1480 STA
REF
SEE A INBD GROOVE CABLE LGV1B INBD GROOVE CABLE LGV1A OUTBD GROOVE CABLE LGV2A
OUTBD GROOVE CABLE LGV2B
BRACKET QUADRANT
SELECTOR VALVE QUADRANT
RIG PIN LG-1
FWD INBD
A
Landing Gear Control System Rigging - Installation Wing Quadrant Rig Pin
Figure 501
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REF 1480 STA
SEE A
CEILING PANEL (REMOVED)
SEE B
TURNBUCKLE 1290 STA CABLE LGV1B A
TURNBUCKLE CABLE LGV1A
NOTE:____ DIRECTION ARROW SHOWS MOVEMENT FOR LANDING GEAR UP. B FWD STA 1320 SAFETY CLIP (EXAMPLE)
Landing Gear Control System Rigging Body Cable Tensioning
Figure 502
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SEE A
CABLE LGV2A
QUADRANT
BRACKET
RIG PIN
LG-2
CABLE LGV2B
FWD
INBD
A
Landing Gear System Rigging Installation Nose-Body Quadrant Rig Pin Figure 503
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4) Tighten cables LGV2A and LGV2B at turnbuckles to 120 (|10) pounds.
NOTE: Adjust the cables until you can easily remove the
____ rigging pin and it does not rub.
The turnbuckles are on the ceiling of the wheel well for the right body landing gear (Fig. 504).
5) Remove rigging pin LG-1 from the selector valve quadrant for the wing landing gear. 6) Remove rigging pin LG-2 from the selector valve quadrant
for the nose/body landing gear. 7) Operate the system 20 times through maximum travel. 8) Put the handle in the OFF position. 9) Install the rigging pin in the quadrant above the selector
valve for the wing gear (Fig. 501).
(e) Set cable tension in cables LGVlA and LGVlB to that shown on Fig. 505.
NOTE: Adjust the cables until you can easily remove the
____
rigging pin.
(f)
Install rigging pin LG-2 in the quadrant above the selector valve for the nose/body landing gear (Fig. 503).
(g)
Set cable tension in cables LGV2A and LGV2B to that shown in Fig. 505.
NOTE: Adjust the cables until you can easily remove the
____
rigging pin.
(h)
Remove rigging pin LG-1 from the selector valve quadrant for the wing landing gear.
(i)
Remove rigging pin LG-2 from the selector valve quadrant for the nose/body landing gear.
(j)
Install the clips that lock the turnbuckles on all turnbuckles adjusted in this procedure.
S 215-006
(2)
Do a check of the adjustment of the control system.
(a)
Operate the system five times through maximum travel.
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Landing Gear Control System Rigging Wheel/Well Cable Tensioning
Figure 504
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