NAVY MIL-T-50356 A-1993 THRUSTER CARTRIDGE ACTUATED M1A2 REMANUFACTURED METAL PARTS ASSEMBLY《M1A2改造金属零件集合发动弹药筒推进器》.pdf

《NAVY MIL-T-50356 A-1993 THRUSTER CARTRIDGE ACTUATED M1A2 REMANUFACTURED METAL PARTS ASSEMBLY《M1A2改造金属零件集合发动弹药筒推进器》.pdf》由会员分享，可在线阅读，更多相关《NAVY MIL-T-50356 A-1993 THRUSTER CARTRIDGE ACTUATED M1A2 REMANUFACTURED METAL PARTS ASSEMBLY《M1A2改造金属零件集合发动弹药筒推进器》.pdf（13页珍藏版）》请在麦多课文档分享上搜索。

1、-. *- MIL-T-5035bA 9999906 I1853705 82T W I INCH-POUND I MIL-T-50356A 19 March 1993 SUPERSEDING 8 October 1969 MIL-T-50356(MU) MILITARY SPECIFICATION THRUSTER, CARTRIDGE ACTUATED, M1A2 REMANUFACTURED METAL PARTS ASSEMBLY his specJcation is approved for use by all Departments and Agencies of the Depa

2、rtment of Defense. 1. SCOPE 1.1 Scope. This specification covers the requirements for the M1A2 Cartridge Actuated Thruster Remanufactured Metal Parts Assembly (see 6.1). 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications and standards. The following specifications and standards f

3、orm a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the issue of the Department of Defense Index of Specifications and Standards (DODISS) and supplements thereto, cited in the solicitation (see 6.2). SPECIFICATIONS

4、 MILITARY MILLA-2550 Ammunition, General Specification For STANDARDS MILITARY MIL-STD-105 MIL-STD-109 MIL-STD-4 13 Sampling Procedures And Tables For Inspection By Attributes Quality Assurance Terms And Definitions Visual Inspection Guide for Elastomeric O-rings Beneficial comments (recommendations,

5、 additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Commander, Indian Head Division, Naval Surface Warfare Center, Standardization Branch (Code 8420), 101 Strauss Avenue, Indian Head, MD 20640-5035, by using the Standardization Documen

6、t Improvement Proposal (DD Form 1426) appearing at the end of this document or by sending a letter. AMSC NIA DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. FSC 1377 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MI

7、L-T-5035bA = 999990b 1853706 7bb * MIL-T-50356A (Unless otherwise indicated, copies of federal and military specifications and standards are available from Standardization Documents Order Desk, Bldg. 4D, 700 Robbins Avenue, Philadelphia, PA 191 11-5094.) 2.1.2 Other Government documents, drawings, a

8、nd publications. The following Government drawings form a part of this specification to the extent specified herein. Unless otherwise specified, the issues are those cited in the solicitation (see 6.2). O DRAWINGS Naval Surface Warfare Center, Indian Head (CAGE Codes 19200 and 19203) 8593855 Thruste

9、r, Cartridge Actuated, MlA2, Metal Pacts Assembly 879763 1 Box, Fiberboard (inner), Packing, Ammunition, For Thruster, Cartridge Actuated, M1A2 8797632 Box, Packing, Ammunition, For Thruster, Cartridge Actuated, M1A2 922 126 1 Box, Fiberboard (Outer), Alternative, Packing Ammunition, for Thruster, C

10、artridge Actuated, M1A2 U.S. Air Force TPO 00-891-5488 Thruster, Cartridge Actuated, M1A2 (Application for copies should be addressed to: Commander, Indian Head Division, Naval Surface Warfare Center, Attn: Data Control Branch (Code 8410), Indian Head, MD 20640-5035.) 2.2 Order of precedence. In the

11、 event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 3. REQUIREMENTS 3.1 Materials. All material

12、s used in the manufacture of the thrusters shall conform to the specifications referred to on the respective drawings unless specific approval in writing covering a departure therefrom has been obtained from the cognizant Navy design activity prior to manufacture. When alternate materials or methods

13、 of manufacture are specified on the drawings, the bidders selections shall be clearly stated in the proposal. The remanufactured thruster metal pacts assembly shall contain a new shear pin, new O-rings, and a new piston locking spring. 3.2 Hydrostatic pressure. The body and head shall withstand a h

14、ydrostatic pressure of 7,500 pounds per square inch (psi) for 15 seconds, minimum, without leaking, deformation, or mechanical failure (see 6.3.1). 3.3 Protective finish. Protective finish shall be in accordance with the applicable specifications and drawings and shall apply to ail surfaces of the c

15、omponent regardless of configuration. Remanufactured 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-50356A exterior components (see 6.4) shall have the existing protective finish stripped and the specified protective finish reapplied. 3.4 Re

16、sidual magnetism. The metal parts assembly shall not deflect the indicator of the compass more than five degrees in either direction using the procedures of 4.5.3. 3.5 Shear pin strength. The shear pin, after application of protective finish, shall shear when a load of 48 it 4 pounds is applied at t

17、he steady rate of 0.125 inch per minute. 3.6 Metal parts assembly. Parts shall be combined to produce an assembly which conforms to the requirements of the metal parts assembly drawing. All threaded joints shall be assembled with sufficient torque to bottom components. 3.6.1 Integrated plant product

18、s. When remanufacturing and loading of the assembly is performed in an integrated plant, the metal parts assembly requirement may be waived and the residual magnetism requirement performed on the loaded assembly only. 3.6.2 Threaded component parts. Class 2A or 2B thread gage shall be used on remanu

19、factured component parts inspection versus class 3A or 3B thread gage required on new hardware for thrusters. 3.6.3 Piston locking spring and end sleeve. The piston locking spring shall enter the spring hole in the piston without any bending along its entire length, If axial misalignment of the pist

20、on locking spring occurs, the cap screw may be backed off sufficiently to permit alignment. 3.6.4 Trunnion rotation. Upon completion of assembly, the trunnion shall be free to rotate 360 degrees. 3.6.5 End sleeve rotation. Upon completion of assembly, the end sleeve shall be free to rotate 360 degre

21、es in a clockwise direction. 3.6.6 Reclaimed parts. Remanufactured thruster parts which may be reclaimed shall meet the following requirements: a. Piston. Only pistons with 1/2 inch length from back face to O-ring groove and Y8 inch length from front face to back face of key escape groove shall be r

22、eclaimed. Nonconforming pistons which have the unlocking undercut of 9/16 inch length shall be modified to meet the 98 inch length requirement of Drawing 8593867. Touch-up plating to the machined area is acceptable. b. Head. Only heads with internal bore diameter of 0.337 + 0.009 inch and no setscre

23、w holes shall be reclaimed. c. Body. Only bodies suitable for nylon pellet type thread fastening shall be reclaimed. The nylon pellet shall be located 0.775 f 0.015 inch from end of body. The chamfer on the outer edge of the threaded end shall be 1/16 x 5/64 and the inner edge shall be 1/16 x 3/64.

24、The length of the trunnion flat shall be 17/32. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-5035bA 9997706 LB53708 539 - MIL-T-50356A O d. Cartridge retainer. Only retainers suitable for nylon pellet type thread fastening shall be reclaim

25、ed. The nylon pellet shall be located 0.453 f 0.015 inch from the end. The chamfer on edge of thread end shall be 3/64 x 3/64. The large flange diameter shall be 1.120 - 0.002. e. Guide. Only guides with a chamfer 1/32 x 5/64 inch on end of firing pin bore and 0.075 - 0.015 striker wall thickness sh

26、all be reclaimed. f. Firing pin. Only pins with overall length of 0.743 - 0.030 and striker end length of 0.229 + 0.003 shall be reclaimed. g. Trunnion. Only trunnions with a 0.206 - 0.014 wall thickness and 1/32 x 1/32 chamfer on inside diameter shall be reclaimed. .3.7 Workmanship. Thrusters shall

27、 be free of cracks, splits, or other defects which might prevent proper mating with connecting parts or proper functioning of the device. 3.7.1 Metal defects. All components shall be free from cracks, splits, cold shuts, inclusions, porosity, or any similar defect. 3.7.2 Burr. No part shall have a b

28、urr which might interfere with the assembly or function of the item or which might be injurious to personnel handling the item. 3.7.3 Foreign matter. No part or assembly shall contain chips, dirt, grease, rust, corrosion, or other foreign matter. 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility fo

29、r inspection. Unless otherwise specified in the contract or purchase order, the contractor is responsible for the performance of all inspection requirements (examinations and tests) as specified herein, Except as otherwise specified in the contract or purchase order, the contractor may use his own o

30、r any other facilities suitable for the performance of the inspection requirements specified herein, unless disapproved by the Government. The Government reserves the right to perform any of the inspections set forth in this specification where such inspections are deemed necessary to ensure supplie

31、s and services conform to prescribed requirements (see 6.2). 4.1.1 Responsibility for compliance. All items shall meet all requirements of sections 3 and 5. The inspection set forth in this specification shall become a part of the contractors overall inspection system or quality program. The absence

32、 of any inspection requirements in the specification shall not relieve the contractor of the responsibility of ensuring that all products or supplies submitted to the Government for acceptance comply with all requirements of the contract. Sampling inspection, as part of manufacturing operations, is

33、an acceptable practice to ascertain conformance to requirements; however, this does not authorize submission of known defective material, either indicated or actual, nor does it commit the Government to acceptance of defective material. 4.1.2 Quality assurance terms and definitions. Reference shall

34、be made to MIL-STD-109 to define the quality assurance terms used. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-5035bA W 999990b 2853709 475 MIL-T-50356A 4.1.3 Inspections. Inspections shall be in accordance with MIL-A-2550. 4.2 Inspection

35、 conditions. Unless otherwise specified (see 6.2), all inspectams !,ail be performed o under the following conditions: a. Temperature: room ambient (68 to 77F) b. Altitude: sea level c. Humidity: 50 percent relative, maximum d. Atmospheric pressure: 14.7 psi 4.3 Quality conformance inspection. 4.3.1

36、 Lot. 4.3.1.1 Submission of product. Unless otherwise specified by the contracting activity, formation and identification of lots shall be in accordance with MIL-STD-105. 4.3.1.2 Size of lot. For the purpose of identification and shipment, the shipping lots of metal parts assemblies shall consist of

37、 1200 assemblies, maximum, provided the homogeneity requirements of inspection lots have been retained. 4.3.2 Examination. On reprocessed and new parts, one hundred percent examination shall be performed for all critical defects. Examination for major and minor defects shall be performed on a defect

38、 basis in accordance with the classification of defects. Four power (4x) magnification may be used in performing visual examination for such defects as burr and foreign matter. Inspection for rubber 0- rings shall be in accordance with MIL-STD-413. When compliance with the applicable requirement is

39、0 in doubt as a result of visual examination, the characteristic shall be measured or gaged to determine acceptability. All nonconforming material shall be rejected. I 4.3.2.1 Examination of reclaimed parts. Examination of reusable parts, which require no reprocessing, shall be limited to inspection

40、 of defects that require visual type inspection. One hundred percent examination shall be performed for all such defects. All nonconforming parts shall be reprocessed or rejected. For the piston and plug assembly, Drawing 8593866, one hundred percent inspection shall be made for all defects listed i

41、n 4.3.2.8 requiring gage inspection. 4.3.2.2 Key, Drawing 8593857, covering a detail of Drawing 8593855. Characteristics Defect MediodofInspedon Critical None defined Major 101 102 103 104 Metal defective Protective finish inadequate or defective Burr or sharp corner Foreign matter Visual Visual Vis

42、ual visual 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-5035bA m 9999906 1853710 I497 m MIL-T-50356A Minor None defined 4.3.2.3 Body Assembly, Drawing 8593859, covering a detail of Drawing 8593855. Critical None defined Major 101 102 103 1

43、04 105 106 107 108 109 110 111 Pellet missing, loose, or improperly inserted Metal defective Burr Foreign matter Protective finish inadequate or defective Thread damaged or not full Chamfer on outer edge of threaded end Chamfer on inner edge of threaded end Location of pellet Length from thread unde

44、rcut to flange Pitch diameter of large external thread, min Minor None defined 4.3.2.4 Trunnion, Drawing 8593860, covering a detail of Drawing 8593855. Critical None defined Major 101 Metal defective 102 103 Wall thickness 104 Chamfer on inside diameter Protective finish inadequate or defective Mino

45、r 201 Burr or sharp corner 202 Foreign matter Maniawisual visual Visual visual Visual Visual visual Visual Gage Gage Gage Visual Visual Gage Visual visual Visual 4.3.2.5 Retainer, Cartridge, Assembly, Drawing 8593862, covering a detail of Drawing 8593855 (after inserting pellet). Critical None defin

46、ed Major 101 102 Location of pellet Flange diameter Gage Gage 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-5035bA m 99999Ob 1853711 023 103 O 104 105 106 107 108 109 110 MIL-T-50356A Pitch diameter of large external thread, min Pellet miss

47、ing, loose, or improperly inserted Chamfer at thread end Metal defective Burr Foreign matter Protective finish inadequate or defective Thread damaged or not full Gage wi Visual Visual Visual Visual Visual Visual Minor None defined 4.3.2.6 Guide, Firing Pin, Drawing 8593863, covering a detail of Draw

48、ing 8593855. Critical None defined Major 101 Metal defective 102 103 Burr or sharp corner 104 Foreign matter 105 Protective finish inadequate or defective Chamfer at end of firing pin bore Minor Nonedefined 4.3.2.7 Pin, Firing, Drawing 8593864, covering a detail of Drawing 8593855. Critical None def

49、ined Major 101 102 Total length 103 Metal defective 104 105 Burr or sharp corner 106 Foreign matter Length from body face to tip of striker Protective finish inadequate or defective Visual Visual Visual Visual visual Gage Gage Visual Visual Visual Visual Minor None defined 7 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-,MIL-T-5035bA M 9999906 3853732 TbT M MIL-T-50356A O 4.3.2.8 Piston and Pl