461ATTACHMENTA9314.pdf
PDF 24 KB Posted
- Attached to
- A-10 ACCESS DOOR WING PANEL Federal contract opportunity
- Solicitation number
- FA821222R0174
About this file
This document provides engineering data requirements for the manufacture of an IB door assembly outer wing panel leading edge for the A-10 aircraft. Key details include:
The contractor will be responsible for researching manuals, specifications and standards to fully understand requirements for manufacturing component parts and assemblies. All deviations from the engineering drawings must be approved by the A-10 engineering organization. When military standards are cancelled, approved industry equivalents must be used and approved by the A-10 engineering organization. Item unique identifiers are required per MIL-STD-130 for assemblies over $5,000 or identified as fatigue critical. Manufacturing processes involving heat at or above the melting point or high pressure fluids require prior approval. Rivets must be installed per G-F601. Note 35 on the drawings is replaced with requirements to provide excess trim and omit perimeter holes, which will be drilled upon installation. Shims must be supplied finished per drawings without holes and individually marked and bagged for installation.
The related federal contract opportunity is a full small business set-aside solicitation from the Air Force Sustainment Center for A-10 access door leading edge wing panel replenishment spares.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| POST AWARD SYNOPSIS.pdf | ||
| FA821222R0174.pdf | ||
| 260FIRSTARTICLE1163.pdf | ||
| 260FIRSTARTICLE9314.pdf | ||
| 158PACKAGINGREQUIREMENTS.pdf | ||
| 462ATTACHMENTA1163.pdf | ||
| ITEMDESCRIPTION1163.pdf | ||
| EDL9314.pdf | ||
| EDL1163.pdf | ||
| 14231CDRL.pdf | ||
| 2169SPECIALPACKAGINGINSTRUCTIONS1163.pdf | ||
| ITEMDESCRIPTION9314.pdf | ||
| PACKAGINGSTATEMENTOFWORK.pdf |
Show all 13
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Text version
REV: 03 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 (LH)
2. PART NUMBER:
160D612502-5
3. NATIONAL STOCK NUMBER:
1560-01-043-9314FJ
PREPARED BY:
RYAN MOORE
OFFICE SYMBOL:
416 SCMS/GUEAB
DATE:
20170220
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: 03 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 (LH)
2. PART NUMBER:
160D612502-5
3. NATIONAL STOCK NUMBER:
1560-01-043-9314FJ
PREPARED BY:
RYAN MOORE
OFFICE SYMBOL:
416 SCMS/GUEAB
DATE:
20170220
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 160D612502-11 (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
160D612502-5 ASSEMBLY.
8.4. SHIMS SHALL NOT BE INSTALLED / BONDED TO THE ADJACENT SKIN / STRUCTURE.
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