Engineering Data Requirements.pdf
PDF 63 KB Posted
- Attached to
- Grip Control Federal contract opportunity
- Solicitation number
- SPRHA4-25-Q-0358
- Issued by
- Defense Logistics Agency Aviation
About this file
This Engineering Data Requirements document provides manufacturing instructions for a Grip Assembly, Pilots Controller for the F-16 aircraft. The document specifies part number 16C1090-1 with National Stock Number 1680-01-263-0648WF, and includes critical technical requirements for production, with particular emphasis on soldering and component specifications.
Key technical instructions include mandatory compliance with specific military standards (MIL-STD-130, MIL-STD-2000), detailed requirements for lead-free solder usage, and explicit guidance on marking, identification, and manufacturing processes. The document highlights significant concerns about lead-free components in military electronic products, noting potential flight safety and national security implications. Manufacturers must follow precise specifications for sources/materials, obtain prior approval for any deviations, and provide written certification of compliance with the detailed technical requirements.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| SPRHA425Q0358 CUI SSI.pdf | ||
| Packaging Statement of Work.pdf | ||
| Manufacturing Qualification Requirements.pdf | ||
| Unmarked Eng Data 2022.pdf | ||
| Engineering Data List.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:
GRIP ASSEMBLY, PILOTS CONTROLLER F-16
2. PART NUMBER:
16C1090-1
3. NATIONAL STOCK NUMBER:
1680-01-263-0648WF
PREPARED BY:
DAYLE LAFOY
OFFICE SYMBOL:
416 SCMS / GUEAA
DATE:
20230404
HILL AFB FORM 462 Page 1 of 2
4. THE FOLLOWING SPECIFICATIONS/STANDARDS, ETC., WILL BE USED IN LIEU OF THE DATA INDICATED. THE
SUPERSEDED DATA WILL NOT BE FURNISHED UNLESS SO INDICATED.
5. THE SOURCES/MATERIALS IF LISTED ON THE STANDARDS, SPECIFICATION AND DRAWINGS ARE THE ONLY
SOURCES/MATERIALS FOR THOSE ITEMS. SUBSTITUTIONS SHALL HAVE PRIOR APPROVAL BY THE COGNIZANT
ENGINEERING ACTIVITY.
6. DEVIATIONS FROM SPECIFICATIONS IDENTIFIED IN CONTROL DRAWINGS ARE NOT AUTHORIZED WITHOUT PRIOR
APPROVAL BY THE COGNIZANT ENGINEERING ACTIVITY.
7. MARKING PER MIL-STD-130 IN LIEU OF FPS-3008.
7.1 APPLY ITEM UNIQUE IDENTIFICATION (IUID) PER 16C1090-1, EO 12C3014-H.
8. THIS IS AN AIRCRAFT PART. USE THE APPROPRIATE PORTION OF MIL-STD-2000 THAT APPLIES TO AIRCRAFT
SOLDERING FOR ALL SOLDERING REQUIREMENTS. *NOTE: J-STD-001 MAY BE USED IN LIEU OF MIL-STD-2000, IS
SPECIFICATION MEETS OR EXCEEDS MIL-STD-2000.
8.1 EFFECTIVE 9 MAY 2005 THE DEPARTMENT OF THE AIR FORCE ISSUED AN AIR WORTHINESS ADVISORY (M-05-01)
REGARDING THE USE OF LEAD-FREE SOLDER IN ELECTRICAL AN ELECTRONIC MILITARY PRODUCTS. TO DATE, NO
LEAD-FREE SOLDER FORMULATION HAS MATCHED THE RELIABILITY AND PERFORMANCE QUALITIES OF THE
STANDARD LEADED SOLDERS. THEREFORE, UNTIL SUCH TIME AS A SUITABLE, RELIABLE, LEAD-FREE SOLDER
REPLACEMENT IS IDENTIFIED, ALL ELECTRONIC EQUIPMENT SUPPLIERS SHALL CONTINUE TO PROVIDE THE
DEPARTMENT OF THE AIR FORCE WITH ITEMS WHICH MEET ALL PERFORMANCE, COMPATABILITY AND RELIABILITY
STANDARDS PREVIOUSLY ESTABLISHED WITH LEADED SOLDERS. FAILURE TO DO SO, COULD ADVERSELY IMPACT THE
PERFORMANCE AND RELIABILITY OF WEAPON SYSTEMS AFFECTING NATIONAL SECURITY.
8.2 THE USE OF LEAD-FREE SOLDER OR LEAD-FREE PLATED COMPONENTS IN MILITARY ELECTRONIC PRODUCTS IS
CONSIDERED A FLIGHT SAFETY AND NATIONAL SECURITY CONCERN. FOR THIS REASON THE US AIR FORCE WANTS TO
BE NOTIFIED WHEN LEAD-FREE COMPONENTS AND MANUFACTURING PROCESSES HAVE BEEN IMPLEMENTED, AS PART
OF SATISFACTORY COMPLIANCE WITH THE REQUIREMENTS OF THIS CONTRACT, THE US AIR FORCE REQUIRES
NOTIFICATION ON A NO-COST BASIS WHEN ANY OF THE FOLLOWING CONDOTIONS EXIST:
1. COMMERCIAL OFF-THE-SHELF (COTS) OR ANY OTHE ELECTRICAL COMPONENTS THAT CONTAIN LEAD-FREE SOLDER
OR LEAD-FREE PLATED COMPONENTS ARE USED IN THE END-ITEM.
2. ANY LEAD-FREE COMPONENT OR PART USED TO MANUFACTURE THE END ITEM THAT IS NOT IDENTIFIED WITH A
SEPARATE PART NUMBER OR DESIGNATION.
8.3 IF NO LEAD-FREE, LEAD-FREE PLATED COTS OR ANY OTHER LEAD-FREE ELECTRICAL OR ELECTRONICS
COMPONENTS EXIST IN THE MANUFACTURED END-ITEM, THE CONTRACTOR SHAL PROVIDE WRITTEN CERTIFICATION
OF COMPLIANCE AS A DELIVERABLE WITH THE CONTRACT.
1. USE INDUSTRY STANDARD IPC-1066, “MARKING, SYMBOLS AND LABELS FOR IDENTIFICATION OF LEAD-FREE AND
OTHER REPORTABLE MATERIALS IN LEAD-FREE ASSEMBLIES, COMPONENTS AND DEVICES.”
2. INCLUDE THE PROGRAM ENGINEER’S EVALUATION OF THE PURCHASING/REPAIR ITEM FOR ANY “LEAD-FREE”
MILITARY PART(S) IN REFERENCE TO IT’S RELIABILITY, PERFORMANCE AND COMPATABILITY FOR THE SYSTEM.
9. 16PR106 IS NOT FURNISHED, BRAID PER 16PR8817 IF APPLICABLE.
10. USE 16PR8817 IN CONJUNTION WITH 16PR145 FOR THE MANUFACTURING IF THIS ITEM.
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:
GRIP ASSEMBLY, PILOTS CONTROLLER F-16
2. PART NUMBER:
16C1090-1
3. NATIONAL STOCK NUMBER:
1680-01-263-0648WF
PREPARED BY:
DAYLE LAFOY
OFFICE SYMBOL:
416 SCMS / GUEAA
DATE:
20230404
HILL AFB FORM 462 Page 2 of 2
11. 16PR145, REVISION “G”, PAGE 9, PARAGRAPGH 3.2.3.2, REFERING TO THE USE OF WHITE TUBING, DOES NOT APPLY TO
THE MANUFACTURE OF THIS ITEM.
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