This quiz assesses knowledge in structural maintenance for aircraft, focusing on the installation and removal of fasteners and bolts. It is designed for journeyman level and tests practical skills vital for ensuring aircraft integrity and safety.
Choose the proper nut
Install washers as necessary.
Torque the nut to proper specifications
Ensure the bolt has a proper interference fit
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Concave surface
Convex surface
Curved surface
Flat surface
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One-eighth (⅛) turn
One-quarter (¼) turn
Three-eighths (3/8) turn.
One-half (½) turn
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Point wrenching
Nut plates
Channel.
Barrel.
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Wing
Castle
Plain text
Catellated shear
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Floating and non floating
Aluminum and stainless steel
Interrupted thread and elastic stop
Prevailing torque and free spinning
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Slotted or beam
Nonmetallic insert.
Deformed thread type
Interrupted thread type
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It with a rigid receptacle
It with a floating receptacle
It with a retaining receptacle
The entire camloc fastener assembly
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Install the receptacle.
Install the stud retaining ring
Check the grip length of the stud
Insert the stud assembly into the grommet
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1/16 inch larger than the stud
1/16 inch smaller than the stud.
Equal to the diameter of the stud head.
Approximately the same size as the diameter of the stud shank.
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Grommet.
Cross-pin.
Rigid receptacle
Floating receptacle.
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Using a reamer to up size the hole
Clamping all repair members in place
Holding the drill at a right angle to the surface
Pilot drilling holes through all mating surfaces
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Use only a reamer to finish the holeburrs.
Use only a drill bit to drill the hole to size
Pilot drill the hole and use a reamer to finish
Pilot drill the hole and use a drill bit to upsize.
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Final.
Starting.
Verification.
Combination.
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Be flush with the top of the locking collar
Extend no more than 1/16 inch through the material
Be flush with the back edge of the material thickness
Extend at least 1/16 inch beyond the top edge of the locking collar
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Swaging the collar with an undersized swaging set
Increasing the hammering force needed to swage the collar
Installing temporary fasteners in every other hole before installation
Lightly tapping the hi-shear rivet pin into the hole before swaging the collar
Burrs.
Cracks.
Elongated holes
Premature fatigue failure
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5° parallel with the axis of the hole.
7° parallel with the axis of the hole.
5° perpendicular with the axis of the hole.
7° perpendicular with the axis of the hole.
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Inspect the formation of the collar
Remove the pulling gun from the collar area
Ensure the end of the pin is flush with the end of the collar
Apply a corrosion preventative compound to the stem break off area
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Inconel
Titanium alloy
Corrosion-resistant steel
High-strength aluminum alloy
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The letters IT in front of the TL symbol
The letters IT before the first dash number.
Indented slots stamped on the head of the fastener
The numbers representing the type of sealant required.
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Grip length
Fastener diameter
Material composition
Threads per inch on the pin
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Grip length
Fastener diameter
Material composition
Depth of the injector ports
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Washer fumbling
Over torquing the nut
Corrosion of the mating surface
Mismatch of the pin and material composition
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Ream holes to final size
Determine grip length required
Secure parts to prevent slippage
Determine rivet diameter requirements
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Height is ¼ of the rivet’s diameter; diameter is 1¼ of the rivet’s diameter
Height is ⅜ of the rivet’s diameter; diameter is 1⅜ of the rivet’s diameter
Height is ½ of the rivet’s diameter; diameter is 1½ of the rivet’s diameter
Height is ⅝ of the rivet’s diameter; diameter is 1⅝ of the rivet’s diameter
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Slightly undersized
Oversized to permit proper sleeve formation
Undersized, and then brought up to final size by reaming
To exact size, producing an interference fit in steel structures.
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Inspect it for flushness
Inspect it for looseness
Shave it to meet flush requirements
Check for gaps between the manufacturer’s head and the surface
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Punch.
Hammer.
Pilot drill
Drill bushing fixture
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Diameter of the Jo-bolt
Head style of the Jo-bolt.
Grip length of the Jo-bolt.
Material composition of the Jo-bolt
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Thread protrusion, and core-bolt flushness
Pin break-off position, and tightness of the core bolt
Position of the pin, and position of the locking collar.
Position of the alignment slots, and locking-collar position
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Drill out the pin
Knock out the pin
Remove the sleeve
Drill out the sleeve
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Hold the drill 90 degrees to the surface of the part
Use the diameter drill bit specified in the TO
Do not use unnecessary pressure
Use a drill-bushing
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Work-center standards
Local regulations
Technical orders
Vendor catalog
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One
Two
Three
A nose assembly is required for every diameter
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Grip gauge
Corebolt gauge
Drive nut gauge
Stem break off gauge
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Grip length of the rivet was too long
Grip length of the rivet was too short
Nut plate was clamped too tight during installation
Nut plate was clamped too loosely during installation
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Wire.
Twist.
Cable.
Strand.
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Wire center
Strand center
Lay or twist center
Independent wire-rope center
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Flexible.
Non-flexible.
Vinyl-coated.
Nylon-coated
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Double the time of normal inspection
Follow the normal inspection schedule
One-half the time of normal inspection
Three-quarters the time of normal inspection
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Cable drum assembly
Turnbuckle assembly
Quadrant assembly
Bell-crank unit
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Can be left in service
Must be repaired or replaced
Should be coated with lubricant
Must be tested for broken wires within the kinked area.
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Torch.
Cold chisel
Cable swager
Cutting machine
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¼º.
½º.
¾º.
1º
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One minute.
Two minutes
Three minutes
Four minutes.
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1100–0.
2024-T.
5052–0.
6061-T.
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Corrosion-resistant stainless steel tubing type 304
2024-T aluminum alloy tubing
5052–0 aluminum alloy tubing.
6061-T aluminum alloy tubing
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Quiz Review Timeline (Updated): Mar 21, 2023 +
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