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Turbine Engine Turbine Disk

Model / MPN: 2-140-011-37 | NSN: 2840-00-148-7919
ITAR Registered seal

Inc 61686 cancelled/replaced by , inc 50572, fiig a10700, app-key g , inc 50571, fiig a10700, app-key g , on 021513 ~(all except usa). An item having provisions (generally machined slots) on the outer periphery for attaching turbine blades, having features for assembling a disk on a hub or shaft in a designated mating arrangement.

Product Details
NATO Stock Number
2840-00-148-7919
Sold in multiples of
1 EA
DEMIL
DEMIL/MLI
End Application
T-55 series engines
General Description
Cres, m3603, rockwell a scale 69 min, 73 max hardness, 11.430 in. Min, 11.435 in. Max od, 0.867 in. Min, 0.870 in. Max o/a lg, 3 holes through body, 0.2491 in. Min, 0.2496 in. Max diameter holes, countersunk 60 degrees by 0.290 in..Min, 0.300 in. Max diameter both sides, holes equally spaced on 3.380 in. Boltcircle dia, 9 holes through body, 0.350 in. Min, 0.360 in. Max diameter holescountersunk 60 degrees by 0.350 in. Min, 0.360 in. Max diameter both sides, holesspaced on 3.380 in. Nom bolt circle dia, 66 blade grooves equally spaced onouter periphery
Solicitations
Solicitation Description Qty UOM Close Date
SPE4A518T2775 Disk, Turbine, Aircra 1 EA 12/12/2017

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2-140-011-37 Cross Reference