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CHAPTER 55 Stabilizers
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A = Added, R = Revised, D = Deleted, O = Overflow, C = Customer Originated Change 55-EFFECTIVE PAGES Page 1 D633W101-BEJ May 05/2004
CHAPTER 55 Stabilizers
CH-SC-SU Subject Page Effectivity 55-00-00 STABILIZERS -HORIZONTAL STABILIZER 2 BEJ ALL 55-00-00 STABILIZERS -VERTICAL STABILIZER 4 BEJ ALL
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777 AIRCRAFT MAINTENANCE MANUAL
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Page 1 D633W101-BEJ Jan 05/2002
STABILIZERS -HORIZONTAL STABILIZER
General The horizontal stabilizer is made of solid laminate carbon fiber reinforced plastic. Separate skin panels cover these areas: * Auxiliary spar-to-front spar
* Front spar-to-rear spar
* Rear spar-to-trailing edge.
The auxiliary box structure is aluminum. The horizontal stabilizer also has secondary structures attached to it. The secondary structures include: * Leading edge
The leading edge is aluminum. The elevator and tip fairing are composite. 55-00-00-001 EFFECTIVITY BEJ ALL 55-00-00 Page 2 D633W101-BEJ Sep 05/2002
777 AIRCRAFT MAINTENANCE MANUAL
STABILIZERS -HORIZONTAL STABILIZER
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STABILIZERS -VERTICAL STABILIZER
General The vertical stabilizer is made of solid laminate carbon fiber reinforced plastic. Separate skin panels cover these areas: * Auxiliary spar-to-front spar
* Front spar-to-rear spar
* Rear spar-to-trailing edge.
The auxiliary box structure is aluminum. These secondary structures attach to the vertical stabilizer: * Leading edge
The secondary structures are made of composite materials except for the leading edge and rudder hinge. 55-00-00-002 EFFECTIVITY BEJ ALL 55-00-00 Page 4 D633W101-BEJ Sep 05/2002 BOEING PROPRIETARY -Copyright # -Unpublished Work -See title page for details.
777 AIRCRAFT MAINTENANCE MANUAL
STABILIZERS -VERTICAL STABILIZER
55-00-00-002 EFFECTIVITY BEJ ALL 55-00-00 Page 5 D633W101-BEJ Jan 05/2002
