NAVY MIL-DTL-32183-2004 CATAPULT AIRCRAFT EJECTION SEAT CKU-5C A REWORK ASSEMBLY《CKU-5C A 再工作组飞机弹射座椅弹射器》.pdf

1、INCH-POUND MIL-DTL-32183 (OS) 21 December 2004 DETAIL SPECIFICATION CATAPULT, AIRCRAFT EJECTION SEAT: CKU-5C/A REWORK ASSEMBLY This specification is approved for use by the Naval Sea Systems Command, Department of the Navy, and is available for use by all Departments and agencies of the Department o

2、f Defense. 1. SCOPE 1.1 Scope. This specification establishes the requirement for the refurbishment (rework) of the CKU-5C/A rocket catapults (ROCAT) for aircraft ejection seat assemblies. This specification includes only the requirements for restoration of salvageable hardware. All other requiremen

3、ts for the CKU-5C/A ROCAT are specified in the new unit specification, MIL-DTL-32127 and drawing 512-174-0068. The earlier versions of the CKU-5C/A ROCAT, the CKU-5/A/A and CKU-5B/A, may be converted to the CKU-5C/A configuration during the rework. 2. APPLICABLE DOCUMENTS 2.1 General. The documents

4、listed in this section are specified in sections 3, 4, or 5 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,

5、 document users are cautioned that they must meet all specified requirements of documents cited in sections 3, 4, or 5 of this specification, whether or not they are listed. 2.2 Government documents. 2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handboo

6、ks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. DEPARTMENT OF DEFENSE SPECIFICATIONS MIL-DTL-32127 Catapult, Aircraft Ejection Seat CKU-5C/A Assembly DEPARTMENT OF DEFENSE STAND

7、ARDS Comments, suggestions, or questions on this document should be addressed to Commander, Indian Head Division, Naval Surface Warfare Center, Technical Information Branch (Code 4230), 101 Strauss Avenue, Indian Head, Maryland 20640-5035, or emailed to amanda.pennnavy.mil. Since contact information

8、 can change, you may want to verify the currency of this address information using the ASSIST Online database at http:/assist.daps.dla.mil. AMSC N/A FSC 1377 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. Source: http:/assist.daps.dla.mil - Downloaded: 2005-06-22T2

9、1:27ZCheck the source to verify that this is the current version before use.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-32183 (OS) 2 DOD-STD-2101 Classification of Characteristics (Copies of these documents are available online at http:/a

10、ssist.daps.dla.mil/quicksearch/ or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.) 2.2.2 Other Government documents, drawings, and publications. The following Government drawings form a part of this specification to the extent specified he

11、rein. Unless otherwise specified, the issues are those cited in the solicitation (see 6.2). DRAWINGS NAVAL SURFACE WARFARE CENTER, INDIAN HEAD DIVISION (CAGE Code 14083) DL 512-174-0068 Catapult, Aircraft Ejection Seat, CKU-5C/A Assembly 512-174-0068 Catapult, Aircraft Ejection Seat, CKU-5C/A Assemb

12、ly 5184315 Plug, Breech 11743978 Nozzle 11743979 Breech 11726650 Tube, Motor 11726656 Tube, Booster 11726657 Tang 11726800 Launcher Tube Assembly 512-174-0076 Plug 512-174-0078 Tang - Modified 512-174-0079 Tube, Metering 512-174-0083 Tang (Copies of drawings should be obtained from the Commanding Of

13、ficer, Indian Head Division, Naval Surface Warfare Center, Attn: Technical Information Branch (Code 4230), Indian Head, MD 20640-5035.) 2.3 Non-Government publications and drawings The following document form a part of this document to the extent specified herein. Unless otherwise specified, the iss

14、ues of the documents which are DOD adopted are those listed in the issue of the DODISS cited in the solicitation. Unless otherwise specified, the issues of documents not listed in the DODISS are the issues of the documents cited in the solicitation (see 6.2). AMERICAN SOCIETY OF MECHANICAL ENGINEERS

15、 (ASME) Source: http:/assist.daps.dla.mil - Downloaded: 2005-06-22T21:27ZCheck the source to verify that this is the current version before use.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-32183 (OS) 3 ASME B46.1 Surface Texture (Surface R

16、oughness, Waviness, and Lay) (DOD adopted) (Copies of this document are available online at http:/www.asme.org or from American Society of Mechanical Engineers, Three Park Avenue, New York, NY 10016-5990) 2.4 Order of precedence. In the event of a conflict between the text of this document and the r

17、eferences 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. Materials, parts and assemblies, reusable and new, shall comply with the req

18、uirements specified on DL 512-174-0068, this specification, and the documents referenced herein. 3.2 Catapult receipt, inspection, and disposition. ROCAT receipt, inspection, and disposition shall meet the requirements specified in 3.2.1 through 3.2.6. 3.2.1 Catapult lot number. Record the lot numbe

19、r of each ROCAT. 3.2.2 Reusable components. The components listed in table I are expected to have a 90 percent or greater recovery rate, except as noted, and are to be retained for reclamation or restoration. Parts are to be inspected according to 4.2.2.1. Reusable components are subject to the limi

20、tations of 3.2.2.1 through 3.2.2.3. TABLE I. Reusable components. Component Number required Drawing/part number Tang 1 512-174-0083 Plug 1 512-174-0076 Breech 1 11743979 Nozzle 1 11743978 Tube, Booster 1 11726656 Launcher Tube Assembly 1 11726800 Tube, Motor 1 11726650 Plug, Breech 4 5184315 Tube, M

21、etering 1 512-174-0079 3.2.2.1 Tang. Tangs conforming to drawing 11726657 may also be reused in the rework assembly when modified in accordance with 3.2.4.1. After modification, tang recovery rate is expected to be 90 percent or greater. Source: http:/assist.daps.dla.mil - Downloaded: 2005-06-22T21:

22、27ZCheck the source to verify that this is the current version before use.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-32183 (OS) 4 3.2.2.2 Nozzle. Nozzles conforming to drawing 11743978 revision (G) and subsequent revisions may be reused

23、in the rework assembly if they meet all of the following requirements. All others must be rejected. a. Overall nozzle height (along ROCAT axis) not less than 2.43 inches b. Diameter of o-ring groove in nozzle interior no greater than 1.233 inches c. Nozzle exhaust port exterior shape is as illustrat

24、ed in Figure 1. Figure 1. Acceptable and Unacceptable Nozzle Exhaust Port Shape. 3.2.2.3 Motor Tube. Reuse of motor tubes requires removal of propellant grain prior to inspection. All motor tubes will require restoration prior to inspection. 3.2.3 New components. All components of the reworked catap

25、ult assembly that are not listed in table 1 shall be new components. 3.2.4 Modified components. Conversion of CKU-5/A/A, and CKU-5B/A catapults to the latest CKU-5C/A catapult configuration shall be accomplished by modifying the tang component as described in 3.2.4.1. 3.2.4.1 Tang. Tangs that confor

26、m to drawing 11726657 shall be modified in accordance with drawing 517-174-0078. The tangs that conform to drawing 11726657 do not have a 15 - 20 chamfer on the end of the bore. 3.2.5 Cartridge disposition. The contracting activity will provide disposition instructions for CCU-22/A/A, and/or CCU-22B

27、/A Impulse Cartridges (see 6.2). Acceptable Nozzle Unacceptable Nozzle Source: http:/assist.daps.dla.mil - Downloaded: 2005-06-22T21:27ZCheck the source to verify that this is the current version before use.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS

28、-,-,-MIL-DTL-32183 (OS) 5 3.2.6 Hardware disposition. Contractor shall report final yield of reusable components, after restoration, modification, and inspection is completed, to the contracting activity before proceeding with assembly. All rejected hardware shall be returned to the Government (see

29、6.2). 3.3 Performance. Reusable components of the reworked ROCATs shall meet the performance requirements of 3.3.1. 3.3.1 Hydrostatic pressure. The motor tube, launcher tube assembly, and booster tube shall withstand the internal hydrostatic pressure test specified in MIL-DTL-32127. During the hydro

30、static pressure test of the launcher tube assembly, ensure that the fiberglass wrap is kept dry at all times. It is acceptable to test only the portion of the launcher tube assembly beyond the holes. The untested portion of the launcher tube assembly shall be approximately 2 1/2” inches in length. 3

31、.4 Identification marking. The reusable components shall require identification markings (part number and serial number) in accordance with the following guidelines. 3.4.1 Stamp out previous ROCAT lot and serial number identification markings on breech. Each breech shall have the previous CKU-5 ROCA

32、T serial number and lot number stamped out. 3.4.2 Identification marking not required. The following reusable components require no part number or serial number marking. a. Plug b. Breech Plug c. Metering Tube 3.4.3 Identification marking required. Unless otherwise specified in the contract or purch

33、ase order (see 6.2), the following reusable components require part number and serial number marking: a. Tang b. Breech c. Nozzle d. Booster Tube e. Launcher Tube Assembly f. Motor Tube These parts shall be marked in accordance with 3.4.3.1 through 3.4.3.3. 3.4.3.1 Parts with existing serial number.

34、 On parts with an existing serial number, add an “R” to the end of the serial number. Use an appropriate permanent marking method (stamp, engrave, permanent ink, etc.). For parts that already have an “R” from previous rework, add an additional “R”. 3.4.3.2 Parts with existing part number but no seri

35、al number. Add a non-recurring serial number to parts that have an existing part number but no serial number. Use an appropriate permanent marking method (stamp, engrave, permanent ink, etc.). Serial number shall begin with an “R” followed by a five-digit, consecutive number. Serial number shall nor

36、mally be located below or following the part number. 3.4.3.3 Parts with no existing part number. Contact the contracting activity for instructions on marking parts with no existing part number. Source: http:/assist.daps.dla.mil - Downloaded: 2005-06-22T21:27ZCheck the source to verify that this is t

37、he current version before use.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-32183 (OS) 6 3.5 Protective finish. Protective finish shall be in accordance with the applicable specification referenced on the drawings and shall apply to all sur

38、faces regardless of configuration. All reusable parts, which fail the protective finish requirements of tables II through X, shall be replated or repaired as applicable. 3.5.1 Protective finish touch up repair. If the defective area of the protective finish is small, the defects may be repaired as f

39、ollows. The protective finish on steel parts may be touched up with zinc chromate primer in accordance with TT-P-1757, type I, class C, color Y. The protective finish on aluminum parts may be touched up with chemical film in accordance with MIL-C-5541, class 1A. 3.6 Workmanship. Workmanship shall be

40、 that required by the applicable drawings, referenced specifications and the best industrial practices governing the quality production of interchangeable parts for maintaining the dimensions, finishes, tolerances, and quality specified herein. All components and assemblies shall be free from burrs,

41、 contamination, corrosion, sharp edges, or foreign material which could result in malfunction of the unit or components, or be a safety hazard in handling. 4. VERIFICATION 4.1 Classification of inspections. The inspection requirements specified herein are classified as follows: a. Conformance inspec

42、tion (see 4.2) 4.1.1 Inspection conditions. Unless otherwise specified in the contract or purchase order (see 6.2), all inspections shall be performed under the following conditions: a. Temperature: Room ambient (65 to 95F) b. Altitude: Normal ground c. Humidity: Room ambient to 95 Percent relative,

43、 maximum. 4.2 Quality conformance inspection. Quality conformance inspection shall consist (at a minimum) of the examinations and tests specified in 4.2.2 and 4.2.3. When specified, items of inspection shall be serialized and inspection data traceable to a specific serial number. The requirements sp

44、ecified are the minimum needed to insure the quality of the rocket catapult. Based upon the manufacturers process or the state of material, additional inspections may be required. The absence of any inspection requirements in the specification shall not relieve the contractor of the responsibility o

45、f ensuring that all products or supplies submitted to the government for acceptance comply with all the requirements of the contract. When specified, sampling inspection is an acceptable practice to ascertain conformance to requirements; however, it does not authorize submission of known nonconformi

46、ng material, either indicated or actual, nor does it commit the Government to accept nonconforming material. 4.2.1 Sampling. One hundred percent examination shall be performed for all examinations of 4.2.2 unless otherwise specified. Sampling for tests shall be as specified in 4.2.3. 4.2.2 Quality c

47、onformance examination. Quality conformance examinations for major and minor characteristics shall be performed in accordance with tables II through X. Classification designations are in accordance with DOD-STD-2101. All defective material shall be removed from the lot. The roughness comparison spec

48、imens prescribed in ASME B46.1 shall be used as a basis of comparison for surface roughness determination. Any component with a critical defect shall be rejected. Source: http:/assist.daps.dla.mil - Downloaded: 2005-06-22T21:27ZCheck the source to verify that this is the current version before use.P

49、rovided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-DTL-32183 (OS) 7 TABLE II. Classification of Motor Tube Defects Tube, Motor, P/N 11726650 Classification Defect Inspection Method Sampling Restoration Notes M101 Metal defective. Visual, Borescope, and Radiographic 100% Footnote 2.1 M102 Protective finish inadequate or defective (after propellant removal). Visual 100% Footnote 2