Attachment 0005 - Critical Characteristics.pdf

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Solicitation for the Overhaul of the Midframe Assembly for the T700 Engine
Solicitation number
W58RGZ-24-R-0035
Issued by

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This document contains an attachment outlining critical characteristics for a midframe assembly and the related federal contract opportunity solicitation. The attachment specifies dimensional and hardness requirements for components of the midframe assembly per the identified drawings, including a minimum axial diameter of 2.050 inches and case thickness between 0.040 to 0.055 inches for specific parts. The solicitation seeks offers for the overhaul of the Midframe Assembly, NSN 2840-01-305-6946, in support of the T700 engine. The solicitation was issued by the Department of the Army Materiel Command Contracting Command at Redstone Arsenal. Offerors should refer to the attached solicitation for additional details on requirements and submission instructions.

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Other files

File Type Posted
Amendment 0003 to Solicitation W58RGZ-24-R-0035.pdf PDF
Amendment 0002 to Solicitation W58RGZ-24-R-0035.pdf PDF
Amendment 0001 to Solicitation W58RGZ-24-R-0035.pdf PDF
Exhibit B - CDRL A002 Report of Shipping Discrepancy.pdf PDF
Attachment 0003 - QE-STD-1.pdf PDF
Exhibit A - CDRL A001 GP Inventory Report.pdf PDF
Attachment 0006 - TDPL.pdf PDF
Attachment 0004 - QE-STD-2.pdf PDF
Exhibit C - CDRL A003 MO Process Plan.pdf PDF
Attachment 0007 - Contractor Overhaul TAV-C Requirements.docx DOCX document
Solicitation W58RGZ-24-R-0035.pdf PDF
Attachment 0002 - Document Summary List (DSL).docx DOCX document
Attachment 0001 - MO Packaging Requirements.pdf PDF
Attachment 0008 - TAV-C Portal User Access Procedures.pdf PDF
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05/31/2023

6055T46G08 2840 01 305 - 6946

Y

Y

Y

Y

N

N

N

N

N

N

N

N

Dimension per Drawing 6055T46, Note 36, Axial Diameter BP minimum 2.050 inches from Surface AA for subcomponent item 3, 'No. 4 Bearing Housing Sumpa' PN 6039T38G08 (Zone C13, Sht. 1) as shown on subcomponent drawing 6039T38 (Zone C16, Sht. 1) Dimension per Drawing 6055T46, Note 36, Case Thickness 0.040-0.055 inches in area 'AF' for subcomponent item 2, 'Outer Midframe Casea' PN 6055T44G05 (Zone J12, Sht. 1) as shown on subcomponent drawing 6055T44 (Zone F22, Sht. 1) Hardness per Drawing 6055T46, Note 36, Rc 38-47 for subcomponent item 2, 'Outer Midframe Casea' PN 6055T44G05 (Zone J12, Sht. 1) as shown on subcomponent drawing 6055T44, Note 6.D.

Hardness per Drawing 6055T46, Note 5A, Rc 38-47 for subcomponent item 18 'Scavenge Tubea' PN 6055T46P08 (Zone B17, Sht.2).

99207 General Electric Company

CAGE

Critical CharacteristicsM ID

Part No NSN

Midframe AssyNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved M&O Sources

01/01/1994CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

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