We appreciate your interest in Hamilton Sundstrand Corporation part number ST93151, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number ST93151 is listed with the NSN 4920-01-083-0429 and description “Stand Maintenance A.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Hamilton Sundstrand Corporation under the CAGE Code 55820 or that similarly fall under the FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 4920-01-083-0429 parts and Stand Maintenance A items your operations require, so request a quote today.
| 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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