The phrase "airframe components" is correct and usable in written English.
It can be used in contexts related to aviation, aerospace engineering, or discussions about aircraft structure and parts.
Example: "The maintenance team conducted a thorough inspection of the airframe components to ensure safety and performance standards were met."
Alternatives: "aircraft parts" or "airframe parts".
In addition, Airbus said, using the rudder in alternating directions "can lead to structural loads that exceed the design strength of the fin and other associated airframe components".
Aerospace executives believe the industry in Britain has four strengths that need further multimillion-pound investment to remain world class: wings, engines, electronic systems, and airframe components.
This demonstrated the potential for porosity to cause fatigue cracks in these airframe components during service.
A fatigue lifing framework using a lead crack concept, based on years of detailed inspection and analysis of fatigue cracks in many specimens and airframe components, has been developed by the DSTO for metallic primary airframe components.
A fatigue lifing framework using a lead crack concept has been developed by the DSTO for metallic primary airframe components.
Bombardier's aerospace segment focuses on the design, manufacture, sale, and support of regional airliners, business jets, and utility aircraft and on the fabrication of airframe components and the provision of defense products and services.
DAMAS is quantitatively validated using archival data from a variety of prior high-lift airframe component noise studies, including flap edge/cove, trailing edge, leading edge, slat, and calibration sources.
To this end this paper presents a fatigue crack growth analysis of a helicopter airframe component, that was used as part of a round-robin study into helicopter fatigue, performed using a non-similitude based crack growth law, termed the Generalised Frost Dugdale law.
Tcom of Columbia won a $12.2 million contract from the Navy for aircraft and airframe structural components.
A major consideration during the design of a camera mount on helicopters is needed to ensure that the vibrations produced by the dynamics of the airframe (rotating components) are not amplified.
The control of vibration is important for four reasons: to improve crew efficiency, to improve the comfort of passengers, to improve the reliability of avionic and mechanical equipment, and to improve the fatigue lives of airframe structural components.
