9995M22G07

Aircraft Gas Turbi Turbine Rotor

NSN 2840-01-139-2392

DEMIL
Shelf Life
UOM
NIIN
Demil:
DEMIL/MLI
Shelf Life:
N/A
UOM:
1 EA
NIIN:
011392392

Product Features

Was compressor rotor, axial, turbine engine; dual rotors, 9 stages; high bypass fan

Product Technical Spec.

End Application:
Aircraft eng f108-cf-100
Design Type:
Axial compressor
Criticality Code Justification:
Agav
Engine Section Location:
Compressor
Stage Number:
9
NSN:
2840-01-139-2392
Item Name:
Rotor,turbine,aircraft Gas Turbi
Cage Code:
58828

Cross Referenced Parts

Part Number
Cage
RNCC
RNVC
RNAAC
Status
MSDS
SADC
Part Number:
9995M22G04
Cage Code:
58828
RNCC:
3
RNVC:
2
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
9995M22G01
Cage Code:
07482
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
9995M22G04
Cage Code:
07482
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
9995M22G06
Cage Code:
07482
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
9995M22G06
Cage Code:
58828
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
9995M22G07
Cage Code:
07482
RNCC:
5
RNVC:
9
RNAAC:
ZZ
Status:
A
MSDS:
SADC:
Part Number:
9995M22G01
Cage Code:
58828
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:

Part Identification

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

Part Materials

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
PN
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:
030003000195
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:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
593
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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Pricing & Availability

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Privacy | Terms

Definition Definition of approved item name (AIN): "Aircraft Gas Turbi Turbine Rotor"

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.

MOE Major Organizational Entities

Entity
DSOR
User:
DEPARTMENT OF THE AIR FORCE Dept. of the Air Force
DSOR:
FT
User:
SINGAPORE Singapore
DSOR:
Import / Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

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


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