Engineering Data Requirements.pdf
PDF 49 KB Posted
- Attached to
- A-10 Aircraft Access Door Federal contract opportunity
- Solicitation number
- FA8212-22-Q-0003
About this file
This document provides engineering data requirements for the manufacture of an A-10 aircraft access door. The contractor must follow specifications for heat treatment of aluminum, cutting processes, and item unique identification marking. Manufacturing must adhere to standards including SAE AMS 2770 and MIL-STD-130. The contractor shall submit deviations, substitutions of cancelled standards, and cutting process requests to the A-10 engineering organization for approval. Hinges must be manufactured and packaged separately from the door assembly.
The related federal contract opportunity is a solicitation from the Department of the Air Force Materiel Command Air Force Sustainment Center to provide replenishment spares for A-10 aircraft access doors. Quoters are requested to contact the point of contact upon requesting the data package through sam.gov for approval to participate. The government reserves the right not to make an award.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Packaging SoW.pdf | ||
| CDRLs.pdf | ||
| Transportation Data for Solicitations.pdf | ||
| Form 260 First Article Requirements.pdf | ||
| IUID Checklist.pdf | ||
| Item Description.pdf | ||
| Packaging Requirements.pdf | ||
| Special Packaging Instructions.pdf | ||
| 00_FA8212-22-Q-0003.pdf | ||
| Engineering Data List.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 The superseded data will not be furnished unless so indicated.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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