Model: 1807M15G05

Aircraft Tu Turbine Blade Damper

Special Features:

Original name damper assembly, high pressure turbine rotor-stage 2. Alsopart number g05 added per cid 219639

Properties:

End Application
Aircraft eng tf39
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
High pressure turbine
Stage Number
2
NSN
2840-01-444-6530
Part Number
1807M15G05
Description
Damper,turbine Blade,aircraft Tu
CAGE
07482

A device used to reduce high cycle fatigue on a blade, turbine rotor, aircraft gas turbine engine. it also acts as a seal. it may be of various shapes and cross sections.

Part 1807M15G05 NSN 2840-01-444-6530

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50557
FIIG:
A10700
Concept No.:
App. Key:
A
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:
4.3 X 4.3 X 4.5
Paclk Weight:
1.0000lbs
Item Weight:
0.3000lbs
Item Dim:
001500060013
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000002E01
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

Freight Classification

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