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NACELLE COMPONENT WEIGHT NACELLE CG LOCATION
LBS (KGS) STATION *[1] WL *[2] BL *[2]
INLET COWL 434 (197) 36.5 96.0 0.0
FAN COWL (LEFT ) 91 (41) 77.1 91.2 31.1(L)
FAN COWL (RIGHT) 95 (43) 79.2 90.1 29.7(R)
THRUST REVERSER (LEFT) 773 (351) 121.6 97.8 23.9(L)
THRUST REVERSER (RIGHT) 736 (334) 121.4 97.9 24.3(R)
CORE COWL (LEFT) 78 (35) 180.3 98.4 17.3(L)
CORE COWL (RIGHT) 76 (34) 180.3 100.1 17.1(R)
PRIMARY EXHAUST NOZZLE PLUG 145 (66) 22 (10) 223.0 204.2 100.0 100.0 0.0 0.0
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Figure 2-10 NACELLE COMPONENT WEIGHTS A ND CG (Continued)
NACELLE COMPONENT WEIGHT NACELLE CG LOCATION
LBS (KGS) STATION *[1] WL *[2] BL *[2]
ENGINE - INCLUDES MOUNTS, EBU SYSTEMS, AND FLUIDS 8,101 (3675) 119.9 96.6 0.3(L)
QEC 8,702 (3947) 117.7 96.6 0.3(L)
TOTAL - BELOW STRUT 10,551 (4786) 118.2 96.6 0.3(L)
STRUT - INCLUDES STRUCTURE AND SYSTEMS, WITHOUT AFT STRUTFAIRING 1,270 (576) 164.7 140.8 1.2(L)
*[1] ± 1.0 INCH
*[2] ± 0.05 INCH
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2.10 STRUT FAIRING AND STRUCTURE
2.10.1 Strut Fairing and Structure Description
The strut provides structure to support the forward and aft engine mounts. The lower portion of the strut is exposed to the engine fire zone and is constructed of fireproof material. Provisions for attachment of the forward bootstrap bracket are incorporated in the forward strut bulkhead.
There are three GSE hard points on each side of the strut. These hardpoints are nutplate locations for the aft bootstrap. Two nutplates are for the drag link bracket location and one nutplate fastens the aft bootstrap support brace to the strut.
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