Model: 9526M40G01

Aircraft Gas Turbin Turbine Case

Special Features:

Originally case, turbine rotor, turbine engine; 1st stage

Properties:

Overall Length
Between 2.704 inches and 2.714 inches
Diameter
Between 25.780 inches and 25.800 inches
End Application
Aircraft eng f101
Criticality Code Justification
Agav
Engine Section Location
Turbine
Material
Aluminum alloy
Material Specification
Ams4132 assn standard single material response
NSN
2840-01-146-9466
Part Number
9526M40G01
Description
Case,turbine,aircraft Gas Turbin
CAGE
07482

A case that is an integral part of an engine, gas turbine, aircraft, designed to surround and protect a nozzle assembly, turbine, aircraft gas turbine engine.

Part 9526M40G01 NSN 2840-01-146-9466

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50553
FIIG:
A10700
Concept No.:
3
App. Key:
D
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:
JF
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:
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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