NAVY MIL-R-60862-1968 REMOVER AIRCRAFT CANOPY OVERHAUL MODIFICATION AND CONVERSION OF《飞机座舱盖的修配 改进 转化清洗剂》.pdf

《NAVY MIL-R-60862-1968 REMOVER AIRCRAFT CANOPY OVERHAUL MODIFICATION AND CONVERSION OF《飞机座舱盖的修配 改进 转化清洗剂》.pdf》由会员分享，可在线阅读，更多相关《NAVY MIL-R-60862-1968 REMOVER AIRCRAFT CANOPY OVERHAUL MODIFICATION AND CONVERSION OF《飞机座舱盖的修配 改进 转化清洗剂》.pdf（17页珍藏版）》请在麦多课文档分享上搜索。

1、MIL-R-60862(MU) 10 April 1968 MILI32FiY SPECIFIaTION RFSIOVER, AIRCRILFT CANOPY OVERHAUL, MODIFICATION AM COION OF P/N 2218-17 To P/N 2218-18 1. SCOPE 1.1 This specification covers the overhaul and modification required to convert Remover, Aircraft Canopy, P/N 2218-17 to the Remover, Aircraft Canopy

2、, P/N 2218-18 configuration 2. APPLICABLE DOCUMENTS 2.1 The following documents of the issue in effect on date of invitation for bids or request for proposal, form a part of this specification to the extent specified herein. SPECIFICATIONS Military MIL-A -2550 MIL-G -4343 MIL-S-5002 MIL-A-8625 MIL+

3、-23827 MI-8937 MIL-C-26074 STANDARDS Military MIL-SID-105 MIL-STD -109 - Ammunition and Special Weapons, General - Grease, Pneumatic System - Surface Treatment, and Metallic Coatings for - Primer, Coating, Zinc Chromate, Low - Moisture - Anodic Coatings, for Aluminum and Aluminum - Grease, Aircraft

4、and Instrument, Gear and - Lubricant, Solid Film, Heat Wed - Coating, Nickel - Phosphorus, Electroless, Specification for Metal Surfaces of Weapons Systems Sensitivity Alloys Actuator Screw Nickel Requirements For - Sampling Procedures and Tables for Inspection - Quality Assurance Terms and Definiti

5、ons by Attributes . FSC 1377 . -, c , PAGES. - - Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-60862 13 7777906 0343636 1 MIL-R-60862 (MU) 2.1 STANDARDS (Contd) Military MIL-STD- MIL-STD-i167 - Ammunition Data Card - Surface Roughness Values

6、Preferred for Arqy Ordnance Material DRAWINGS Munitions Command c9233331 C9233334 - Carton, Packing Ammunition for Remover, - Box, Packing, Ammunition for One (1) Remover, Aircraft; Canopy, P/N 2218-18 Aircraft Canopy, P/N 2218-18 Talley Industries (Code Ident. No. 98708) 2218-18 - Actuator, Electro

7、 Mechanical, Ballistic Emergency Removal PUBLICATIONS Air Force Technical Manual T.O. -4-11-3 - Overhaul Instructions with Parts Breakdown, Canopy Actuator, Part No. 2218-18 (Copies of specifications, standards and drawings required by contractors in connection with specific procurement functions sh

8、ould be obtained from the procuring activity or as directed by the Contracting Officer.) 3. RlQu1-s 3.1 General.- Materials, parts and asseniblies shall comply with the reqirements specified in T .O. llP4-11-3, referenced specifications and standards. 3.1.1 When converting Remover, Aircraft Canopy,

9、P/N 2218-17 to Remover, Aircraft Canopy, P/N 2218-18, the following paragraphs contained in T.O. u94-ll-3 shall not apply: 2-2, j thru m 2-4, j thru w 2-6, e and f 3-3, a thru h 2-5, f thru U 2-7, c thz3.l P . . -2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license

10、from IHS-,-,-MIL-R -60862 (MU) 3.2 Assembly torque.- The assembly torques for the installation of actuator component parts shall be in accordance with requirements specified in Xigure 2-7 of T.O. W4-11-3. 3.3 Remover assembly.- The overhauled remover shall contain new parts ln accordance with Table

11、I. Name of Part Seal, O-Ring Seal, O-Ring Seal, O-Ring Seal, O-Ring Seal, O-Ring Seal, O-Ring (2 each reqd) Seal, O-Ring Seal, O-Ring Seal, O-Ring Seal, O-Ring Seal, O-Ring Seal, O-Ring Gasket, Cover Gasket Gromet Spring Spring, Compression Cartridge Bushing (2 each reqd) Retainer Pin, Shear Pin, St

12、raight Wiper, Tube Wiper, Tube Label, Identification Label, Warning Label, Warning Set Screw Cotter Pin Set Screw . Set Screw Plug, Shipping cap, Plu; Part Number m 9021-010 I43 9021-012 N.3 9021-021 m 9021-029 m 9021-030 H 921-034 MS 9021-135 2-25 (Tetraflour, Inc .) 2-26 (Tetraflour , Inc ) 2-29 (

13、Tetraflour, Inc . ) 2-30 (Etraflour , Inc . ) 2-31 (Tetraflour , nc ) 2218-53 (Talley Ind.) 2218-37 (Talley Ind . ) 1144-57 (Talley Ind ) 1146-221 (Talley Ind. ) 2218-67 (Talley Ind. ) M3 35490-4 &S 24585-219 . 2218-24 (Talley Ind. j 2218-60 (Talley Ind . ) 2218-25 (Talley Ind.) 2218-27 (Talley Ind.

14、 ) ci0536008 1424-128 (Talley Ind. ) B8593294 AN565D103m 381-1-5-12 (replace with latest AN565D103W5 AN56!jA4H2 PD40 (Protective Closures nc.) 12 (Protective Closures nc. ) 1605-50 (Talley Inde) Standard M3 24665-88) 3 . Provided by IHSNot for ResaleNo reproduction or networking permitted without li

15、cense from IHS-,-,-MIL-R-O%(MU) - 3.3.1 The following listed parts from Remover, P/N 2218-17, shall be 3.3.1.1 Replace Shear Pin, Piston, P/N 51700-30 with Pin, Retaining 3.3.1.2 Replace Motor D.C. P/N 2218-86 with Motor, D.C. P/N 2218-107. 3.3.2 The following listed parts from Remover, P/N 2218-17

16、shall be removed, discarded and replaced as noted: P/N 2218-111 (Talley Ind. ) , 2 each required. modified as noted below: Drawing 2218-108. 3.3.2.1 Modify Retainer P/N 2218-85 to contain a flat as depicted on 3.3.2.2 Modi Switch Housing, P/N 2218-48 in accordance with Drawing Di0551939 3.4 Function

17、al. 3.4.1 Operating load.- The Remover shaJ.1 be cycled electrically in accordance with the Alternative Actuator Test Procedure, paragraph 3-2, T.O. iE4-11-3. and motor current drain shall comply with requirements in paragraph 3-2, The time required for linear extension, linear retraction T -0 iE4-U

18、-3. 3.4.2 Bearing center dimensions.- The bearing center dimensions of the Remover while subjected to the normal operating load shall comply with requirements of paragraph 3-1. f. (1) thru f. (4) of T.O. 1U4-11-3. 3.4.3. Air firing.- The Remover shall stroke in accordance with the requirements of pa

19、zagraph 3-1. j, T.O. 1324-11-3, when 375 - 450 pounds per square inch (psi) air pressure is applied to the firing head. 3.5 Protective finish.- Protective finish shall be in accordance with T.O. 1194-11-3, applicable specifications and drawings, and shall apply to all surfaces of the component, rega

20、rdless of configuration. shall have the existing protective finish stripped and the specified protective finish reapplied (See 6.1). T.O. llP4-11-3, referenced specifications and the following: other metal defects. Exterior components 3.6 Workmanship.- The requirements for workmanship are as specifi

21、ed in 3.6.1 Metal defects.- The parts shall be free from cracks, splits or 4 . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-60862 13 W 7799706 O343639 7 W -_I_ _a_-_- . MIL-A -60862(W) 3.6.2 Burr.- The part shall not have a burr which might

22、interfere with - assenibly or function of the item or which might be injurious to personnel handling the. item. 3.6,s Foreign matter.- The pmt or assembly shall not contain chips, dirt, rust, corrosion or other foreign mtter. 4. QUALITY ASSUFANCE PROVISIONS 4.1 Responsibility for inspection. - Unles

23、s otherwise specified in the contract or purchase order, the supplier is responsible for the performance of ali inspection requirements as specified herein. specified in the contract or order, the supplier may use his own or any other facilities suitable for the performance of the inspection requri-

24、ements speci- fied herein, unless disapproved by the Government. The Government reserves the right to perform any of the inspections set forth in the specification where such inspections are deemed necessary to assure supplies and services conform to prescribed requirements. Except as otherwise 4.1.

25、1 Quality assurance tem and definitions.- Reference shall be made to MIL-STD-109 to define quality assurance terms used. 4.1.2 Inspection. - Inspection shall be in accordance with MIL-A-2550 except as specified herein. 4.2 InsDection Drovisions. 4.2.1 Lot, 4.2.1.1 Submission of product.- The product

26、 shall be submitted in - accordance with MIL-STD-105. 4.2.1.2 Size of lot.- A lot shall consist of an identifiable group of assenibled units containing metal pmts assemblies provided the homogeneity of the rebuild process has been retained. accepted cartridges. The assemby shall be loaded with 4.2.2

27、 Examination.- One hundred percent examination shall be performed for all critical defects and defects indicated in paragraph 2.4, a thru i, T.O. llp4-11-3 unless otherwise specified. Examination for major or minor defects shall be performed on a defect basis in accordance with the classifica- tion

28、of defects contained herein, using the sampling plans and criteria in Tables II and III. criteria in Table II shall be used. group, the criteria in Table III shall be used. shall be rejected. visual examination for such defects as burr and foreign matter. For an individual defect (single characteris

29、tic), the All nonconforming material Four power (4X) magnification may be used in performing For total defects within a major or minor Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-60862 13 7777706 03LI1640 3 W MIL* -60862 (MU) 4.2.2.1 Reclai

30、med parts - Examination of reusable parts which require no reprocessing shaU. be limited to inspection of defects that require visual ty-pe inspection. such defects. Ail nonconforming parts shall be rejected. 4.2.2.2 Reprocessed parts.- Examination shall be limited to a visual One hundred percent ex

31、amination shall be performed for all type inspection unless otherwise specified. All nonconforming material shall be rejected. TABLE II Maj or Lot Size Sample Size Accept Reject 1 - 300 io Examination 301 - i300 ll0 1 2 1301 - 3200 150 2 3 3201 - 8000 225 3 4 8001 - 22000 300 4 5 TABLE III Total All

32、owable Defects Per Sample Size SaJirple Sizes for Major Defects Number of Defects 5.n Class 2- 3 4- 7 8 - 19 20 - 43 Over - 43 Sample Sizes for Minor Defects Number of Defects in Class 2- 3 4- 7 8 - 16 Over - 4% 17 - 48 6 110 1 2 3 4 6 110 2 3 4 6 8 150 2 3 4 5 8 150 3 4 5 11 8 2 3 4 5 225 3 4 5 8 1

33、1 225 4 5 8 11 17 Minor Accept Reject 3 4 5 6 300 4 5 7 10 i4 300 5 7 10 i4 20 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-6062 13 = 7797906 0341641 5 _ MIL* -60862(Mu) 4.2.2.3 Clevis, Mounting, Drawing 2218-22 covering a detail of Drawing

34、2218-18 Defect CRITICAL None defined MAJOR 101. 102. 103. Diameter of inline holes 104. Metal defective 105. 106. Surface finish improper 107. Burr 108. Foreign matter Pitch diameter of thread, max. Minor diameter of thread, max. Protective finish inadequate or defective Method of Inspection Gage Ga

35、ge GWZe Visual Visual Visual Visud Visual MINOR None defined 4.2.2.4 Sleeve, Adjusting, Drawing 2218-23 covering a detail of Drawing 2218-18 CRITICAL None defhed . MJOR 101. 102. 103. 104. 105 106. i07 108. Pitch diameter of thread, max. Minor diameter of thread, mx. Metal defective Protective finis

36、h inadequate or defective Lacquer stripe missing Surface finish improper Burr Foreign matter MINOR None defined - .- _ 7 Gage Gage visual Visual Visual Visual Visual Visual . . - Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-60862 33 9997906

37、031-1361-12 7 M MIL-R-60862 (MU) 4.2.2.5 Pube, intermediate, Drawing 2218-29 covering a detail of Drawing 2218-18 Defect Method of Inspection CRITICAL None defined MAJOR 101. Pitch diameter of threads, max., 2 holes 102. 103. Metal defective 104. 105. 106. Surface finish improper 107. Burr 108. Fore

38、ign matter Minor diameter of thread, max. Protective finish inadequate or defective Solid film lubricant inadequate or defective MINOR Gage Gage visual visual Visual visual Visual Visual None defined 4.2.2.6 Tube, Anti-Rotation, Drawing 2218-30 covering a detail of Drawing 22 18 -18 CRITICAL None de

39、fined MLJOR 101. 102. 103. Splines damaged 104. Metal defective 105. 106. 107. Surface finish improper 108. Burr 109. Foreign matter Pitch diameter of threads, max. Minor diameter of thread, max. Protective finish inadequate or defective Solid film lubricant inadequate or defective MINOR None define

40、d 8 Gage Gage Visual Visual Visual Visual Visual Visual Visual . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-bOb2 13 9777706 0343643 7 MIL-R -60862(MU) 4.2.2.7 Tube, Ballnut Adapter, Drawing 2218-31 covering a detail of Drawing 2218-18 Defe

41、ct Method of Inspect ion CRITICAL None defined MKJOR 101. Metal defective 102. 103. 104. Surface finish improper 105. Burr 106. Foreign matter Protective finish inadequate or defective Solid film lubrication inadequate or defective Visual Visual Visual Visual Visual Visual MINOR None defined 4.2.2.8

42、 Tube, Outside, Drawing 2218-34 covering a detail of Drawing 2218-18 CRITICAL None defined 101. 102. 103. 104. 105. Splines damaged 106. Metal defective 107. 108. Surface finish improper 109. Burr 110. Foreign matter Pitch dimeter of large outside thread, min. Major diameter of lazge outside thread,

43、 min. Pitch diameter of small outside thread, min. Major diameter of small outside thread, min. Protective finish inadequate or defective MINOR None defined Gage Gage Gage Gage VisuaL Visual Visual Visual Visual Visual . 9. Provided by IHSNot for ResaleNo reproduction or networking permitted without

44、 license from IHS-,-,-MIL-R -60862 (MU) 4.2.2.9 End Cover, Drawing 2218-38 covering a detail of Drawing 2218-18 Defect Method of Inspection CRITICAL None defined MAJOR 101. Metal defective Visual 102. Protective finish inadequate or defective Visual 103. Surface finish improper Visual 105. Foreign m

45、atter Visual 104. Burr visual MNOR None defined 4.2.2.10 Sleeve, Holder, Drawing 2218-46 covering a detail of Drawing 2 218 -18 CRITICAL None defined 101. 102. 103. Metal defective 104. 105. Surface finish improper 106. Burr 107. Foreign matter Pitch diameter of thread, max, Minor diameter of thread

46、, max. Protective finish inadequate or defective Gage Gage Visual Visual Visual Visual Visual MiNOR None defined 4.2.2.11 Ccrver, Housing, Drawing 2218-54 covering a detail of Drawing 2218-18 CFUT1CA.L None defined . Provided by IHSNot for ResaleNo reproduction or networking permitted without licens

47、e from IHS-,-,- .- . I MIL-R-60862 13 m 7777706 0343645 2 m 4.2.2.11 (Contd) Defect 101. Metal defective 102. 103. Surface finish iqroper 104. Burr 105. Foreign matter Protective finish inadequate or defective ma.-60862 (MU) Method of inspection Visual Visual Visual Visual Visual MINOR None defined

48、4.2.2.12 Gear, Housing, Drawing 2218-75 covering a detail of Drawing 2218-18 CRITICAL None defined MAJOR . 101. 102. 103. 104 105. 106. i07 i08 a 109. Pitch diameter of large inside thread, max. Minor diameterd large inside thread, max. Pitch diameter of outside thread on boss, min. Major diameter o

49、f outside thread on boss, min. Metal defective Protective finish inadequate or defective Surface finish -roper Burr Foreign matter Gage Gage Gage Gage visual visual Visual Visual Visual MINOR None defined 4.2.2.13 Head, Firing, Drawing 2218-87 covering a detail of Drawing 22 18 - 18 CRITICAL None defined 11 Provided by IHSNot for Re