Would structures Flashcards

1
Q

What species of wood is used as a standard for strength properties of other species of wood used an aircraft structures

A

Spruce is used as a standard of which all would your compared

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2
Q

Is Northern white pine an acceptable substitute for spruce

A

Yes but only if the pine is larger to make up for it slower strength

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3
Q

Are not allowed in aircraft wood

A

Knots are allowed if within limitations.

Factors that determine if knots are acceptable include the type of not, location, spacing, and number of nights

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4
Q

What type of wood quality must be used in the repair of aircraft structures

A

The wood must be of aircraft quality an equivalent in its original strength or greater

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5
Q

What is the difference between laminated wood and plywood

A

Laminated wood and plywood consist of two or more layers of wood which have been glued together.

Laminated wood has the grain of all layers approximately parallel. The grain of plywood runs 90° with the adjacent ply

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6
Q

What are two types of glue used for Aircraft wood repair

A

They are casein and synthetic resin glue.

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7
Q

What method is used to prepare plywood for bending

A

The wood is soaked in hot water, and then placed in a form until completely dry

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8
Q

What are the results of using insufficient gluing pressure When making a wood join

A

The results will normally be thick glue lines which indicate a week joint

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9
Q

What is recommended clamping pressure for a glued join

A

125 to 150 psi

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10
Q

How long should a wood glue joint be kept under pressure before removing the clamps

A

Depending on the temperature of the curing room.

The curing temperatures are from 70°F and up. Higher temperatures will cause the glue to set faster. To be certain that the glue joint is satisfactory, it is recommended that it remain under pressure at about 85°F for a period of at least seven hours. Full joint strength will develop only after conditioning for at least two days

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11
Q

What are some of the various methods used to apply pressure to joints in aircraft gluing operations

A

Brad’s, nails, screws, clamps, or hydraulic an electrical power pressure

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12
Q

Why does the strength of a scarf joint depend upon the accuracy of the two beveled services

A

Because and inaccurate bevel will reduce the amount of affective glue area

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13
Q

Why is sanding unacceptable and preparing a joint for splicing

A

The dust created from sanding will clog the pores of wood preventing proper penetration of glue

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14
Q

What type of patch is preferred for repair of stressed plywood skin and why

A

A properly prepared and inserted scarf patch is the best repair for plywood, and it is preferred for most skin repairs. It differs from a splayed patch in that the edges are scarfed to a 12 to 1 slope instead of a 5 to 1 slope, and it uses reinforcements under the patch where the glue joint occurs

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15
Q

Are mineral streaks acceptable in aircraft wood

A

Yes, providing careful inspection fails to reveal any decay

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16
Q

How do you inspect for decay and would

A

Visual, odor, tapping, probe, prying

17
Q

How can the moisture content of would be determined

A

Use a moisture meter.

However, the most accurate method is to take a sample of the wood, wet, dry it in an oven at a temperature of 100 to 105°C, re-weigh it, and then compute the moisture content by using the following formula

W1-w2
———— x 100
W2

W1 equals the weight of the wood sample before drying

W2 equals the weight of the wood sample after drawing

18
Q

What area of wood spar may not be spliced

A

It may not be spliced or under the wing attachment fittings, landing gear fittings, engine mount fittings, or lift and interplane strut fittings

19
Q

What type of joint is generally used in splicing structural members in aircraft

A

A scarf joint

20
Q

What is compression wood and why is it not acceptable for aircraft structures

A

high specific gravity and has the appearance of an excessive growth of Summer wood ( Hard, non-porous).

This defect is difficult to recognize and is very detrimental to strength. Reject all material containing compression would

21
Q

What are three forms of wood

A

Solid, ply, and laminate

22
Q

What are two forms of wood that are acceptable for the repair of wood Aircraft skins

A

The plywood and laminated woods are preferred for this application

23
Q

What would be the greatest amount of splices placed into one spar

A

2

24
Q

What is the largest whole diameter that can be repaired in a plywood wings spar when using a fabric patch

A

1 in.