NAVY MIL-C-81590 (3)-1974 COCKPIT CANOPY SYSTEM FIXED WING SINGLE AND MULTI-PLACE FIGHTER ATTACK AND TRAINER AIRCRAFT GENERAL SPECIFICATION FOR《战斗机 攻击机和航天飞机的座舱天篷系统及固定机翼单层及多层部位总说明书》.pdf

《NAVY MIL-C-81590 (3)-1974 COCKPIT CANOPY SYSTEM FIXED WING SINGLE AND MULTI-PLACE FIGHTER ATTACK AND TRAINER AIRCRAFT GENERAL SPECIFICATION FOR《战斗机 攻击机和航天飞机的座舱天篷系统及固定机翼单层及多层部位总说明书》.pdf》由会员分享，可在线阅读，更多相关《NAVY MIL-C-81590 (3)-1974 COCKPIT CANOPY SYSTEM FIXED WING SINGLE AND MULTI-PLACE FIGHTER ATTACK AND TRAINER AIRCRAFT GENERAL SPECIFICATION FOR《战斗机 攻击机和航天飞机的座舱天篷系统及固定机翼单层及多层部位总说明书》.pdf（2页珍藏版）》请在麦多课文档分享上搜索。

1、c Yb- MIt-C-Bl1590 (3) 15 - 777770b 0427087 O I 9 mL-c-81590 (AS ) Amendment - 3 22 November 1974 MILITARY SPECIFICATION Superseding Amendment 2 20 September 1971 COCKPIT CANOPY SYSTEN, FIXED WING SINGLE TRAINER AIRCRAFT, GENERAL SPECIFICATION FOR AND MULTI-PLACE, FIGHTER , ATTACK, MID This amendmen

2、t forms part ofblilitavy Specification MIL-C-81590(AS) , dated 12 August 1968, and has been approved by the Naval Air Systems Command, Department of the Navy. Paragraph 2.1: Under “Specifications Military“ , insert after “MIL-A-8867“ “MIL-E-9426 - Escape System Testing, Ejection Seat, Ty-pe, Ground

3、and Flight Performance Tests, General Specification for“ Under STANDARDS Military , insert after “MIL-STD-850“ “MILSTD-882 - System Safety Program for Systems and- Associated Subsystems and Equipment, Requirements for Paragraph 3.5. i. 8.6 - 4th line, delete - “ED-592B“ , insert “1311-5928“ Paragrap

4、h 3.6.3.2 - Delete in entirety and substitute the following: “External emergency canopy releases shall be provided on both the left and right sides of the airplane. Controls shall be located to be accessible following a gear-up crash landing, as well as with the airplane in the normal static positio

5、n. In addition, the contTols shall be located at a height not greater than seven (7) feet above ground level with the airplane in normal static landing configuration at a weight equal. to airplane basic weight plus ten (10) percent internal fuel. Airplane basic weight is actual weight empty plus tra

6、pped fuel and oil and all fixed armament and equipment for normal operation,“ FSC-1560 Obtained From GLOBAL ENGINEERING DOCUMENTS 2625 So.Hickory St. Santa Ana, CA 92707 (71 41540-9870: (21 31624-1 216: (800)854-7179 Licensed by Information Handling ServicesProvided by IHSNot for ResaleNo reproducti

7、on or networking permitted without license from IHS-,-,-Paragraph 3.7.3 - 3rd line delete: “Warning or safety stop provisions shall be , . . between the canopy and its mating s t ruo t Ure. It Add new sub-paragraph - “3.7.3.3. Personnel Safety. Warning, safety stop provisions or other positive safet

8、y devioe applications, singly or in combination, shall be incorporated into power actuated canopy systems to preclude injury to personnel from entrapment between the canopr and its mating structure. It Add new paragraph - “3.12 System Safety. System Safety Engineering in accordance with MIL-STD-882

9、requirements shall be applied throughout the oanopy system design phase to ensure the timely identifications of hazards and the initiation of those actions necessary to prevent or oontrol hazards within the Paragraph 4.3.2.3 - 2nd line, after the mords, “Testing pertt, insert “MIL-E-9426 or“ NIL-C-5570 (3) 15 W 777770b 0927090 7 I MIIr-C-81590(AS) Amendment-3 Project No. i56-NO99 .fr U. S. GOVERNM&T PRINTINI OFFICG 1975.603-115/4223 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-