(2)
Open the access door 312AR.
(3)
Put an ACCESS PLATFORM 2M (6 FT) in position at the access door 811.
(4)
Open the access door 811.
(5)
Put an ACCESS PLATFORM 2M (6 FT) in position at the access door 812.
(6)
Open the access door 812.
(7)
Put an ACCESS PLATFORM 2M (6 FT) in position at the access door 824.
(8)
Open the access door 824.
(9)
Put an ACCESS PLATFORM 2M (6 FT) in position at the cargo compartment door 825.
(10)
Open the cargo compartment door 825.
(11)
Put an ACCESS PLATFORM 2M (6 FT) in position at the cargo compartment door 826.
(12)
Open the cargo compartment door 826.
(13)
Remove the floor panels 211GF, 211KF, 241BF, 241FF (Ref. TASK 53-12-11-000-001) (Ref. TASK 53-32-12-000-002).
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
Subtask 27-21-00-860-050
B. Aircraft Maintenance Configuration
(1)
Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
(2)
Make sure that the air conditionning does not operate (Ref. TASK 12-33-21-618-001).
(3)
The aircraft must stay at least three hours in this configuration in order to get an uniform stabilized temperature.
(4)
Make sure that there is no neon light on, near the cable, in the cable routing aera.
(5)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(6)
Pressurize the Blue hydraulic system (Ref. TASK 29-10-00-863-003).
(7)
On the center pedestal, on the panel 110VU, make sure that the RUD TRIM indicator shows 0.
(8)
On the overhead panel 23VU, make sure that the FLT CTL/FAC1 pushbutton switch is pushed (the OFF legend is off).
(9)
On the overhead panel 24VU, make sure that the FLT CTL/FAC2 pushbutton switch is pushed (the OFF legend is off).
(10)
Operate the rudder pedals fully more than ten times and put them in the zero position.
(11)
Put warning notices in position on the rudder pedals (CAPT and F/0) to tell persons not to operate them.
(12)
Install the PIN - RIGGING (98D27207547000) or RIGGING PIN SET (98D27207516000) (6) on the cable quadrant (5).
(13)
Depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003).
(14)
De-energize the aircraft electrical cicuits (Ref. TASK 24-41-00-862-002).
(15)
Remove the control rod (7) between the mixer and the cable quadrant
(5) (Ref. TASK 27-21-00-840-001).
(16)
Do a check of the dimension 25 +2 -2 mm (0.9842 +0.0787 -0.0787 in.) on the cable quadrant (5). If the dimension is not correct, adjust it as follows:
(a)
Remove the lockwire from the nuts (3) and discard it.
(b)
Loosen the nuts (3).
(c)
Turn the bolts (4) until you get the correct dimension.
(d) Tighten the nuts (3). Do not safety the nuts (3) at this time. R **ON A/C 106-149, 218-299, 301-399, 401-499,
Subtask 27-21-00-860-050-A
B. Aircraft Maintenance Configuration
(1)
Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
(2)
Make sure that the air conditionning does not operate (Ref. TASK 12-33-21-618-001).
(3)
The aircraft must stay at least three hours in this configuration in order to get an uniform stabilized temperature.
(4)
Make sure that there is no neon light on, near the cable, in the
cable routing aera.
(5)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(6)
Pressurize the Blue hydraulic system (Ref. TASK 29-10-00-863-003).
(7)
On the center pedestal, on the panel 110VU, make sure that the RUD TRIM indicator shows 0.
(8)
On the overhead panel 23VU, make sure that the FLT CTL/FAC1
pushbutton switch is pushed (the OFF legend is off).
(9)
On the overhead panel 24VU, make sure that the FLT CTL/FAC2
pushbutton switch is pushed (the OFF legend is off).
(10)
Operate the rudder pedals fully more than ten times and put them in the zero position.
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