Model or part number: 1-100-417-05
About this product
Titanium alloy,m3400 fscm 91547,rockwell c scale 36 max hardness,painted finish,p6441 fscm 91547,2.351 in. Nom o/a lg,tapered od disk,7.274 in. Min,7.284 in. Max largest od disk,7.146 in. Min,7.156 in. Max smallest od disk,0.677 in. Min,0.682 in. Max lg disk,38 blade grooves equally spaced on outer periphery,2 hubs,1st end 4.430 in. Min,4.440 in. Max od hub,1.202 in. Min,1.212 in. Max distance from 1st end to disk,2nd end 4.421 in. Min,4.422 in. Max od hub,0.453 in. Min,0.466 in. Max distance from 2nd end to disk,4.082 in. Min,4.087 in. Max dia bore
Factory New, New Material, New Surplus, Overhauled, Serviceable, Repairable, and AS Removed / Used material will be accompanied by a Certificate of Conformance, and any other documents/trace when applicable. We have a 7 year record retention.
We are committed to quality and follow an AS9120 quality management system. AeroBase Group is HAZMAT certified and registered with DDTC,
ITAR, and Aviation Suppliers Association (ASA). All products are 100% inspected.
Quality Commitment »
Delivery of IN-STOCK orders ship same-day when order is placed before 2:00 PM EST.
Delivery dates for NON-STOCK items are estimates based on current backlog and are subject to confirmation at the time of order.
Inc 61831 cancelled/replaced by ,inc 50561, fiig a10700, app-key f ,inc 50562, fiig a10700, app-key f ,inc 50563, fiig a10700, app-key f ,inc 50564, fiig a10700, app-key f ,inc 50565, fiig a10700, app-key f ,inc 50566, fiig a10700, app-key f ,on 021513 ~(all except usa). A disk having provisions on the outer periphery for attaching compressor blades and an integral hub that provides support and alignment for the compressor rotor. See also disk,axial compressor,turbine engine.
Packing shall be accomplished to meet the performance test requirements of astm-d4169, distribution cycle 18, assurance level 1.
Packing shall be accomplished in accordance with table c.Ii for the packing level specified. closure, sealing and reinforcement shall be in accordance with the appropriate shipping container specification.
Options can be exercised as to specific method of preservation or dod approved packaging materials to be used. however, basic preservation method shall be retained, supplemental data shall be complied with, and unit package dimensions shall not be increased by more than one inch. equal or better protection shall be given the item and there shall be no increase in the package cost.
No special marking.
Physical protection.
No requirement.
Parts Of Gas Turbine Aircraft Engines, Other Than For Use In Civil Aircraft
Engines and Turbines For Military Aircraft
Parts For Gas Turbines, N.e.s.
No special type of cargo code applicable.
Motors and parts, (machinery and parts),(less than 35 feet).
Supplies and equipment for aircraft and aerial targets, including aircraft and maintenance parts, aircraft accessories, aircraft.
Shipment is not a consolidation and does not exceed 84 inches in any dimension.
Other or no special handling required (sh)
Code | Definition |
---|---|
FN | Factory New. Parts manufactured by the OEM and includes manufacturer certification. |
NE | New. Parts manufactured by the OEM. May include manufacturer certification or company certification. |
NS | New Surplus. New material item purchased from excess inventory. |
OH | Overhauled. Product has been rebuilt and tested in accordance with the manufacturer's specifications by a repair shop (MRO). |
SV | Serviceable product. |
AR | As Removed. Product removed from aircraft or platform with no guarentee on the functionality of the part. |
RP | Repairable. Product can be repaired by a MRO and be given a FAA 8130 or EASA Form 1 certification. |
Part Number | RNVC | RNAAC | DAC | CAGE |
---|---|---|---|---|
1-100-417-05 | 2 | CT | 1 | 99193 |
1-100-417-05 | 2 | ZG | 5 | D0272 |
1-100-417-02 | 8 | CT | 1 | 99193 |
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