Model: 856A3276G01

Case Rear Fla Strengthening Ring

Properties:

Overall Length
48.000 inches
Overall Height
0.800 inches
Overall Width
42.000 inches
End Application
Kc-135r aircraft age.
General Description
C/o ring 1; handle 4; bolt 6; 48.000 in. Lg; 42.000 in. W; 0.800 in. Th; required to strengthen low pressure turbine case rear flange during module assembly
NSN
4920-01-157-5894
Part Number
856A3276G01
Description
Strengthening Ring,case Rear Fla
CAGE
58828

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
U
ESD:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
095190
UFC:
49790
LTL:
70.0
LCL:
70.0
WCC:
713
TCC:
Z
SHC:
Z
ACC:
Trailers/Vehicles

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