NAVY MIL-C-46942 (2)-1966 CATAPULT AIRCRAFT EJECTION SEAT M5A1 ASSEMBLY《航空器座椅弹射器M5A1型组件》.pdf
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NAVY MIL-C-46942 (2)-1966 CATAPULT AIRCRAFT EJECTION SEAT M5A1 ASSEMBLY《航空器座椅弹射器M5A1型组件》.pdf
1、* MIL-(2-46942 (MU) AMENDMENT 2 4 October 1966 SUPERSEDING MIL-C-46942 (MU) Amendment 1 3 June 1966 MILITARY SPECIFICATION CATAPULT, AIRCRAFT EJECTION, SEAT, M5A1, ASSEMBLY This amendment forms a part of Military Specification MIL-C-46942 (MU) dated 22 July - -1 1963. 1 Paragraph 3.5.1 Table I Veloc
2、ity at -65O F Delete “48 fpstr and substitute “45 fpatt i i I * Add paragraph: 1t3.5.1.1 Initiation. - The catapult shall be fired by a source delivering an output equal to that of an M3A1 Initiator at the end of I 10 feet of aircraft hose, size No. 4, MS28741, at 70 + 5 F .I1 - - : * Indicates changes, additions, deletions or modifications madeto paragraphs that were not a part of Amendment 1, dated 3 June 1966. custodian: Army - Mu Preparing activity: Army - MU Project No. 1377-Al21 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
