Wood Structures Flashcards

1
Q

Is any form of decay permitted

A

Any form of decay is not permitted

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2
Q

A faint line running across the grain of a wood spar generally indicates

A

compression failure

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3
Q

In cases of elongated bolt holes in a wood spar or cracks in the vicinity of boltholes…

A

a new section of spar should be spliced in, or the spar replaced entirely

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4
Q

The cantilever wing uses

A

no external bracing

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5
Q

The strength of a well-designed and properly prepared wood splice is provided by the

A

Glue

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6
Q

Laminated wood is sometimes used in the construction of highly stressed aircraft components. This wood can be identified by its

A

parallel grain construction

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7
Q

The I-bean wooden spar is routed

A

to reduce weight

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8
Q

Any wooden member that has been over stressed is subject to which type of failure?

A

Compression

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9
Q

Compression failure in wood aircraft structures are characterized by buckling of the fibers that appear as streaks in the surfaces

A

at right angles to the grain

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10
Q

Laminated wood spars may be substituted for solid rectangular

A

if the same quality wood is used in both

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11
Q

Glue deterioration in wood aircraft structure is indicated

A

when a joint has separated and the glue surfaces shows only the imprint of the wood fibers clinging to the glue

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12
Q

Where is information found concerning acceptable species substitutions for wood materials used in aircraft repairs?

A

AC 43.13-1B

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13
Q

When patching a plywood skin, abrupt changes in cross-sectional areas which develop dangerous stress concentration should be avoided by using

A

circular or elliptical patches

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14
Q

Pin knot clusters are permitted in wood aircraft structures provided

A

they provide a small effect on grain direction

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15
Q

Which of the following condition will determine acceptance of wood with mineral streaks?

A

Careful inspection fails to reveal any decay

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16
Q

Is any amount of decay acceptable

A

Decay is NOT acceptable in any form or amount