TO 00-25-172 - Robins Air Force Base
TO 00-25-172 - Robins Air Force Base
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 />
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