(2)  
Under severe impact loads, it is not desirable for the body gear or nose gear to break free of the airplane. Therefore no structural fuses are incorporated in attaching these gear to the structure.
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A 
747-400 MAINTENANCE MANUAL 
FWD 
SEE A 
LANDING GEAR 
SUPPORT BEAM WING LANDING GEAR AFT TRUNNIONFLAP TRACK 
BEARING 
LANDING GEAR
BEAM UPPER 
PIN CONNECTION
SUPPORT BEAM
CHORD WEB
A 
REAR SPAR 
A 
WING LANDING GEAR 
BEAMFWD FORWARD TRUNNION BEARING 
LOWER CHORD 
LANDING GEAR SUPPORT BEAM 
A 
REAR SPAR GATE FITTING 
LANDING GEAR 
TANGS ON RETAINER
PIN RETAINER - ENSURE 
SUPPORT BEAM 
ENGAGE SLOTS IN PIN
GREASE FITTING 
AND INSERT
STRUCTURAL FUSE -
SUPPORT BEAM 
REAR SPAR
OUTBOARD BEARING PIN 
GATE 
PIN
FITTING 
BEARING RETAINER 
SPHERICAL 
BEARING
HINGE
A-A 
Structural Fuse - Landing Gear Support Beam to Rear Spar Figure 1 
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A
747-400 
MAINTENANCE MANUAL
SEE A 
FORWARD TRUNNION BEARING HOUSING 
STRUCTURAL FUSE -LANDING GEAR TRUNNION BEARING RETAINING NUT 
TRUNNION FORK 
FWD  TRUNNION BEARING  STRUCTURAL FUSE -FORWARD TRUNNION SUPPORT PINS (4 PLACES)  
A 
Structural Fuse - Wing Landing Gear Forward Trunnion
Figure 2
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A
LANDING GEAR 
SUPPORT BEAM
747-400 MAINTENANCE MANUAL 
SEE A 
STRUCTURAL FUSE -TRUNNION AND TRUNNION SLEEVE TO AFT TRUNNION BEARING (2 LOCATIONS EACH GEAR) 
WING GEAR TRUNNION 
FWD 
A
Structural Fuse - Wing Landing Gear Trunnion Bolt 
Figure 3
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 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 起落架 LANDING GEAR 1(22)