Home »
FSC NSN Catalog »
Prime Moving; And Components Aircraft Gas Turbines And Jet Engines »
1-100-078-07

Tur Centrifugal Compressor Rotor

Model / MPN: 1-100-078-07 | NSN: 2840-00-176-3745

Inc 60245 cancelled/replaced by , inc 50588, fiig a10700, app-key j , inc 50587, fiig a10700, app-key j , on 021513 ~(all except usa). An item consisting of a series of blades on one or both sides of the rotor disk extending from the axis of rotation radially to the rim of the disk. It is designed to centrifugally cause the air between the blades to move outward to the rim of the compressor section of a turbine engine.

Product Details

NATO Stock Number

2840-00-176-3745

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

End Application

T-53 series engines

General Description

Titanium alloy m3403, fscm 91547, shot peened ams2430, 36 blades, 13.048 in. Min, 13.051 in. Max od, 4.8694 in. Min, 4.8700 in. Max id bore, 12 holes 0.337 in. Min, 0.344 in. Max diameter on 5.440 in. Nom bolt circle dia, 3 thd holes on 5.440 in. Nom bolt circle dia, 0.250-28unf class 2b thd, thd holes countersunk 90 degrees by 0.280 in. Nom dia, 12 holes 0.154 in. Min, 0.159 in. Max diameter 0.150 in. Nom deep on 5.290 in. Nom bolt circle dia

1100 Series Parts

Pricing and Availability

Send us a request for quote using the form below. Our team will contact you with an up to date pricing and availability quote ASAP.

Certified Quality Assurance

ISO 9001:2015 + AS9120B
Counterfeit Parts Prevention
100% Product Inspections
7 Year Record Retention
On Time Delivery
HAZMAT Certified
Worldwide Shipping

Tur Centrifugal Compressor Rotor

Pricing and Availability

Certified Quality Assurance

1-100-078-07 Cross Reference