Model: 6013T63P02

Aircraft Turbine Nozzle Support

Properties:

Inside Diameter
Between 16.517 inches and 16.519 inches
Overall Length
Between 2.528 inches and 2.530 inches
Outside Diameter
Between 17.682 inches and 17.686 inches
Mounting Hole Diameter
Between 0.042 inches and 0.046 inches
Mounting Hole Quantity
60
End Application
Acft.Eng. T64-100
Criticality Code Justification
Agav
Material
Nickel alloy
NSN
2840-01-245-2835
Part Number
6013T63P02
Description
Support,turbine Nozzle,aircraft
CAGE
99207

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

Part 6013T63P02 NSN 2840-01-245-2835

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:
PL
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
6.2000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

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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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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