757 Airplane Recovery Document 飞机恢复文件(17)

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17. Vertical Stabilizer
A.  The torque box spars, ribs, and stringers are aluminum. The leading edge panels and inspar skin panels are also aluminum. The trailing edge panels are graphite/kevlar/fiberglass. The rudder is made of graphite/epoxy. The dorsal fin is aluminum and tip is aluminum and kevlar or fiberglass.
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GENERAL DATA
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757

AIRPLANE RECOVERY DOCUMENT
Figure 1-4 COMPOSITE STRUCTURE

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GENERAL DATA
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MATERIALS

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GENERAL DATA
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Figure 1-6 MAJOR STRUCTURAL PARTS OF THE VERTICAL STABILIZER MADE FROM COMPOSITE
MATERIALS

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GENERAL DATA
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1-10-2 General Arrangement
1.  This subject contains 3-views and primary airplane dimensions for the 757-200 and 757-300 models (see Figure 1-7, Figure 1-8, Figure 1-9 and Figure 1-10).
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GENERAL ARRANGEMENT
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757
AIRPLANE RECOVERY DOCUMENT

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GENERAL ARRANGEMENT
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CONFIGURATION

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GENERAL ARRANGEMENT
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1-10-2

GENERAL ARRANGEMENT
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757
AIRPLANE RECOVERY DOCUMENT

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GENERAL ARRANGEMENT
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1-10-3 Structural Sections
1.  This subject shows the different structural sections of the airplane. The structural sections are shown in an exploded form, so that they can be better visualized (see Figure 1-11).

NO.  DESCRIPTION  NO.  DESCRIPTION 
11  WING CENTER SECTION ASSY  46  BODY INSTL -SECTION 46 
12  OUTBOARD WING ASSY  48  BODY INSTL -SECTION 48 
13  INBOARD SPOILER ASSY  49  WING-TO-BODY FAIRING INSTL 
13  OUTBOARD SPOILER ASSY  61  MAIN LANDING GEAR INSTL 
14  INBOARD LEADING EDGE SLAT  62  NOSE LANDING GEAR INSTL 

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STRUCTURAL SECTIONS
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757
AIRPLANE RECOVERY DOCUMENT
Figure 1-11 STRUCTURAL SECTIONS (Continued)

NO.  DESCRIPTION  NO.  DESCRIPTION 
14  OUTBOARD LEADING EDGE SLAT  70  VERTICAL STABILIZER INSTL 
15  AILERON INSTL  73  RUDDER INSTL 
16  INBOARD TRAILING EDGE FLAP  75  DORSAL FIN ASSY 
16  OUTBOARD TRAILING EDGE FLAP  79  VERTICAL STABILIZER TIP INSTL 
　
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