Aerospace Performance Parts is pleased to offer immediate purchasing options for Texas Instruments Inc part number KDS 2840-4003, which you have taken interest in. This Lock Turbine Rotor Blade Aircraf item is listed alongside the NSN 2840-01-307-6361 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 KDS 2840-4003 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from Texas Instruments Inc under CAGE Code 3999F, 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 2840-01-307-6361 part number KDS 2840-4003 today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-307-6361 Item PartTypeName: LOCK,TURBINE ROTOR BLADE,AIRCRAF | 2840 | 013076361 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| KDS 2840-4003 | 2 | 1 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 0.666 INCHES MINIMUM AND 0.676 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 0.658 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.074 INCHES MINIMUM AND 0.083 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F110GE129 ACFT ENGINE |
| FEAT | SPECIAL FEATURES | USED ON THE REAR HIGH PRESSURE TURBINE |
| MATT | MATERIAL | TITANIUM |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | C50TF70,CL-A MFR REF SINGLE MATERIAL RESPONSE |
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