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NPFC - MIL-DTL-9490

FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR

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Organization: NPFC
Publication Date: 22 April 2008
Status: active
Page Count: 98
scope:

This specification establishes general performance, design, develop, and quality assurance requirements for the flight control systems of manned piloted aircraft. Flight Control Systems (FCS) includes all components used to transmit flight control commands from the pilot or other sources to appropriate force and moment producers. Flight control commands may result in control of aircraft flight path, attitude, airspeed, aerodynamic configuration, ride, and structural modes. Among components included are the pilot's controls, dedicated displays and logic switching, transducers, system dynamic and air data sensors, signal computation, test devices, transmission devices, actuators, and signal transmission lines dedicated to flight control- Excluded are aerodynamic surfaces, engines, helicopter rotors, fire control devices, crew displays and electronics not dedicated to flight control. The interfaces of flight control systems with related subsystems are defined.

intended Use:

This is a general requirements specification applicable to flight control systems and is based upon service experience to date. Deviations to the requirements of the specification may be granted... View More

Document History

April 9, 2019
Flight Control Systems - Design, Installation and Test of Piloted Aircraft, General Specification for
A description is not available for this item.
MIL-DTL-9490
April 22, 2008
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
This specification establishes general performance, design, develop, and quality assurance requirements for the flight control systems of manned piloted aircraft. Flight Control Systems (FCS)...
September 5, 2007
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
October 5, 1992
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
June 6, 1975
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
This specification establishes general performance, design, development and quality assurance requirements for the flight control systems of USAF manned piloted aircraft. Flight control systems (FCS)...
March 9, 1966
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
March 13, 1964
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
This specification covers the general requirements for the design, installation and test of the operating mechanism of all flight control systems for all U, S. Air Force piloted aircraft. In the...
July 18, 1958
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
August 9, 1957
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.

References

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