Model: 2-100-180-12

Tur Centrifugal Compressor Rotor

Special Features:

36 blades, splined bore, 79 teeth, 3.2917 in. Nom pitch dia, 30 degrees pressure angle

Properties:

General Description
36 blades, splined bore, 79 teeth, 3.2917 in. Nom pitch dia, 30 degrees pressure angle
NSN
2840-00-860-0618
Part Number
2-100-180-12
Description
Compressor Rotor,centrifugal,tur
CAGE
99193

Inc 60245 cancelled/replaced by ,inc 50588, fiig a10700, app-key j ,inc 50587, fiig a10700, app-key j ,on 021513 ~(all except usa). An item consisting of a series of blades on one or both sides of the rotor disk extending from the axis of rotation radially to the rim of the disk. It is designed to centrifugally cause the air between the blades to move outward to the rim of the compressor section of a turbine engine.

Part 2-100-180-12 NSN 2840-00-860-0618

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
60245
FIIG:
A23900
Concept No.:
App. Key:
A
Cond. Code:
2
Status:
C

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:
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
25.5 X 22.5 X 12.0
Paclk Weight:
32.0000lbs
Item Weight:
20.0000lbs
Item Dim:
016501650050
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
SPI No.:
SPI Rev.:
SPC Mkg:
99
LVL_A:
E
LVL_B:
F

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
123270
UFC:
62600
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
593
TCC:
Z
SHC:
9
ACC:
Construction Materials

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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