Aviation Refueling Unit 1) Tank: a) 3,000-gallon stainless steel bolster style tank with baffles and water drain b) Manhole 20” with 10” fill cover and normal vent c) Cable operated 4” emergency valve with screen d) Truck lighting system to conform to US DOT guidelines 2) 40 GPM Pumping: a) 2” positive displacement pump b) 2-1 micron filters with water absorbing flow stop cartridge c) 2 ½” diameter pressure gauge with 1 – 160 psi range d) Stainless steel piping downstream of the filters e) Provision for UND Aerospace to install an electronic metering system and liquid control system i) Liquid control meter LCR2 heads must be capable of recording fueling and defueling transactions activity 3) Overwing fueling and defueling (2 hose reels capable of fueling and or defueling): a) 1 ½” hose reel with non-ferrous internal and 2” isolation valve b) Certified 1” x 35’ aircraft refueling hose c) 1” nozzle with 100 mesh strainer 4) Bottom loading system: a) High level shut off with pre-check b) 2” bottom loading adapter with isolation valve c) 2 ½” diameter pre-check gauge with 0-160 psi range d) Bottom loading gate for brake interlock 5) Safety and Miscellaneous Features: a) Brake interlock system for each nozzle holder, bottom load adapter and PTO pump on b) Spring rewind static reel with 50’ of cable and 100-amp grounding clamp c) Two 20 lb. UL rated fire extinguishers (Purple K) d) Unit painted white e) Operating CD or manual including maintenance information and parts list...
