757 Airplane Recovery Document 飞机恢复文件(18)

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17  FIXED TRAILING EDGE  80  HORIZONTAL STABILIZER INSTL 
19  WING TIP INSTAL  83  ELEVATOR INSTL 
31  STRUT ASSY *[1]*[2]  89  HORIZONTAL STABILIZER INSTL 
32  COWL INSTL *[1]*[2]  RADOME ASSY 
33  POWER PLANT INSTL *[1]*[2]  NOSE LANDING GEAR DOOR INSTL 
41  BODY INSTL -SECTION 41  MAIN LANDING GEAR DOOR INSTL 
43  BODY INSTL -SECTION 43  APU DOOR INSTL 
44  BODY INSTL -SECTION 44  TAIL CONE INSTL 

*[1] FOR ROLLS-ROYCE ENGINE *[2] FOR PRATT & WHITNEY ENGINE
1-10-3

STRUCTURAL SECTIONS
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1-10-4 Centerline Diagrams
1.  
This subject shows illustrations for the different fuselage sections and their body stations, for the (Figure 1-12, Figure 1-13, Figure 1-14, Figure 1-15, Figure 1-16, Figure 1-17 and Figure 1-18).

2.  
Centerline diagrams for the wing, horizontal and vertical staibilizer are also provided, see (Figure 1-19, Figure 1-20 and Figure 1-22).

3.  
Diagrams for horzontal stabilizer and vertical fin movement are also shown (seeFigure 1-21 and Figure 1-22).

1-10-4

CENTERLINE DIAGRAMS
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1-10-4

CENTERLINE DIAGRAMS
Page 1-28 Jul 01/2005 D623N004
 

1-10-4

CENTERLINE DIAGRAMS
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1-10-4

CENTERLINE DIAGRAMS
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1-10-4

CENTERLINE DIAGRAMS
Page 1-31 Jul 01/2005 D623N004
 

1-10-4

CENTERLINE DIAGRAMS
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1-10-4

CENTERLINE DIAGRAMS
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1-10-4

CENTERLINE DIAGRAMS
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757

AIRPLANE RECOVERY DOCUMENT
Figure 1-19 WING STATION DIAGRAM

1-10-4

CENTERLINE DIAGRAMS
Page 1-35 Jul 01/2005 D623N004
 

STABILIZER NEUTRAL 
POINT  B STA  BBL  BWL 
1  1926  32  246 
2  1760  56  242 
3  1994  296  274 
4  1925  300  275 
5  1747  61  243 

STABILIZER 48 LEADING EDGE UP 
POINT  B STA  BBL  BWL 
1  1926  32  241 
2  1760  56  248 
3  1996  296  266 
4  1927  300  271 
5  1748  61  251 

1-10-4
CENTERLINE DIAGRAMS
Page 1-36 Jul 01/2005 D623N004
　
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