AMCR MIDTERMS Flashcards
The most common technique of joining sheets of
aluminum is this. A _____ is a metal pin with a formed head on one end. A
_____ is inserted into a drilled hole, and its shank is then deformed by a hand or
pneumatic tool. ____ create a union at least as strong as the material being
joined.
Rivets
It has been used since sheet metal was first utilized in
aircraft and remains the single most used aircraft fastener today.
Solid Shank Rivet
When a rivet is driven, its cross-sectional area _____ along with its
bearing and shearing strengths.
increases
Rivet Codes that are used today
Air Force - Navy, or AN system,
and the Military Standards 20 system, or MS20.
The two most common rivet head styles
Universal head and Countersunk
What is the code of the universal head
470
What is the code of countersunk
426
These were developed to streamline airfoils and permit a
smooth flow over an aircraft’s wings or control surfaces.
AN426 (countersunk rivets)
before a
countersunk rivet can be installed, the metal must be ________
countersunk or dimpled
It is a process in which the metal in the top sheet is cut away in the
shape of the rivet head.
Countersinking
It is a process that
mechanically “dents” the sheets being joined to accommodate the rivet head.
Dimpling
Rivet Code of a universal head
AN470 - MS20470
Rivet Code of a flat head
AN442
Rivet Code of a roundhead
AN430
Rivet Code of a Brazier Head
AN455
To provide a smooth finish after
the rivet is driven, the protruding rivet head is removed using a ____ . This
rotary cutter shaves the rivet head flush with the skin, leaving an aerodynamically
clean surface.
Microshaver
An alternative to leaving the rivet head sticking up slightly is to use the _________.
Alcoa crown flush rivet
the amount of force that is
needed to cut a rivet into two
Shear Strength
the amount of force that will
cause the rivet to tear out from the metal
Bearing Strength
Rivets made of pure aluminum have no identifying marks on their manufactured head
and are designated by the letter A in the rivet code.
1100 Aluminum (Rivet Code: A)
is the most widely used for manufacturing and maintenance of
modern aircraft. Rivets made of this alloy have a dimple in the center of the head and
are represented by the letters AD in rivet part codes. Because AD rivets are so common
and require no heat treatment, they are often referred to as “field rivets.”
2117 Aluminum Alloy (AD) or 2117-T3
Some aircraft parts are made of magnesium. If aluminum rivets were used on these
parts, dissimilar metal corrosion could result. For this reason, magnesium structures
are riveted with 5056 rivets which contain about 5 percent magnesium. These rivets
are identified by a raised cross on their heads and the letter B in a rivet code.
5056 Aluminum Alloy (B)
the aluminum industry modified 2017 alloy to produce a new version of 2017 aluminum,
called the _________.
crack free rivet alloy
are identified by a raised dot in the center of their head and the letter D in rivet
codes. Because D-rivets are so hard they must be heat treated before they can be used.
2017 Aluminum Alloy (D)
are identified by two raised dashes on their head.
DD-Rivets / 2024 Aluminum Alloy (DD)
This alloy contains zinc as the major alloying ingredient and is precipitation heat-treated.
This alloy is used by the Boeing Airplane Company as a replacement for 2024T31 rivets
in the manufacture of the 767 widebody aircraft.
7050-T73 Aluminum Alloy (E)
Stainless steel rivets are used for fastening corrosion-resistant steel sheets in
applications such as firewalls and exhaust shrouds. They have no marking on their
heads.
Corrosion Resistant Steel (F)
This rivets are identified with two recessed dimples in their heads. They are used in
place of corrosion-resistant steel rivets when their somewhat lower shear strength is
not a detriment.
Monel (M)
used for fastening
steel and titanium alloy.
Titanium (T)
AMS
Aeronautical Material Specifications
AN
Air Force-Navy
AND
Air Force-Navy Design
AS
Aeronautical Standard
ASA
American Standards Association
ASTM
American Society for Testing and Materials
MS
Military Standard
NAF
Naval Aircraft Factory
NAS
National Aerospace Standard
SAE
Society of Automotive Engineers
These rivets are installed with
access to only one end of the rivet.
Special Rivets or Blind Rivets
These rivets have limited use on aircraft and are never used for structural repairs. Useful for temporarily lining
up holes; used in some homebuilt aircraft
Pop Rivets
develop the maximum strength from the sheet metal
as determined by the amount of load that the sheet
metal must carry.
Rivet Layout Pattern
metal sheet will tear out in extreme conditions
If it’s too close to the edge
metal sheet separates; contaminants enter the join
causing corrosion for instance.
If it’s too far from the edge
no closer than _____ rivet shank diameters from
the edge and no further back than _____ diameters
2, 4
the distance between adjacent rivets in a row.
Rivet Pitch