Model: 1-140-290-02

Turbine Nozzle Retainer Assembly

Properties:

End Application
T-53 series engines
General Description
Cres, ams5510, rockwell 30t scale 76 max hardness, 14.850 in. Min, 14.880 in. Max od, 12.780 in. Min, 12.785 in. Max id, 2.250 in. Nom o/a lg, 44 holes 0.220 in. Nom diameter through support flange, equally spaced on 14.250in. Bolt circle dia, 24 holes 0.060 in. Min, 0.065 in. Max diameter through bodyod, equally spaced, 0.105 in. Min, 0.115 in. Max from end
NSN
2840-00-019-8009
Part Number
1-140-290-02
Description
Retainer Assembly,turbine Nozzle
CAGE
99193

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:
SX
CRITL:
X

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

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 nozzle retainer assembly (NSN 2840-00-019-8009) 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 »
Highest Rated Parts
Recently Purchased Parts
Hot Parts