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321-802-5889
321-733-7477
Model or part number: 1-110-520-19
This product is available in the following quantities and conditions.
Total: 44 Note: Availability of this item was last updated 10/04/2024, and may have changed since then. Request a quote for up to date pricing and availability.
About this product
Cres ams5532 and nickel alloy m3602 fscm 91547,5.588 in.Min,5.590 in.Max id support,3 holes 0.2820 in.Min,0.2825 in.Max dia through nozzle flange on 13.060 in.Nom bolt circle dia,20 holes 0.190 in.-32 unc cl 3b thd through nozzle flange on 13.060 in.Nom bolt circle dia,thd holes countersunk 90 deg by 0.220 in.Nom dia on vane trailing rough support on 6.160 in.Nom bolt circle dia,3 holes 0.190 in.-32 unf cl 3b thd through support on 6.160 in.Nom bolt circle dia,thd holes countersunk 90 deg by 0.220 in.Nom dia on vane trailing edge side,2.982 in.Min,2.987 in.Max o/a lg;
NSN 2840-00-570-9803 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 single stationary item designed for the purpose of directing air at the proper angle and velocity to a rotor, turbine, aircraft gas turbine engine. it has provisions for attaching to a case (3), turbine, aircraft gas turbine engine. it may have an inner support shroud.
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.
All packaging data is mandatory for compliance and no substitutions are permitted. fast packs should be included in this category.
No special marking.
Unheated general purpose.
Rigid metal container, sealed.
Mil-prf-83671, class 1, rigid foam-in-lace polyurethane.
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 and metal products, nos, (less than 35 feet).
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.
Low sensitivity, category iv, aa&e, unclassified
| 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 |
|---|---|---|---|---|
| 1-110-520-19 | 2 | CT | 2 | 99193 |
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