We are pleased to offer procurement for Hamilton Sundstrand Corporation part number ST93151 here on NSN Portal, a Stand Maintenance A product that is listed with the NSN 4920-01-083-0429 for ease of identification. You have reached our Request for Quote (RFQ) form for this listing, where you are encouraged to submit details on your requirements to receive tailored purchasing options from our staff. As you will see, we ask that you offer key information on your pricing target, desired quantity, and more, as this will ensure that the representative who responds to your request is able to provide the most fitting solutions for your needs.
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Whether you procure part number ST93151 or other NSN products from our website, you can rest assured that we uphold full traceability for all items. For example, this particular listing traces back to Hamilton Sundstrand Corporation through the CAGE Code 55820, as well as falls under FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment based on having the NSN 4920-01-083-0429. Furthermore, every purchase will be delivered with any applicable qualifying certifications or manufacturer trace documentation as per our NO CHINA SOURCING pledge. If you are ready to experience why professionals rely on us for their needs, request a quote for part number ST93151 today and take advantage of our industry-leading services.
| MRC | Criteria | Characteristic |
|---|---|---|
| SUPP | III SUPPLEMENTARY FEATURES | TEST STAND FIXTURE 30""L X 24""W X 35.5""H, BOOM ASSY 66""L X 6""W X 90""H, CONTROL CONSOLE ASSY 66.19""L X 44.44""W X 53.50H, WEIGHTS - TEST STAND FIXTURE 580LBS, JET FUEL STARTER TURBINE 60LBS, ACCESSORY DRIVE GEARBOX 85LBS, WATER DYNAMOMETER 70LBS, STARTER 35LBS, CONTROL CONSOLE ASSY 450LBS |
| FEAT | SPECIAL FEATURES | TEST CELL CONTAINS THE TEST STAND FIXTURE. A REDUCTION DRIVE GEARBOX, A STARTER MOTOR, FUEL SYSTEM VALVES AND ASSOC WIRING AND PLUMBING ARE MOUNTED ON THE TEST STAND FIXTURE. A WATER DYNAMOMETER MOUNTED ON THE TEST STAND PROVIDES POWER LOADING FOR THE TURBINE. AN EGT THERMOCOUPLE DUCT AND CUSTOM EXHAUST DUCT ASSY CONNECTS THE TURBINE WITH EXISTING FACILITY DUCTS. A BOOM MOUNTED JUNCTION BOX PROVIDES FOR AIR/ELECTRICAL CONNECTION WITH THE TEST STAND FIXTURE. A BOOM C/O WIRING AND HOSES CONNECTS THE BOOM JUNCTION BOX WITH THE WIRING DUCT FOR THE CONTROL ROOM. TEST STAND FUEL AND WATERBRAKE CONTROLS ARE IN THE TEST CELL. AN INTERFACE (BOX) PROVIDES THE CONTROL INTERFACE BETWEEN THE CONTROL ROOM AND TEST CELL |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | TEST STAND, JET FUEL STARTER |
| AGAV | III END ITEM IDENTIFICATION | F16A/B ACFT,AGE. |
| FTLD | III FUNCTIONAL DESCRIPTION | USED TO FUNCTIONALLY TEST THE JET FUEL STARTER |
| RDAL | III REFERENCE DATA AND LITERATURE | T.O. 33D4-6-634-1, -4 |
| AFPM | ASSEMBLY FORM | RIGID |
| CGYB | WORK HOLDING DEVICE POSITION ADJUSTABILITY | ADJUSTABLE |
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