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AM-AM
AP-AP
Aerodynamic Smoothness Figure 201 (Sheet 10)
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AR-AR
AIRFLOW
AU-AU
AT-AT
Aerodynamic Smoothness Figure 201 (Sheet 11)
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LOWER BIFURCATIONBIFURCATION
(PERPENDICULAR TO AIRFLOW) (PERPENDICULAR TO AIRFLOW)
AW-AW AX-AX
Aerodynamic Smoothness
Figure 201 (Sheet 12)
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[78]
AZ-AZ
AY-AY
PRESSURE
RELIEF DOOR
ENGINE FLANGE
[81]
1
FAN COWL
BB-BB
BA-BA
Aerodynamic Smoothness Figure 201 (Sheet 13)
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BQ
BC BC AFT STRUT FAIRING
BK-BK
24.4
BD-BD
INCHES THROAT 5 INCHES FROM END
INTERNAL
BNCH CH BG
CRITICAL BN
15 INCHES INTERNAL CRITICAL AREA AREA
BO BG
BOCE
PRIMARY NOZZLE
BF-BF
BP BP
10 INCHES INSIDE CRITICAL AREA
CE BQ
FAN COWL
INLET COWL
THRUST
REVERSER
UPPER
T/R STRUT PLUG
BIFURCATION
FAIRING ASSEMBLY
[82]
[83]
ENGINE
BE
FLANGE
AIRFLOW
FWD
EXAMPLE INBOARD AND OUTBOARD BE [84]
BC-BC 1
BD-BD
PLUG ASSEMBLY
ATTACH BOLT AIRFLOW SLEEVE
OPENING [87] ASSEMBLY
1
[86]
[85]
ENGINE
FLANGE
(EXAMPLE, 16 LOCATIONS) BF-BF
BE-BE
Aerodynamic Smoothness
Figure 201 (Sheet 14)
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BH
CORE COWL
Aerodynamic Smoothness
Figure 201 (Sheet 15)
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(PERPENDICULAR TO AIRFLOW)
(EXAMPLE BOTH SIDES)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：747-400 AMM 飞机维护手册 动力装置 POWER PLANT 2(59)
