Thank you for taking interest in Hamilton Sundstrand Corporation part number ST93151, which is listed with the NSN 4920-01-083-0429 and a product description of “Stand Maintenance A.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
Note : We Will Not Share Your Information To Any Third Parties.
Alongside part number ST93151, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Stand Maintenance A part with the NSN 4920-01-083-0429. For example, you can browse other Hamilton Sundstrand Corporation components that were produced under CAGE Code 55820 or listings that belong to FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number ST93151 and other desired offerings on Aerospace Spare.
| 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 |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
Request for Quote
