Model: 9938M48G05

Turbine En Compressor Stator Arm

Properties:

End Application
Aircraft eng f101
General Description
Matl steel per ams 5643; arm 0.553 in. Min and 0.564 in. Max across tapered to 0.37 in. Across; vane attaching hole 0.34 in. Min and 0.36 in. Max by 0.2262 in. Min and 0.2270 in. Max
NSN
3040-01-146-5649
Part Number
9938M48G05
Description
Arm,compressor Stator,turbine En
CAGE
58828

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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