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19

AIRCRAFTSAFETYPRECAUTIONSDURING FUELLINGOPERATIONS

All engines in the aircraft, including any auxiliarypower units, shall be stopped

with their ignition switches in the ‘OFF’ position, exceptwhereCASA is

satisfied that theoperationof such anengineor auxiliarypower unitwill not

present ahazard andwhere a statement to that effect, togetherwith any

special conditions for operation, is included in relevant documentation.

When anexternal electrical supply isused, the connectionsbetween that

supply and the aircraft electrical system shall bemade and securely locked

before the fuellingoperation is connected and shall not bedisconnecteduntil

theoperationhasbeen completed, except that connectors,whichprovide

control toensureeffectiveengagement beforeexternal power canbe supplied

to the aircraft, neednot be locked.

Aperson shall not, and thepilot in command and theoperator shall take

reasonable steps toensure that apersondoesnot, during fuellingoperations:

• operateor performmaintenanceworkon the aircraft’s radar equipment

except thatwhere the fuel is kerosene, operationormaintenancemaybe

carriedout provided the radar transmitter isde-activated; or

• exceptwhere the fuel involved is kerosene, carryoutmaintenanceon any

electrical, electronicor radio systemswithin the aircraft or operate such

equipment other than the aircraft’s interior lightingor electrical apparatus

necessary for the fuellingprocess.

The aircraft and all itemsof fuellingequipment (includingdrums, funnels and

other loose itemsof equipment,whereused) shall be connected in such away

as toensure that they areof the sameelectrical potential and,where a suitable

earthpoint is available at the fuelling site, both the aircraft and theequipment

shall beeffectively connected to that point:

• where the fuellingoperation isperformedby abarge to a seaplane, the

barge shall beeffectively connected to the aircraft in such away as to

ensure that thebarge, the fuellingequipment and the aircraft are at the

sameelectrical potential.

refuelling

1 — P I LOT RESPONS I B I L I T I ES