Part Number NAS1564D8-6 Tube Reducer Body

SKU: 4730004211351

NAS1564D86 Tube Reducer Body Datasheet

National aerospace standards part number NAS1564D8-6

Thread Direction:

Right-hand

Thread Size:

9/16-18

Tube Outside Diameter For Which Designed:

0.375 inches

Tube Outside Diameter For Which Designed:

0.500 inches

First End Seat Angle In Deg:

37.0

Second End Seat Angle In Deg:

37.0

End Application:

Hercules C-130 aircraft and F-18 aircraft

Flange Width:

Between 0.204 inches and 0.234 inches

Flange Outside Diameter:

Between 0.579 inches and 0.682 inches

Screw Thread Series Designator:

Unf

Working Pressure And Service Type:

3000.0 pounds per square inch any acceptable

Working Tempurature And Service Type:

Not rated

Material:

Aluminum alloy, QQ-A-225/4, alloy 2014, T6 or aluminum alloy, QQ-A-225/6, alloy 2024, T6 or aluminum alloy, QQ-A-225/6, alloy 2024, T851

Style Designator:

Reducer body

Surface Treatment:

Anodized, MIL-A-8625, type 2

Specification Data:

80205-NAS1564 professional/industrial association standard

Manufacturer Cage:

80205

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