Model: 2-141-057-17

Turbine Eng Turbine Disk And Hub

Special Features:

Cres, m3603, fscm 91547, rockwell a scale 69 min, 73 max hardness, 3.805 in. Min, 3.815 in. Max o/a lg, 9.820 in. Nom od disk, 1.394 in.Min, 1.397 in. Max lg disk, 60 blade grooves equally spaced on diskod, 2 stepped hubs, 2.830 in. Min, 2.840 in. Max od 1st step 1st end, 0.700 in. Nom lg 1st step 1st end, 3.320 in. Nom diameter 2nd step 1stend, 0.603 in. Min, 0.607 in. Max lg 2nd step 1st end, externalsplines 1st step 2nd end, 69 teeth, 30 degrees pressure angle, 2.8750 in.Nom pitch dia, 0.380 in. Min, 0.420 in. Max lg splines, 0.681 in.Min, 0.738 in. Max lg 2nd step 2nd end, stepped bore, 3.805 in. Min, 3.815 in. Max o/a lg bore, 2.5576 in. Min, 2.5579 in. Max diameter 1ststep 1st end, 0.950 in. Nom lg 1st step 1st end, 2.566 in. Min, 2.576 in. Max diameter 2nd step 1st end, 0.600 in. Nom lg 2nd step 1stend, 2.2133 in. Min, 2.2137 in. Max diameter 1st step 2nd end, 0.275 in.Min, 0.295 in. Max lg 1st step 2nd end, 2.425 in. Min, 2.435 in. Maxdia 2nd step 2nd end, 0.165 in. Min, 0.205 in. Max lg 2nd step 2ndend, internal splines 3rd s

Properties:

General Description
Cres, m3603, fscm 91547, rockwell a scale 69 min, 73 max hardness, 3.805 in. Min, 3.815 in. Max o/a lg, 9.820 in. Nom od disk, 1.394 in.Min, 1.397 in. Max lg disk, 60 blade grooves equally spaced on diskod, 2 stepped hubs, 2.830 in. Min, 2.840 in. Max od 1st step 1st end, 0.700 in. Nom lg 1st step 1st end, 3.320 in. Nom diameter 2nd step 1stend, 0.603 in. Min, 0.607 in. Max lg 2nd step 1st end, externalsplines 1st step 2nd end, 69 teeth, 30 degrees pressure angle, 2.8750 in.Nom pitch dia, 0.380 in. Min, 0.420 in. Max lg splines, 0.681 in.Min, 0.738 in. Max lg 2nd step 2nd end, stepped bore, 3.805 in. Min, 3.815 in. Max o/a lg bore, 2.5576 in. Min, 2.5579 in. Max diameter 1ststep 1st end, 0.950 in. Nom lg 1st step 1st end, 2.566 in. Min, 2.576 in. Max diameter 2nd step 1st end, 0.600 in. Nom lg 2nd step 1stend, 2.2133 in. Min, 2.2137 in. Max diameter 1st step 2nd end, 0.275 in.Min, 0.295 in. Max lg 1st step 2nd end, 2.425 in. Min, 2.435 in. Maxdia 2nd step 2nd end, 0.165 in. Min, 0.205 in. Max lg 2nd step 2ndend, internal splines 3rd step 2nd
NSN
2840-00-591-0741
Part Number
2-141-057-17
Description
Disk And Hub,turbine,turbine Eng
CAGE

Inc 61833 cancelled/replaced by ,inc 50566, fiig a10700, app-key f ,inc 50565, fiig a10700, app-key f ,on 021513 ~(all except usa). A disk having provisions on the outer periphery for attaching turbine blades and an integral hub that provides support for the turbine and/or a means of attachment for a shaft. See also disk,turbine,turbine engine.

Part 2-141-057-17 NSN 2840-00-591-0741

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
61833
FIIG:
A23900
Concept No.:
App. Key:
A
Cond. Code:
2
Status:
C

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
U
ESD:
ESD:
MMAC:
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
10.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
RATING VARIABLE
WCC:
593
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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