Model: 9687M92G14

Aircraft Turbine Nozzle Support

Properties:

Inside Diameter
Between 25.035 inches and 25.055 inches
Overall Length
12.568 inches
Outside Diameter
28.233 inches
Mounting Hole Diameter
Between 0.345 inches and 0.346 inches
Mounting Hole Quantity
32
End Application
Engine, aircraft, turbofan, model tf39ge1a
Criticality Code Justification
Agav
Material
Steel
NSN
2840-00-563-9154
Part Number
9687M92G14
Description
Support,turbine Nozzle,aircraft
CAGE
07482

A support used for a nozzle,turbine,aircraft gas turbine engine.

Part 9687M92G14 NSN 2840-00-563-9154

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
51909
FIIG:
A521B0
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:
39.2 X 39.2 X 22.2
Paclk Weight:
148.0000lbs
Item Weight:
68.0000lbs
Item Dim:
034803480145
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
P
SPI No.:
F005639154
SPI Rev.:
B
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:
--
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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