NAVY MIL-A-8861 B (1)-1994 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS [Use In Lieu Of NAVY MIL-A-008861 A CANC NOTICE]《飞机强度和刚度飞行载荷》.pdf

《NAVY MIL-A-8861 B (1)-1994 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS [Use In Lieu Of NAVY MIL-A-008861 A CANC NOTICE]《飞机强度和刚度飞行载荷》.pdf》由会员分享，可在线阅读，更多相关《NAVY MIL-A-8861 B (1)-1994 AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS [Use In Lieu Of NAVY MIL-A-008861 A CANC NOTICE]《飞机强度和刚度飞行载荷》.pdf（1页珍藏版）》请在麦多课文档分享上搜索。

1、MIL-A-8861B(AS)AMENDMENT 105 DECEMBER 1994MILITARY SPECIFICATIONAIRPLANE STRENGTH AND RIGIDITYFLIGHT LOADSThis amendment forms a part of MIL-A-8861B(AS), dated7 February 1986, and is approved for use within the Naval Air SystemsCommand, Department of the Navy, and is available for use by allDepartme

2、nts and Agencies of the Department of Defense.PAGE 22.1.1: Delete MIL-D-8706, Data and Tests, Engineering, Contract requirementsfor Aircraft Weapons Systems.2.1.2: Add under “PUBLICATIONS,” first line:NAVYSD-8706 - Design Examinations, Engineering, AircraftWeapons Systems.PAGE 264.2.1: Delete MIL-D-8706 and substitute SD-8706.Custodian:Navy - ASPreparing activity:Navy - AS(Project 1510-N066) AMSC N/A 1of1 FSC 1510DISTRIBUTION STATEMENT A: Approved fov public release, distribution is unlimited.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-