V45 航空仪表 标准查询与下载

NAVY MIL-I-85569 A NOTICE 1-1997 C-10250A/ALR-67(V)型控制指示器

This notice should be filed in front of MIL-I-85569A(AS), dated 20 May 1987

INDICATOR, CONTROL C-10250A/ALR-67(V)

NAVY MIL-I-85083 A NOTICE 1-1997 IP-722F/AVA-1型模拟显示指示器

This notice should be filed in front of MIL-I-S5083A(AS), dated 26 June 1985.

INDICATOR, ANALOG DISPLAY IP-722F/AVA-1

AIR FORCE MIL-PRF-38120 B-1997 EFU-20/A流量和转换速率指示器

This specification covers one type of in-flight refueling rate of flow and fuel transfer indicator, designated EFU-20IA.

INDICATOR, RATE OF FLOW AND TRANSFER EFU-20/A

AIR FORCE MIL-I-38468 A NOTICE 1-1997 GMU-59/A液氧量指示器

This notice should be filed in front of MIL-I-38468A, dated 2 May 1983

INDICATOR, LIQUID OXYGEN QUANTITY, GMU-59/A

SAE ARP1834A-1997 ARP 4761飞机的安全性评价的数字系统和设备使用故障/失效分析

ARP 1834 provides general guidance for the selection, approach to, and performance of various kinds of F/FA of digital systems and equipment. Its prime objective is to present several industry- acceptable, cost-effective methods for identifying, analyzing, and documenting digital-equipment failure modes and their effects. The analysis techniques and considerations presented here are directed to digital-equipment hardware faults and failures exclusively. ARP 1834 is not intended as an exhaustive treatment of the enormously complex process involved in the analytical failure evaluation of complete digital systems, nor as a universally applicable, definitive listing of the necessary and sufficient steps and actions for such evaluation. ARP4761 provides updated methods and processes for use on civil aircraft safety assessment. When analyzing these types of systems, ARP4761 should be used in lieu of the ARP. ARP1834 addresses the following areas of consideration in the preparation and performance of F/FAs for digital equipment: a. Possible Analysis approaches: Top-Down and/or Bottom-Up (Section 3); b. Fault/Failure Modes, as they affect equipment operation and performance (Section 4); c. Fault Monitoring Methodology; Reasons for, types of, and effectiveness (Section 5); and d. Analysis Methods: Preparation for, types of, effectiveness and coverage (Section 6)

Fault/Failure Analysis for Digital Systems and Equipment Use ARP 4761 for Aircraft Safety Assessment

NAVY MS33632 NOTICE 1-1997 两极转数表传感器和每分钟百分比转速表指示器配线图

This notice should be filed in front of MS33632, dated 2 December 1960. MS33632 is inactive for new design and is no longer used, except for replacement purposes.

WIRING DIAGRAM - TWO-POLE TACHOMETER GENERATOR AND PERCENT RPM TACHOMETER INDICATOR

NAVY MIL-I-21685 NOTICE 1-1997 MW-2型旋转拨号式罗盘中继器指示器

MIL-I-21685(AS) is inactive for new design and is no longer used, except for replacement purposes.

INDICATOR, COMPASS REPEATER, ROTATING DIAL, TYPE MW-2

AIR FORCE MIL-I-27247 C NOTICE 1-1997 同步温度指示器

This notice should be filed in fiont of MIL-I-27247Cy dated 20 March 1985.

INDICATOR, TEMPERATURE, SYNCHRO

AIR FORCE MIL-I-9443 D NOTICE 2-1997 MJ-2型发动机排气热电偶温度指示器

This notice should be filed in front of MIL-I-9443D, dated 30 May 1975.

INDICATOR, TEMPERATURE, THERMOCOUPLE, ENGINE EXHAUST, TYPE MJ-2

SAE ARP1665A-1997 飞机接收机和压力骤增测试和测试方法定义

The test procedure applies to the refueling manifold system connecting the receiver aircraft fuel tanks to the refueling source fuel pump(s) for both ground and aerial refueling. The test procedure is intended to verify that the limit value surge pressure specified for the receiver fuel system is not exceeded when refueling from a refueling source which meets the requirements of AS1284 (reference 2). This recommended practice is not directly applicable to surge pressure developed during operation of an aircraft fuel system, such as initiating or stopping engine fuel feed or fuel transfer within an aircraft, or the pressure surge produced when the fuel pumps are first started to fill an empty fuel manifold.

Definition of Pressure Surge Test and Measurement Methods for Receiver Aircraft

AIR FORCE MIL-I-25861 D NOTICE 1-1997 0-4000 PSI完全发光液压压力指示器

This notice should be filed in fiont of MIL-I-25861D(USAF), dated 24 July 1981.

INDICATOR, PRESSURE, HYDRAULIC, 0-4,000 PSI, INTEGRALLY LIGHTED

SAE AIR1812A-1997 环境控制系统寿命周期成本

This report contains background information on life cycle cost elements and key ECS cost factors. Elements of life cycle costs are defined from initial design phases through operational use. Information on how ECS designs affect overall aircraft cost and information on primary factors affecting ECS costs are discussed. Key steps or efforts for comparing ECS designs on the basis of LCC are outlined. Brief descriptions of two computer programs for estimating LCC of total aircraft programs and their use to estimate ECS LCC, are included. The purpose of this document is to provide qualitative information on life cycle cost (LCC) aspects of environmental control systems (ECS) design.

Environmental Control Systems Life Cycle Cost

AIR FORCE MIL-I-7084 A NOTICE 1-1997 0-4,000 PSI液压压力指示器

This notice should be filed in &ont of MIL-I-7084q dated 15 February 1984

INDICATOR, PRESSURE, HYDRAULIC, 0-4,000 PSI

AIR FORCE MIL-I-9343 C NOTICE 1-1997 MJ-1型发动机排气热电偶温度指示器

This notice should be filed in front of MIL-I-9343C, dated 5 April 1985.

INDICATOR, TEMPERATURE, THERMOCOUPLE, ENGINE EXHAUST, TYPE MJ-1

AIR FORCE MIL-I-25091 B NOTICE 1-1997 MA-2型1-7/8 英寸标度盘加压机座舱空气压力指示器

This notice should be filed in front of MTL-I-25091B7 dated 25 March 85.

INDICATOR, CABIN AIR PRESSURE, PRESSURIZED AIRCRAFT, 1-7/8 INCH DIAL, TYPE MA-2

AIR FORCE A-A-59130-1997 频谱分析仪10千赫至50吉赫

This CID outlines the minimum requirements for a programmable spectrum analyzer, with up to 100 Hertz (Hz) resolution bandwidth, which operates in the 10 Kilohertz (KHz) to 50 Gigahertz (GHz) range. The spectrum analyzer's features shall also include in

ANALYZER, SPECTRUM 10 KHZ TO 50 GHZ

AIR FORCE MIL-PRF-27197 D-1997 马赫数和最大允许空速速度指示器

This specification covers nonlighted and integrally lighted combination indicated airspeed (US) and mach number indicators.

INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED

AIR FORCE MIL-PRF-38135 C-1997 AVU-19A型待命指示空速指示器

This specification covers the standby, integrally-lighted, 1 -7/8 inch, round dial pitot static airspeed indicator, designated AW- 19/A.

INDICATOR, INDICATED AIRSPEED AVU-19A, STANDBY

AIR FORCE MIL-I-7112 B NOTICE 2-1997 0 DEG. C至300 DEG. C气缸盖电阻温度指示器

This notice should be filed in fiont of MIL-1-71 12B, dated 8 February 1985.

INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, CYLINDER HEAD, 0 DEG. C TO 300 DEG. C

JJG(民航) 037-1996 ПС11-02无线电高度表测试仪(试行)

Verification Regulation of ПС11-02 Radio Altimeter Calibration Equipment