Model: 2-140-058-11

Turbine Nozzle Ring

Description:

Engine t-55 end item identification.

Properties:

End Application

Engine t-55

General Description

Cres ams5532, rockwell 30t scale 72 min, 91.5 max hardness, 16.265 in.Min, 16.295 in. Max id 1st end, 16.110 in. Nom id 2nd end, 0.170 in. Nomstep lg 2nd end, 16.680 in. Nom od flange 1st end, 0.032 in. Min, 0.040 in.Max flange thk, 1.060 in. Nom o/a h, 21 holes 0.373 in. Min, 0.380 in.Max diameter equally spaced on 1st end od, 0.396 in. Min, 0.400 in. Max lgfrom flange to center of holes

NSN

5365-00-031-9683

Part Number

2-140-058-11

Description

Ring,turbine Nozzle

CAGE

99193

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators

HMIC

PMIC

ESD/EMI

ENAC

MMAC

CRITL

HMIC:

PMIC:

ESD:

MMAC:

CRITL:

Freight Classification

NMFC

UFC

LTL

LCL

WCC

TCC

SHC

ACC

NMFC:

133300

UFC:

63220

LTL:

RATING VARIABLE

LCL:

RATING VARIABLE

WCC:

713

TCC:

SHC:

ACC:

Equipment for Aircraft

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