Model: 1-110-520-19

Aircraft Gas Turb Turbine Nozzle

Special Features:

Cres ams5532 and nickel alloy m3602 fscm 91547, 5.588 in.Min, 5.590 in.Max id support, 3 holes 0.2820 in.Min, 0.2825 in.Max diameter through nozzle flange on 13.060 in.Nom bolt circle dia, 20 holes 0.190 in.-32 unc cl 3b thd through nozzle flange on 13.060 in.Nom bolt circle dia, thd holes countersunk 90 degrees by 0.220 in.Nom diameter on vane trailing rough support on 6.160 in.Nom bolt circle dia, 3 holes 0.190 in.-32 unf cl 3b thd through support on 6.160 in.Nom bolt circle dia, thd holes countersunk 90 degrees by 0.220 in.Nom diameter on vane trailing edge side, 2.982 in.Min, 2.987 in.Max o/a lg;

Properties:

End Application
T-53 series engines
NSN
2840-00-570-9803
Part Number
1-110-520-19
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 1-110-520-19 NSN 2840-00-570-9803

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:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
28.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
030660
UFC:
14960
LTL:
70.0
LCL:
70.0
WCC:
576
TCC:
Z
SHC:
5
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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