AttachmentA2407.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:

Flap Track Assembly – INBD (WS 109.88)

2. PART NUMBER:

160D611632-6

3. NATIONAL STOCK NUMBER:

1560-01-522-2407

PREPARED BY:

RYAN MOORE

OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20210527

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 27

May 2021. 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 160D611632 FOR PART NUMBER 160D611632-18

(MIL-I-6866 AND MIL-I-25135), 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 LOCATED AS

DEFINED BY THE CAD MODEL AND DRAWING 160D611632. 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).

11. THE 160D611632-6 3D MODEL MUST BE USED IN CONJUNCTION WITH 160D611632 DRAWING TO ENSURE PROPER CONFIGURATION.

THE MODEL MAY NOT CONTAIN ALL OF THE REQUIRED SUBCOMPONENTS.

12. DOCUMENTS LE160Y6100 (LOFT DATA BOOK) AND LM160D611624 (FLAP TRACK LOFT MASTER: 1:1 FORMAT) WILL NOT BE

PROVIDED DUE TO THE CREATION / INCLUSION OF THE 3D MODELS.