Model: 2-140-073-06

Turbine Engine Turbine Rotor Case

Special Features:

Flange, cres ams5645, body, cres ams5510, rockwell b scale 90 max hardness, 125 microinch aa surface finish, 7.165 in. Nom o/a lg, 19.240 in. Nom od flange, tapered body, 18.279 in. Min, 18.280 in. Max largest od body, 16.730 in. Min, 16.731 in. Max smallest od body, tapered id, 16.560 in. Min, 16.561 in. Max smallest id countersunk 0.015 in. Nom lg by 45 deg, 18.000 in. Min, 18.001 in. Max largest id countersunk 0.060 in. Nom lg by 45 deg, 42 holes 0.271 in. Min, 0.291 in. Max diameter through flange equally spaced on 18.740 in. Nom bolt circle dia, 3 holes 0.190 in.-32 nf series cl 3b thd through flange on 18.740 in. Nom bolt circle dia, thd holes countersunk 90 degrees by 0.220 in. Nom diameter on back surface of flange, 3 thd holes, 0.250 in.-28 unf series cl 3b thd, through flange on 18.740 in. Nom bolt circle dia, thd holes countersunk 90 degrees by 0.280 in. Nom diameter on back surface of flange, 14 holes 0.256 in. Min, 0.261 in. Max diameter through body equally spaced on outer periphery, 2.264 in. Min, 2.274 in. Ma

Properties:

General Description
Flange, cres ams5645, body, cres ams5510, rockwell b scale 90 max hardness, 125 microinch aa surface finish, 7.165 in. Nom o/a lg, 19.240 in. Nom od flange, tapered body, 18.279 in. Min, 18.280 in. Max largest od body, 16.730 in. Min, 16.731 in. Max smallest od body, tapered id, 16.560 in. Min, 16.561 in. Max smallest id countersunk 0.015 in. Nom lg by 45 deg, 18.000 in. Min, 18.001 in. Max largest id countersunk 0.060 in. Nom lg by 45 deg, 42 holes 0.271 in. Min, 0.291 in. Max diameter through flange equally spaced on 18.740 in. Nom bolt circle dia, 3 holes 0.190 in.-32 nf series cl 3b thd through flange on 18.740 in. Nom bolt circle dia, thd holes countersunk 90 degrees by 0.220 in. Nom diameter on back surface of flange, 3 thd holes, 0.250 in.-28 unf series cl 3b thd, through flange on 18.740 in. Nom bolt circle dia, thd holes countersunk 90 degrees by 0.280 in. Nom diameter on back surface of flange, 14 holes 0.256 in. Min, 0.261 in. Max diameter through body equally spaced on outer periphery, 2.264 in. Min, 2.274 in. Max dista
NSN
2840-00-582-1471
Part Number
2-140-073-06
Description
Case,turbine Rotor,turbine Engine
CAGE
99193

Inc 61679 cancelled/replaced by ,inc 50554, fiig a10700, app-key d ,inc 50553, fiig a10700, app-key d ,on 021513 ~(all except usa) a case designed to surround a turbine rotor,turbine engine. Excludes case and nozzle,turbine,turbine engine.

Part 2-140-073-06 NSN 2840-00-582-1471

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
61679
FIIG:
A23900
Concept No.:
3
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:
A
ESD:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
593
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

Pricing & Availability Check

Submit this form for stock availability and pricing.
Part Number:
Quantity:
Email Address:
Phone Number:
Your Name:
Company:



Privacy Policy    Terms & Conditions

How to Order  

Ordering from buyaircraftparts.com

If you would like to order this turbine engine turbine rotor case (NSN 2840-00-582-1471) please submit the pricing and availability form above to receive an up to date quote by email. If you agree to the pricing and terms you can e-sign your order online!

We are pleased to have the opportunity to serve you.

Have a Question

Hours: 08:00-18:00 Eastern Standard Time
Phone: +1 470-231-0824
Email: Contact Form »
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

Highest Rated Parts
Recently Purchased Parts
Hot Parts