462 ATTACHMENT A 1163.pdf

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Attached to
A-10 ACCESS DOOR WING PANEL (15 DAY SYNOPSIS) Federal contract opportunity
Solicitation number
FD20202200174
Issued by
Department of the Air Force Materiel Command Air Force Sustainment Center

About this file

This document provides engineering data requirements and instructions for the manufacture of an A-10 aircraft outer wing panel access door. Key details include the part numbers, national stock numbers, and specifications required for production. The contractor must comply with all technical data and standards in the engineering package and obtain approval for any deviations. Processes like laser cutting require pre-approval, and non-heat cutting methods are currently prohibited. Riveting must follow standard G-F601. Hole drilling instructions are modified from the technical data. Five shim part numbers are also defined with requirements for surface finish, hole omission, and individual marking and bagging.

The related federal contract opportunity is a pre-solicitation notice for a forthcoming solicitation from the Air Force Sustainment Center. The requirement is for 53 units of one national stock number and 46 units of another for a total anticipated contract value of $395,582.32. First article units are due 90 days after award with production batches due 295 and 1290 days after award respectively. First articles may be waived for incumbent contractors. This will be a 100% small business set-aside.

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Other files for this federal contract opportunity

Other files attached to A-10 ACCESS DOOR WING PANEL (15 DAY SYNOPSIS), newest first.
File Type Posted
158 PACKAGING REQUIREMENTS.pdf PDF
1423-1 CDRL.pdf PDF
EDL 9314.pdf PDF
ITEM DESCRIPTION 1163.pdf PDF
2169 SPECIAL PACKAGING INSTRUCTIONS 1163.pdf PDF
461 ATTACHMENT A 9314.pdf PDF
PACKAGING STATEMENT OF WORK.pdf PDF
260 FIRST ARTICLE 1163.pdf PDF
260 FIRST ARTICLE 9314.pdf PDF
ITEM DESCRIPTION 9314.pdf PDF
EDL 1163.pdf PDF
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Text version

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:

IB DOOR ASSEMBLY, OUTER WING PANEL, LEADING EDGE (RH)

2. PART NUMBER:

160D612502-6

3. NATIONAL STOCK NUMBER:

1560-01-032-1163FJ

PREPARED BY:

RYAN MOORE

OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20180504

HILL AFB FORM 462 Page 1 of 2

Distribution Statement: D: Distribution authorized to Department of Defense and U.S. DOD contractors only, for administrative and operational use. Date of determination is 10 February 2017. 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.

1. 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 PROPER A-10 ENGINEERING ORGANIZATION FOR COORDINATION AND APPROVAL.

2. WHEN MILITARY DOCUMENTS LISTED IN THE ENGINEERING TDP (TECHNICAL DATA PACKAGE) 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.

3. 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)

4. "IUID" (ITEM UNIQUE IDENTIFIER) IS REQUIRED IAW MIL-STD-130 FOR THE ASSEMBLY. 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.

5. 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.

6. RIVETS SHALL BE INSTALLED IAW G-F601.

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:

IB DOOR ASSEMBLY, OUTER WING PANEL, LEADING EDGE (RH)

2. PART NUMBER:

160D612502-6

3. NATIONAL STOCK NUMBER:

1560-01-032-1163FJ

PREPARED BY:

RYAN MOORE

OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20180504

HILL AFB FORM 462 Page 2 of 2

7. NOTE 35 OF PL160D612502 SHALL BE DISREGARDED AND REPLACED WITH THE FOLLOWING REQUIREMENT:

7.1. ADD APPROXIMATELY 0.125” EXCESS TRIM TO THE PERIMETER OF THE PART AT THE 160D612502-12 (SKIN) PART

LEVEL. EXCESS MATERIAL WILL BE TRIMMED AT INSTALLATION.

7.2. DO NOT DRILL PILOT HOLES OR MOUNTING HOLES AROUND THE PERIMETER OF PART. HOLES WILL BE

DRILLED AT INSTALLATION. OMITTED HOLES INCLUDE (REFERENCE 3D MODEL AND DRAWING):

7.2.1. (33) EACH 0.381” DIAMETER COUNTERSINK DIAMETER, 0.199” DIAMETER THRU, 100 DEGREE COUNTERSINK

ANGLE HOLES,

7.2.2. (2) EACH 0.381” DIAMETER COUNTERSINK DIAMETER, 0.193” DIAMETER THRU, 100 DEGREE COUNTERSINK

ANGLE HOLES,

7.2.3. (2) EACH 0.250 - 0.254” DIAMETER THRU HOLES.

8. SHIMS 160D612502-27, 160D612502-29, 160D612502-31, 160D612502-33, AND 160D612502-51 SHALL BE SUPPLIED:

8.1. FINISHED IAW DRAWING REQUIREMENTS (Z-R901, CODE DA),

8.2. WITHOUT HOLES; HOLES WILL BE DRILLED TO MATCH SKIN / STRUCTURE UPON INSTALLATION,

8.3. MARKED IAW DRAWING REQUIREMENTS (Z-R701, CODE RS / TG WHERE APPLICABLE), ALL SHIMS SHALL BE INDIVIDUALLY MARKED AND BAGGED WITH THE BAG(S) TEMPORARILY AFFIXED TO THE INSIDE OF THE

160D612502-6 ASSEMBLY.

8.4. SHIMS SHALL NOT BE INSTALLED / BONDED TO THE ADJACENT SKIN / STRUCTURE.

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