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TO 00-25-172 - Robins Air Force Base

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<strong>TO</strong> <strong>00</strong>-<strong>25</strong>-<strong>172</strong><br />

similar to an electrical condenser (capacitor) plate. The potential<br />

required for a discharge from these floating objects to<br />

the tank is less than that required to cause a discharge from<br />

the liquid surface to the tank. Therefore, the hazard is greatly<br />

increased by the presence of such objects. The <strong>Air</strong> <strong>Force</strong><br />

now incorporates a conductivity additive to decrease the relaxation<br />

time of electrostatic charges in order to preclude<br />

these problems. Also, the use of a higher flash point fuel<br />

such as JP-8 or JP-5 in lieu of JP-4, when permitted by the<br />

applicable aircraft technical orders, reduces the vapor ignition<br />

hazard. Research has suggested that if fuel flow is kept<br />

below the following maximum rates, hazardous levels of<br />

static electricity charges will not occur:<br />

2.9 GROUNDING AND BONDING POLICY.<br />

Grounding is not required for parked aircraft or aircraft fuel<br />

servicing operations unless required by specific MDS technical<br />

orders. In any case, aircraft stored/parked at the<br />

AMARG desert storage (<strong>TO</strong> 1-1-686) do not need to be<br />

grounded. <strong>Air</strong>craft will be bonded to fuel servicing equipment<br />

at all times during fuel servicing operations. Hydrant<br />

fuel servicing vehicles and hose carts will also be bonded to<br />

the hydrant system in addition to bonding to the aircraft.<br />

(This hydrant-servicing vehicle or hose cart bonding requirement<br />

applies only when the aircraft is not grounded.)<br />

NOTE<br />

These limits do not apply for JP fuels having antistatic<br />

additives with at least 50 Conductivity<br />

Units (CU).<br />

Nozzle/Hose/<br />

Gallons/Minutes<br />

Pipe Diameter<br />

0.75 inches 32<br />

1.50 inches 1<strong>25</strong><br />

2.<strong>00</strong> inches 2<strong>25</strong><br />

2.50 inches 352<br />

3.<strong>00</strong> inches 470<br />

4.<strong>00</strong> inches 627<br />

5.<strong>00</strong> inches 783<br />

6.<strong>00</strong> inches 940<br />

2.7 LIGHTNING.<br />

Even if an aircraft were statically grounded, a severe hazard<br />

to servicing personnel could exist if lightning strikes the aircraft<br />

or within several hundred feet of the aircraft. Servicing<br />

personnel should be evacuated from the area when there is<br />

danger of a direct or close proximity lightning strike. Personnel<br />

inside an aircraft will be in no danger as long as all<br />

aircraft doors, hatches, and canopies are closed. Potentials in<br />

the range of several million volts exist between clouds and<br />

earth. High points such as vertical stabilizers and antenna<br />

masts are most susceptible to strikes. These strikes are of<br />

short duration (approximately 1/1<strong>00</strong> second duration per<br />

strike) and even though high energy levels exist, the ramp<br />

grounding system will generally conduct the energy safely to<br />

earth. An electrical storm can be dangerous even if several<br />

miles from the servicing area.<br />

2.8 OTHER SOURCES OF STATIC ELECTRICITY.<br />

Operating aircraft engines, rotor blades, and propeller blades,<br />

can generate high static electricity voltages. These static<br />

sources are especially hazardous because the static voltages<br />

may be generated continuously as long as the engines/blades<br />

continue to operate.<br />

When applicable, aircraft/equipment must be<br />

grounded and/or bonded prior to connecting the<br />

single point nozzle to the aircraft; however, the<br />

hydrant coupler will be connected to the hydrant<br />

outlet prior to bonding the hydrant servicing vehicle<br />

to the aircraft.<br />

Grounding/Bonding clamps/plugs shall not be allowed<br />

to drag across the ramp. Clamps/plugs shall<br />

be carried to reels on equipment.<br />

NOTE<br />

• If the bonding wire becomes disconnected, reconnect<br />

it immediately. The sequence makes no<br />

difference.<br />

• Bonding is not required for all-metal pantograph,<br />

as long as there is a continuous metal<br />

structure from the fuel servicing equipment to<br />

the aircraft.<br />

a. Grounding of aircraft or supporting servicing equipment<br />

during either fuel servicing, Liquid Nitrogen<br />

(LIN) servicing, or Gaseous Nitrogen (N 2 ) servicing is<br />

not required. Recent electrostatic studies have demonstrated<br />

that grounding aircraft or supporting servicing<br />

equipment for these situations is unnecessary. Unless<br />

required by specific MDS technical orders, grounding<br />

is not required for aircraft except for the following<br />

four operations (only one grounding wire is necessary):<br />

(1) Undergoing munitions loading/unloading operations.<br />

(i.e, loading bombs, missiles, etc., to combat<br />

aircraft store and release locations.) <strong>Air</strong>craft<br />

grounding is not required for driving/carrying on<br />

munitions or hazardous cargo onto cargo aircraft.<br />

2-2

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