EDR.pdf

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SOLICITATION Acces Doors for A-10 Federal contract opportunity
Solicitation number
FA8212-19-R-0002
Issued by
Department of the Air Force Materiel Command Lifecycle Management Center Hill Air Force Base

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Updated EDR

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Other files attached to SOLICITATION Acces Doors for A-10, newest first.
File Type Posted
EDL.pdf PDF
FA821219R0002Amend01.pdf PDF
Attachment_2_PKG._Rqmt.pdf PDF
Attachment_1_CDRL.pdf PDF
Attachment_6_Itm_dsc._NSN_9211.pdf PDF
Attachment_4_SPI_ATTACH.pdf PDF
Attachment_3_Tranportation_data.pdf PDF
Attachment_5_SOW_pckg.pdf PDF
Attachment_7_.pdf PDF
FA821219R0002.pdf PDF
Attachment_6_EDL.pdf PDF
Attachment_8_SQSS.pdf PDF
Attahcment_7_EDR.doc DOC document
Attachment_5_Item_Description.pdf PDF
FA821219Q0007.pdf PDF
Attachment_3_Transportation.pdf PDF
Attachment_2_packaging.pdf PDF
Attachment_4_SOW_for_packaging.docx DOCX document
Attachment_1_CDRL.pdf PDF
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Text version

REV: ENGINEERING DATA REQUIREMENTS

(ATTACHMENT “A”)

NOTE: MILITARY SPECIFICATIONS / STANDARDS WILL NOT BE FURNISHED IN THE BID SET.

1. THE FOLLOWING INSTRUCTIONS ARE FURNISHED FOR THE MANUFACTURE OF:

DOOR ASSEMBLY, WING

2. PART NUMBER:

160D610103-140

3. NATIONAL STOCK NUMBER:

1560-01-213-9211FJ

PREPARED BY:

JAMES SHULL

OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20181220

HILL AFB FORM 462 Page 1 of 2

4. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

5. Contractor is responsible to completely research these manuals, specifications, and standards and fully understand the requirements necessary for manufacture of component parts and assemblies. All deviations, minor and major, from the engineering drawing package shall be submitted to the proper A-10 engineering organization for coordination and approval.

6. When military documents listed in the engineering drawing are cancelled they shall be replaced by the industry equivalent document specified on the military document's cancellation notice. The characteristics of type, grade, class, etc. specified in the cancelled military document shall be maintained or exceed those characteristics when applying the industry equivalent document(s). The contractor will coordinate with the proper A-10 engineering organization for authorization and approval of these substitutions prior to the manufacturing of this component.

When there is no listed replacement the contractor shall request and recommend a substitute document from the proper A-10 engineering organization by contacting the government contracting official.

7. Use of Northrop Grumman specification Z-R701 in conjunction with MIL-STD-130 is mandatory to ensure the proper marking of the parts. (Z-R701 has unlimited data rights in JEDMICS)

8. "IUID" (Item Unique Identifier) is required IAW MIL-STD-130. Specific instructions for marking methods, location, content and format shall be specified by the contractor and submitted to the government for approval prior to contract delivery. The contractor must demonstrate the marking does not adversely affect item integrity or performance and will remain readable and attached throughout the useable life of the item. IUID is required for items where the individual cost per unit is greater than $5,000 or if the item has been identified as fatigue critical regardless of the items per unit cost.

9. Use of any process or manufacturing technique which creates a net edge on a metallic part by relying on heat at or above the parts melting point to produce the cut is not generally authorized (i.e. laser cutting, electrical discharge machine (EDM), plasma cutting, etc.) Without prior A-10 system program office approval. Likewise, other non-heat generating cutting processes involving high pressure fluids and slurries (i.e., water jet) are also not currently approved for use in the production of A-10 parts. Only those processes controlled by A-10 approved program specifications and A-10 drawings are permitted to be used in the manufacture of A-10 parts and assemblies.

10. Heat Treatment of Wrought Aluminum: Utilize SAE AMS 2770 for heat treatment of wrought aluminum alloy in lieu of SAE AMS-H-6088.

11. Do not install any hinges. Manufacture hinges and package hinges and hinge fasteners separately. Hinges will be installed and located on aircraft upon installation of asset. Ensure hinges and hinge fasteners are included within the asset packaging.

REV: ENGINEERING DATA REQUIREMENTS

(ATTACHMENT “A”)

NOTE: MILITARY SPECIFICATIONS / STANDARDS WILL NOT BE FURNISHED IN THE BID SET.

1. THE FOLLOWING INSTRUCTIONS ARE FURNISHED FOR THE MANUFACTURE OF:

DOOR ASSEMBLY, WING

2. PART NUMBER:

160D610103-140

3. NATIONAL STOCK NUMBER:

1560-01-213-9211FJ

PREPARED BY:

JAMES SHULL

OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20181220

HILL AFB FORM 462 Page 2 of 2

12. WARNING - The documents listed In the Engineering Data List (EDL) contain technical data whose export is restrictive by the Arms Export Control Act (Title 22, USC, Section 2751, ET SEQ.), or the Export Administration Act of 1979, as amended, Title 50 U.S.C, Append 2401 ET SEQ. Violators of these export laws are subject to severe criminal penalties.

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