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PART 01 Ç×°ø±â ±¸Á¶
Chapter 1_ ±âü ±¸Á¶ ÀÏ¹Ý Airframe Structure General
1-1 Ç×°ø±â ±¸¼º(Aircraft Composition)
1-2 ±âü ±¸¼º(Airframe Composition)
1-3 ±âü ±¸Á¶ ±â´É(Airframe Structure Function)
1-4 ±âü ±¸Á¶ ÀÀ·Â(Airframe Structural Stress)
1-5 1Â÷ ±¸Á¶¿Í 2Â÷ ±¸Á¶(Primary Structure and Secondary Structure)
1-6 Ç×°ø±â ±¸Á¶ ¼³°è ¹æ½Ä(Aircraft Structure Design Criteria)
Chapter 2_ µ¿Ã¼ Fuselage
2-1 Æ®·¯½º ±¸Á¶(Truss Structure)
2-2 ÀÀ·Â¿ÜÇÇ ±¸Á¶(Stress Skin Structure)
2-3 ¿©¾Ð ±¸Á¶(Pressurization Structure)
2-4 Ç×°ø±â ÃâÀÔ¹®(Door)°ú â(Window)
Chapter 3_ ³¯°³ Wing
3-1 ³¯°³ Çü»ó(Wing Configuration)
3-2 ³¯°³ ±¸Á¶(Wing Structure)
3-3 ³¯°³º¸(Wing Spar)
3-4 ³¯°³ ¸®ºê(Wing Rib)
3-5 ³¯°³ ¿ÜÇÇ(Wing Skin)
Chapter 4_ ²¿¸®³¯°³ Tail Wing, Empennage
4-1 ²¿¸®³¯°³ÀÇ Çü»ó(Empennage Configuration)
4-2 ¼öÆò ²¿¸®³¯°³(Horizontal Tail Wing)
4-3 ¼öÁ÷ ²¿¸®³¯°³(Vertical Tail Wing)
Chapter 5_ ±â°ü ¸¶¿îÆ® ¹× ³ª¼¿ Engine Mount and Nacelle
5-1 ±â°ü ¸¶¿îÆ®(Engine Mount)
5-2 ³ª¼¿(Nacelle)
Chapter 6_ ºñÇàÁ¶Á¾°èÅë Flight Control System
6-1 ºñÇàÁ¶Á¾°èÅë ÀϹÝ(Flight Control System General)
6-2 Á¶Á¾¸é(Flight Control Surface)
6-3 ºñÇàÁ¶Á¾°èÅëÀÇ °Ë»ç¿Í Á¤ºñ(Flight Control System Inspection and Maintenance)
Chapter 7_ Ç×°ø±â Âø·úÀåÄ¡°èÅë Aircraft Landing Gear System
7-1 Âø·úÀåÄ¡ÀÇ Çü½Ä(Landing Gear Type)
7-2 Âø·úÀåÄ¡ÀÇ Á¤·Ä(Landing Gear Alignment)
7-3 Ç×°ø±â Á¦µ¿ÀåÄ¡°èÅë(Aircraft Brake System)
7-4 Ç×°ø±â ¹ÙÄû¿Í ŸÀ̾î(Aircraft Wheel and Tire)
PART 02 Ç×°ø±â ½Ã½ºÅÛ
Chapter 1_ Ç×°ø±â ¿¬·á°èÅë Aircraft fuel system
1-1 ¿¬·á°èÅëÀÇ ±âº»ÀûÀÎ ±¸ºñ ¿ä°Ç(Basic fuel system requirement)
1-2 Ç×°øÀ¯ÀÇ Á¾·ù(Type of Aviation Fuel)
1-3 Ç×°ø±â ¿¬·á°èÅë(Aircraft Fuel System)
1-4 ¿¬·á°èÅë ±¸¼ºÇ°(Fuel System Component)
1-5 ¿¬·á°èÅëÀÇ ¼ºñ½Ì(Fuel System Servicing)
Chapter 2_ °´½Ç ȯ°æ Á¦¾î°èÅë Cabin Environmental Control System
2-1 Ç×°ø±â »ê¼Ò°èÅë(Aircraft Oxygen System)
2-2 Ç×°ø±â ¿©¾Ð°èÅë(Aircraft Pressurization System)
2-3 °ø±âÁ¶È°èÅë(Air Conditioning System)
2-4 Ç×°ø±â °¡¿±â(Aircraft Heater)
Chapter 3_ Á¦ºù ¹× Á¦¿ì°èÅë Ice and Rain Protection System
3-1 °áºù Á¦¾î°èÅë(Ice Control System)
3-2 ¹æºù°èÅë(Anti-icing System)
3-3 Á¦ºù°èÅë(De-icing System)
3-4 Áö»ó Ç×°ø±â Á¦ºùÀÛ¾÷(Ground De-icing of Aircraft)
PART 03 ±âü ±¸Á¶ÀÇ °µµ
Chapter 1_ ºñÇà»óÅÂ¿Í ÇÏÁß Flight Condition and Load
1-1 ±âüÀÇ ÇÏÁß(Airframe Load)
1-2 ¼Óµµ-ÇÏÁß¹è¼ö ¼±µµ(V-n Diagram)
1-3 ÇÏÁß¹è¼ö¿Í ¾ÈÀü°è¼ö(Load Factor and Safety Factor)
1-4 Ç×°ø±â ±âü¿¡ ÀÛ¿ëÇÏ´Â ÇÏÁß(Affecting Load to Airframe)
Chapter 2_ Áß·®°ú ÆòÇü Weight & Balance
2-1 Áß·®°ú ÆòÇü ÀϹÝ(General)
2-2 Áß·®°ú ÆòÇü°ü¸® ÀÌ·Ð(Weight and Balance Management Theory)
2-3 Áß·®°ú ÆòÇü°ü¸® ¿ë¾î(Weight & Balance Terminology)ÀÇ ÀÌÇØ
2-4 Áß·®°ú ÆòÇüÃøÁ¤Àåºñ(Weight and Balance Equipment)
2-5 ¿þÀ×ÀÛ¾÷(Weighing) ½Ã Áغñ ¹× ¾ÈÀüÀýÂ÷
2-6 ¹«°ÔÁß½É(C.G) °è»ê
2-7 ´ëÇü Ç×°ø±âÀÇ Áß·®°ú ÆòÇü(Weight and Balance for Large Airplane)
Chapter 3_ ºÎÀçÀÇ °µµ Material Strength
3-1 ±¸Á¶ ÇÏÁß(Structure Load)
3-2 ±¸Á¶ ºÎÀç¿Í ³»·Â(Structural Member and Proof Stress)
3-3 Èû°ú ¸ð¸àÆ®(Force and Moment)
3-4 ÆòÇü¹æÁ¤½Ä(Equation of Equilibrium)
3-5 ºÎÀçÀÇ °µµ(Material Strength)
Chapter 4_ °µµ¿Í ¾ÈÁ¤¼º Strength and Stability
4-1 Àç·áÀÇ ±â°èÀû ¼ºÁú(Mechanical Property of Material)
4-2 ±¸Á¶ÀÇ ¾ÈÁ¤¼º(Structural Stability)
Chapter 5_ ±¸Á¶ ½ÃÇè Structure Test
5-1 ÀϹݻçÇ×(General)
5-2 Á¤ÇÏÁß ½ÃÇè(Static Load Test)
5-3 ³«ÇÏ ½ÃÇè(Drop Weight Test)
5-4 ÇÇ·Î ½ÃÇè(Fatigue Test)
5-5 Áö»ó Áøµ¿ ½ÃÇè(Ground Vibration Test)
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