(7) Engage the nuts (3) on the lugs (4) and tighten.
Subtask 23-51-34-865-053
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s): R 4RN, 5RN, 6RN, 8RN, 9RN
1EFF : ALL 1 23-51-34Page 405 1 1 Feb 01/02 1 1 1CES 1 Subtask 23-51-34-740-050
C. Do the BITE test of the AMU-ACP (Ref. TASK 23-51-00-740-002). NOTE : As an alternative procedure, you can do this operational test
____
without the CFDS (Ref. TASK 23-51-00-710-001).
5. Close-up
________
Subtask 23-51-34-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
R (2) Close the access door 824 (Ref. TASK 52-41-00-410-002).
(3) Remove the access platform(s).
1EFF : ALL 1 23-51-34Page 406 1 1 Feb 01/02 1 1 1CES 1 STATIC DISCHARGING - DESCRIPTION AND OPERATION
______________________________________________
1. General
_______
R During flight, the aircraft becomes charged with static electricity. If the discharge of the static electricity is not controlled, it causes interference in the communications and navigation systems.
To decrease the effect of this interference, static dischargers are installed.
2. Component Location
__________________ R (Ref. Fig. 001)
-------------------------------------------------------------------------------STATIC DISCHARGERS LOCATION QUANTITY ZONE
-------------------------------------------------------------------------------Wing Tip Fence 4 534(634)
Elevator Tip 1 335(345)
Horizontal Stabilizer Tip 1 332(342)
Vertical Stabilizer Tip 1 324
Rudder Tip 1 326
Wing Fixed Trailing Edge 1 534(634)
Aileron Trailing Edge 4 590(690)
Elevator Trailing Edge 3 335(345)
Rudder Trailing Edge 3 326
No.2 Flap Track Movable Fairing 1 531(631)
No.3 Flap Track Movable Fairing 1 532(632)
No.4 Flap Track Movable Fairing 1 533(633)
Engine Pylon Rear Fairing 1 470(480)
3. System Description
__________________ Each static discharger assembly has a retainer and a static discharger. The retainer is attached to the structure by rivets. The static discharger is attached to its retainer by one screw, to make it easy to replace.
Static discharger assemblies are installed at the tips of:
-
the wing-tip fence
-
the horizontal stabilizer
-
the vertical stabilizer
-
the elevators
-
the rudder
and on the trailing edges of:
-
the wing fixed structure
-
the ailerons
-
the elevators
-
the rudder
1EFF : ALL 1 23-60-00Page 1 1 1 Aug 01/04 1 1 1CES 1
Static Dischargers - Location
Figure 001
1EFF : ALL 1 23-60-00 Page 2
1 1 Feb 01/98
1 1
1CES 1
-
the flap-track movable-fairings
-
the engine-pylon rear-fairings.
Two types of retainer are installed:
-a flat retainer at the trailing edges
-an angular retainer at the tips.
Two types of static discharger are installed:
- one with a straight mounting, installed at the trailing edges
- one with a 30-degree angle mounting, installed at the tips.
The two types are not interchangeable.
4. Power Supply
____________ R Not Applicable.
5. Interface
_________ R Not Applicable.
6. Operation/Control and Indicating
________________________________
The static dischargers:
-decrease the voltage level necessary to start corona discharge
-make regions of very low radio-frequency field-strength and thus cause the discharge to occur in these regions
-discharge the static electricity charge.
The effect is to decrease the interference in the communications and navigation systems.
1EFF : ALL 1 23-60-00Page 3 1 1 Nov 01/04 1 1 1CES 1 STATIC DISCHARGER - DESCRIPTION AND OPERATION
_____________________________________________
1. General_______
The full description and operation of the static dischargers is given in (Ref. 23-60-00).
1EFF : ALL 1 23-61-00Page 1 1 1 Feb 01/98 1 1 1CES 1 STATIC DISCHARGER - INSPECTION/CHECK
____________________________________
TASK 23-61-00-200-001
-Check Resistance of Tip to Retainer - Check Bonding of Retainer to Structure
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