NAVY MIL-S-8812 D (1)-1977 STEERING SYSTEM AIRCRAFT GENERAL REQUIREMENTS FOR《飞机转向系统一般要求》.pdf

《NAVY MIL-S-8812 D (1)-1977 STEERING SYSTEM AIRCRAFT GENERAL REQUIREMENTS FOR《飞机转向系统一般要求》.pdf》由会员分享，可在线阅读，更多相关《NAVY MIL-S-8812 D (1)-1977 STEERING SYSTEM AIRCRAFT GENERAL REQUIREMENTS FOR《飞机转向系统一般要求》.pdf（2页珍藏版）》请在麦多课文档分享上搜索。

1、4 .MIL-S-8832D (3) Lb m 7777906 0387773 i.I m I MIL-S-8812D - AMENDMENT 1 11 February 1977 MILITARY SPECIFICATION STEERING SYSTEM: AIRCRAFT, GENERAL REQUIREMENTS FOR This amendment forms a part of Military Specification MIL-S-8812, dated 3 September 1975, and is approved for use by all Departments a

2、nd Agencies of the Depart- ment of Defense. PAGE 2 2.1, Under llSPECIFICATIONS, MILITARY“: Delete: “MIL-C-38999 Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect, Environmental Resisting Removable Crimp Type Contacts, Reliability Assurance Pro gram“ and substitute: “MI L-C-

3、 83723 Connectors, Electrical, (Circular, Environment Resisting), Receptacles and Plugs, General Specification for“. PAGE 7 3.4.2.10, Delete and substitute: “3.4.2.10 Failure mode and malfunction effects. The system design failure mode, (i.e., fail operative, fail-safe inoperative), shall be compati

4、ble with aircraft requirements and as approved by the procuring activity. undesirable steering effects that cannot be overcome by normal and natural application of steering cockpit controls. from these power sources shall not require pilot interpretation and action to disengage the system upon failu

5、re. system shall interfere with the required motion of the rudder pedals, flight controls or prevent shimmy stability. No single electrical or hydraulic failure shall result in The system design failure mode No malfunction of the steering control The steering system shall be so designed that no stee

6、ring ally open selector valve, ground. system malfunction, including a failed hydraulic- can result in turning the wheel(s) when off the THIS DOCUMENT CONTAINCgPAGES _.- FSC 1620 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL- S- 881 2D AMENDMEN

7、T 1 PAGE 9 3.4.8.4: Insert the following first sentence: “Wiring routing shall be such that the wires do not channel water into the connector.“ 3.4.8.5: Change to read: “Connectors. Component external connectors shall be in accordance with MIL-C-83723 (Series III), threaded, self locking. ._ Custodi

8、ans: Navy - AS Air Force - 11 Army - AV Reviewer activities: Amy - AV Air Force - 99 - *U. S. GOVERNMENT. PftlNfiNG OFFICE: l97770&020/1526 Fage 2 of 2 Preparing activity: Air Force - 11 Project No. 1620-0118 - Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-