S 495-176

 (5)  
Install the rig pins NS1 (15, View A-A, Fig. 501), NS2 (59, Detail C, Fig. 501), NS3 (55, Detail D, Fig. 502), and NS6 (24, View C-C, Fig. 501). Make sure they have a free fit.

 NOTE: The rig pins have a free fit if you can install or remove
____ them with two fingers. Some resistance is permitted on rig pin NS6 only .
 

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 S 095-177
 (6)  
Remove all of the rig pins.

 S 735-178

 (7)  
Do the System Test - Nose Wheel Steering.

_________________________________
 TASK 32-51-00-825-001
 3. Rigging Check of the NGPP/Rudder Interconnect System (Fig. 501, 502)
____________________________________________________
 A. General
 (1)  
The NGPP/rudder interconnect system is correctly adjusted if the conditions that follow occur:

 (a)  
The rudder pedal steering will not operate when the NGPP cable loop disengages the rudder pedal steering. The hydraulic power must be on.

 (b)  
Rig pins NS6 (24, View C-C, Fig. 501) and NS7 (40, Detail A, Fig. 502) can be installed only when the piston position quadrant (46) is turned clockwise to the air mode. To do a check of the free fit of rig pin NS7 turn the piston position quadrant to the air mode (rudder pedal steering disengaged) and install NS6. NS6 can be a tight fit because of the load on the interconnect springs.

 NOTE: The rig pins have a free fit if you can install or
____ remove them with two fingers. Some resistance is permitted on rig pin NS6 only.
 (c)  
The NGPP cables for the NGPP/rudder interconnect have the correct tension (do the check with the hydraulic power off).

 (2)  
There must be no more than a 5°F difference between the inner and the outer temperatures of the airplane. The temperatures must be stable for one hour or more before you do the adjustment and also during the adjustment.

 B.
Equipment

 (1)  
Rig Pins from Set B20003-XX (AMM 20-10-24/201):

 (a)  
NS6 - P/N B20003-5

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 (b)  
NS7 - P/N B20003-15

 (2)  
Cable Tensiometer, 0 to 200 pound range for
 3/32 inch diameter cable - Commercially
 Available

 (3)  
Line to hold the NLG Top Torsion Link (Rope or
 Cord)

 C.
References

 (1)  
AMM 07-11-02/201, Jacking Airplane Nose

 (2)  
AMM 20-10-24/201, Rig Pins

 (3)  
AMM 29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems

 (4)  
AMM 32-00-15/201, Landing Gear Door Locks

 (5)  
AMM 32-00-20/201, Landing Gear Downlocks

 D.
Access

 (1)  
Location Zones
 115 NLG Wheel Well (Left)
 116 NLG Wheel Well (Right)
 119 Main Equipment Center (Left)
 120 Main Equipment Center (Right)
 211 Control Cabin (Left)
 212 Control Cabin (Right)
 711 Nose Landing Gear (NLG)

 E.
Prepare to do the Rigging Check

 S 495-004
 (1)  Make sure the downlocks are installed for the nose and main landing gear (AMM 32-00-20/201)
 S 495-149
 WARNING:_______OBEY THE INSTALLATION PROCEDURE FOR THE DOOR LOCKS. THE DOORS OPEN AND CLOSE QUICKLY. THE MOVEMENT OF THE DOORS CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
 (2)  Open the doors for the nose landing gear and install the door lock (AMM 32-00-15/201).
 

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 S 865-005
 WARNING: MAKE SURE YOU REMOVE THE HYDRAULIC PRESSURE TO THE SYSTEM FOR
_______ THE NOSE WHEEL STEERING BEFORE YOU DO THE CHECK. IF YOU DO NOT REMOVE THE HYDRAULIC PRESSURE, THE NOSE WHEELS CAN TURN WHEN YOU MOVE THE TILLER. THE MOVEMENT OF THE NOSE WHEEL CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (3)  
Remove the pressure from the left hydraulic system
 (AMM 29-11-00/201).

 F.
Do the Rigging Check

 S 835-179
 (1)  Make sure the conditions of this rigging check are satisfactory. If they are not, do the next task, Rigging of the NGPP/Rudder
　
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