Model: 3029T96P01

Aircraf Turbine Rotor Blade Lock

Properties:

Overall Length
Between 0.900 inches and 0.920 inches
Overall Width
Between 0.350 inches and 0.360 inches
Material Thickness
Between 0.036 inches and 0.044 inches
End Application
Engine, acft, model no. J85ge-21
Criticality Code Justification
Agav
Stage Number
1
Material
Steel
Reference Data And Literature
2j-j85-94
NSN
2840-01-005-0182
Part Number
3029T96P01
Description
Lock,turbine Rotor Blade,aircraf
CAGE
99207

An item used to maintain the position of a blade, turbine rotor, aircraft gas turbine engine in the proper place on a disk, turbine, aircraft gas turbine engine. this item eliminates axial movement of the blade.

Part 3029T96P01 NSN 2840-01-005-0182

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50458
FIIG:
A503Q0
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:
U
ESD:
ESD:
MMAC:
OK
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.1000lbs
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:
013120
UFC:
05380
LTL:
100.0
LCL:
--
WCC:
576
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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