FA481926Q0029 - Q and A.pdf

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Attached to
Lifting Equipment Load Testing
Solicitation number
FA481926Q0029
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About this file

This is a Questions and Answers document for federal contract opportunity FA481926Q0029. The document addresses a single inquiry regarding sling specifications for aircraft handling equipment. The F-16 sling is specified as 11 feet in length and constructed of wire rope. The F-22 sling consists of three legs with varying lengths: two legs measuring 15 feet 6 inches each and one leg measuring 13 feet, constructed of synthetic sling material. The document does not provide pictures or additional specifications beyond these dimensions and material compositions.

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Other files

File Type Posted
US-MOD-50-UI-compressed.pdf_safe (1).pdf PDF
F-22 Sling.pdf PDF
F-16 Sling.pdf PDF
Stament of Work.pdf PDF
ASME B30.20 Below-theHook Lifting Devices (006).pdf PDF
Wage Determination.pdf PDF
Stament of Work.pdf PDF
ASME B30.26 (Shackles).pdf PDF
Solicitation - FA481926Q0029.pdf PDF
ASME B30.9 SLINGS.pdf PDF

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FA481926Q0029

Questions and Answers

1. What is the length of the F-22 and F-16 slings? Are they synthetic slings or wire rope?

Do you have any pictures?

F-16 Sling is 11 feet, Wire rope.

F-22 Sling is 2 legs 15 feet 6 inch, One leg 13 feet, synthetic sling.

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