Model: 6019T89G12

Aircraft Turbine Nozzle Support

Properties:

Inside Diameter
Between 9.570 inches and 9.580 inches
Overall Length
Between 2.130 inches and 2.190 inches
Outside Diameter
Between 17.067 inches and 17.070 inches
Mounting Hole Diameter
Between 0.190 inches and 0.191 inches
Mounting Hole Quantity
24
End Application
Engine, acft, turbofan, model tf34ge100
Criticality Code Justification
Agav
Material
Steel
NSN
2840-00-596-8825
Part Number
6019T89G12
Description
Support,turbine Nozzle,aircraft
CAGE

A support used for a nozzle,turbine,aircraft gas turbine engine.

Part 6019T89G12 NSN 2840-00-596-8825

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
51909
FIIG:
A521B0
Concept No.:
1
App. Key:
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:
OP
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
20.5 X 20.5 X 6.5
Paclk Weight:
12.5000lbs
Item Weight:
9.0000lbs
Item Dim:
017000250170
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000001D63
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
013535
UFC:
05675
LTL:
77.5
LCL:
77.5
WCC:
593
TCC:
Z
SHC:
Z
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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