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时间:2011-04-15 08:40来源:蓝天飞行翻译 作者:航空
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 70-23-00
 ALL  ú ú N01 Page 203 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
INCH THREAD DIMENSION  TORQUE, POUND-INCHES
OIL LUBRICATED  ANTISEIZE COATED 
MAX  MIN*  MAX  MIN* 
TYPE I  TYPE II  TYPE I  TYPE II
0.112 -40  6  4.5  5  4.5  3.5  4
0.138 -32  11.5  8.5  10  8.5  6.5  7.5
0.164 -32  22  16  20  16.5  12.5  15
0.164 -36  24  18  22  18  13.5  16
0.190 -24  30  23**  27**  21.5  16  19.5
0.190 -32  36  24**  32**  26  19.5  23**
0.250 -20  70  50**  65**  50  37**  45**
0.250 -28  85  65**  75**  60  45**  54**
0.3125-18  150  110** 135** 105  80**  95**
0.3125-24  170  125** 150** 120  90** 110**
0.375 -16  270 200** 250** 185  140** 170**
0.375 -24  300  225** 275** 215  160** 190**
0.4375-14  425  325  375  300  225  270 
0.4375-20  475  350  425  340  255  310 
0.500 -13  650  500  600  450  340  400 
0.500 -20  750  550  675 515 390 460 
INCH THREAD DIMENSION  TORQUE, NEWTON-METERS 
OIL LUBRICATED ANTISEIZE COATED 
MAX  MIN*  MAX  MIN* 
TYPE I TYPE II TYPE I  TYPE II 
0.112 -40  0.678  0.508  0.565  0.508  0.395  0.452
0.138 -32  1.299  0.960  1.130  0.960  0.734  0.847
0.164 -32  2.486  1.808  2.260  1.864  1.412  1.695
0.164 -36  2.712  2.034  2.486  2.034  1.525  1.808
0.190 -24  3.390  2.599**  3.051**  2.429  1.808  2.203
0.190 -32  4.067  2.712**  3.616**  2.938  2.203  2.599**
0.250 -20  7.909  5.649**  7.344**  5.649  4.180**  5.084**
0.250 -28  9.604  7.344**  8.474**  6.779  5.084**  6.101**
0.3125-18  16.948  12.428** 15.253** 11.863  9.039** 10.734**
0.3125-24  19.207  14.123** 16.948** 13.558  10.169** 12.428**
0.375 -16  30.506  22.597** 28.246** 20.902  15.818** 19.207**
0.375 -24  33.895  25.422** 31.071** 24.292  18.078**  21.467** 
0.4375-14  48.019  36.720  42.369  33.895  25.422  30.506 
0.4375-20  53.668  39.545  48.019  38.415  28.811  35.025 
0.500 -13  73.440  56.492  67.791  50.834  38.415  45.194 
0.500 -20  84.739 62.142 76.265 58.187 44.064  51.973

L-90034
* USE TYPE I MINIMUM VALUES WHEN YOU MUST ALIGN THE LOCK HOLES (COTTER PINS AND LOCKWIRE)
 AT THE ASSEMBLY. USE TYPE II MINIMUM VALUES WHEN IT IS NOT NECESSARY TO ALIGN THE LOCK
 HOLES AT THE ASSEMBLY.

** FOR THE SCREWS WITH A THREAD DIMENSION THAT IS LARGER THAN 0.164, AND WITH ONLY A SCREWDRIVER SLOT (NO EXTERNAL WRENCH SHAPE) 22 POUND-INCHES (2.486 NEWTON-METERS) MINIMUM IS PERMITTED.
Standard Nuts, Bolts, Screws, and Self-Locking Nuts on a Stud
Figure 202

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 70-23-00
 ALL  ú
 ú  N01  Page 204
 ú  Jun 18/99 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
K28948
S 912-033-N00
 (2)  Thin nuts, nuts with slots, and bolts that are not solid
 (a)  
The torque limits in the Figure 202 apply to the thin nuts and nuts with slots.

 (b)  
The height of the nut must be larger than 75 percent of the large diameter of the thread.

 (c)  
When the nut height is 40 to 75 percent of the large diameter, decrease the torque by 50 percent.

 (d)  
The height of nuts with slots is measured from the bottom of the nut to the bottom of the slots.

 (e)  
Values do not apply to bolts and screws that are not solid.


 S 912-034-N00
 (3)  Lockwire and cotter pins
 
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