09_Engineering Data Requirements.pdf

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, AIRCRAFT

2. PART NUMBER:

160D215009-37

3. NATIONAL STOCK NUMBER:

1560-01-094-4532 FJ

PREPARED BY:

Jaime Meredith

SIGNATURE: OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20190627

HILL AFB FORM 462 Page 1 of 2

1. WARNING - The documents listed on this 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.

2. Weldbond Process (Per A-F502) used in manufacture is hereby cancelled and replaced by Adhesive Bonding (Per S-F501).

3. For P/N 160D215009-71, disregard Note 26.

4. For P/N 160D215009-73, disregard Note 26 and heat treat to T6 Condition per Note 6.

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. 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.

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

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, AIRCRAFT

2. PART NUMBER:

160D215009-37

3. NATIONAL STOCK NUMBER:

1560-01-094-4532 FJ

PREPARED BY:

Jaime Meredith

SIGNATURE: OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20190627

HILL AFB FORM 462 Page 2 of 2

10. Omit Mating/Mounting Holes: omit mating/mounting hole(s) in part. The part will be matched/back drilled upon installation.

11. Excess Perimeter Material: Contractor will provide 1/4 inch excess trim around entire perimeter of part. Excess trim will be removed upon installation.

12. 3D model for P/N 160D215009-51 STRL PLATE incorrectly dimensions the 12 equally spaced holes.

Manufacture using the 4.75” DIA per DWG 160D215009.

13. 3D model & DWG 160D215009 REV N both incorrectly locate P/N 160D950293-17 LUG.

Orientation of Lug shall be rotated 180° so that the .281” DIA HOLE shown in DWG 160D950293 REV C aligns concentrically with .281” DIA HOLE in P/N 160D215009-51 STRL PLATE as shown in DWG 160D215009 REV N Zone 3B2.