W50S8X26QA028_QMSN262004_CRHP_SF1442_Atch-05_Fig_B11-11_USAF_Tiedown_Profile.png

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W50S8X26QA028 HH-60G STATIC DISPLAY CONCRETE PAD
Solicitation number
W50S8X26QA028
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About this file

This is a technical specification document for Air Force Aircraft Tiedown Pavement Recess Design (B11-5.3.1). The specification establishes requirements for ground-level pavement construction to accommodate aircraft tiedown equipment and grounding cable attachment points.

The specification mandates that the top of static ground shall be set at pavement grade or no more than 6 millimeters (0.25 inch) below grade. A smooth, rounded-edge recess measuring 75 millimeters (3 inches) wide and not exceeding 150 millimeters (6 inches) in length must be provided in the pavement surrounding the tiedown eye for accessibility and grounding cable attachment. The design requires installation of dowel rods as indicated in aircraft technical orders or facility requirements documents, with specifications that tie dowels must be placed at 914 millimeters (3 feet) intervals from the tiedown center point when occurring 914 millimeters or farther from a single joint, or at 457 millimeters (1.5 feet) intervals when located 914 millimeters or less from adjacent joints with parallel orientation bars. The bar material shall be number 7 (0.875") non-deformed ASTM A615M steel with a minimum slab thickness of 254 millimeters (10 inches). For asphalt pavements, pier dimensions must accommodate anticipated uplift forces of 17,100 kilograms (37,700 pounds) minimum, requiring minimum pier dimensions of 1.83 meters by 1.83 meters (6 feet by 6 feet). Preexisting slabs require installation of 1-inch by 16-inch dowel rods centered at half slab depth on all four sides with specified anchor block dimensions.

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Other files

File Type Posted
Questions and Answers.pdf PDF
W50S8X26QA028_QMSN262004_CRHP_SF1442_Atch-02_WD_CA20260018_Mod-8.txt TXT text file
Solicitation Amendment W50S8X26QA0280002 SF 30.pdf PDF
Site Visit sign In sheet.pdf PDF
W50S8X26QA028_QMSN262004_CRHP_SF1442_Atch-06_Site_Map.pdf PDF
W50S8X26QA028_QMSN262004_CRHP_SF1442_Atch-04_Fig_B11-9_Grounding.png PNG image
W50S8X26QA028_QMSN262004_CRHP_SF1442_Atch-01_Weather_Data.pdf PDF
W50S8X26QA028_QMSN262004_CRHP_SF1442_Atch-07_Submittal_Register.pdf PDF
W50S8X26QA028_QMSN262004_CRHP_SF1442_Atch-03_Fig_B11-6_Mooring_Point.png PNG image
W50S8X26QA028_QMSN262004_CRHP_SF1442_Atch-02_WD_CA20260018_Mod-7.txt TXT text file
W50S8X26QA028_QMSN262004_CRHP_SF1442_Atch-06_Site_Map.pdf PDF
W50S8X26QA028_QMSN262004_CRHP_SF30_Amendment01.pdf PDF
W50S8X26QA028_QMSN262004_CRHP_SF1442_Confromed_Amendment.pdf PDF
W50S8X26QA026_CRHP_Pad_SF1442_Atch-01_Weather_Data.pdf PDF
W50S8X26QA026_CHRP_Pad_SF1442_Atch-03_Fig_B11-6_Mooring_Point.png PNG image
Solicitation - W50S8X26QA028.pdf PDF
W50S8X26QA026_CHRP_Pad_SF1442_Atch-02_WD_CA20260018_Mod-7.txt TXT text file
W50S8X26QA026_CHRP_Pad_SF1442_Atch-06_Site_Map.pdf PDF
W50S8X26QA026_CHRP_Pad_SF1442_Atch-04_Fig_B11-9_Grounding.png PNG image
W50S8X26QA026_CHRP_Pad_SF1442_Atch-05_Fig_B11-11_USAF_Tiedown_Profile.png PNG image
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