This final part of module 6 assesses knowledge on aircraft maintenance, focusing on structural repairs, corrosion identification, and material properties. It is crucial for understanding safety and operational standards in aerospace engineering.
Pure aluminum tubing
Stainless steel tubing
Aluminum allot tubing
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Fuselage area below the galley and toilet
Cargo floor
Wing leading edge
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A flared tube assembly
A flareless tube assembly
Two check valves.
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Wings
Fuselage
Engine
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Determine the direction of the edge of the fabric
Refer to the structure repair manual
Using the wrap compass
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Bolts and Nuts
Turnbuckles
Locking wires
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Saw tooth serrations
Two or more tabs
Thin metal places
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Turnbuckles
Flareless tube fittings
Easy nuts
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White
Greenish film
Red
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Electrochemical
Fretting
Pitting
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AN-16
AN-18
AN-22
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An inspection hole in the barrel
A groove or knurl on the barrel
The letter “L” stamped on the barrel
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Remove any internal stresses caused by cold working
Prevent the rivets from age hardening
Allow the rivets to age harden
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24.2kg
34.80kg
23.2k
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Use UNC or UNF threads
Are interchangeable with the metric threads
Have BA and BSF threads
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To withstand load from the fibre
To accommodate fibre in a better pattern
To transfer stresses to the fibre
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Increase conductivity and current carrying capacity
Increase cable strength and fatigue resistance
Prevent oxidation and facilitate soldering
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It is a process where the metal is quenched after heat treatment to develop its properties
It is a process where the metal is quenched after heat treatment and left it for some time to develop its properties
It is a process where the metal is left is cooled in still air after heat treatment to develop its properties
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