Model: 1-140-272-01

Turbine Eng Turbine Disk And Hub

Special Features:

Cres; m3603; electrofilm p6435-2 internal spline; rockwell a scale 69 min; 73 max hardness; 9.913 in. Nom o/a lg; 8.629 in. Min; 8.639 in. Max od; 7.730 in min; 7.770 in. Max id 1st end; 1.905 in. Min; 1.910 in.Max od 2nd end; 1.882 in. Min; 1.892 in. Max od 2nd end 1st step; 0.550 in. Nom lg 2nd end; externalthd 1st step 2nd end; 1.9670-18 ns cl 3thd; 1.9264 in. Min; 1.9309 in. Max pitch dia; 0.450 in. Nom thd lg; 1.877 in. Min; 1.887 in. Max diameter 2nd step 2nd end0.100 in. Lg 2nd step 2nd step 2nd end; 1.9683 in. Min; 1.965 in. Max od 3rd step 2nd end; 1.770 in. Nom lg 4th step2nd end end; 2.740 in. Nom lg 4th step 2nd end; 2.1655 in. Min; 2.1658 in. Max 0d 5th step 2nd end; 1.520 in. Nom lg 5th step 2nd end; 2.410 in. Nom od 6th step 2nd end; internal thd 2nd end; 0.390 in. Thd lg; 1.5620-16 uns cl 3b; 1.5214 in. Min; 1.5254 in. Max pitch dia; internal spline; 24 teeth; 1.438 in. Min; 1.443 in. Max id; 1.5000 in. Nom pitch dia; 30 degrees pressure angle

Properties:

General Description
Cres; m3603; electrofilm p6435-2 internal spline; rockwell a scale 69 min; 73 max hardness; 9.913 in. Nom o/a lg; 8.629 in. Min; 8.639 in. Max od; 7.730 in min; 7.770 in. Max id 1st end; 1.905 in. Min; 1.910 in.Max od 2nd end; 1.882 in. Min; 1.892 in. Max od 2nd end 1st step; 0.550 in. Nom lg 2nd end; externalthd 1st step 2nd end; 1.9670-18 ns cl 3thd; 1.9264 in. Min; 1.9309 in. Max pitch dia; 0.450 in. Nom thd lg; 1.877 in. Min; 1.887 in. Max diameter 2nd step 2nd end0.100 in. Lg 2nd step 2nd step 2nd end; 1.9683 in. Min; 1.965 in. Max od 3rd step 2nd end; 1.770 in. Nom lg 4th step2nd end end; 2.740 in. Nom lg 4th step 2nd end; 2.1655 in. Min; 2.1658 in. Max 0d 5th step 2nd end; 1.520 in. Nom lg 5th step 2nd end; 2.410 in. Nom od 6th step 2nd end; internal thd 2nd end; 0.390 in. Thd lg; 1.5620-16 uns cl 3b; 1.5214 in. Min; 1.5254 in. Max pitch dia; internal spline; 24 teeth; 1.438 in. Min; 1.443 in. Max id; 1.5000 in. Nom pitch dia; 30 degrees pressure angle
NSN
2840-00-943-2215
Part Number
1-140-272-01
Description
Disk And Hub,turbine,turbine Eng
CAGE
99193

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 1-140-272-01 NSN 2840-00-943-2215

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

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 eng turbine disk and hub (NSN 2840-00-943-2215) 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