Aerospace Performance Parts is pleased to offer immediate purchasing options for Robertson Fuel Systems Llc part number HM022-010-300, which you have taken interest in. This Tank Refueling Aircraft item is listed alongside the NSN 1560-01-483-4399 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number HM022-010-300 or any other FSC 1560 Airframe Structural Components components we carry from Robertson Fuel Systems Llc under CAGE Code 1T765, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 1560-01-483-4399 part number HM022-010-300 today, knowing we will support all your operational needs with care.
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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