EDR.pdf
PDF 93 KB Posted
- Attached to
- F-16 Manual Trim Panel Federal contract opportunity
- Solicitation number
- SPRHA4-26-Q-0253
- Issued by
- Defense Logistics Agency Aviation
About this file
This is an Engineering Data Requirements document (Hill AFB Form 462) for the manufacture of a Panel, Manual Trim component for the F-16 aircraft. The part number is 16C0650-803 with National Stock Number 6615-01-450-2802WF. The document was prepared by Eric Simpkinson of the 416 SCMS/GUEAA office on September 30, 2020, and serves as Attachment "A" to a contract solicitation. Military specifications and standards will not be furnished in the bid set.
The document establishes critical manufacturing requirements and material specifications. Contractors must use SAE AMS-QQ-A-250/4 material in lieu of QQ-A-250/4 and comply with MIL-STD-130 marking standards for human-readable (minimum 1/8-inch characters) and machine-readable 2D matrix codes (minimum 1/4-inch square, constructed as two codes) containing CAGE, part number, and serial number. No substitutions of listed sources or materials are permitted without prior cognizant engineering activity approval, and deviations from control drawing specifications are not authorized without advance approval. The document emphasizes a critical Air Force airworthiness requirement: all electronic equipment suppliers must continue using leaded solder formulations, as no lead-free solder replacement has yet matched the reliability and performance standards of leaded solders. Contractors must notify the Air Force on a no-cost basis if any lead-free components are used and must provide written certification of compliance if no lead-free components exist in the end-item. Contractors must also use IPC-1066 standards for marking lead-free materials and include the program engineer's evaluation of any lead-free parts regarding reliability, performance, and system compatibility. The Engineering Support Activity (ESA) is the point of contact for these requirements.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| SPRHA426Q0253.pdf | ||
| EDL.pdf | ||
| CDRLCPP.pdf | ||
| MQR.pdf | ||
| SOW.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:
PANEL, MANUAL TRIM F-16
2. PART NUMBER:
16C0650-803
3. NATIONAL STOCK NUMBER:
6615-01-450-2802WF
PREPARED BY:
ERIC SIMPKINSON
OFFICE SYMBOL:
416 SCMS/GUEAA
DATE:
20200930
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.
A. Minimum 1/8th inch on Human readable to include:
1. CAGE (17V)
2. P/N (1P)
3. Serial Number (1S)
B. Minimum 1/4 inch square on Machine Readable 2D Matrix – construct 2 – to include
1. CAGE (17V)
2. P/N (1P)
3. Serial Number (1S)
C. Label shall contain all data on existing label, if existing label is to be replaced.
D. Same Label Material shall be used as specified in drawing for existing label.
E. MIL-STD-130, ANSI/AIM BCII, ISO 15434, ISO 15415, and ISO 15418
8. USE MATERIAL PER SAE AMS-QQ-A-250/4 IN LIEU OF QQ-A-250/4.
9. 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 AND 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, COMPATIBILITY, 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.
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:
PANEL, MANUAL TRIM F-16
2. PART NUMBER:
16C0650-803
3. NATIONAL STOCK NUMBER:
6615-01-450-2802WF
PREPARED BY:
ERIC SIMPKINSON
OFFICE SYMBOL:
416 SCMS/GUEAA
DATE:
20200930
HILL AFB FORM 462 Page 2 of 2
10. 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 CONDITIONS EXIST:
1. COMMERCIAL OFF-THE-SHELF (COTS) OR ANY OTHER 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.
11. 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 SHALL 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 ITS' RELIABILITY, PERFORMANCE AND COMPATIBILITY FOR THE SYSTEM.
12. POC FOR THIS MATTER IS THE ENGINEERING SUPPORT ACTIVITY (ESA).
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