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时间:2011-04-06 23:12来源:蓝天飞行翻译 作者:航空
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B.  MIL-T-6845, MIL-T-8504 AND MIL-T-8808 CRES FLARED TUBE ENDS
C.  MIL-T-6845 CRES WITH BACS13AP PRESET SLEEVE

D.  HOSE END FITTINGS WITH STEEL INSERTS (NIPPLES)
E.  ALL TITANIUM TUBE ENDS
TORQUE VALUES APPLICABLE TO THE FOLLOWING TUBE ENDS:
A.  ALUMINUM WITH BACS13BD & BACS13BX SWAGED SLEEVES
B.  6061-T6 ALUMINUM WITH PRESET BACS13AP SLEEVES
C.  ANNEALED CRES WITH PRESET BACS13AP SLEEVES

D.  FLARELESS TYPE HOSE END FITTINGS WITH ALUMINUM INSERTS (NIPPLES)
E.  ALUMINUM FLARED TUBE ENDS
Installation Torque for Flareless Fittings
Figure 403 (Sheet 1)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.

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747-400
MAINTENANCE MANUAL

CARE SHOULD BE TAKEN IN SELECTING THE CORRECT TORQUE FOR REDUCER FITTINGS. THE BOSS OR BULKHEADSIZE DETERMINES THE FITTING INSTALLATION TORQUE.
TUBE MATERIAL SPECIFICATIONS:
A. 6061-T6 ALUMINUM - MIL-T-7081, WW-T-700/6
B. ANNEALED CRES - MIL-T-8504, MIL-T-8606, MIL-T-8808
C. 1/8 HARD CRES - MIL-T-6845 D 21-6-9 CRES - BMS 7-185
E. TI-3AL-2.5V - BMS 7-234
TORQUE VALUES ARE APPLICABLE TO STANDARD MS FLARELESS TUBE ENDS (BACS13AP SLEEVES) ON MIL-T-6845 (304-1/8 HARD) TUBING WITH A MINIMUM WALL THICKNESS AS GIVEN BELOW:

SIZE  -4  -5  -6  -8  -10  -12 
THICKNESS WALL  0.020  0.020  0.028  0.035  0.049  0.049 

TORQUE EXCEPTION FOR SPECIAL THIN WALL MIL-T-6845 (304-1/8h) TUBING IS AS FOLLOWS:
SIZE  -8  -10  -12 
THICKNESS WALL  0.028  0.035  0.042 
(POUND-INCHES) TORQUE  375  575  725 


TORQUE VALUES ARE APPLICABLE TO STANDARD MS FLARELESS TUBE ENDS (BACS13AP SLEEVES) ON 6061-T6 ALUMINUM AND ANNEALED CRES TUBING WITH A MINIMUM WALL THICKNESS AS GIVEN BELOW:
SIZE  -3  -4  -5  -6  -8  -10  -12  -16 
THICKNESS WALL  0.028  0.028  0.028  0.028  0.028  0.028  0.028  0.035 

TORQUE EXCEPTION FOR SPECIAL THIN WALL ANNEALED CRES TUBING IS AS FOLLOWS:
SIZE  -6  -10  -12 
THICKNESS WALL  0.020  0.020  0.020 
(POUND-INCHES) TORQUE  160  250  325 

Installation Torque for Flareless Fittings
Figure 403 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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747-400
MAINTENANCE MANUAL

RESISTANCE BETWEEN BULKHEAD FITTINGS AND HYDRAULIC TUBE

TUBE SIZE  MAXIMUM RESISTANCE (MILLIOHM) 
ALUMINUM  TITANIUM 
PERMASWAGE  WELD-ON 
-04  ____  6  12 
-06  0.70  4  8 
-08  ____  2.5  5 
-10  0.41  1.5  3 

Resistance Between Bulkhead Fittings and Hydraulic Tubing
Figure 404

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E47335
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747-400
MAINTENANCE MANUAL

RESISTANCE ACROSS UNION/TEE FITTINGS (TUBE-TO-TUBE)

TUBE SIZE  MAXIMUM RESISTANCE (MILLIOHM) 
ALUMINUM  TITANIUM 
-04  ____  12 
-06  1.30  8 
-08  ____  5 
-10  0.75  3 

Resistance Across Union/Tee Fittings (Tube-To-Tube)
Figure 405

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