Model: 9511M79G01

Turbine En Compressor Stator Arm

Properties:

End Application
Aircraft eng f101
General Description
Matl titanium alloy per ams 4911; arm 0.553 in. Min and 0.564 in. Max wide by 0.12 in. Min and 0.13 in. Max thick tapered to 0.364 in. Wide by 0.026 in. Min and 0.036 in. Max thick at leg end; vane attaching hole 0.35 in. Min and 0.36 in. Max long by 0.2267 in. Min and 0.2270 in. Max wide; for compressor stator stages 1gv and 3
NSN
3040-01-146-5635
Part Number
9511M79G01
Description
Arm,compressor Stator,turbine En
CAGE
07482

Material Classification

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

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.1000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
Q
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
593
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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