757 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 3(14)

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A
757 MAINTENANCE MANUAL
 4)  The left and right elevator trailing edge upper surfaces (Fig. 505) move less than 0.10 inch (2.5 mm) when auxiliary pitot systems No. 1 and 2 are pressurized and not pressurized (AMM 34-11-00/201).
 B.  Equipment
 (1)  
Adjustment Equipment for the Neutral Shift
 Transducers (PROCEDURE 1):

 (a)  
Breakout Box - A27063-2 (Part of Flight
 Controls Position Sensors Rigging Set,
 A27063-88)

 (b)  
Cable Assembly - A27063-27 (Part of Flight
 Controls Position Sensors Rigging Set,
 A27063-88)

 (c)  
Power Supply - Powertron Model 5900
 Industrial Test Equipment Corp.
 Port Washington, New York

 (2)  
Adjustment Equipment for the Neutral Shift
 Transducers (PROCEDURE 2):

 (a)  
Breakout Box - A27063-2 (Part of Flight
 Controls Position Sensors Rigging Set,
 A27063-88)

 (b)  
Cable Assembly - A27063-26 (Part of Flight
 Controls Position Sensors Rigging Set,
 A27063-88)

 (c)  
Cable Assembly - A27063-27 (Part of Flight
 Controls Position Sensors Rigging Set,
 A27063-88)

 (d)  
Ratiometeric Digital Phase Angle
 Voltmeter - North Atlantic Model
 225-400R30
 North Atlantic Industries Inc.
 Hauppauge, New York

 (3)  
Adjustment Equipment for the Neutral Shift
 Transducers (PROCEDURE 3):

 (a)  
Breakout Box - A27063-2 (Part of Flight
 Controls Position Sensors Rigging Set,
 A27063-88)

 (b)  
Cable Assembly - A27063-26 (Part of Flight
 Controls Position Sensors Rigging Set,
 A27063-88)

 (c)  
Cable Assembly - A27063-27 (Part of Flight
 Controls Position Sensors Rigging Set,
 A27063-88)

 (4)  
Adjustment Equipment for the Neutral Shift
 Transducers (PROCEDURE 4):

 (a)  
Voltmeter - Phase Synchronous Model 101,
 101-AA01
 Electronic Aviation
 Renton, Washington

 

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757
MAINTENANCE MANUAL

 (5)  Gage Assembly - B27039-3 (Part of Elev & Stab
 Trim Control Systems Rigging Equipment,
 B27039-1)

 NOTE: The gage assembly is used to set
____
 stabilizer jackscrew Dimension B in the
 correct position to adjust the elevator
 system.

 (6)  Holding Tool, Elevator Tension Regulator -B27022-4

 NOTE: This tool is used when new control
____
 cables are adjusted for the first time.

 (7)  
Rig Pins from Set B20003-XX (AMM 20-10-24/201):

 (a)  
E/ST6 - P/N B20003-21

 (b)  
E/ST7 - P/N B20003-21

 (c)  
E/ST8 - P/N B20003-21

 (d)  
E/ST9 - P/N B20003-21

 (e)  
E/ST10 - P/N B20003-21

 (f)  
E/ST11 - P/N B20003-21

 (8)  
Spring Removal Tool, Decentering, Elevator
 Controls - B27060-1

 (9)  
Surface Protractor - Commercially Available

 (10)
 Cable Tensiometer, 0 to 250 pounds (0 to 1,100 newtons) -Commercially Available

 C.
Consumable Materials

 (1)  
C00308 Compound, Corrosion Preventive
 MIL-C-11796, Class III

 (2)  
D00002 Compound, Anti Seize - AMS-3080

 D.
References

 (1)  
AMM 06-41-00/201, Fuselage Access Doors and Panels

 (2)  
AMM 06-42-00/201, Empennage Access Doors and Panels

 (3)  
AMM 22-00-02/201, Autoflight BITE

 (4)  
AMM 22-12-01/401, Autopilot Pitch Control Servo

 (5)  
AMM 24-22-00/201, Electrical Power - Control

 (6)  
AMM 27-38-00/501, Elevator Position Indicating System

 (7)  
　
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