2155948_EI_AFLC_FORM2559.pdf

TECHNICAL DATA PACKAGE – ENGINEERING NOTES (ENs)

OF 4 PAGES

NATIONAL STOCK NUMBER

1680-01-482-4674FG

PART NUMBER

5-51393-6

DATE

January 26, 2017

AFLC FORM 2559 (COMPUTER GENERATED) PREVIOUS EDITION WILL BE USED

1. PART MARKING PER MIL-STD-130, METHOD PER THE DRAWING REQUIREMENTS AND BAC 5307.

MARKING MUST INCLUDE NATIONAL STOCK NUMBER, PART NUMBER, CURRENT DESIGN

AUTHORITY CODE (98748), ACTUAL MANUFACTURER'S CAGE CODE (-----), DATE OF MANUFACTURE, AND "FOR MILITARY USE ONLY". PARTS WILL NOT BE MARKED WITH THE ORIGINAL DESIGN

AUTHORITY (BOEING) CAGE CODE.

2. DELETE REFERENCE TO 2-5000 AND BAC 5005

3. SURFACE TEXTURE PER ASME B46.1 IN LIEU OF BACD 2097

4. DIMENSIONS AND TOLERANCES PER ASME Y14.5.

5. USE MIL-PRF-23827 AIRCRAFT AND INSTRUMENT GREASE IN LIEU OF BAC 5008, TYPE I.

6. USE AN3-6A AND AN3-7A BOLTS PER AIA/NAS NASM3.

7. USE MS21042-3 SELF-LOCKING NUTS PER AIA/NAS NASM21042 IN LIEU OF AN365-1032.

8. FINISH CODE F-12.46 DEFINED: ASSEMBLE WITH WET MIL-PRF-23377, TYPE I, CLASS C2 PRIMER ON

FAYING SURFACES.

9. USE SAE AMS-QQ-A-225 AND AMS-QQ-A-225/6 ALUMINUM ALLOY 2024-T4 RODS IN LIEU OF QQ-A- 268.

10. FINISH CODE F-2.20 DEFINED: ANODIZE ACCORDING TO MIL-A-8625, TYPE I OR IC (PREFERRED), CLASS 1.

11. HEAT TREAT STEEL PER SAE AMS-H-6875 AND SAE AMS 2759 IN LIEU OF MIL-H-6875 AND BAC 5601.

12. FINISH CODE F-1.10 DEFINED: APPLY NO FINISH, EXCEPT THAT TEMPORARY PROTECTION MAY BE

APPLIED FOR HANDLING, TRANSPORTATION AND STORAGE.

13. FINISH CODE F-1.20 DEFINED:

A. THREADED PARTS TO MEET THE REQUIREMENTS OF AMS-QQ-P-416, TYPE I, CLASS 2.

B. NON-THREADED PARTS TO MEET THE REQUIREMENTS OF AMS-QQ-P-416, TYPE II, CLASS 2

14. MAGNETIC PARTICLE INSPECT PER ASTM E1444 IN LIEU OF MIL-I-6868 WITH THE FOLLOWING

ADDITIONAL REQUIREMENT: THE INTENSITY OF VISIBLE LIGHT REFERRED TO IN PARAGRAPH 5.7.1

IS TO BE A MINIMUM OF 200FC. (ACCEPTANCE CRITERIA PER MIL-STD-1907).

15. PHOSPHATE COATING PER MIL-DTL-16232 IN LIEU OF MIL-C-12968.

16. USE 4340 STEEL BARS PER SAE 6415 IN LIEU OF MIL-S-5000.

17. USE 4340 STEEL TUBING PER SAE AMS 6415 IN LIEU OF AMS 6413.

18. USE FORGING STEEL PER SAE AMS-F-7190 IN LIEU OF MIL-F-7190.

OF 4 PAGES

NATIONAL STOCK NUMBER

1680-01-482-4674FG

PART NUMBER

5-51393-6

19. FINISH CODE F-1.60 DEFINED: CADMIUM PLATE ACCORDING TO SAE AMS-QQ-P-416, TYPE I OR III, CLASS 2, FOLLOWED BY A 3 TO 5 WEIGHT PERCENT CHROMIC ACID DIP ON EXTERIOR SURFACE OF HOLLOW, OPEN-END MEMBER. APPLY ONE COAT OF MIL-PRF-23377, TYPE I, CLASS C2 PRIMER

ON INTERIOR SURFACE ACCORDING TO MANUFACTURERS APPLICATION INSTRUCTIONS AND MIL-

DTL-18264.

20. USE 4140 STEEL BAR PER AMS 6349 OR AMS 6382 IN LIEU OF MIL-S-5626

21. USE 8740 STEEL BARS PER AMS 6322, AMS 6325 & AMS 6327 IN LIEU OF MIL-S-6049.

22. AMS 6253 CANCELED WITHOUT REPLACEMENT.

23. DELETED

24. FINISH CODE F-1.65 DEFINED: ZINC PLATE AND BAKE EXTERIOR SURFACE OF UNPLUGGED

TUBULAR AND HOLLOW PARTS ACCORDING TO ASTM B633, TYPE II, CLASS Fe/Zn 12. APPLY TWO

COATS OF MIL-PRF-23377, TYPE I, CLASS C2 PRIMER ACCORDING TO THE MANUFACTURERS

APPLICATION INSTRUCTIONS AND MIL-DTL-18264.

25. USE SAE 4130 OR 8630 STEEL TUBING PER SAE AMS-T-6736 IN LIEU OF MIL-T-6732 AND MIL-T-6736.

26. USE SAE 4130 STEEL SHEET PER SAE AMS 6350 IN LIEU OF AN-QQ-S-685.

27. USE SAE 30301 CRES SHEET PER SAE AMS 5517 IN LIEU OF MIL-S-5059.

28. SPOT AND SEAM WELD PER BAC 5977 CLASS B (OPTIONAL SAE AMS-W-6858 CLASS B) IN LIEU OF

BAC 5933 CLASS B.

OF 4 PAGES

NATIONAL STOCK NUMBER

1680-01-482-4674FG

PART NUMBER

5-51393-6

29. WHEN CHECKED BELOW OR LISTED IN THESE NOTES, DEFINITIONS APPLICABLE TO THIS PRODUCT

ARE OR HAVE:

(A) ENGINEERING CRITICAL IN APPLICATION: An item, which requires special manufacturing processes, controls, and testing of material or end items. Because of its use or application, failure to maintain the highest reliability of such an item could be catastrophic resulting in loss of life or serious injury, loss of a weapon system or extensive secondary damage, with direct impact on the capability to respond to a national emergency or to achieve wartime sustainability.

(B) CRITICAL CHARACTERISTICS: Characteristics which, when defective, are likely to result in hazardous or unsafe conditions for individuals using, maintaining or depending upon the product; or, are likely to prevent performance of the tactical function of a major end item such as an aircraft, missile, space vehicle, engine or a major part thereof. (Derived from MIL-STD-1916).

(C) MAJOR CHARACTERISTICS: Characteristics (other than critical or minor), which, when defective, are likely to result in failure or to reduce the usability of the product or a major end item for its intended purpose. (Derived from MIL-STD-1916).

(D) MINOR CHARACTERISTICS: All characteristics not designated as critical or major but for which full conformity is required

(E) COMPLEX: Items having quality characteristics not wholly visible (hidden characteristics), in the end product for which contractual conformance must be established progressively through precise measurements, tests or controls applied during purchasing, manufacturing, performance, assembly and functional operation either as an individual item or in conjunction with other items [FAR SUBPART 46.203(b)].

(F). COMMERCIAL: Described in commercial catalogs, drawings or industrial standards [FAR SUBPART 46.203(a), (1)].

THIS PRODUCT HAS BEEN DETERMINED TO BE OR CONTAINS (AS CHECKED BELOW):

_____ Engineering critical in application.

______ Critical characteristics.

____ Major characteristics.

__X___ Minor characteristics, all except critical and major.

______ Complex.

______ Available as a commercial product.

OF 4 PAGES

NATIONAL STOCK NUMBER

1680-01-482-4674FG

PART NUMBER

5-51393-6

When materials, processes or components are to be obtained from directed sources as indicated herein or in the specifications, alternate sources may only be utilized upon prior approval by the contracting officer of this procuring activity as a deviation.

Bidders shall notify this procuring activity at the time of quotation of any drawing, specification or standard which is of more current data revision than those shown on the data listing or in these engineering notes.

Determination of acceptability of the more currently dated data will be made by the responsible engineering office of this procuring activity.

Lower tier specifications listed in or referenced by first tier specifications may not be shown on the data lists or engineering notes accompanying this contract but are nonetheless required by this contract for compliance.

Exceptions would occur only when such lower tier requirements have been specifically waived or substitute specifications/requirements are designated herein.

Reports, process sheets, inspection methods sheets and all other documents required by specifications imposed by this contract for contractor compliance which were previously required to be submitted to a prime design contractor shall be held at that facility for review by government personnel.

When prime design source specifications require or provide for participation by that prime source quality, manufacturing, laboratory or engineering support services, these requirements or provisions do not apply when the contract was issued by this procuring activity. For these services or direction pertaining thereto, contact the cognizant government contract administration office or this procuring activity for assistance.

The contractor is responsible for assuring that all dimensions, conditions, tests and test results identified in these engineering notes, applicable drawings, specifications and contract quality requirements are met by themselves and their suppliers. This requirement applies to all characteristics whether those characteristics have been specifically designed as being critical, major or are those minor characteristics not specifically designated as such.

PROCESS DATA REQUIREMENTS (CHECK WHEN APPLICABLE)

Prior to beginning of manufacture, the contractor will notify the engineering office of this procuring activity of all manufacturing process and processing procedures intended for use in production of this product. Once these processes are established, no changes shall be made without prior approval of the engineering office of this procuring activity.

SERIALIZATION OF PARTS (CHECK WHEN APPLICABLE)

Serialization of each part/assembly (contract end item) is required.