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时间:2011-02-12 08:51来源:蓝天飞行翻译 作者:admin
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 Emergency Exits  13 301-399,
 FUSELAGE 06-41-53
 DESCRIPTION AND OPERATION  1 ALL
 General  1 ALL
 Lower Half of the Fuselage.  1 ALL
 Lower Half of the Fuselage  1 ALL
 Lower Half of the Fuselage  16 ALL
 Lower Half of the Fuselage  16 ALL
 Lower Half of the Fuselage  30 ALL
 Upper Half of the Fuselage  37 ALL
 Upper Half of the Fuselage  37 ALL
 Fuselage Upper Section.  44 ALL
 Upper Half of the fuselage  60 ALL
 Upper Half of the Fuselage  67 001-049, 051-099
 06-CONTENTS Page 2
 Aug 01/05 
R
 CES 

 

 CHAPTER 06
__________
 DIMENSIONS AND AREAS
 TABLE OF CONTENTS_________________
 SUBJECT_______  CH/SE/SU________  C_  PAGE EFFECTIVITY____ ___________
 101-149, 151-199
 201-299, 401-499
 Upper Half of the Fuselage  79  301-399,
 Upper Half of the Fuselage  79  ALL
 Aft Fuselage. Tail Section.  85  ALL
 NACELLES AND PYLONS  06-41-54
 DESCRIPTION AND OPERATION  1  ALL
 General  1  ALL
 Left Pylon and Nacelle.  1  ALL
 Right Pylon and Nacelle.  1  ALL
 STABILIZERS  06-41-55
 DESCRIPTION AND OPERATION  1  ALL
 General  1  ALL
 This subject describes the  1  ALL
 positions of access doors and
 panels on the Vertical and
 Horizontal Stabilizer.
 Horizontal Stabilizer  1  ALL
 Lower Surface of the Horizontal  1  ALL
 Stabilizer
 Upper Surface of the Horizontal  1  ALL
 Stabilizer
 Left side of the Vertical  1  ALL
 Stabilizer
 Right side of the Vertical  1  ALL
 Stabilizer
 WINGS  06-41-57
 DESCRIPTION AND OPERATION  1  ALL
 General  1  ALL
 Left wing  1  ALL
 Right Wing  16  ALL

 06-CONTENTS Page 3 Aug 01/05 R CES


 DIMENSIONS AND AREAS - GENERAL - DESCRIPTION AND OPERATION
__________________________________________________________
 1. General
_______
 This chapter defines:

 -Dimensions and areas (Ref. ATA 06-10),
 -Zoning (Ref. ATA 06-20),
 -Stations (Ref. ATA 06-30),
 -Access Provisions (Ref. ATA 06-40).

  1EFF : ALL  1 06-00-00Page 1 1 1 Feb 01/98 1 1 1CES 1


 DIMENSIONS AND AREAS - DESCRIPTION AND OPERATION
________________________________________________
R
 1. General_______ 
R  **ON A/C 001-049, 051-099, 101-149, 201-299, 
R  A. Dimensions and areas 
R  (Ref. Fig. 001) 
R  (1) Wings 
R  (a) Span: 34100 mm (111.8767 ft.) 
R  (b) Area: 122.4 m2 (1317.50 ft.2) 
R  (c) Sweep angle: (at 25% MAC) 24 Deg. 58' 
R  (2) Stabilizers 
R  (a) Datum area of horizontal stabilizer: 
R  31 m2 (333.68 ft.2) 
R  (b) Datum area of vertical stabilizer: 
R  21.5 m2 (231.42 ft.2) 
R  (3) Fuselage 
R  (a) Overhall Length: 37573 mm (123.2710 ft.)> 
R  (b) Datum Length: 31115 mm (102.0833 ft.) 
R  (c) Width: 3950 mm (155.5118 in.) 
R  (4) Landing gear 
R  (a) NLG wheel axis to MLG axis distance: 12640 mm (41.4698 ft.) 
R  (b) L and R MLG center-to-ce,ter distance: 7590 mm (298.8190 in.)

 1EFF : ALL 1 06-10-00Page 1 1 1 May 01/05 1 1 1CES 1


 Dimensions and Areas Figure 001 
R 1EFF : 1 1 1CES  001-049, 051-099, 101-149, 201-299,  1 111 06-10-00 Page 2 May 01/05

 

R **ON A/C 151-199, 401-499,

 A. Dimensions and areas
 (Ref. Fig. 001A)

 (1)
 Wings

 (a)
 Span: 34100 mm (111.8767 ft.)

 (b)
 Area: 122.4 m2 (1317.50 ft.2)

 (c)
 Sweep angle: (at 25% MAC) 24 Deg. 58'

 

 (2)
 Stabilizers

 (a)
 Datum area of horizontal stabilizer:
 31 m2 (333.68 ft.2)


 (b)
 Datum area of vertical stabilizer:


 21.5 m2 (231.42 ft.2)

 (3)
 
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