Model: 6030T79G08

Aircraft Gas Turbine Front Frame

Special Features:

Matl ams 2473

Properties:

Overall Length
Between 15.806 inches and 15.814 inches
End Application
Engine, acft, model no. Tf34-ge-100
Criticality Code Justification
Matt and feat and abhp and agav
Material
Nickel alloy
NSN
2840-01-004-8115
Part Number
6030T79G08
Description
Frame,front,aircraft Gas Turbine
CAGE
99207

A frame used for and part of the front section of an aircraft gas turbine engine. May include struts with or without variable guide vanes.

Part 6030T79G08 NSN 2840-01-004-8115

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52345
FIIG:
A522Q0
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:
28.6 X 28.6 X 18.8
Paclk Weight:
68.0000lbs
Item Weight:
44.0000lbs
Item Dim:
026002600161
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F010048115
SPI Rev.:
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:
85.0
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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