Model: 4070T12P01

Aircra Compressor Blade Retainer

Special Features:

Material steel, ams 5688; any acceptable surface treatment; strength not rated; material hardness rating 60.0 rockwell c min and 72.0 rockwell c max; not casehardened; internal ring style; 90 degree parallel end style; inside diameter 15.562 in. Min and 15.772 in. Max; outside diameter 15.870 in. Min and 16.070 in. Max; cross-sectional shape style rounded corners; major thickness 0.039 in. Min and 0.041 in. Max; external usage design

Properties:

Material
Steel
NSN
2840-01-139-7398
Part Number
4070T12P01
Description
Retainer,compressor Blade,aircra
CAGE
99207

An item specifically designed to position and/or restrain the movement of one or more blade, or blade set, compressor, aircraft gas turbine engine. It may be the full 360 degrees required for one compressor stage or a segment thereof.

Part 4070T12P01 NSN 2840-01-139-7398

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52400
FIIG:
A522S0
Concept No.:
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:
SX
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.5000lbs
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:
194120
UFC:
95100
LTL:
RATING VARIABLE
LCL:
77.5
WCC:
713
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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