NAVY MIL-C-60810-1969 CATAPULT AIRCRAFT EJECTION SEAT M10 REMANUFACTURED METAL PARTS ASSEMBLY《M10型飞机弹射座椅弹射器的再造金属组装部件》.pdf

1、MIL-C-b0LO 13 m 777770b 0341lb7 3 m 6-/5 - 03 - MIL-C-OO MJ) SUPERSEDING 20 July 196 6 FA-PD-MI -2680 8 July 1965 MILITARY SPECIFICATION CATAPULT, AIRCRAFT EJECTION SEAT: Ml0 REMANUFACTURED METAL PARTS ASSEMBLY 1. SCOPE 1.1 This specification covers Catapult, Aircraft, Ejection Seat, M10, Remanufact

2、ured Metal Parts Assembly. and used in conjunction with other propellant actuated devices in aircrew emergency escape systems. 1.2 Items to be re-worked under this specification to the remanufactured MlO Catapult configuration shall be limited to XM10, XMlOE1 and M10 Catapults. 2, APPcABmDocuMENTs T

3、he assembly will ultimately be loaded 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 MI L-A-2550 MIL-C-5541 STANDARDS Military MIL-STD-io5 MI L-STD-10

4、9 msn-ii67 ,. - Ammunition and Special Weapons, General Specification for - Chemical Films and Chemical Film Materials for Aluminum and Aluminum Alloys - Sampling Procedures and Tables for Inspection by Attributes - Quality Assurance Terms and Definitions - Ammunition Data Card DRAWINGS Munitions Co

5、mmand F8596929 - Catapult, Aircraft Ejection Seat, MlO, Metal Parts Assemby THi$ DNUMENT CONTAINS 17 PAGES, Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-60LO 13 = 9999906 034LLb 5 -8596929 - Box, Packing, Ammunition, for Catapult, MlO - Cont

6、ainer, Ammunition, Fiber, M425 for Catapult, - Inspection Equipment List for Catapult, Aircraft in Fiber Container, M425 Ml0 : Ejection Seat, MlO, Metal Parts Assembly (Copies of specifications, standards, and drawings required by suppliers in connection with specific procurement functions should be

7、 obtained from the procuring activity or as directed by the contracting officer. ) specification to the extent specified herein. 2.2, Other publications,- The foilowing document forms a part of this Unless otherwise indicated. the issue in shall apply. ASA (Application Association, effect on date of

8、 invitation for bids or request for proposai 46.1 - Surface Texture, for copies should be addressed to the American Standards 10 East 40th Street, New York, N.Y. 10016) 3.1 General.- Materials, parts and assemblies shall comply with the re- quirements specified on the applicable drawings and referen

9、ced specifications. 3.2 Hydrostatic pressure,- The components listed in table 1 shall with- stand the corresponding internal pressure for i5 seconds, minimum, without application of any external load None defined. l2 Provided by IHSNot for ResaleNo reproduction or networking permitted without licens

10、e from IHS-,-,-4.2.2.17 (Cont d, MAJOR Defect 101. 102 Metal defective 103. 104. Burr 105. Foreign matter Diameter of undercut on nozzle body, max. Protective finish, inaaequate or defective MINOR 201. 202. Diameter of undercut on nozzle body, min. Cup protruding above groove in nozzle Method of Ins

11、pection Gage Visual Vi sua1 Visual Visual Gage Visual 4.2.2.18 Drawing F8596929. Catapult, Aircraft Ejection Seat, MlO, Metal Parts Assembly, CRIIICAL None defined. MAJOR 101, Any part missing, except as otherwise classified Visual 102. Improper assembly Visual 103. “O“ Ring not lubricated Visual 10

12、4. Thread damaged Visual lO5. Burr Visual 106, Foreign matter Visual MINOR Visual 201. Shipping plug missing 202. Protective finish inadequate or defective Visual 4.2.2.19 Container , Ammunition , Fiber, Drawing 8826681, CRITICAL None defined. None defined. Provided by IHSNot for ResaleNo reproducti

13、on or networking permitted without license from IHS-,-,-MIL-C-60810 13 W 9977706 0341380 6 W MI LC-60810 (MU) 4.2.2.19 (Contd,) Defect MINOR 201. 202. 203. 204. 205, 207. 206. 208. Gap between body and cover, max. Contents loose Metal ends loose or distorted Cut or damaged through all impregnated la

14、yers Marking missing, incorrect or illegible Tape incomplete or badly wrinkled Length of tear tab, min. Color of tape, incorrect . Method of Inspection Manual Manual Manual Visual Visual Visual Visual Visual 4.2.2.20 Box, Packing, Ammunition, Drawing 8826676. CRITICAL None defined. MAJOR None define

15、d. MINOR 201. 202. 203. 204. 205. 206. 207. 208. Contents loose Hardware missing, loose, broken or improperly engaged Strapping missing, loose, broken or improperly assembled Contents of box exposed Box damaged Marking, missing, incorrect or illegible Number of units incorrect Car seal missing, unse

16、aled or improperly positioned Manual Manual and Visual Manual and Visual Visual Visual Visual Visual Visual 4.2.3 Inspection Testing.- The following tests shall be performed 5n accordance with the provisions of- 4.3. Provided by IHSNot for ResaleNo reproduction or networking permitted without licens

17、e from IHS-,-,-mcc-60810 ( MIT) 4.2.3.1 Hydrostatic pressure. - Each component listed in 3.2 sha,ll be subjected to an internalbyrostatic pressure. comply with the requirements of 3.2 shall be cause for rejection of the component. Failure of any component to 4.2.3.1.1 Breech, launcher trunnion.- Eac

18、h breech, launcher trunnion Failure of any component to shall be subjected 00 a hydrostatic pressure. comply with the requirements of 3.2.1 shall be cause for rejection of the component. 4.2,3.2 Air pressure.- Each nozzle assembly shall be subjected to an air pressure test. of 3.3 shall be cause for

19、 rejectLon of the assembly. Failure of any assembly to comply with the requirements 4.2.3.3 Protective finish, Replated components.- The number of specimens and acceptance criteria for protective finish test shall be in accorance with the applicable military standard listed on the brawing, 4.2.3.4 R

20、esidual magnetism.- Each catapult shall be tested for excessive Failure of any unit to comply with 3.6 shall be cause for residual magnetism. rejection of the catapult. 4.2.4 Inspection Equipment .- The examinatzon and tests shall be mad using equipment listed on IEL-8596929. 4.3 Test Methods and Pr

21、ocedures. 4.3.1 Hydrostatic pressure.- Each component listed in 3.2 and 3.2.1 shall be individually mounted in the device, using the fixtures for sealing all openings and subjected to the hyroatatic pressure to determine compliance with the requirements listed in 3.2 and 3.2.1. shall be sealed such

22、that the pressure shall be applied to an area 2$ inches minimum, fromthe open end of the breech and transmit no load to the bottom surface. The breech, launcher trunnion 4.3.2 Air Pressure,- The cup in the nozzle assembly shall be subjected to the air pressure test, as to seal all openings before th

23、e air pressure is applied so that each cup will be subjected equally to the required pressure, The nozzle assembly shall be so placed in the fixture 4.3.3 Protective finish, replated components .- Test procedures for pm- tective finish shall be in accordance with the applicable military standard - “

24、 referenced on the drawing. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-LOBLO 13 W 7777906 03LlLLB2 T W MI -c-60810 (MU) 4.3.4 Residual Magnetism.- The catapult shall be tested for excessive residual magnetism in an area free of local magne

25、tic effects by placing the catapult 6 inches from, and at the same height as the compass, in sinorth- south horizontal position with the compass set in an east-west heading. catapult shall be moved slowly past the compass in a longitudinal direction for its entire length, rotated i80 degrees in the

26、horizontal position and moved slowly back past the compass. The 5. PlU2PARATION FOR DELIVERY 5.1 Facking and marking.- (Level A).- Packing and marking shall be in accordance with dradngs c826676 and 8826681. 5.2 Data cards.- Data card informtion shall be as specified in MIlrSm- 1167. 6. NOTES 6.1 Or

27、dering data.- Procurement documents should specify the title, number and date of this specification. 6.2 A mechanical failure is defined as any deformation or breakage of a part, the occurrence of which is other than a design function. 6.3 When remanufacturing and loading of assembly are performed b

28、y the same facility, the residual magnetism requirement shall be performed on the loaded assembly only. 6.4 Special instructions covering modification, repair and assembly of remanufactured components are as follows: 6.4.1 Nozzle assemblies which do not contain the undercut on the nozzle body shall

29、be modified to contain an undercut of 2.490 - ,010 diameter to a length of 1.0 as shown on drawing F8596944, Section A-A and top view. 6.4.2 The nozzle cups shall be removed from the nozzle assembly and the New nozzle cups shall be nozzle exit port area shall be thoroughly cleaned. assembled in acco

30、rdance with drawing 8596938. 6.4.3 The two-piece steel bottom can shall be replaced with the one-piece impact extruded aluminum can conforming to the requirements of drawing F8597937. 16 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_ MIL-C-bO1O 13

31、 m 7977706 0341183 1 = m-60810 (MU) 6.5 Protective finish. 6.5.1 The remanufactured exterior components are as follows: Motor tube head, drawing F8596937. Head sleeve , drawing F859694.1. Launcher tube, drawing F8596942. Launcher trunnion breech , drawing F859693O 6.5.2 Exposure of base metal on int

32、ernal aluminum components shall be 6.6 Supersession data.- This specification includes the requirements treated with a Chemical Film, Grade A or By Class 1, MTL-C-5541. of Purchase Description FA-PD-MI-2680 dated 8 July 1965. Custodian: Army - MU Preparing activity: Army - MU *? Project No. 1377-A202 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-