Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number ST93151, a Hamilton Sundstrand Corporation item with the NSN 4920010830429 that is listed alongside the description “Stand Maintenance A.” If you are interested in part number ST93151 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number ST93151 is specifically listed with the NSN 4920-01-083-0429, and this code can be used to determine that it falls under FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment. Additionally, while tracing back to Hamilton Sundstrand Corporation, this NSN part was specifically produced under CAGE Code 55820. With our services and dedication to simple procurement in mind, get started with us 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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