Model: 3013676

Tur Centrifugal Compressor Rotor

Special Features:

Titanium alloy, ams4298, 26 blades, 9.342 in. Min, 9.346 in. Max od, 6holes 0.320 in. Min, 0.322 in. Max diameter on 3.000 in. Nom bolt circle dia.

Properties:

General Description
Titanium alloy, ams4298, 26 blades, 9.342 in. Min, 9.346 in. Max od, 6holes 0.320 in. Min, 0.322 in. Max diameter on 3.000 in. Nom bolt circle dia
NSN
2840-00-080-7856
Part Number
3013676
Description
Compressor Rotor,centrifugal,tur
CAGE
00198

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 3013676 NSN 2840-00-080-7856

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:
12.4 X 12.4 X 5.0
Paclk Weight:
8.1000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
SPI No.:
SPI Rev.:
SPC Mkg:
LVL_A:
LVL_B:

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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