Model Contract Attachment 1 Salient Characteristics FA930125Q0004 20241202.pdf

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Attached to
T-38 Orbital Riveter Federal contract opportunity
Solicitation number
FA9301-25-Q-0004
Issued by
Department of the Air Force Materiel Command Test Center

About this file

This is a salient characteristics document outlining technical specifications for an Orbital Riveting Machine ("Spin Riveter") requested by the 412th Maintenance Group at Edwards Air Force Base, California. The document specifies requirements for a Taumel T-501 bench top model or equivalent to be installed in Building 1600 Room 512 (Aircraft Structural Repair Shop).

The required specifications include a maximum heading capacity of 0.550" diameter with 1.5" stroke length, US-3 control panel compatible with 208-230/460V-3-60 Hz power, orbital head with 0.350" diameter standard form tool for creating double-flush shop heads on T-38 aircraft brake assembly rivets, dual hand safety controls with proximity touch pads, foot activation device with safety guard, and an air filter/regulator/lubricator unit. The machine will be used specifically for working with solid shank, mild steel rivets for T-38 aircraft brake assemblies.

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Model Contract FA930125Q0004 20241210.pdf PDF
Combined_Synopsis _ Solicitation FA930125Q0004 20241210.pdf PDF

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Text version

Salient Characteristics FA9301-25-Q-0004 page 1 of 1

DEPARTMENT OF THE AIR FORCE

HEADQUARTERS 412 TH TEST WING

(AFMC) EDWARDS AIR FORCE BASE

CALIFORNIA

MEMORANDUM FOR AFMC AFTC/PZIOB

FROM: 412 MXS/MXMFS

SUBJECT: Bldg. 1600 Rm 512 (Aircraft Structural Repair Shop) Orbital Riveter cost estimate

Background: The 412 MXG is requesting the addition of an Orbital Riveting Machine (“Spin Riveter”) in the 412 MXS Structures Shop, Bldg.1600 Rm 512. The requested machine is the Taumel T-501 bench top model with added options, or its equivalent. Characteristics are as follows:

• Orbital Headforming Machine, bench top model, max. heading capacity: 0.550" dia. (no minimum), machine stroke length 1.5"

• Control panel US-3 for 208-230/460V-3-60 Hz, low voltage controller.

• Orbital Head with Standard Form Tool, diameter 0.350” to create double-flush shop heads on solid shank, mild steel rivets for T-38 aircraft brake assemblies.

• Dual Hand Safety Controls for no repeat/no tie-down operation activated with proximity touch pads

• Foot Activating Device with safety guard, cable and plug

• Air Filter/Regulator/Lubricator Unit

If there are any other questions or concerns, please feel free to contact me, Christopher Ball, DSN 527-4437, christopher.ball@us.af.mil.

Digitally signed by

BALL.CHRISTOPH BALL.CHRISTOPHER.S.116820 9114

ER.S.1168209114 Date: 2024.12.02 08:50:02 -08'00'

Christopher S. Ball, WS-14, DAF 412MXS Aircraft Structures Section Chief mailto:christopher.ball@us.af.mil

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