• Shuffle
    Toggle On
    Toggle Off
  • Alphabetize
    Toggle On
    Toggle Off
  • Front First
    Toggle On
    Toggle Off
  • Both Sides
    Toggle On
    Toggle Off
  • Read
    Toggle On
    Toggle Off
Reading...
Front

Card Range To Study

through

image

Play button

image

Play button

image

Progress

1/14

Click to flip

Use LEFT and RIGHT arrow keys to navigate between flashcards;

Use UP and DOWN arrow keys to flip the card;

H to show hint;

A reads text to speech;

14 Cards in this Set

  • Front
  • Back
A faint line running arcoss the grain of wood spar generally indicates?
Compression failure.
Pin knot clusters are permitted in wood aircraft structure provided?
They produce a small effect on grain direction.
In case of elongated bolt holes in a wood spar or cracks in the vicinity of bolt holes?
A new section of spar should be spliced in or the spar replaced entirely.
Where is information found concerning acceptable species substitutions for wood materials used in aircraft repair?
Ac 43.13-1B
Which statement about wood decay is correct?
Decay is not acceptabe in any form or amount.
Laminated wood spars may be substituted for solid rectangular wood spars?
If the same quality wood is used in both.
Glue deterioration in wood aircraft structures is indicated?
When a joint has separated and the glue surface shows only the imprint of the wood with no wood fibers clinging to the glue.
The I-beam wooden spar is routed to?
Reduce weight.
When patching a plywood skin, abrupt changes in cross-sectional areas which will develop dangerous stress concentration should be avoided by using?
Circular or elliptical patches.
Laminated wood is some times used in the constructuction of highly stressed aircraft components. This wood can be identified by its?
Parallel grain construction.
Which of the following conditions will determine acceptance of wood with mineral streaks?
Careful inspection fails to reveal any decay.
The strength of a well-designed and properly prepared wood splice joint is provided by the?
Glue.
The cantilever wing uses?
No external bracing.
Compression failures in wood aircraft structures are characterized by buckling of the fibers that appear as streaks on the surface?
at right angles to the grain.