Model: 3013511

Turbine Eng Turbine Disk And Hub

Special Features:

Nickel alloy, cres, cpw203 fscm 00198, 8.547 in. Min, 8.549 in. Max o/aod, 3.945 in. Min, 3.960 in. Max o/a lg, 1st end stepped hub, 1.1200 in. Min, 1.1207 in. Max od 1st step 1st end, 0.200 in. Min, 0.210 in. Max lg 1st step 1st end, ext splines 2nd step 1st end, 38 teeth, 30 degrees pressure angle, 1.2188 in. Nom pitch dia, 0.540 in. Min, 0.570 in. Max lg 2nd step 1st end, 1.110 in. Min, 1.130 in. Max od 3rd step 1st end, 0.070 in. Min, 0.080 in. Max lg 3rd step 1st end, 1.3000 in. Min, 1.3007 in. Max od 4th step 1st end, 0.155 in. Min, 0.160 in. Max lg 4th step 1st end, 1.820 in. Min, 1.830 in. Max od 5th step 1st end, 0.125 in. Min, 0.145 in. Max lg 5th step 1st end, 6th step 1st end tapered, 1.675 in. Min, 1.685 in. Max smallest od 6th step 1st end, 0.635 in. Min, 0.705 in. Max lg 6th step 1st end, 1.770 in. Min, 1.825 in. Max lg from 1st end to disk, 1.640 in. Min, 1.660 in. Max lg disk, 2nd end plain hub, 1.408 in. Min, 1.412 in. Max od hub 2nd end, 0.495 in. Min, 0.515 in. Max lg from 2nd end to disk, 4 hole

Properties:

General Description
Nickel alloy, cres, cpw203 fscm 00198, 8.547 in. Min, 8.549 in. Max o/aod, 3.945 in. Min, 3.960 in. Max o/a lg, 1st end stepped hub, 1.1200 in. Min, 1.1207 in. Max od 1st step 1st end, 0.200 in. Min, 0.210 in. Max lg 1st step 1st end, ext splines 2nd step 1st end, 38 teeth, 30 degrees pressure angle, 1.2188 in. Nom pitch dia, 0.540 in. Min, 0.570 in. Max lg 2nd step 1st end, 1.110 in. Min, 1.130 in. Max od 3rd step 1st end, 0.070 in. Min, 0.080 in. Max lg 3rd step 1st end, 1.3000 in. Min, 1.3007 in. Max od 4th step 1st end, 0.155 in. Min, 0.160 in. Max lg 4th step 1st end, 1.820 in. Min, 1.830 in. Max od 5th step 1st end, 0.125 in. Min, 0.145 in. Max lg 5th step 1st end, 6th step 1st end tapered, 1.675 in. Min, 1.685 in. Max smallest od 6th step 1st end, 0.635 in. Min, 0.705 in. Max lg 6th step 1st end, 1.770 in. Min, 1.825 in. Max lg from 1st end to disk, 1.640 in. Min, 1.660 in. Max lg disk, 2nd end plain hub, 1.408 in. Min, 1.412 in. Max od hub 2nd end, 0.495 in. Min, 0.515 in. Max lg from 2nd end to disk, 4 holes 0.208
NSN
2840-00-253-1675
Part Number
3013511
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 3013511 NSN 2840-00-253-1675

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:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
--
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:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
671
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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