Wooden Aircraft Structures

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Questions and Answers

Which material was among the first used to construct aircraft?

  • Plywood
  • Metal
  • Fabric
  • Wood (correct)

What were most of the airplanes built during World War One constructed of?

  • Wood frames with fabric coverings (correct)
  • Wood frames with metal coverings
  • Metal frames with metal coverings
  • Metal frames with fabric coverings

What was the material of choice for aircraft construction into the 1930s?

  • Metal
  • Plywood
  • Wood (correct)
  • Fabric

Which airplane company designed and developed the bomber named the Mosquito?

<p>De Havilland (D)</p> Signup and view all the answers

What were the airplanes made of that De Havilland produced during the late 1940s?

<p>Spruce, birch plywood, and balsa wood (A)</p> Signup and view all the answers

Which material did Howard Hughes use to construct the Spruce Goose aircraft?

<p>Wood (A)</p> Signup and view all the answers

What was the empty weight of the Spruce Goose aircraft?

<p>300,000 pounds (A)</p> Signup and view all the answers

How many Pratt and Whitney engines powered the Spruce Goose aircraft?

<p>8 engines (C)</p> Signup and view all the answers

What was the altitude at which the Spruce Goose aircraft flew during its taxi tests?

<p>70 feet (D)</p> Signup and view all the answers

What is the current status of wood aircraft production?

<p>Wood aircraft are no longer produced (B)</p> Signup and view all the answers

Which type of wood is typically used for construction and graded based on strength, load carrying ability, and safety?

<p>Softwood (B)</p> Signup and view all the answers

What are the acceptable defects in wood species used for aircraft repair?

<p>Cross grain, wavy grain, hard knots, pitch pockets (B)</p> Signup and view all the answers

What is the mil spec for solid spruce?

<p>Mills 6073 (D)</p> Signup and view all the answers

What is the mil spec for plywood?

<p>Mills P6070B (B)</p> Signup and view all the answers

Where can one purchase wood components for aircraft repair?

<p>Specialty aircraft supply companies (A)</p> Signup and view all the answers

Which one of these is a type of defect that should be rejected in wood?

<p>Compression wood (D)</p> Signup and view all the answers

What are checks?

<p>Longitudinal cracks extending across the annual rings (B)</p> Signup and view all the answers

What are shakes?

<p>Longitudinal cracks usually between two annual rings (D)</p> Signup and view all the answers

What are splits?

<p>Longitudinal cracks caused by artificially induced stress (C)</p> Signup and view all the answers

What is compression wood characterized by?

<p>Excessive growth of summer wood (B)</p> Signup and view all the answers

According to the text, what is the purpose of the AC mentioned?

<p>To outline acceptable methods for aircraft inspection and repair (D)</p> Signup and view all the answers

According to the text, when can the repairs identified in the AC be used for FAA approval of major repairs?

<p>When listed in FAA Form 337 (A)</p> Signup and view all the answers

According to 14 CFR Part 65, what is required for a certificated mechanic to perform work for which they are rated?

<p>Previous performance of the work concerned at an earlier date (A)</p> Signup and view all the answers

According to the text, why should an aircraft constructed or comprised of wood components be placed in a dry, well-ventilated hangar for inspection?

<p>To allow thorough drying of interior sections and compartments (B)</p> Signup and view all the answers

According to the text, what is permissible for light structures using single plywood covering?

<p>Undulation or bulging between panels (A)</p> Signup and view all the answers

Which of the following is a potential indication of deterioration in the plywood and spruce structures of a wooden aircraft?

<p>Contours and alignment of leading and trailing edges (C)</p> Signup and view all the answers

What may be required if there is deterioration in the leading and trailing edges of a wooden aircraft?

<p>Detailed internal inspection (B)</p> Signup and view all the answers

What can cause wood and glue deterioration inside a wooden aircraft structure?

<p>Moisture (A)</p> Signup and view all the answers

Why is glue joint inspection challenging in wooden aircraft structures?

<p>Limited access and difficulty in assessing joint integrity (C)</p> Signup and view all the answers

How can water penetration be detected in a wooden aircraft structure?

<p>Dark gray streaks, discoloration, or corrosion around screws and fittings (A)</p> Signup and view all the answers

Flashcards

Wood in Aircraft

One of the first materials used in aircraft construction.

WWI Airplane Material

Wood frames covered with fabric.

Aircraft Material of Choice (Pre-1940s)

Wood remained the primary material for aircraft until the 1930s.

Mosquito Bomber Designer

De Havilland designed and developed the Mosquito bomber.

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De Havilland Aircraft Materials (1940s)

Spruce, birch plywood, and balsa wood.

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Spruce Goose Material

Wood.

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Spruce Goose Empty Weight

300,000 pounds.

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Spruce Goose Engine Count

8 engines.

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Spruce Goose Flight Altitude

70 feet.

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Current Status of Wood Aircraft

Wood aircraft are no longer produced.

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Wood type for construction

Softwood.

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Acceptable Wood Defects

Cross grain, wavy grain, hard knots, pitch pockets

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Solid Spruce Mil Spec

Mills 6073

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Plywood Mil Spec

Mills P6070B

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Wood Component Source

Specialty aircraft supply companies.

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Wood defect to reject

Compression wood

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Checks (Wood)

Longitudinal cracks extending across the annual rings

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Shakes (Wood)

Longitudinal cracks usually between two annual rings

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Splits (Wood)

Longitudinal cracks caused by artificially induced stress

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Compression Wood

Excessive growth of summer wood

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Purpose of AC

To outline acceptable methods for aircraft inspection and repair.

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AC Repair Approval

When listed in FAA Form 337

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Mechanic's Work Requirement

Previous performance of the work concerned at an earlier date.

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Hangar Ventilation Purpose

To allow thorough drying of interior sections and compartments.

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Acceptable Plywood Bulging

Undulation or bulging between panels

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Deterioration Indication

Contours and alignment of leading and trailing edges.

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Required Action for Deterioration

Detailed internal inspection

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Cause of Wood Deterioration

Moisture

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Challenge in Glue Joint Inspection

Limited access and difficulty in assessing joint integrity.

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Detecting Water Penetration

Dark gray streaks, discoloration, or corrosion around screws and fittings

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Study Notes

Inspection and Repair of Wooden Aircraft Structures

  • Contours and alignment of leading and trailing edges need to be checked for shape deviation, as it indicates deterioration in the plywood and spruce structures.
  • Deterioration in leading and trailing edges may affect the main wing structure, requiring a detailed internal inspection.
  • Splits in fabric covering on plywood surfaces should be investigated to assess the condition of the plywood skin beneath.
  • Moisture can cause wood and glue deterioration inside a structure, even without external indications.
  • Musty or multi-odor during initial inspection indicates moisture, fungal growth, and possible decay inside the aircraft structure.
  • Glue joint inspection in wooden aircraft structures is challenging due to limited access and difficulty in assessing joint integrity.
  • Wood shrinkage caused by temperature and humidity changes can lead to glue joint deterioration, especially in cyclic environments.
  • Glue joint failure can occur due to aging, moisture, mechanical forces, or incorrect application of pressure during manufacturing.
  • Wood decay and dry rot are easily detectable through discoloration, softening, or crushing of the wood.
  • Water penetration can be detected through dark gray streaks, discoloration, or corrosion around screws and fittings.
  • Fabric covering on plywood surfaces provides an indication of the wood condition underneath and should be inspected for cracks or swelling.
  • Mechanical defects, such as compression failures, cracks, or missing/loose attachments, should be checked in structural members and spars.

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