Term 1 of 65
What are the Ailerons, Rudder, and Elevator?
The same thickness as the original metaerial.
The strength of the aircraft structure can be enhanced.
The three Primary flight Control Surfaces of an aircraft
The fuselage, wings, empennage, landing gear, and powerplants.
Term 2 of 65
True or False: Longerons do not run the entire length of the aircraft fuselage.
True
False
Term 3 of 65
How does metrology work?
by continuously measuring dimensions and coordinate points, focusing on the product's
key characteristics.
checking each jet's signature, which makes an aircraft appear on digital detection devices
It interferes with production flow, as the shim needs time to reach green strength.
A chrome conversion coating on aluminum and its alloys
,Term 4 of 65
What is the point at which load would cause an initial indication of a permanent distortion called?
structural members
yield strength
relatively equal
The skin
Term 5 of 65
What is a non flammable, chromic acid based coating chemical?
Liquid and solid
yield strength
Alodine 1201
Damage so severe that the part cannot be restored to its original strength
Term 6 of 65
What do Longer out times allow?
checking each jet's signature, which makes an aircraft appear on digital detection devices
the assembly of larger components and also aid in clean up of unused material
The fuselage, wings, empennage, landing gear, and powerplants.
The property of a metal, which allows little bending, or deformation without shattering
, Term 7 of 65
What are the first steps towards an automated OML control system?
Precise measurement of composite parts
The fuselage, wings, empennage, landing gear, and powerplants.
Longerons, bulkheads, and stringers
The three Primary flight Control Surfaces of an aircraft
Term 8 of 65
What is an example of negligible damage?
Approved changes and improvements to an original aircraft design, which can be in the
form of approval documents or kits that include specially fabricated parts and assemblies
To eliminate gaps, spaces, and differences that may exist between two aircraft parts or
components.
Small dents, scratches, cracks, or holes that can be sanded or hammered out or repaired
without the use of additional material
The property of a metal, which permits it to be permanently drawn, bent, or twisted into
various shape without breaking
Term 9 of 65
What are the parts of an aircraft structure designed to carry loads and or stresses called?
yield strength
A high malleability
structural members
relatively equal
The benefits of buying summaries with Stuvia:
Guaranteed quality through customer reviews
Stuvia customers have reviewed more than 700,000 summaries. This how you know that you are buying the best documents.
Quick and easy check-out
You can quickly pay through credit card or Stuvia-credit for the summaries. There is no membership needed.
Focus on what matters
Your fellow students write the study notes themselves, which is why the documents are always reliable and up-to-date. This ensures you quickly get to the core!
Frequently asked questions
What do I get when I buy this document?
You get a PDF, available immediately after your purchase. The purchased document is accessible anytime, anywhere and indefinitely through your profile.
Satisfaction guarantee: how does it work?
Our satisfaction guarantee ensures that you always find a study document that suits you well. You fill out a form, and our customer service team takes care of the rest.
Who am I buying these notes from?
Stuvia is a marketplace, so you are not buying this document from us, but from seller Americannurse. Stuvia facilitates payment to the seller.
Will I be stuck with a subscription?
No, you only buy these notes for $12.99. You're not tied to anything after your purchase.