We appreciate your interest in Robertson Fuel Systems Llc part number HM022-010-300, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number HM022-010-300 is listed with the NSN 1560-01-483-4399 and description “Tank Refueling Aircraft.” 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 Robertson Fuel Systems Llc under the CAGE Code 1T765 or that similarly fall under the FSC 1560 Airframe Structural Components, 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 1560-01-483-4399 parts and Tank Refueling Aircraft items your operations require, so request a quote today.
| 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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