Model: 9521M13G02

Aircraft Gas Turbine Front Frame

Special Features:

Axial compressor; frame assembly has variable struts

Properties:

End Application
F110 aircraft gas turbine engine
Part Name Assigned By Controlling Agency
Original name case and nozzle assembly, turbine, aircraft
Number Of Variable Guide Vanes
17
Reference Data And Literature
2j-f110-4, fig 1, ind 1
NSN
2840-01-190-9258
Part Number
9521M13G02
Description
Frame,front,aircraft Gas Turbine
CAGE

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 9521M13G02 NSN 2840-01-190-9258

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:
PR
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
46.0 X 46.0 X 16.0
Paclk Weight:
233.0000lbs
Item Weight:
133.0000lbs
Item Dim:
042004200105
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F011909258
SPI Rev.:
E
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:
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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