462ENGINEERINGDATAREQUIREMENTS4391.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:

WING TIP ASSY, RH, WING TIP & FAIRING CHAFF / FLARE, OUTER WING PANEL

2. PART NUMBER:

162D612550-1002

3. NATIONAL STOCK NUMBER:

1560-01-591-4391

PREPARED BY:

RYAN MOORE

OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20201126

HILL AFB FORM 462 Page 1 of 3

Distribution Statement: D: Distribution authorized to Department of Defense and U.S. DOD contractors only, for administrative and operational use. Date of determination is 4 December 2020. Refer other requests for this document to OO-ALC/416 SCMS/GUEAB, Hill AFB, UT, 84056.

Destruction Notice: For classified document, follow the procedures in DOD 5220.22M, Industrial Security Manual, Section 11-19 or DOD 5200.1 R, Information Security Program Regulation, Chapter IX. For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document.

WARNING - the documents listed on this document and the associated Engineering Data List (EDL) contain technical data whose export is restrictive by the Arms Export Control act (Title 22, U.S.C., 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.

4. THE SUPPLIED TECHNICAL DATA PACKAGE (162D612550-1002) MAY BE PROVIDED IN SIEMENS NX FORMAT AS A

MODEL BASED DEFINITION (MBD) AND SHALL SERVE AS THE ENGINEERING BASELINE FOR THIS ACQUISITION. THE GEOMETRY OF THE BASELINE TECHNICAL DATA PACKAGE (TDP) IS DEFINED BY THREE DIMENSIONAL (3-D) MODELS IN THE ABOVE DESCRIBED FORMAT. THIS INCLUDES 3-D MODELS AND OTHER DATA MASTERED IN A PRODUCT LIFECYCLE MANAGEMENT (PLM) SYSTEM. THE PLM DATA FIELDS NEEDED FOR MANUFACTURING ARE ALSO OUTPUT IN A HUMAN READABLE FORMAT THAT THE GOVERNMENT WILL PROVIDE AS A “PART REPORT.” 3-D MODELS MAY BE AVAILABLE IN ALTERNATE FORMATS (E.G. IGES/STEP), INQUIRES FOR ALTERNATE FILE FORMATS

SHALL BE REQUESTED FROM ENGINEERING THROUGH THE GOVERNMENT CONTRACTING OFFICIAL.

5. THE PRIME CONTRACTOR MAY USE A TRANSLATOR TO CONVERT BETWEEN NX AND IGES/STEP IN SUPPORT OF THEIR SUBCONTRACTORS; HOWEVER, THE PRIME CONTRACTOR SHALL DEMONSTRATE THE TRANSLATION

PROCESS TO THE GOVERNMENT AND OBTAIN GOVERNMENT AUTHORIZATION TO PROCEED BEFORE

MANUFACTURING TO THE CONVERTED 3-D SOLID MODEL. FOR A TRANSLATOR TO BE AUTHORIZED, THE CONTRACTOR MUST SHOW THAT THE DELIVERED 3-D SOLID MODEL CONTAINS ALL OF THE NECESSARY INFORMATION REQUIRED TO ACCURATELY PRODUCE PARTS AS DEFINED IN THE ORIGINAL NX MODEL. THE 3-D MODELS SHALL DEFINE PRODUCT CONFIGURATION PER ASME Y14.41 MODEL ONLY (AKA “MODEL BASED

DEFINITION”) IN LIEU OF DRAWINGS.

6. THE PRIME CONTRACTOR IS RESPONSIBLE TO COMPLETELY RESEARCH THESE MODELS, 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 TDP SHALL BE SUBMITTED TO THE PROPER A-10 ENGINEERING ORGANIZATION FOR COORDINATION

AND APPROVAL.

7. WHEN MILITARY DOCUMENTS LISTED IN THE ENGINEERING TDP 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.

8. 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)

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9. ITEM UNIQUE IDENTIFICATION (IUID) SHALL BE APPLIED TO THE ASSEMBLY PER THE REQUIREMENTS IN THE TECHNICAL DATA PACKAGE, WITH APPROPRIATE MODIFICATIONS IF NECESSARY. SPECIFIC DATA ELEMENTS (I.E.

MANUFACTURER’S CAGE CODE AND LETTER DESIGNATION [REFERENCE DOCUMENT 162S900706]) OF THE NAMEPLATE SHALL BE MODIFIED TO IDENTIFY THE PRIME CONTRACTOR. IF THIS INFORMATION IS NOT DEFINED BY DOCUMENT 162S900706, THE CONTRACTOR SHALL PRESENT THE PROPOSED CHANGE TO GOVERNMENT ENGINEERING VIA ENGINEERING CHANGE REQUEST/ORDER OR A REQUEST FOR VARIANCE (RFV). THE CONTRACTOR SHALL NOT IMPLEMENT MODIFICATIONS TO THE NAMEPLATE INFORMATION UNTIL THE PROPOSED

MODIFICATIONS HAVE BEEN APPROVED BY THE APPROPRIATE A-10 ENGINEERING AUTHORITY.

10. 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.

11. THE PRIME CONTRACTOR SHALL USE SERIAL NUMBERS TO CONTROL AND PROVIDE TRACEABILITY OF THE WING

TIP ASSY (162D612550-1002). THE PRIME CONTRACTOR SHALL PRESENT THE SERIALIZATION METHOD TO THE GOVERNMENT IN THE FORM OF A REVISION TO THE SERIAL NUMBER CONTROL PLAN (162S900706), OR RFV, FOR APPROVAL PRIOR TO USE. THIS PLAN WILL DEFINE THE SERIALIZATION ASSIGNMENT, CONTROL, AND DOCUMENTATION. ADDITIONALLY, THE PRIME CONTRACTOR SHALL REVIEW THE EXISTING NAMEPLATES DELIVERED UNDER THE TDP FOR CONTINUED USE UNDER THIS CONTRACT. IF CHANGES ARE REQUIRED, THE PRIME CONTRACTOR SHALL PRESENT THE NECESSARY DESIGN CHANGES TO THE APPLICABLE ENGINEERING AUTHORITY.

18. IF THE PRIME CONTRACTOR IDENTIFIES ANY PROPRIETARY REQUIREMENTS (E.G. PROCESS SPECIFICATIONS, MATERIAL SPECIFICATIONS, ETC.) WITHIN THE TDP WHERE A NON-PROPRIETARY ALTERNATIVE DOES NOT EXIST, THEY SHALL DOCUMENT THE SPECIFIC CASE. THEY THEN SHALL PROVIDE A SUITABLE NON-PROPRIETARY ALTERNATIVE SOLUTION (E.G. REDESIGN, ALTERNATE NON-PROPRIETARY PROCESS SPECIFICATION, ETC.) WITH A TECHNICAL JUSTIFICATION TO INCLUDE ANALYSIS OR TEST DATA, IF APPLICABLE, TO THE GOVERNMENT IN THE

FORM OF A TDP CHANGE REQUEST.

SOME SPECIFICATIONS REFERENCED IN THE TECHNICAL DATA PACKAGE (TDP) MAY NOT BE PROVIDED DUE TO PROPRIETARY AND/OR INTELLECTUAL PROPERTY RIGHTS. EXAMPLES OF THIS TYPE OF DATA CAN OFTEN BE

IDENTIFIED AS DOCUMENTS WITH FORMATS SIMILAR TO:

• BACXXXX,

• BMS X-XXX,

OR

• P.S. XXXX.

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19. IF ERRORS, INCONSISTENCIES, OR PROBLEMS WITHIN THE TDP ARE ENCOUNTERED, THE PRIME CONTRACTOR SHALL DOCUMENT THE SPECIFIC CASE AND PROVIDE A SOLUTION TO THE GOVERNMENT IN THE FORM OF TDP

CHANGE REQUEST.

20. TOOLING DEVELOPMENT: TOOLING IS REQUIRED FOR THE MANUFACTURE OF THIS PART. THE CONTRACTOR MAY

NEED TO DEVELOP/MANUFACTURE ITS OWN TOOLING AS REQUIRED. PRIOR TO TOOL DEVELOPMENT, THE CONTRACTOR SHALL ADVISE THE GOVERNMENT IN WRITING OF THEIR INTENT TO DEVELOP NEW TOOLING. THE CONTRACTOR SHALL NOT PROCEED TO DEVELOP NEW TOOLING WITHOUT THE EXPRESS CONSENT OF THE

GOVERNMENT PROCURING AGENCY.

21. THE PRIME CONTRACTOR SHOULD WORK THROUGH THE GOVERNMENT PROCURING AGENCY TO CONTACT THE ENGINEERING ORGANIZATION LISTED IN THE OFFICE SYMBOL BLOCK LOCATED AT THE BOTTOM OF THIS DOCUMENT IN ORDER TO MAKE SURE ANY NEWLY DEVELOPED TOOLING AND FIXTURES WILL PRODUCE AN ACCEPTABLE PART THAT WILL FIT ON THE AIRCRAFT. THIS WILL MAKE SURE CHANGES AND CHECKS ARE DONE

EARLY TO PREVENT FAILURE OF THE FIRST ARTICLE.