General Flashcards

1
Q

How is the locking feature of the fiber-type locknut obtained?

A

By the use of an unthreaded fiber locking insert.

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2
Q

How is a clevis bolt used with a fork-end cable terminal secured?

A

With a shear nut tightened to a snug fit, but with no strain imposed on the fork and safetied with a cotter pin.

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3
Q

Aircraft bolts with a cross or asterisk marked on the bolthead are

A

standard steel bolts.

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4
Q

Which statement regarding aircraft bolts is correct?

A

In general, bolt grip lengths should equal the material thickness.

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5
Q

Generally speaking, bolt grip lengths should be

A

equal to the thickness of the material which is fastened together.

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6
Q

Self-locking nuts may be used on aircraft provided that

A

the bolt or nut is not subject to rotation.

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7
Q

Unless otherwise specified, torque values for tightening aircraft nuts and bolts relate to

A

clean, dry threads.

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8
Q

Where is an AN clevis bolt used in an airplane?

A

Only for shear load applications.

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9
Q

Unless otherwise specified or required, aircraft bolts should be installed so that the bolthead is

A

upward, or in a forward direction.

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10
Q

When the specific torque value for nuts is not given, where can the recommended torque value be found?

A

AC 43.13-1B.

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11
Q

A fiber-type, self-locking nut must never be used on an aircraft if the bolt is

A

subject to rotation.

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12
Q

A bolt with a single raised dash on the head is classified as an

A

AN corrosion-resistant steel bolt.

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13
Q

A particular component is attached to the aircraft structure by the use of an aircraft bolt and a castle tension nut combination. If the cotter pin hole does not align within the recommended torque range, the acceptable practice is to

A

change washers and try again.

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14
Q

Aircraft bolts are usually manufactured with a

A

class 3 fit for the threads.

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15
Q

Which of these publications contains standards for protrusion of bolts, studs, and screws through self-locking nuts?

A

AC 43.13-1B.

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16
Q

A particular component is attached to the aircraft structure by the use of an aircraft bolt and a castellated tension nut combination. If the cotter pin hole does not align within the recommended torque range, the acceptable practice is to

A

change washers and try again.

17
Q

A bolt with an X inside a triangle on the head is classified as an

A

NAS close tolerance bolt.