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Airbus A330/340 Flight Control Actuation System Layout
标准号：
AIR4253A
标准名称： Description of Actuation Systems for Aircraft With Fly-By-Wire Flight Control Systems
同源图形
Phase I Hydraulic Sc
Phase J Secondary Se
Phase II Hydraulic S
Phase II Secondary S
Mechanical Schematic
Hydraulic Schematic,
Electrical Interface
YF-16 Horizontal Tai
F-111 SAS Servoactua
F-16 Primary Control
Electrical Interface
F/A-18 A/B/C/D Ailer
F/A-18 A/B/C/D Leadi
F/A-18 A/B/C/D Ailer
F/A-18 A/B/C/D Stabi
F/A-18 A/B/C/D Trail
F/A-18 A/B/C/D Stabi
F-15 S/MTD Stabilato
F-15 S/MTD Aileron/F
F-15 S/MTD Rudder Se
Tornado Control Syst
Tornado Taiileron Ac
Tornado Taileron Act
Tornado Rudder Actua
Tornado Spoiler Actu
Simplified Schematic
SSME TVC Servoactuat
Simplified Schematic
Equalization and Fau
Rudder/Speed Brake G
Rudder/Speed Brake V
LAVI Primary Flight
JAS-39 Canard, Inboa
JAS-39 Electrical Fl
V-22 Flight Control
V-22 Swashplate Actu
V-22 Flaperon Actuat
V-22 Conversion Actu
Saab 2000 Rudder Con
Saab 2000 Rudder Ser
IDF Flaperon, Horizo
B-2 Gust Load Allevi
B-2 FCAS Architectur
B-2 Actuator Loop Cl
C-17 Flight Control
C-17 Primary Flight
C-17 Spoiler Actuati
C-17 Flap Actuation
C-17 Slat Actuation
C-17 Pitch Trim Actu
X-31A Trailing Edge
X-31A Rudder/Canard
X-31A Thrust Vector
X-31A Leading Edge F
Boeing 777 Primary F
Boeing 777 Aileron P
X-29A Flight Control
X-29A Strake Actuato
Airbus A330/340 Fly-
Airbus A330/340 Rudd
N-250 Flight Control
N-250 Outboard Ailer
N-250 Inboard Ailero
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