Model: 703173

Aircraft Gas Tur Compressor Case

Special Features:

Hardness rate rockwell c25-33 or equiv.

Properties:

Diameter
58.200 inches
End Application
Tf33-pw-102 turbine fan jet engine, kc-135 aircraft
Design Type
Axial compressor
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Case rear compressor, inner
Engine Section Location
Compressor
Material
Stainless steel
Reference Data And Literature
T.O.2j-tf33-34 fig 14, ind 1
NSN
2840-01-160-7250
Part Number
703173
Description
Case,compressor,aircraft Gas Tur
CAGE
77445

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

Part 703173 NSN 2840-01-160-7250

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50547
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:
RV
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
36.5 X 36.5 X 16.5
Paclk Weight:
58.0000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F009663003
SPI Rev.:
C
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
671
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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