NSNs Tech Characteristics Amd 2 Appdx B.pdf

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Multiple Award Indefinite Delivery/Indefinite Quantity (IDIQ) in support of the Value Engineering and Sourcing Support Tool (VESST) on behalf of the Defense Logistics Agency (DLA), Aviation. The VESST program will support aviation related requirements.
Solicitation number
9Q0HDLA38001
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NSNs Tech Characteristics Amd 2 Appdx B

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9Q0HDLA38001 RFP QandA from VESST Vendors Amd 2.docx DOCX document
NSN 1560-014068974 Photo Amd 2 Appdx B.pdf PDF
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Technical Characteristics of

NSNs 1560-014068974 & 2995-009688429

1560-014068974:

For most manufactured components of this item, the material is Aluminum Alloy 356.0-T6 per SAE-AMS- 4260, -4284, -4217, or ASTM B26. Alternate material is 6061-T6, T651, or T6511 per SAE-AMS-QQ- 200/8, SAE-AMS-QQ-225/8, or SAE-AMS-QQ-250/11. The steel component that engages the square drive of the mating assembly is manufactured using 4340 steel per SAE-AMS- 6409, -6414, -6415, -6484 or ASTM A322.

Aluminum parts are to be anodized per MIL-A-8625, Type II, Class I. Exterior surfaces are then to be primed with MIL-PRF-23377, Type I. A topcoat is not required.

The steel component is to be heat treated per SAE-AMS-H-6875 to 25-30 HRC. It is also to be cadmium plated per SAE-AMS-QQ-P-416, Type II, Class I.

This item is used on the SH-60.

2995-009688429:

This item is constructed from 0.032” thick Aluminum Alloy 2024-T3 per ASTM B209. The tubing is ½” OD, 0.035” wall thickness, 2024-T3 aluminum per ASTM B210 or B221.

The assembly is to be Conversion Coated per MIL-DTL-5541 and primed with MIL-PRF-23377, Type I. It is also to be top coated with MIL-PRF-85285, color 27875, 27880, 27885, or 27886 semi-gloss white per

FED-STD-595.

This item is used on the E-2C.

File details come from the government source that posted it. Updated .