462ATTACHMENTA6480FJ.pdf

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Attached to
A-10 Inboard Flap Track Assembly Federal contract opportunity
Solicitation number
FA821221Q0803
Issued by
Department of the Air Force Materiel Command Air Force Sustainment Center

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File Type Posted
SECTIONC6480FJ.pdf PDF
IUID1116FJ.pdf PDF
ENGINEERINGDATALIST1116FJ.pdf PDF
PACKAGINGREQUIRMENTS.pdf PDF
SECTIONC1116FJ.pdf PDF
ITEMDESCRIPTION6480FJ.pdf PDF
260FIRSTARTICLE6480FJ.pdf PDF
ENGINEERINGDATALIST6480FJ.pdf PDF
SPECIALPACKAGINGINSTRUCTION1116FJ.pdf PDF
STATEMENTOFWORK.pdf PDF
IUID6480FJ.pdf PDF
FA821221Q0803.pdf PDF
SPECIALPACKAGINGINSTRUCTION6480FJ.pdf PDF
ITEMDESCRIPTION1116FJ.pdf PDF
260FIRSTARTICLE1116FJ.pdf PDF
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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:

Flap Track Assembly – INBD (B.L. 37.68)

2. PART NUMBER:

160D611631-3

3. NATIONAL STOCK NUMBER:

1560-01-059-6480

PREPARED BY:

RYAN MOORE

OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20201206

HILL AFB FORM 462 Page 1 of 1

Distribution Statement: D: Distribution authorized to Department of Defense and U.S. DOD contractors only, for administrative and operational use. Date of determination is 7 July 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 CONTRACTOR IS RESPONSIBLE TO COMPLETELY RESEARCH THESE MANUALS, SPECIFICATIONS, AND STANDARDS AND

FULLY UNDERSTAND THE REQUIREMENTS NECESSARY FOR THE MANUFACTURE OF COMPONENT PARTS AND ASSEMBLIES. ALL DEVIATIONS, MINOR AND MAJOR, FROM THE ENGINEERING DATA PACKAGE SHALL BE SUBMITTED TO 416 SCMS/GUEAB

STRUCTURES ENGINEERING FOR COORDINATION AND APPROVAL.

5. 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. THIS APPLIES TO THE ORIGINAL AIRCRAFT MANUFACTURER’S SPECIFICATIONS THAT ARE CITED IN THE DRAWING, AS WELL. 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). WHEN THERE IS NO LISTED REPLACEMENT THE CONTRACTOR SHALL REQUEST AND RECOMMEND A SUBSTITUTE DOCUMENT FROM 416 SCMS/GUEAB STRUCTURES

ENGINEERING THROUGH THE GOVERNMENT CONTRACTING OFFICIAL.

6. 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)

7. "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.

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. IN LIEU OF THE PENETRANT INSPECTION REQUIREMENTS DEFINED BY DRAWING 160D611631 FOR PART NUMBER 160D611631-13

(MIL-I-6866 AND MIL-I-8950), THE FOLLOWING REQUIREMENTS SHALL BE SUBSTITUTED: PRIOR TO SHOT PEENING, PENETRANT

INSPECT MACHINED PART PER ASTM E1417, TYPE I, SENSITIVITY LEVEL 3 (OR HIGHER).

10. THE LOCATION OF THE 5 EACH 0.2535” NOMINAL DIAMETER HOLES (GEAR RACK MOUNTING HOLES) SHALL BE AS DEFINED BY

THE CAD MODEL AND DRAWING 160D611631. THESE HOLES ARE SIZED AT THE MINIMUM DIAMETER IN THE MODEL BUT THE HOLE DIAMETER SIZE TOLERANCE SHALL BE 0.2525” TO 0.2545” (SAME SIZE REQUIREMENT AS DRAWING). THE POSITION

TOLERANCE ON SAID HOLES SHALL BE 0.003” (NOT DEFINED IN DRAWING/MODEL).

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