You have arrived on the Request for Quote (RFQ) page for part number HM022-010-300, a Robertson Fuel Systems Llc component that is listed with the product description “Tank Refueling Aircraft” and NSN 1560-01-483-4399 for fast identification. By using the form supplied below, you can offer details regarding your requirements to secure customized procurement solutions for your consideration. As our goal is to provide quick service, you can expect a response within 15 minutes of our staff members reviewing your submission. Alternatively, if you use the email or phone number at the bottom of the webpage, you can directly connect with our experts to discuss your needs.
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Alongside Robertson Fuel Systems Llc part number HM022-010-300, you can seamlessly search for more items from this manufacturer or CAGECode 1T765 using our curated catalogs. Similarly, we also offer means for locating other products that belong to FSC 1560 Airframe Structural Components, which this component falls under having the NSN 1560-01-483-4399. Whether you desire part number HM022-010-300 or other NSN components, you can rest assured that our entire inventory is sourced from reputable manufacturers and suppliers. Bearing this in mind, kick off procurement today to see why so many customers select Aero Defence Solutions as their trusted purchasing hub.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-483-4399 Item PartTypeName: TANK,REFUELING,AIRCRAFT | 1560 | 014834399 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
HM022-010-300 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AXQD | Capacity | 800.0 GALLON, US MEASURE |
SUPP | Supplementary Features | THE TANKS CAN ACCEPT FUEL THROUGH: THE HELICOPTER'S SINGLE POINT PRESSURE REFUELING ADAPTER, THE IN-FLIGHT REFUELING PROBE, REFUELING THE TANK MANIFLD OR THE FILLER OPENING IN THE TOP OF EACH TANK. USING THE TBFDS TANK'S INTERNAL PUMPS, FUEL CAN BE TRANSFERRED TO THE HELICOPTER'S TANKS, OR DISPENSED TO OTHER AIRCRAFT OR VEHICLES USING THE FORWARD AREA REFUELING EQUIPMENT (FARE). THE FARE IS TWO POINT CAPABLE, WITH A COMBINED FLOW RATE OF 120 GPM, AND 200 FEET SEPARATION FRO THE HOST AIRCRAFT TO THE AIRCRAFT OR VEHICLES BEING REFUELED. |
ABMK | Overall Width | 58.000 INCHES NOMINAL |
FEAT | Special Features | BALLISTIC TOLERANCES: .50 CAL, 12.7MM, 14.4MM, 20MM; CRASHWORTHINESS: 10 G'S FORWARD, 7.5 G'S AFT, 3G'S VERTICAL, 3G'S LATERAL |
CXCY | Part Name Assigned By Controlling Agency | TANK ASSEMBLY, BULK FUEL |
ABHP | Overall Length | 62.000 INCHES NOMINAL |
AGAV | End Item Identification | HELICOPTER(CH-53E)TACTICAL BULK FUEL DELIVERY SYSTEM |
CZEK | Aircraft Mission Design Series | CH-53E |
MRC | Decoded Requirement | Clear Text Reply |
CRTL | Criticality Code Justification | FEAT |
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