27-92-41 01D-001 18 cotter pins 27-92-41 01D-001A 18 cotter pins 27-92-41 01D-001B 18 cotter pins 27-92-41 01D-001C 18 cotter pins 27-92-41 01D-001D 18 cotter pins 27-92-41 01D-001E 18 cotter pins 27-92-41 01D-001F 18 cotter pins 27-92-41 01D-001G 18 cotter pins 27-92-41 01D-001H 18 cotter pins 27-92-41 01D-001J 18 cotter pins 27-92-41 01D-001K
 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
 Power 27-92-41-400-001 Installation of the Side Stick Assembly 19VU (18VU) 27-92-41-400-002 Installation of the Transducer Units
 (4CE1,4CE2,4CE3,4CE4) 27-92-41-991-002-A Fig. 402 27-92-41-991-014 Fig. 413
 3. Job Set-up
__________
 Subtask 27-92-41-860-056
 A. Aircraft Maintenance Configuration
 (Ref. Fig. 413/TASK 27-92-41-991-014)

 (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.


 1EFF : ALL 1 27-92-41Page 476 1 1 May 01/04R 1 1 1CES 1


 (4)
 On the battery power center 105VU:

 -make sure that the protective cover is removed.

 (5)
 Make sure that the side stick assembly is installed on the HOLDER -SIDE STICK (98D27303001001).

 (6)
 Make sure that the PIN-SIDE STICK LOCKING (98D27903500000) is installed.

 (7)
 Make sure that the RIGGING PIN (98DNSA20206080) (7) is in position on the roll transducer unit (8) and on the pitch transducer unit (6).

 (8)
 Make sure that the warning notice which tells persons not to operate the side stick is in position on the side stick.


 Subtask 27-92-41-480-057
 B. Installation of the Tools
 (Ref. Fig. 413/TASK 27-92-41-991-014)

 (1)
 Install the TOOL - ARTIFICIAL FEEL RODS (98D27303004000) (5) on the structure of the side stick (10).

 (2)
 Put the dial test indicator at the bellcrank of the pitch transducer unit (6).

 (3)
 Adjust the dial test indicator to the 0 position.

 (4)
 Remove the blanking cap from the electrical connector (15): (Ref. Fig. 402/TASK 27-92-41-991-002-A)

 -
for the CAPT side stick, electrical connector 2197VC

 -
for the F/O side stick, electrical connector 2188VC.

 

 (5)
 Connect the 28 VDC POWER SUPPLY TOOL (355M03200001) to the electrical connector (15) and to the 28 VDC aircraft network.

 (6)
 Set the switch of the 28 VDC POWER SUPPLY TOOL (355M03200001) to the ON position.


 Subtask 27-92-41-080-055
 C. Removal of the Tools
 (1) Remove the PIN-SIDE STICK LOCKING (98D27903500000) (10) from the center universal joint of the side stick assembly. (Ref. Fig. 402/TASK 27-92-41-991-002-A)
 1EFF : ALL 1 27-92-41Page 477 1 1 May 01/04R 1 1 1CES 1


 (2)
 Remove the RIGGING PIN (98DNSA20206080) (7) from the pitch transducer unit (6). (Ref. Fig. 413/TASK 27-92-41-991-014)

 (3)
 Make sure that the dial test indicator stays at 0 mm +0.01 mm (+0.0003 in.) -0.01 mm (-0.0003 in.).


 (a) If it is not the case, do the adjustment of the input rods of the pitch transducer unit (6) (Ref. TASK 27-92-41-400-002).
 4. Procedure
_________ Subtask 27-92-41-420-061
 A. Installation of the Side Stick Spring Rods
 (1)
 Clean the component interface and/or the adjacent area.

 (2)
 Do an inspection of the component interface and/or the adjacent area.

 (3)
 Install one spring rod (19) (pitch damper side).

 (4)
 Make sure that the spring rod (19) is installed in the direction identified during the removal.

 (5)
 Install the bolts (17).

 (6)
 Set the switch of the 28 VDC POWER SUPPLY TOOL (355M03200001) to the OFF position.

 (7)
 Adjust the length of the spring rod (19) to get 0 at the dial test indicator. Adjust the spring rod (19) as follows:

 (a)
 Cut and discard the lockwire.

 (b)
 Loosen the nut (20) and disengage the lockwasher (21).

 (c)
 Turn the body (22) of the spring rod (19).

 

 (8)
 Put the nut (20) in contact with the lock washer (21). Do not tighten the nut (20) at this time.
 
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