Model: 4009T25G01

Aircraft Gas Turbine Rear Frame

Properties:

Inside Diameter
15.515 inches
Overall Length
4.524 inches
Outside Diameter
17.000 inches
End Application
Aircraft eng j85
Criticality Code Justification
Abhp and abkv and aarx
Part Name Assigned By Controlling Agency
Original name mainframe and brack
Number Of Variable Guide Vanes
6
Material
Nickel alloy
NSN
2840-00-853-6904
Part Number
4009T25G01
Description
Frame,rear,aircraft Gas Turbine
CAGE
99207

A frame used for and part of the rear section of an aircraft gas turbine engine. May include struts.

Part 4009T25G01 NSN 2840-00-853-6904

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52347
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:
OK
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
20.5 X 20.5 X 12.5
Paclk Weight:
24.2000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000005D64
SPI Rev.:
SPC Mkg:
17
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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