Model: 9104M10P07

Aircraft Turbine Blade Retainer

Special Features:

High pressure turbine rotor assembly; 2nd stage; cbore for 29 holes eq sp, 29 pockets

Properties:

Overall Length
0.694 inches
Outside Diameter
Between 22.854 inches and 22.885 inches
End Application
Aircraft eng tf39
Criticality Code Justification
Agav
Stage Number
2
Material
Steel
Reference Data And Literature
2j-tf39-4, fig 59 ind 25
NSN
2840-01-138-5658
Part Number
9104M10P07
Description
Retainer,turbine Blade,aircraft
CAGE
07482

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

Part 9104M10P07 NSN 2840-01-138-5658

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52404
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:
NY
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
26.5 X 26.5 X 20.5
Paclk Weight:
15.0000lbs
Item Weight:
5.0000lbs
Item Dim:
024502450010
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000002E81
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
50.0
WCC:
671
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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Phone: +1 470-231-0824
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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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