Aerospace Performance Parts is pleased to offer immediate purchasing options for General Electric Company part number 706B109P4, which you have taken interest in. This Bolt Compressor Blade Rotor item is listed alongside the NSN 2840-00-703-2217 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 706B109P4 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from General Electric Company under CAGE Code 07482, 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 2840-00-703-2217 part number 706B109P4 today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-00-703-2217 Item PartTypeName: BOLT,COMPRESSOR BLADE,ROTOR | 2840 | 007032217 | N | |||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | ||||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 706B109P4 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | ENGINE MODEL J79 |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ROUND HEAD 0.461 IN. MIN 0.471 IN. MAX DIA,0.140 IN. MIN 0.150 IN.MAX THK HEAD,0.3269 IN. MIN 0.3271 IN. MAX DIA SHANK,0.3125-24 NSTHREAD,THREADED END HAS HEX WRENCHING FACILITY 0.100 IN.MIN 0.120 IN.MAX DEPTH 0.156 IN. MIN 0.158 IN. MAX DI |
| ZZZV | FSC APPLICATION DATA | AIRCRAFT JET ENGINE |
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