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Station Definitions Used Herein
标准号：
AIR5924
标准名称： Guidelines for the Integration of Electronic Engine Control Systems with Transport Category Aircraft Systems
同源图形
Typical FADEC System
Example of Thrust vs
Normal Mode Thrust S
Logic for Mode Selec
Altitude Dependent T
Engine Idle Selectio
Example of Multiplie
Thrust Schedule Usin
Thrust Rating Select
Ambient Temperature
Thrust* as a Functio
Moving Thrust Lever
Non-Moving Thrust Le
All Engines Operatin
One Engine Inoperati
Typical Cross-Manifo
Typical Body or Nace
Total Air Temperatur
Non-Aspirated TAT Pr
Engine Inlet Mounted
Typical FADEC Select
Typical Presentation
Typical FADEC Engine
Typical EICAS System
相关图形
Definitions with CAI
GJB 3390-98
Ada语言编程支持环境
Flow Schematic and S
AIR1191A
Performanc
Flow Schematic and S
AIR1191A
Performanc
Boeing 767 Forward a
AIR1673A
Aircraft C
Boeing 767 Forward a
AIR1673A
Aircraft C
Boeing 767 Forward a
AIR1673A
Aircraft C
Boeing 767 Forward L
AIR1673A
Aircraft C
Boeing 767 Forward a
AIR1673A
Aircraft C
FIGURE 3.3.3-1 - LTP
AIR4288
Linear Tok
Basic WDM Architectu
AIR5601
A Guidelin