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PART 01 Ç×°ø±â ±¸Á¶Chapter 1_ ±âü ±¸Á¶ ÀÏ¹Ý Airframe Structure General1-1 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 Fuselage2-1 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 Wing3-1 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, Empennage4-1 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 Nacelle5-1 ±â°ü ¸¶¿îÆ®(Engine Mount)5-2 ³ª¼¿(Nacelle) Chapter 6_ ºñÇàÁ¶Á¾°èÅë Flight Control System6-1 ºñÇàÁ¶Á¾°èÅë ÀϹÝ(Flight Control System General) 6-2 ºñÇà 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 System7-1 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 ½Ã½ºÅÛChapter 1_ Ç×°ø±â ¿¬·á°èÅë Aircraft fuel system1-1 ¿¬·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 System2-1 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 System3-1 °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) Chapter 4_ Ç×°ø±â À¯¾Ð°èÅë Aircraft Hydraulic System4-1 °³¿ä(Introduction)4-2 À¯¾Ð°èÅë(Hydraulic Power System)4-3 À¯¾Ð°èÅëÀÇ ±¸¼ºÇ°(Hydraulic System Component)4-4 B 737 NG Ç×°ø±â À¯¾Ð°èÅë(Boeing 737 Next Generation Aircraft Hydraulic System).4-5 Ç×°ø±â °ø¾Ð°èÅë(Aircraft Pneumatic Systems).PART 03 ±âü ±¸Á¶ÀÇ °µµChapter 1_ ºñÇà»óÅÂ¿Í ÇÏÁß Flight Condition and Load1-1 ±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 & Balance2-1 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 ÀÌÇØ2-4 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 Strength3-1 ±¸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 Stability4-1 Àç·áÀÇ ±â°èÀû ¼ºÁú(Mechanical Property of Material) 4-2 ±¸Á¶ÀÇ ¾ÈÁ¤¼º(Structural Stability) Chapter 5_ ±¸Á¶ ½ÃÇè Structure Test5-1 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) ?Âü°í¹®Çå?INDEX