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Page Title: RECOMMENDED READING LIST
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COMPOSITE MATERIAL
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Aviation Structural Mechanic (H&S) 3&2 - How airplanes are built and how to maintain them
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CHAPTER 2 AIRCRAFT  HARDWARE  AND  SEALS

Another  type  of  structural  sandwich  construction consists of a low-density balsa wood core combined with  high-strength  aluminum  alloy  facings  bonded  to each side of the core. The grain in the balsa core runs perpendicular  to  the  aluminum  alloy  facings,  and  the core and aluminum facings are firmly bonded together under  controlled  temperatures  and  pressures. The facings in this type of construction carry the major bending loads, and the cores serve to support the facings and carry the shear loads. The outstanding characteristics  of  sandwich  construction  are  strength, rigidity,  lightness,  and  surface  smoothness. RECOMMENDED READING LIST NOTE: Although the following references were current  when  this  TRAMAN  was  published,  their continued  currency  cannot  be  assured.  Therefore,  you need to be sure that you are studying the latest revision. General Advanced Composite Repair Manual,  Tech Order   1-1-690,   Secretary   of   the   Air   Force, Washington, D.C., 1990. Fabrication,  Maintenance,  and  Repair  of  Transparent Plastics, NAVAIR 01-1A-12, Naval Air Systems Command Headquarters, Washington, D.C., 1982. Airspace  Metals–General  Data  and  Usage  Factors, NAVAIR 01-1A-9, Naval Air Systems Command Headquarters,  Washington,  D.C.,  1989. Aircraft  Radomes  and  Antenna  Covers,  NAVAIR 01-1A-22,   Naval   Air   Systems   Command Headquarters,  Washington,  D.C.,  1990. General  Manual  for  Structural  Repair,  NAVAIR 01-1A-1,   Commander,   Naval   Air   Systems Command,   Washington,   D.C.,   15   July   1969, Change 11, 15 August 1989. 1-45

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