Model: 692506

Aircraft Combustion Chamber Case

Special Features:

Bore 4.000 in. Min & 4.002 in. Max dia; 8 holes 0.220 in. Min & 0.225 in. Max diameter each having boss 0.56 in. Min & 0.68 in. Max dia; holes tapped 0.25-28unf-3b; af to. 2g-gtcp85-54 applies

Properties:

Overall Length
Between 0.614 inches and 0.619 inches
Diameter
Between 9.229 inches and 9.233 inches
Engine Section Location
Turbine
Material
Steel
Material Specification
Ams5385 assn standard single material response
NSN
2840-00-022-7923
Part Number
692506
Description
Case,combustion Chamber,aircraft
CAGE
99193

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

Part 692506 NSN 2840-00-022-7923

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50545
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:
SU
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
4.9000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
ZZ
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
593
TCC:
Z
SHC:
9
ACC:
Trailers/Vehicles

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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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