DLA MIL-DTL-85069 D-2012 SLEEVES AND GROMMETS FASTENER [Superseded DLA MIL-S-85069 1 A CANC NOTICE 5 DLA MIL-S-85069 1 A VALID NOTICE 4 DLA MIL-DTL-85069 2 B CANC NOTICE 1 DLA MIL-.pdf

1、Comments, suggestions, or questions on this document should be addressed to DLA Aviation VEB, 8000 Jefferson Davis Highway, Richmond, VA 23297-5616, or e-mailed to STDZNMGTdla.mil. Since contact information can change, you may want to verify the currency of this address information using the ASSIST

2、database at https:/assist.daps.dla.mil/. AMSC N/A FSC 5365 INCH-POUND MIL-DTL-85069D 10 February 2012 SUPERSEDING See 6.3 DETAIL SPECIFICATION SLEEVES AND GROMMETS, FASTENER This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This

3、specification covers the requirements for fastener sleeves and grommets for use in over-sized fastener holes in aerospace structures. 1.2 Classification. Sleeves and grommets are classified as shown in tables III through V. 1.3 Part or identification number (PIN). The PIN to be used for sleeves and

4、grommets acquired to this specification is created as follows (see 6.2 and tables III through V). Part numbers from the legacy specification sheets have been retained to support continued procurement. M 85069 / XX - XX Example PIN: M85069/10-12 Legacy specification sheet dash number (see tables III

5、through V) Legacy specification sheet slash number (see tables III through V) Specification number Military designator Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-85069D 2 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this

6、section are specified in sections 3 and 4 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users ar

7、e cautioned that they must meet all specified requirements of the documents cited in sections 3 and 4 of this specification, whether or not they are listed. 2.2 Non-government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specifie

8、d, the issues of these documents are those cited in the solicitation or contract. ASME ASME B46.1 - Surface Texture (Surface Roughness, Waviness, and Lay) (Copies of this document are available online at http:/www.asme.org/ or from ASME, P.O. Box 2300, Fairfield, NJ 07007-2300.) AMERICAN SOCIETY FOR

9、 QUALITY (ASQ) ASQ Z1.4 - Sampling Procedures and Tables for Inspection by Attributes (Copies of this document are available online from http:/www.asq.org/ or from the American Society for Quality, 600 North Plankinton Avenue, Milwaukee, WI 53203.) SAE INTERNATIONAL SAE AMS2700 - Passivation of Corr

10、osion Resistant Steels SAE AMS 5525 - Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V 1800 F (982 C) Solution Heat Treated SAE AS87132 - Lubricant, Cetyl Alcohol, 1-Hexadecanol, Application to Fasteners (Copies of these documents are availa

11、ble online at http:/www.sae.org or from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001.) 2.3 Order of precedence. Unless otherwise noted herein or in the contract, in the event of a conflict between the text of this document and the references cited herein, the text of this doc

12、ument takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-85069D 3 3. REQUIREMENTS 3.1 Conformance insp

13、ection. When specified (see 6.2), samples shall be subjected to conformance inspection in accordance with 4.2. 3.2 Design and construction. 3.2.1 Construction. The fastener sleeve or grommet shall be drawn from sheet or strip stock to form a one-piece tubular section and head. The thickness of the t

14、ubular wall and head shall be uniform. Sleeve tubular sections shall be grooved in 0.062-inch increments to aid in adjusting the sleeve to the desired length. 3.2.2 Material. Sleeve and grommet material shall conform to UNS S66286 corrosion and heat-resistant steel in accordance with SAE AMS 5525 (s

15、ee 4.3.3). 3.2.3 Head structure and grain flow. When visually examined, the sleeve or grommet may show axial grain flow lines in the tubular section typical of a drawn sleeve or grommet. The flow lines shall be continuous at the fillet radius. 3.2.4 Protective coatings. The fastener sleeves and grom

16、mets shall be passivated in accordance with SAE AMS2700. 3.2.5 Lubrication. The fastener sleeves and grommets shall be lubricated with cetyl alcohol or left bare. Cetyl alcohol, if used, shall conform to SAE AS87132. Packaging shall be marked as shown to indicate use or non-use, as indicated: L - lu

17、bricated with cetyl alcohol B - no lubrication 3.2.6 Surface texture. Surfaces shall be free of cracks or draw marks; slight visible orange peeling effect shall be permitted. Unless otherwise specified (see 6.2), grommet surface texture shall be not more than 125 microinches in accordance with ASME

18、B46.1. 3.2.7 Shape. Fastener sleeves and grommets shall be round and shall show no evidence of distortion. 3.2.8 Grip length. Grooved sleeves or non-grooved grommets may be procured at the required length. Alternatively, grooved sleeves may be broken at incremental lengths using the proper tooling .

19、 The step plate tool indicates the grip length at which the sleeve will break along the groove without damage to the sleeve. 3.3 Metallurgical properties. 3.3.1 Cracks. The fastener sleeves and grommets shall be free of cracks. A crack is identified as a clean crystalline break passing through the g

20、rain or boundary without the inclusion of foreign elements. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-85069D 4 3.3.2 Discontinuities. There shall be no laps or folds, seams or discontinuities, or other interruption in grain flow. 4. VER

21、IFICATION 4.1 Classification of inspections. The inspection requirements specified herein are classified as conformance inspection (see 4.2). 4.2 Conformance inspection. 4.2.1 Sampling for examination. Test samples shall be selected at random in accordance with ASQ Z1.4, with the sampling level as s

22、pecified in table I. The acceptance quality limit (AQL) shall be as specified in the contract or purchasing order (see 6.2). Identical sample items may be used for any of the tests, provided that selection of random samples is maintained and known characteristics of the samples are not used to influ

23、ence the integrity of the test results. TABLE I. Conformance examination. Test Reference paragraph ASQ Z1.4 sampling inspection level Inspection lot 4.2.2 - Examination 4.3.1 II Material certification 4.3.3 - Grip length break 4.3.4 II 4.2.2 Inspection lot. A lot shall consist of sleeves or grommets

24、 made from the same lot of material and fabricated as a single continuous production run in which the forming machine set-up remains unchanged except for head configuration. A lot shall be restricted to one sleeve or grommet diameter or material thickness. A lot of material shall be defined as the q

25、uantity of sheet or strip steel made from a single heat. It shall be controlled and shipped with appropriate mill certification. In addition, the manufacturer shall maintain a record of inspections by lot number for a period of three years. 4.2.3 Certified test report. The manufacturer shall furnish

26、 certification that the product conforms to this specification. The record shall state that the product meets all the requirements of this specification. 4.3 Examination and tests. 4.3.1 Examination. Each of the sample sleeves or grommets selected for examination shall be examined for conformance to

27、 the requirements for dimensions, workmanship, identification, and to all requirements not covered by the tests. Samples failing to meet examination requirements shall result in rejection of the lot. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MI

28、L-DTL-85069D 5 4.3.2 Strength. The strength of the fastener sleeve or grommet combination is considered the strength of the fastener alone. The wall thickness of the sleeve or grommet is considered thin enough so that there shall be no material decrease in thickness when under load. Sleeve or gromme

29、t thickness shall be measured by any approved means. Sleeves or grommets that do not meet the dimensional requirements for thickness as shown in figures 1 through 4 shall result in rejection of the lot. 4.3.3 Material certification. Mill certification on all materials shall be kept on file by the ma

30、nufacturer and shall be available to the procuring agency for a period of three years. 4.3.4 Grip length break. Using different fastener sleeves, break at different lengths with the proper tooling. Grooved sleeves shall be broken only one time. To adjust to length at a location other than the breaki

31、ng area of the step plate, the sleeve may be ground to length using the painted section of the step plate. Sleeves that fail to break cleanly at the grooves shall result in rejection of the lot. 5. PACKAGING 5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in

32、 the contract or order (see 6.2). When packaging of materiel is to be performed by DoD or in-house contractor personnel, these personnel need to contact the responsible packaging activity to ascertain packaging requirements. Packaging requirements are maintained by the Inventory Control Points packa

33、ging activities within the Military Service or Defense Agency, or within the military services system commands. Packaging data retrieval is available from the managing Military Departments or Defense Agencys automated packaging files, CD-ROM products, or by contacting the responsible packaging activ

34、ity. 6. NOTES (This section contains information of a general or explanatory nature that may be helpful, but is not mandatory.) 6.1 Intended use. The fastener sleeves and grommets specified herein are intended for structural and non-structural application in aerospace structures and other military e

35、quipment. The function of the sleeves and grommets is to serve as a repair method for holes that have become damaged, elongated, or corroded, and to protect the structure in soft or brittle material. The sleeve is intended to increase the integrity of the overall joint, not the strength of the indiv

36、idual fastener. 6.1.1 Length adjustment. Fastener sleeves and grommets that are manufactured with proper head configuration and diameter may be procured at the required length. Alternatively, sleeves may be adjusted to the correct length for each individual fastener. 6.1.2 Installation of sleeves an

37、d grommets. Fastener sleeves and grommets should be installed with reasonable care to ensure that they seal properly, inhibit corrosion, and establish, preserve, or restore the structural integrity of joints in modification, repair, or in the original manufacture of aerospace or military hardware. T

38、he installation information and the processing Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-85069D 6 specifications should be followed. Tools are available to facilitate and ensure proper installation of the sleeve or grommet. 6.1.2.1 Gene

39、ral purpose and restrictions. The fastener sleeves and grommets will be used to replace oversize shank fasteners for repair and maintenance. The sleeves and grommets will be used with standard diameter straight shank fasteners. They will be used under the same restrictions as oversize fasteners and

40、in compliance with the specific users repair procedures and restrictions. 6.1.2.2 Number of fasteners. There will be no restrictions on the number of fasteners installed with sleeves or grommets when the edge distance from the center of the hole is two times the diameter and greater. 6.1.2.3 Fastene

41、rs. The fastener or attaching element (nut or collar) will contain a counter-bore to accept the protrusion of the sleeve or grommet; or a washer will be used; or the sleeve or grommet will be flush on the backside of the stackup. 6.1.2.4 Fastener restrictions. The fastener sleeves or grommets will n

42、ot be used with tapered shank fasteners or blind fasteners. 6.1.2.5. Interference. Interference (hole-to-sleeve) will be not greater than 0.003 inch where the material thickness is less than 0.5 inch. Interference will be not greater than 0.0015 inch where material thickness is greater than 0.5 inch

43、. 6.1.3 Applications. Appropriate engineering approval will be required in the following applications: a. In fluid containers having no self-sealing feature, as in fuel, oil, or water tanks. b. Fatigue and fracture critical locations. c. Where the edge distance from the center of the hole is less th

44、an 1.5 diameters. d. Where the number of discrepant holes being repaired is greater than 10-percent of the total number of holes in a pattern. e. Where more than three adjacent holes are discrepant. 6.2 Acquisition requirements. Acquisition documents should specify the following: a. Title, number, a

45、nd date of this specification. b. PIN to include classification of sleeve or grommet required (see 1.3). c. Conformance inspection requirements (see 3.1). d. Surface texture exceptions (see 3.2.6). e. AQL (see 4.2.1). f. Packaging (see 5.1). Provided by IHSNot for ResaleNo reproduction or networking

46、 permitted without license from IHS-,-,-MIL-DTL-85069D 7 6.3 Supersession data. This specification supersedes the documents listed in table II. TABLE II. Supersession data. Document Date MIL-DTL-85069C 25 January 2006 MIL-S-85069/1A 16 September 1981 MIL-DTL-85069/2B 25 January 2006 MIL-DTL-85069/3B

47、 25 January 2006 MIL-DTL-85069/4B 25 January 2006 MIL-DTL-85069/5B 25 January 2006 MIL-DTL-85069/6B 25 January 2005 MIL-DTL-85069/7B 25 January 2006 MIL-DTL-85069/8B 25 January 2006 MIL-DTL-85069/9B 25 January 2006 MIL-DTL-85069/10A 25 January 2006 MIL-DTL-85069/11A 25 January 2006 6.4 Subject term

48、(key word) listing. Aircraft Cadmium Countersunk Discrepant hole Drawn Flush Grip length Grooved Hard seat One piece Oversize Protection Protruding head Reduced head Shank Shear Step plate Structural Swaged Tension Tubular 6.5 Changes from previous issue. Marginal notations are not used in this revi

49、sion to identify changes with respect to the previous issue due to the extent of the changes. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-85069D 8 NOTES: 1. Dimensions are in inches and shall apply prior to surface finish. Refer to table III. 2. Sleeves may be procured in standard required lengths or may be adjusted to