Model: 9523M35G01

Turbine En Compressor Stator Arm

Special Features:

T.O. 2j-f110-14; vane activation; 1st and 2nd stages

Properties:

End Application
F101/f110ge129 aircraft eng
General Description
Matl titanium alloy per ams 4911; 1.944 in. Long; vane arm 0.553 in. Min and 0.564 in. Max wide by 0.12 in. Min and 0.13 in. Max thick tapered to 0.398 in. Wide by 0.055 in. Min and 0.065 in. Max thick; vane attaching hole 0.34 in. Min and 0.36 in. Max long by 0.2262 in. Min and 0.2270 in. Max wide
NSN
3040-01-146-5644
Part Number
9523M35G01
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:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
--
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
ZZ
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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