| ABMK |
OVERALL WIDTH |
58.000 INCHES NOMINAL |
| 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. |
| CZEK |
AIRCRAFT MISSION DESIGN SERIES |
CH-53E |
| AXQD |
CAPACITY |
800.0 GALLON, US MEASURE |
| 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 |
| AGAV |
END ITEM IDENTIFICATION |
HELICOPTER(CH-53E)TACTICAL BULK FUEL DELIVERY SYSTEM |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| ABHP |
OVERALL LENGTH |
62.000 INCHES NOMINAL |