Engineering_Instructions.pdf

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:

SKIN AIRCRAFT

2. PART NUMBER:

160D611502-8

3. NATIONAL STOCK NUMBER:

1560-01-124-4882FJ

PREPARED BY:

Cassidy Bond

OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20190408

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1. THE FOLLOWING SPECIFICATIONS/STANDARDS, ETC. WILL BE USED IN LIEU OF THE DATA INDICATED. THE

SUPERSEDED DATA WILL NOT BE FURNISHED UNLESS SO INDICATED.

2. 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 ENGINEERING ORGANIZATION LISTED IN THE OFFICE SYMBOL BLOCK LOCATED AT THE

BOTTOM OF THIS DOCUMENT FOR COORDINATION AND APPROVAL.

3. 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 THE ENGINEERING ORGANIZATION LISTED IN THE OFFICE SYMBOL

BLOCK OF THIS DOCUMENT BY CONTACTING THE GOVERNMENT CONTRACTING OFFICIAL.

4. 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)

5. "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 IDENTIFED AS FATIGUE CRITICAL REGARDLESS

OF THE ITEMS PER UNIT COST.

6. 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. ANY METHOD TO CUT, FORM OR FASTEN A COMPONENT OUTSIDE OF THE ACCEPTED LEGACY AEROSPACE MANUFACTURING PROCESSES WILL REQUIRE PRIOR A-10 SYSTEM

PROGRAM OFFICE APPROVAL.

7. EXCESS PERIMETER MATERIAL: CONTRACTOR WILL PROVIDE 1/4 INCH EXCESS TRIM MATERIAL AROUND ENTIRE

PERIMETER OF PART. EXCESS TRIM WILL BE REMOVED UPON INSTALLATION.

8. THE COMPLETE TECHNICAL DATA PACKAGE REQUIRES THE USE OF 3D CAD MODELS IN CONJUNCTION WITH DRAWING 160D611502. NOTE THAT THE 3D MODEL DOES NOT CONTAIN ALL THE REQUIRED DETAILS TO MANUFACTURE THE APPROPRIATE CONFIGURATION (E.G. THE 3D MODEL DOES NOT DEPICT PART NUMBER 160D631027-1 (SUPPORT BRACKET INSTALL) OR THE ADDITIONAL TRIM DEFINED BY DRAWING 160D611502, NOTE 28)