Model: 9671M05G05

Aircraft Gas Turbine Rear Frame

Special Features:

Used on the low pressure turbine rear assembly

Properties:

End Application
Aircraft eng tf-39
Criticality Code Justification
Feat
Part Name Assigned By Controlling Agency
Original name frame assembly, turbine
Number Of Variable Guide Vanes
8
Reference Data And Literature
T.O. 2j-tf39-4, fig 183
NSN
2840-00-103-0812
Part Number
9671M05G05
Description
Frame,rear,aircraft Gas Turbine
CAGE
07482

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

Part 9671M05G05 NSN 2840-00-103-0812

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:
NY
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
62.5 X 55.5 X 21.0
Paclk Weight:
363.0000lbs
Item Weight:
139.0000lbs
Item Dim:
050005000120
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F004325269
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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