Model: 1364M25P01

Aircra Turbine Component Support

Properties:

Inside Diameter
Between 15.580 inches and 15.620 inches
Overall Length
Between 2.150 inches and 2.190 inches
Outside Diameter
Between 19.140 inches and 19.200 inches
Mounting Hole Diameter
Between 0.210 inches and 0.218 inches
Mounting Hole Quantity
19
End Application
F110-ge-129 aircraft engine
Criticality Code Justification
Agav
Material
Nickel alloy
NSN
2840-01-368-6236
Part Number
1364M25P01
Description
Support,turbine Component,aircra
CAGE
07482

A support designed for a turbine assembly,aircraft gas turbine engine or one of its components. Excludes support,seal,aircraft gas turbine engine.

Part 1364M25P01 NSN 2840-01-368-6236

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52560
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:
PR
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
--
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
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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