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321-802-5889
321-733-7477
Model or part number: 1-190-036-02
About this product
Rockwell 30t scale 76 max hardness,0.840 in. Nom lg,0.420 in nom w,0.240 in nom o/a h,0.040 in nom shoulder located on one end,0.040 in nom h shoulder,0.220 in nom dia hole located on shoulder end,0.210 in nom distance to hole center from edge along lg,0.020 in nom distance to hole center from edge along w,0.047 in min,0.062 in max dia hole through corner on shoulder end,25 deg min,35deg max angle of corner hole on ll edge,0.093 in min,0.125 in from corner,0.093 in min,0.125 in max distance to corner hole center from corner,0.093 in min,0.125 in max distance to hole center from bottom edge along h,0.165 in on end oppsite shoulder,0.176 in min,0.196 in max radius of slot end,69 deg min,79 deg max angle chamfer of slot w/shoulder of slot radius on side w/shoulder,85 deg min,95 deg max angle chamfer of slot radius on side oppsite shoulder
Front Turbine Blade Plate Ring NSN 2840-01-010-5941.
NSN 2840-01-010-5941 Datasheet
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.
A metallic item of various shapes designed to reduce vibration and to secure a component part of an engine, gas turbine, aircraft to the engine case or housing as modified. for mounting accessories to the outside of the engine, see plate, mounting.
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.
Metal hardware.
Construction materials: includes paint and related materials, prefabricated building, wood products, metal and composition mater.
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 |
|---|---|---|---|---|
| 1-190-036-02 | 2 | CT | 1 | 99193 |
| 1-190-036-01 | 9 | CT | 2 | 99193 |
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