Model: 1285M66G02

Aircraft Turbine Nozzle Support

Special Features:

Material incoloy 903

Properties:

Inside Diameter
20.586 inches
Overall Length
1.897 inches
Outside Diameter
24.860 inches
Mounting Hole Diameter
Between 0.481 inches and 0.490 inches
Mounting Hole Quantity
23
End Application
Aircraft eng f108
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Support-seal outer hpt sttr.
Material
Nickel alloy
Reference Data And Literature
T.O. 2j-f108-14, fig. 72-41-00-1, ind. 30
NSN
2840-01-187-8178
Part Number
1285M66G02
Description
Support,turbine Nozzle,aircraft
CAGE
58828

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

Part 1285M66G02 NSN 2840-01-187-8178

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:
PN
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
250.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
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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