Aerospace Performance Parts is pleased to offer immediate purchasing options for Microwave Engineering Corporation part number 111R113P25, which you have taken interest in. This Blade Compressor Aircraft Gas Tu item is listed alongside the NSN 2840-01-106-2596 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 111R113P25 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from Microwave Engineering Corporation under CAGE Code 06351, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 2840-01-106-2596 part number 111R113P25 today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-106-2596 Item PartTypeName: BLADE,COMPRESSOR,AIRCRAFT GAS TU | 2840 | 011062596 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 111R113P25 | 3 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 2.750 INCHES MINIMUM AND 2.752 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 0.390 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.010 INCHES MINIMUM AND 0.020 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG J79 |
| APGF | DESIGN TYPE | COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| CZCJ | STAGE NUMBER | 10 |
| FEAT | SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| MATT | MATERIAL | STEEL BLADE |
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