|
Airbus A220 |
Analysis |
Test Equipment: Wing test system |
|
Airbus A350 |
Analysis |
Mechanical Actuators: Primary flight controls actuation; high-lift, wing trailing edge actuation system (A350-900) |
|
Airbus A400M |
Analysis |
Servoactuators: Fly-by-wire servoactuators for control of primary flight services |
|
Bell 525 Relentless |
Analysis |
Electromechanical Actuators: Primary flight control actuation |
|
Bell Boeing V-22 Osprey |
Analysis |
Servoactuators: Flap, elevator & swashplate actuators |
|
Bell Nexus 4EX |
Analysis |
Electromechanical Actuators: Flight control actuation systems |
|
Bell V-280 Valor |
Analysis |
Rotary Actuators: ; Electromechanical Actuators: ; Automatic Flight Control Systems: Integrated flight control system including flight control computer (FCC) electronics, software, and flight control actuation |
|
Boeing 767 |
Analysis |
Mechanical Actuators: Precision control components; Mechanical Actuators: Leading edge slat actuator, autopilot actuators, refueling boom actuators (KC-46A Pegasus); Rotary Actuators: Inboard/outboard leading edge rotary actuators (KC-46A Pegasus); Mechanical Actuators: Refueling boom actuation system (KC-46A Pegasus); Automatic Flight Control Systems: Stabilizer trim controls, elevator feel system (KC-46A Pegasus); Servovalves: Electro-hydraulic servovalves (KC-46A Pegasus) |
|
Boeing 777 |
Analysis |
Mechanical Actuators: Precision control components |
|
Boeing 787 Dreamliner |
Analysis |
Electromechanical Actuators: Lateral control electronics for control of fly-by-wire & spoiler actuators |
|
Boeing MQ-25 |
Analysis |
Mechanical Actuators: Wing flight control actuation and wingfold actuation systems |
|
Bombardier Challenger 300 series |
Analysis |
Automatic Flight Control Systems: Fly-by-wire spoiler & pitch trim systems, including flight control computers, actuator control electronics, electrohydraulic & electromechanical flight control actuators & pilot controls |
|
COMAC C919 |
Analysis |
Electromechanical Actuators: High lift system |
|
Dynetics X-61A Gremlin |
Analysis |
Electromechanical Actuators: Electromechanical actuation systems for precision motion control for GAV tail fin control, GAV wing deploy and fin control for the attitude-controlled Bullet. |
|
Embraer E-Jet 170/190 series |
Analysis |
Fly-by-Wire Systems: Fly-by-wire control system: flight control computers, hydraulic actuators of the primary surfaces, spoilers, & ground spoilers |
|
Gulfstream G280 |
Analysis |
Electromechanical Actuators: Flight control actuators, high lift system; Automatic Flight Control Systems: Flight control computer |
|
Gulfstream G500 |
Analysis |
Mechanical Actuators: Flap actuation, power drive, transmission components & accessories; Aircraft & Helicopter Controllers: Pilot directional control system, including rudder pedals, sensors & linkages; Automatic Flight Control Systems: High lift system including flight control computers & software |
|
Gulfstream G600 |
Analysis |
Mechanical Actuators: Flap actuation, power drive, transmission components & accessories; Aircraft & Helicopter Controllers: Pilot directional control system, including rudder pedals, sensors & linkages; Automatic Flight Control Systems: High lift system including flight control computers & software |
|
Gulfstream G650 |
Analysis |
Mechanical Actuators: Flap actuators & torque tube driveline connecting hydraulic drive unit |
|
KAI KUH-1 Surion Korean Utility Helicopter |
Analysis |
Test Equipment: Test rig |
|
Lockheed Martin F-35 Lightning II |
Analysis |
Mechanical Actuators: Leading edge flap drive system; primary flight control actuation system (electro-hydrostatic actuation system; and the wingfold actuation system |
|
Northrop Grumman UCAS X-47 |
Analysis |
Automatic Flight Control Systems: Flight control system |
|
Sikorsky S-97 Raider |
Analysis |
Mechanical Actuators: Active vibration actuation |
