UNLIMITED FREE
ACCESS TO THE WORLD'S BEST IDEAS

SUBMIT
Already a GlobalSpec user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your GlobalSpec Experience

Select Your Free Newsletters

Industry Newsletters

Select Your Free Product Alerts

Finish!
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

NPFC - MIL-F-9490

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

inactive
Buy Now
Organization: NPFC
Publication Date: 5 September 2007
Status: inactive
Page Count: 1

Document History

MIL-DTL-9490
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)...
MIL-F-9490
September 5, 2007
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-F-9490
October 5, 1992
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-F-9490
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)...
MIL-F-9490C (1)
March 9, 1966
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-F-9490C
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...
MIL-F-9490
July 18, 1958
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
MIL-F-9490B
August 9, 1957
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
A description is not available for this item.
View Less
View All

References

This document references:
MIL-A-8860 - Airplane Strength and Rigidity, General Specification for
Published by NPFC on June 24, 2019
A description is not available for this item.
This document references:
MIL-A-8865 - Airplane Strength and Rigidity Miscellaneous Loads
Published by NPFC on June 24, 2019
A description is not available for this item.
This document references:
MIL-A-8870 - Airplane Strength and Rigidity Vibration, Flutter, and Divergence
Published by NPFC on June 11, 2019
A description is not available for this item.
This document references:
NAS516 - FITTING, LUBRICATION, .1250 INCH DRIVE, FLUSH TYPE
Published by AIA/NAS on December 6, 2019
A description is not available for this item.
This document is referenced by:
DEF STAN 00-970: PT1 SEC3 - Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 3: Structure
Published by MODUK on July 13, 2015
INTRODUCTION This section specifies the requirements for structural strength of the aircraft. Requirements are provided to cover the following aspects: Static Strength and Deformation Fatigue...
View Less
View All
Advertisement