• RIGGING-LIFTING 0146 RIGGING-LIFTING 0146
    HVG RIGGING-LIFTING 0146

    HVG RIGGING-LIFTING 0146: Aircraft Steel Wire Rope 6*19

    Aircraft steel wire rope is mainly used to control the aircraft rudder and aileron, engines, landing gear, compass and so on. It is also required a high corrosion resistance to stand dew and polution. Besides, they can serve in many circumstances. And Special specification can be made according to customers requirement.

    Product Details:

    • 1. Item: Aircraft steel wire rope 6*19
    • 2. Construction: 6*19
    • 3. Type: steel wire rope
    • 4. Finish: Galvanized or ungalvanized
    • 5. Material: Steel
    • 6. Usage: Pulling, lifting and transportion

    Safety Notice:

    • 1. In operation, the wire rope should be in steady speed
    • 2. Never overload, and never shock load a wire rope
    • 3. Wire rope should be inspected regularly, including abrasion of wire rope, condition of broken wire and metal parts
    • 4. It is important to clean and replace lubricant to the wire rope periodically.

    Sketch of the aircraft steel wire rope 6*19

    Technical specification:

    • Specification:

    Diameter

    Nominal Tensile Strength of Wire

    Minimum Breaking Load of Fiber Core Rope

    Min.Breaking Load of Steel Core Rope

    Approx Weight of Steel Core

    Approx Weight of Fiber Core

    Rope

    Wire

    3

    0.2

    2062

    6.3

    7.3

    4.2

    3.8

    3.3

    0.22

    1770

    6.5

    7.59

    5.74

    4.5

    3.6

    0.24

    1770

    7.8

    9.1

    6

    5.4

    4.2

    0.28

    1770

    10.6

    12.3

    8.2

    7.4

    4.8

    0.31

    1770

    1.9

    16

    10.71

    9

    5.1

    0.34

    1770

    15.6

    18.1

    12.1

    10.9

    6

    0.4

    1670

    19

    23.7

    16.7

    15.1

    6.3

    0.42

    1670

    22.2

    26.1

    18.41

    16.65

    7.5

    0.5

    1670

    32.9

    37.1

    26

    23.59

    8.25

    0.55

    1670

    38.4

    44.9

    32

    28.55

    9

    0.6

    1670

    45.7

    53.4

    37.6

    33.98

    9.75

    0.65

    1670

    50.3

    62.6

    44.1

    39.88