Model: 9671M05G42

Aircraft Gas Turbine Rear Frame

Special Features:

Used on the low pressure turbine

Properties:

End Application
Aircraft eng tf39
Criticality Code Justification
Feat
Part Name Assigned By Controlling Agency
Original name frame, rear, aircraft gas turbine engine
Number Of Variable Guide Vanes
8
Reference Data And Literature
T.O. 2j-tf39-4, fig 63, ind 149
NSN
2840-01-024-6640
Part Number
9671M05G42
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 9671M05G42 NSN 2840-01-024-6640

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:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
61.2 X 57.7 X 26.2
Paclk Weight:
381.0000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F011526309
SPI Rev.:
G
SPC Mkg:
ZZ
LVL_A:
LVL_B:

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:
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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