Aerospace Performance Parts is pleased to offer immediate purchasing options for Eaton Aerospace Ltd part number T161614, which you have taken interest in. This Fixture Aircraft Ma item is listed alongside the NSN 4920-00-547-1647 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 T161614 or any other FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment components we carry from Eaton Aerospace Ltd under CAGE Code 62983, 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 4920-00-547-1647 part number T161614 today, knowing we will support all your operational needs with care.
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | III END ITEM IDENTIFICATION | MULTI-APPLICATION ON F-100,F-4E,F/TF-15A ACFT VARIABLE DISPLACEMENT HYDRAULIC PUMP ASSEMBLY |
| SR-5 | DESIGN CONTROL REFERENCE | T161614 |
| SR-5 | MANUFACTURERS CODE | 62983 |
| CWFR | NOMINAL OVERALL LENGTH | 4.000 INCHES |
| FTLD | FUNCTIONAL DESCRIPTION | USED IN SUPPORT OF THE HYDRAULIC MOTOR, CONSTANT SPEED DRIVE; USED DURING DEPOT LEVEL MAINTENANCE OF THE M61A1 20 MM GUN |
| SR-5 | THE MANUFACTURERS DATA | |
| RDAL | REFERENCE DATA AND LITERATURE | 42D58G; SERD NO. 0725; TO 9H4-2-40-23 |
| CZDH | NOMINAL OVERALL DIAMETER | 3.500 INCHES |
| FEAT | SPECIAL FEATURES | FIXTURE IS A SPLIT COLLAR ASSEMBLY ONE END OF WHICH SUPPORTS THE RIM OF THE DRIVE SHAFT, THE OTHER END INTERFACES WITH THE BEARING ASSEMBLY FIXTURE AND POSITIONS THE DRIVE SHAFT AND PISTON SUBASSEMBLY SO THAT THE BEARINGS AND SPACES MAY BE INSTALLED ON THE DRIVE SHAFT WITHOUT DAMAGING THE PISTON SUBASSEMBLY |
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