(a) Each nozzle must be a ``deadman'' type.
(b) Each hose must have a storage reel.
(c) Each hose must have a static grounding device.
(d) Each electric fuel transfer pump must have a control with a fuel transfer pump operation indicator light at the pump.
(e) There must be a fuel pump shut off at each of the access routes required by Sec. 108.235(f).
(f) Each fuel transfer pump and each hose reel must have a means to contain fuel spills or leaks.
(g) Each hose must meet chapter 3 ``Aircraft Fueling Hose'' of National Fire Protection Association Standard for Aircraft Fuel Servicing (N.F.P.A. No. 407-1975).