NOTE: 1. THE BREAKING STRENGTH MUST BE DIVIDED BY AN APPLICABLE FACTOR OF SAFETY THAT IS CONTROLLED BY THE AMOUNT OF SAFETY REQUIRED FOR THE WORK TO BE DONE
2. SEE THE MANUFACTURER’S CATALOGS FOR SPECIFIC LOAD RATINGS
3-20-4
MATERIALS AND ATTACHMENTS
Page 3-29 Jul 01/2005 D623N004
757
AIRPLANE RECOVERY DOCUMENT
Figure 3-13 SLING CONFIGURATIONS
3-20-4
MATERIALS AND ATTACHMENTS
Page 3-30 Jul 01/2005 D623N004
757
AIRPLANE RECOVERY DOCUMENT
Figure 3-14 WIRE ROPE CLIPS
DIAMETER OF ROPE NUMBER OF CLIPS SPACE BETWEEN CLIPS
INCHES MILLIMETERS INCHES CENTIMETERS
1/4 6 2 1 1/2 3.81
5/16 8 2 1 7/8 4.76
3/8 9 2 2 1/4 5.72
7/16 11 2 2 5/8 6.67
1/2 13 3 3 7.62
9/16 14 3 3 3/8 8.57
5/8 16 3 3 3/4 9.53
3/4 19 4 4 1/2 11.43
7/8 22 4 5 1/4 13.34
1 25 4 6 15.24
1 1/8 29 5 6 3/4 17.15
1 1/4 32 5 7 1/2 19.05
3-20-4
MATERIALS AND ATTACHMENTS
Page 3-31 Jul 01/2005 D623N004
ROPE DIA. A B C D E F G H WT. LB EACH
1/4 2.19 1.63 1.50 .88 .41 .28 .06 .23 0.075
5/16 2.50 1.88 1.81 1.06 .50 .34 .08 .28 0.14
3/8 2.88 2.13 2.13 1.13 .63 .41 .11 .34 0.25
7/16 3.25 2.38 2.38 1.25 .72 .47 .13 .38 0.36
1/2 3.63 2.75 2.75 1.50 .81 .53 .14 .41 0.51
9/16 3.63 2.75 2.69 1.50 .88 .59 .14 .41 0.51
5/8 4.25 3.25 3.13 1.75 .97 .66 .16 .50 0.75
3/4 5.00 3.75 3.81 2.00 1.22 .78 .22 .66 1.47
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址:757 Airplane Recovery Document 飛機恢復文件(66)