Aerospace Performance Parts is pleased to offer immediate purchasing options for Pratt And Whitney Canada Inc part number 195880, which you have taken interest in. This Plate Assembly item is listed alongside the NSN 2810-00-396-4165 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 195880 or any other FSC 2810 Gasoline Reciprocating Engines Aircraft Prime Mover and Components components we carry from Pratt And Whitney Canada Inc under CAGE Code 00198, 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 2810-00-396-4165 part number 195880 today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2810-00-396-4165 Item PartTypeName: PLATE ASSEMBLY | 2810 | 003964165 | N | |||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | ||||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 195880 | 6 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | ACFT ENG R2800 |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 4CONSISTS OF PART NUMBERS 152827,195894,152834,AN124989 19 EA,120612 2 EA AND 121389 2 EA; 2 HOLES 0.214 IN. MIN AND 0.224 IN. MAX DIA; 5 HOLES 0.276 IN. MIN AND 0.286 IN. MAX DIA; 19 HOLES 0.126 IN. MIN AND 0.131 IN. MAX DIA; FOR UPPER FIR |
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