Model: 9550M58G20

Aircraft Gas Turbi Turbine Rotor

Special Features:

Used on hpt rotor rear shaft damper sleeve, per new t.O. 2j-f101-590

Properties:

End Application
Aircraft eng f101
Design Type
Axial compressor
Engine Section Location
High pressure turbine
NSN
2840-01-411-3346
Part Number
9550M58G20
Description
Rotor,turbine,aircraft Gas Turbi
CAGE
07482

A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. It consists of disks, blades, hubs, and the like. It is the moving part of a turbine assembly, aircraft gas turbine engine. It has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.

Part 9550M58G20 NSN 2840-01-411-3346

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50591
FIIG:
A10700
Concept No.:
App. Key:
J
Cond. Code:
1
Status:
A

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:
48.1 X 41.1 X 29.4
Paclk Weight:
350.0000lbs
Item Weight:
249.0000lbs
Item Dim:
030003000000
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F011465709
SPI Rev.:
I
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
200.0
WCC:
671
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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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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