Model: 815686

Aircraft Gas Tur Compressor Case

Special Features:

This is a redesigned case featuring a reinforced 6th stator support land; replaces p/n 454832

Properties:

Overall Length
Between 18.028 inches and 18.032 inches
Diameter
Between 35.433 inches and 35.443 inches
End Application
Tf33 aircraft gas turbine eng
Design Type
Axial compressor
Hardness Rating
26.0 rockwell c and 32.0 rockwell c
Criticality Code Justification
Abhp and abmz and feat and czbj
Part Name Assigned By Controlling Agency
Original name case, front compressor
Engine Section Location
Compressor
Material
Steel
Material Specification
Ams6415 assn standard single material response
Reference Data And Literature
T.O. 2j-tf33-44, fig 11, ind 1; 2j-tf33-14, fig 13, ind 1
NSN
2840-01-458-2761
Part Number
815686
Description
Case,compressor,aircraft Gas Tur
CAGE
77445

A case that is an integral part of an engine, gas turbine, aircraft, designed to surround and protect a rotor, compressor, aircraft gas turbine engine.

Part 815686 NSN 2840-01-458-2761

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50547
FIIG:
A10700
Concept No.:
3
App. Key:
D
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:
RV
CRITL:
Y

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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