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ARP920A
DESIGN AND INSTALLATION OF PITOT-STATIC SYSTEMS FOR TRANSPORT AIRCRAFT
DESIGN AND INSTALLATION OF PITOT-STATIC SYSTEMS FOR TRANSPORT AIRCRAFT
1996-10-01
有效
【范围】 This SAE Aerospace Recommended Practice (ARP) covers the design and installation requirements for pitot-static systems. 1.1 Purpose: The purpose of this Aerospace Recommended Practice is to present recommendations for the design and installation of pitot and static systems for transport type aircraft. This document also makes recommendations for several system configurations and sets forth the acceptable quality control requirements and the means by which they are to be controlled.strRefField
【与前一版的变化】

引用文件/被引文件

Pitot or Pitot-Static Pressure Tubes
Airspeed Tubes - Electrically Heated
Flight Test Procedures for Subsonic Transport Pitot-Static Systems
Maintenance Procedures for Pitot-Static Systems for Transport Aircraft
Airworthiness Standards: Transport Category Airplanes
Advisory Circular - Altimeter and Static System Tests and Inspections
Environmental Test Procedures for Airborne Electronic Equipment
Identification of Pipe

包含图表

TABLE 1
TABLE 2
TABLE 3
TABLE 4
Schematic-Pitot-Syst
Schematic-Pitot-Syst
Drain Hole Cross Sec
FAA Allowable Static
Static Position Erro
Static Position Erro
Normal and Alternate
FIGURE 8
FIGURE 9
formula 1
Geometry of Skin Wav
Typical Curve of Eff
Typical Curve of Eff
The Basic System
formula 2
formula 3
formula 4
formula 5
formula 6
formula 7
formula 8
formula 9
formula 10
formula 11
formula 12
formula 13
formula 14
formula 15
formula 16
formula 17
Variation of Viscous
formula 18
formula 19
formula 20
formula 21
formula 22
formula 23
formula 24
FIGURE B6
formula 25
formula 26
Typical Static Press
formula 27
formula 28
formula 29
formula 30
formula 31
formula 32
formula 33
formula 34
formula 35
formula 36
formula 37
formula 38
FIGURE C1
formula 39
formula 40
formula 41
formula 42
formula 43
formula 44
formula 45
formula 46
formula 47
FIGURE E1
formula 48
formula 49
formula 50
formula 51
formula 52

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