Engineering Data Requirements.docx

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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:

XXXXXXXXXXXXXXXX

2. PART NUMBER:

3. NATIONAL STOCK NUMBER:

1234-12-123-1234FG

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 THE SUPERSEDED DATA WILL NOT BE FURNISHED UNLESS SO INDICATED.

(ATTACHMENT “A”)

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

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

TRIM TAB ASSEMBLY - DECELERON

2. PART NUMBER:

162D712140-1002

3. NATIONAL STOCK NUMBER:

1560-01-624-9367FJ

Distribution Statement: D: Distribution authorized to Department of Defense and U.S. DOD contractors only, for administrative and operational use. Date of determination is 17 March 2016. Refer other requests for this document to OO-ALC/508 ACSS/SU, 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 (162D712140-1002) WILL 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.”

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)

9. ITEM UNIQUE IDENTIFICATION (IUID) SHALL BE APPLIED TO THE ASSEMBLY, PER MIL-STD-130N. SUPPLIERS WILL INCORPORATE THE 2-D IUID MARKING ON THEIR INDIVIDUAL ID PLATES. THE HEIGHT OF EACH ALPHANUMERIC CHARACTER IN THE HUMAN READABLE FORMAT SHALL BE A MAXIMUM OF 0.125 INCH. MARKINGS FOR BOTH THE MACHINE READABLE FORMAT AND HUMAN READABLE FORMAT SHALL BE TO SAE AS9132 WITH AN ALLOWABLE DEPTH OF 0.0005 TO 0.0030 INCH. THE LOCATION OF THE IUID MARKING IS NOT REQUIRED ON THE ENGINEERING DRAWINGS I.E. AN ENGINEERING CHANGE ORDER TO UPDATE THE DRAWINGS IS NOT REQUIRED. THE MARKINGS SHALL ONLY BE PLACED IN AREAS THAT WILL NOT BE DETRIMENTAL TO THE PART. INTRUSIVE MARKINGS SHALL NOT BE USED TO MARK FATIGUE AND FRACTURE CRITICAL (F&FC) OR CRITICAL SAFETY ITEM (CSI) PARTS. THE CONTRACTOR SHALL IDENTIFY THESE LOCATIONS AND GAIN THE APPROPRIATE A-10 ENGINEERING AUTHORITY APPROVAL PRIOR TO IMPLEMENTING.

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 TO THE TRIM TAB (162D712140-1002) ASSEMBLIES. THE PRIME CONTRACTOR SHALL PRESENT THE SERIALIZATION METHOD TO THE GOVERNMENT IN THE FORM OF A REVISION TO THE SERIAL NUMBER CONTROL PLAN, 162S900706, 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.

12. FOR PART NUMBERS 162D712140-1002 AND 162D712140-2052 (REFERENCE PART REPORT 162D712140-1001 AND 162D712140-2051 RESPECTIVELY), PART REPORT NOTE GDT-27 AND/OR GDT-02 (IF PRESENT) SHALL NOT BE APPLIED. THESE PARTS/ASSEMBLIES SHALL MEET TDP REQUIREMENTS IN AN UN-RESTRAINED AND UN-WEIGHTED CONDITION.

13. WHEN FABRICATING PARTS IAW S-F502 PER PART REPORT REQUIREMENTS:

A. OPTION 2 OF PARAGRAPH 4.2.2.2 SHALL NOT BE USED.

B. ALL REFERENCES TO BMS 8-79 SHALL BE DISREGARDED.

C. FM300M FILM ADHESIVE SHALL NOT BE USED.

D. WHEN CORE SPLICING OR CURING OF B-M101 FOAMING ADHESIVE IS ACCOMPLISHED OTHER THAN AS PART OF AN ASSEMBLY BOND, THE CURE CYCLE TIME LIMITS SHALL BE 60 MINUTES MINIMUM TIME AT TEMPERATURE AND 120 MINUTES MAXIMUM TIME AT TEMPERATURE.

14. THE REQUIREMENTS OF 160D900004 SHALL APPLY AFTER PART/ASSEMBLY INSTALLATION AND APPROPRIATE RIGGING PROCEDURES ARE PERFORMED. THOUGH PART NUMBERS REFERENCED IN THE DRAWING REFER TO LEGACY PARTS (160D…), ALL REQUIREMENTS SHALL BE APPLICABLE FOR EQUIVALENT PARTS PROCURED (162D…).

15. FOR INFORMATION ONLY: MULTIPLE REFERENCES TO T.O. 1A-10C-520 EXIST IN THE PROVIDED TECHNICAL DATA PACKAGE. THIS T.O. DEFINES THE REPLACEMENT OF THE THIN-SKINNED WING ASSEMBLY WITH THE ENHANCED WING ASSEMBLY. T.O. 1A-10C-520 IS NOT REQUIRED FOR THE MANUFACTURE OF PART NUMBER 162D712140-1002 OR ITS SUBCOMPONENTS. THE PARTS PROCURED UNDER THIS CONTRACT WILL BE USED ON “AIRCRAFT MODIFIED BY T.O. 1A-10C-520”.

16. THE TRIM TAB ASSEMBLY IS AN INTERCHANGEABLE ITEM IN ACCORDANCE WITH MIL-I-8500 AS DEFINED BY THE TECH DATA PACKAGE. A FIRST ARTICLE DEMONSTRATION IS REQUIRED TO PROVE INTERCHANGEABILITY IN ACCORDANCE WITH MIL-I-8500, INCLUDING BACKWARD INTERCHANGEABILITY WITH ENHANCED WING ASSEMBLY (EWA) COMPONENTS/ASSEMBLIES, AND SHALL BE COMPLETED PRIOR TO FIRST ARTICLE ACCEPTANCE. THE CONTRACTOR SHALL BE RESPONSIBLE TO DEFINE THE METHOD OF CONTROLLING INDIVIDUAL INTERCHANGEABLE AND REPLACEABLE (I&R) FEATURES, THROUGH THE USE OF TOOLING AND/OR OTHER MEANS.

17. IF THE PRIME CONTRACTOR IDENTIFIES ANY PROPRIETARY REQUIREMENTS (E.G. PROCESS SPECIFICATIONS, MATERIAL SPECIFICATIONS, ETC.) WITHIN THE TDP WHERE A NON-PROPRIETARY ALTERNATIVE DOESN’T 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.

THE FOLLOWING SPECIFICATIONS WILL NOT BE PROVIDED WITH THE TECHNICAL DATA PACKAGE DUE TO PROPRIETARY RIGHTS (LIST MAY NOT BE ALL INCLUSIVE):

18. 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.

19. TOOLING DEVELOPMENT: TOOLING IS REQUIRED FOR THE MANUFACTURE OF THIS PART. THE CONTRACTOR WILL 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. THE TOOLING LISTED BELOW IS NOT CURRENTLY AVAILABLE TO CONTRACTORS FOR MANUFACTURING BUT TOOLING DRAWINGS/3-D MODELS MAY BE AVAILABLE FOR USE AS POSSIBLE TOOLING DESIGN CONCEPTS. ANY TOOLING DRAWINGS/3-D MODELS PROVIDED ARE TO BE USED FOR REFERENCE ONLY (REFERENCE ENGINEERING DATA LIST (EDL) FOR TOOLING INFORMATION). THE ACCURACY OF THESE TOOLING DRAWINGS/MODELS HAS NOT BEEN VERIFIED; IF THE CONTRACTOR CHOOSES TO USES THIS DATA IT IS AT THEIR OWN DISCRETION. THE GOVERNMENT IS NOT LIABLE FOR ANY INACCURACIES PRESENT IN THIS TECHNICAL DATA. THE CONTRACTOR MAY REQUEST TO INSPECT SIMILAR EXISTING LEGACY TOOLING. ARRANGEMENTS FOR TOOL INSPECTION (OF THE EXISTING GOVERNMENT LEGACY TOOLING, IF REQUIRED) SHALL BE MADE BY CONTACTING THE APPROPRIATE CONTRACTING PERSONNEL AND THE ENGINEERING AUTHORITY LISTED AT THE BOTTOM OF THIS DOCUMENT THROUGH THE APPROPRIATE CONTRACTING PERSONNEL.

PARTIAL TOOL LISTING IS AS FOLLOWS:

20. 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.

21. IF POSSIBLE, THE FORGINGS SHALL BE PROCURED FROM SOURCES USING THE ORIGINAL CERTIFIED FORGING PROCEDURES AND DIES/TOOLING.

A. PRIOR TO CONTRACT AWARD, THE DETAILED PART BIDDER SHALL PROVIDE CERTIFICATION FROM THE FORGING SOURCE TO THE GOVERNMENT THAT THE CERTIFIED DIES AND PROCEDURES ARE AVAILABLE AND THE FORGING SOURCE HAS AN AGREEMENT WITH THE DETAILED PART BIDDER TO PROVIDE FORGINGS FOR THEIR USE IN THE EVENT THEY ARE THE SUCCESSFUL BIDDER.

B. PRIOR TO PRODUCTION, FORGING LOT QUALIFICATION SHALL BE ACCOMPLISHED AS SPECIFIED ON THE FORGING DRAWING. THE DETAILED PART CONTRACTOR SHALL ASSURE THAT THIS HAS BEEN ACCOMPLISHED BY THE FORGING SOURCE AND SHALL SUBMIT CERTIFIED DOCUMENTATION OF ACCOMPLISHMENT TO THE GOVERNMENT.

C. PRIOR TO CONTRACT AWARD, THE CONTRACTOR SHALL ADVISE THE GOVERNMENT IN WRITING OF THEIR INTENT TO PROCURE NEW FORGING DIES AND THE PROPOSED FORGING SOURCE. THE CONTRACTOR SHALL NOT PROCEED TO OBTAIN NEW DIES WITHOUT THE EXPRESS CONSENT OF THE GOVERNMENT PROCURING AGENCY. THE GOVERNMENT SHALL HAVE UNLIMITED USE OF THE DIES DEVELOPED UNDER THIS CONTRACT. THE CONTRACTOR SHALL INFORM THE FORGING HOUSE IN WRITING AT THE SAME TIME THE ORDER FOR THE DIES IS PLACED THAT THE GOVERNMENT HAS UNLIMITED USE RIGHTS OF THE DIES AND FORWARD A COPY OF THIS LETTER TO THE GOVERNMENT CONTRACTING OFFICER.

22. TRIM TAB ASSEMBLY 160D712140-1002 SHALL BE BALANCED IN ACCORDANCE WITH THE REQUIREMENTS AS DEFINED BY THE ASSOCIATED PART REPORT. A BALANCE DATA SHEET SHALL BE PROVIDED BY THE PRIME CONTRACTOR FOR EACH ASSEMBLY PRODUCED. THE BALANCE PROCEDURE DEFINED IN T.O. 1A-10C-3-1 IDENTIFIES BALANCE TOOLING PART NUMBER 162D712100-1001SMT AS A SUITABLE ALTERNATE TO PART NUMBER 160D712100-001SMT. 162D712100-1001SMT DOES NOT EXIST; 162D712100-1001_BAF MAY BE USED AS A SUBSTITUTE.

PREPARED BY:

RICHARD TILTON

OFFICE SYMBOL:

GBMAF

DATE:

20080411

PREPARED BY:

JAMES SHULL

OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20220104

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