Model: 105B1880P2

Aircraft Gas Turbine En Air Seal

Special Features:

T.O. 2j-j79-44, fig 35, ind 15

Properties:

Overall Length
Between 2.900 inches and 2.920 inches
Overall Width
Between 0.360 inches and 0.400 inches
End Application
Aircraft eng j79, j85, t58, t64
Criticality Code Justification
Czbj and abhp and abmk and feat
Part Name Assigned By Controlling Agency
Original name strip, sealing
Engine Section Location
Turbine
Stage Number
3
Material
Titanium alloy
Material Specification
B50t83a mfr ref single material response
NSN
2840-00-869-6965
Part Number
105B1880P2
Description
Seal,air,aircraft Gas Turbine En
CAGE
07482

A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an engine, gas turbine, aircraft. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal.

Part 105B1880P2 NSN 2840-00-869-6965

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50595
FIIG:
A10700
Concept No.:
App. Key:
H
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:
PL
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
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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