EDR1029.pdf
PDF 62 KB Posted
- Attached to
- F-16 Flap, Wing Dive Brake
- Solicitation number
- SPRHA426R0305
- Issued by
-
Defense Logistics Agency Aviation
About this file
This document is an Engineering Data Requirements specification (HILL AFB Form 462) for the manufacture of a Flap, Wing-Leading Edge Maneuver Assembly, Part Number 16W1022-812 (National Stock Number 1560-01282-1029WF). The specification was prepared by Tim Lucas at Hill Air Force Base on December 2, 2022.
The document establishes manufacturing requirements and guidelines including the substitution of MIL-STD-130 for FPS-3008 marking standards and the use of IGES loft data (16W329-8, 16W391-8, 16W1330-10) in lieu of unavailable drawing 16PR006. Master tooling is required to manufacture this part and must be obtained directly from Lockheed Martin Co., as the government does not have access to it. All deviations from specifications in control drawings require prior approval from OO-ALC Engineering, and material substitutions require approval from the OO-ALC cognizant engineering activity. The specification mandates Item Unique Identifier (IUID) compliance with both human-readable and machine-readable 2D matrix markings using MIL-STD-130, ANSI/AIM BCII, ISO 15434, ISO 15415, and ISO 15418 standards. Human-readable markings must include minimum 1/8 inch lettering of CAGE code (17V), Part Number (1P), and Serial Number (IS), while machine-readable matrix must be minimum 1/4 inch square and include the same data elements. Parts must be delivered in primed condition without finished paint coating, and drawing 16PR100 is not required for manufacture.
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Other files
| File | Type | Posted |
|---|---|---|
| SPI.pdf | ||
| CDRLFATR.pdf | ||
| EDL1028.pdf | ||
| EDR1028.pdf | ||
| SOW.pdf | ||
| SPRHA426R0305.pdf | ||
| EDL1029.pdf | ||
| MQR.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:
FLAP, WING-LEADING EDGE MANEUVER, ASSY
2. PART NUMBER:
16W1022-812
3. NATIONAL STOCK NUMBER:
1560-01282-1029WF
PREPARED BY:
Tim Lucas
OFFICE SYMBOL:
416SCMS/GUEAA
DATE:
02 Dec 2022
HILL AFB FORM 462 Page 1 of 1
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SUPERSEDED DATA WILL NOT BE FURNISHED UNLESS SO INDICATED.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 SOURCE/MATERIAL IF LISTED ON THE STANDARDS, SPECIFICATION AND DRAWINGS ARE THE ONLY
SOURCE/MATERIALS FOR THOSE ITEMS. SUBSTITUTIONS SHALL HAVE PRIOR APPROVAL BY OO-ALC COGNIZANT
ENGINEERING ACTIVITY.
6. DEVIATIONS FROM SPECIFICATIONS IDENTIFIED IN CONTROL DRAWINGS ARE NOT AUTHORIZED WITHOUT PRIOR
APPROVAL BY OO-ALC ENGINEERING.
7. USE MIL-STD-130 IN LIEU OF FPS-3008.
8. 16PR006 IS NOT FURNISHED. USE IGES LOFT DATA 16W329-8, 16W391-8, 16W1330-10 FOR THE MANUFACTURE OF
16W1022-812.
9. MASTER TOOLING IS REQUIRED TO MAKE THIS PART. THE GOVERNMENT DOES NOT HAVE ACCESS TO THIS MASTER
TOOLING. ANY MANUFACTURERS WHO WISHES TO OBTAIN THIS TOOLING MUST CONTACT LOCKHEED MARTIN CO.
10. IUID (ITEM UNIQUE IDENTIFIER) REQUIREMENTS AND EXPECTATIONS WHICH THE CONTRACTOR MUST ENSURE ARE
COMPLIED WITH.
A. CONTRACTORS DRAWINGS SHALL BE CHANGED OR SUPPLEMENTED BY CONTRACTOR FOR IUID COMPLIANCE.
B. LABEL SHALL CONTAIN ALL DATA ON EXISTING LABEL, (IF EXISTING LABEL IS TO BE REPLACED), ONLY DELETE
EXISTING LABEL WITH GOVERNMENT ENGINEERING PERMISSION.
C. USE HRI (HUMAN READABLE) AND MACHINE READABLE MATRIX. (USAF NOT EQUIPED TO READ BARCODE).
D. IUID MATRIX NEEDS TO BE HIGHLY VISIBLE, IN A LOCATION EASILY ACCESSIBLE.
E. IUID MARKING MUST BE PERMANENT.
F. MIL-STD-130, ANSI/AIM BCII, ISO 15434, ISO 15415, AND ISO 15418
I. IUID MARKING SPECIFICATIONS.
1. MINIMUM 1/8 INCH LETTERING ON HUMAN READABLE TO INCLUDE:
A. CAGE (17V)
B. P/N (1P)
C. SERIAL NUMBER (IS)
2. MINIMUM 1/4 INCH SQUARE ON MACHINE READABLE 2D MATRIX -CONSTRUCT 2 - TO INCLUDE
A. CAGE (17V)
B. P/N (1P)
C. SERIAL NUMBER (IS)
11. 16PR100 IS NOT REQUIRED FOR MANUFACTURE AND WILL NOT BE FURNISHED.
12. DELIVER PARTS IN THE PRIMED CONDITION. DO NOT APPLY FINISHED PAINT COATING.
File details come from the government source that posted it. Updated .