Model: 1-110-520-21

Aircraft Gas Turb Turbine Nozzle

Special Features:

15.525 min 15.54 max in. Od; 5.588 min 5.59 max in. Id support; 20 holes 0.19-32nf 3b thd through nozzle flange on 13.06 in. Nom bolt circle dia; thd holes countersunk 90 degrees by 0.22 in. Nom dia; 3 holes 0.282 min 0.2825 max in. Diameter through nozzle flange on 13.06 in. Nom bolt circle dia; 8 holes 0.34 in. Nom diameter through support on 6.16 in. Nom bolt circle dia; 3 holes 0.19-32nf 3b thd through support on 6.16 in. Nom bolt circle dia; thd holes countersunk 90 degrees by 0.22 in. Nom diameter on vane trailing edge side

Properties:

Overall Length
Between 2.983 inches and 2.988 inches
End Application
T-53 series engines
NSN
2840-00-087-6851
Part Number
1-110-520-21
Description
Nozzle,turbine,aircraft Gas Turb
CAGE
99193

A single stationary item designed for the purpose of directing air at the proper angle and velocity to a rotor, turbine, aircraft gas turbine engine. it has provisions for attaching to a case (3), turbine, aircraft gas turbine engine. it may have an inner support shroud.

Part 1-110-520-21 NSN 2840-00-087-6851

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50585
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:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
132560
UFC:
61410
LTL:
77.5
LCL:
85.0
WCC:
593
TCC:
Z
SHC:
R
ACC:
Construction Materials

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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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