You are currently exploring our in-stock options for part number ST93151 with the NSN 4920010830429. This product is listed with the description “Stand Maintenance A” and is manufactured by Hamilton Sundstrand Corporation. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number ST93151 is listed alongside the NSN 4920-01-083-0429 and belongs to the FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment. Additionally, it is also under the CAGE Code 55820, which is assigned to Hamilton Sundstrand Corporation. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number ST93151 seamless.
| 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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