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and
(b) may be assigned to emergency duties in the aircraft under subsection 12 of
section 20.11 of the Civil Aviation Orders.
passenger zone in relation to an aircraft, means an area within the aircraft
which has:
(a) seats for 72 or less passengers; and
(b) an exit.
5 STARTING AND GROUND OPERATIONS OF ENGINES
5.1 The pilot in command or in his absence any other person responsible for
starting or ground operation of an aircraft shall ensure that:
5.1.1 In the case of land aircraft, passenger loading equipment to permit rapid
evacuation of passengers and crew is kept immediately available during the
starting of engines.
5.1.2 In the case of seaplanes, water transport of a capacity sufficient to enable rapid
evacuation of passengers and crew is immediately available during the starting
of engines.
5.1.3 Where any fuel or other flammable material is spilled within 15 metres (50 ft)
of an aircraft, the aircraft engines shall not be started or operated until the fire
hazard has been removed.
5.1.4 An aircraft engine shall not be started or operated:
(a) within 5 metres (17 ft) of any sealed building; or
(b) within 8 metres (25 ft) of other aircraft; or
(c) within 15 metres (50 ft) of any exposed public area; or
(d) within 15 metres (50 ft) of any unsealed building in the case of an aircraft
with a maximum take-off weight exceeding 5 700 kg (12 566 lb); or
(e) within 8 metres (25 ft) of any unsealed building in the case of an aircraft
with a maximum take-off weight not exceeding 5 700 kg (12 566 lb);
and turbine engines, in addition, shall not be operated within the appropriate
distance specified below of any other aircraft, fuelling equipment or exposed
public areas which lie to the rear of and within a 15 degree arc either side of
the exhaust outlet axis of that engine:
Issue 7: 8 December 2004
Amdt No. 213
SECTION 20.9 -8-
Issue 7
Engine
Type
Power Condition Minimum Distance
Metres
Turbo-prop At or below normal slow
taxiing power
15 (50 ft)
At power used to initiate
movement of a stationary
aircraft
23 (75 ft)
Turbo-jet At or below normal slow
taxiing thrust
30 (100 ft)
At thrust used to initiate
movement of a stationary
aircraft
46 (150 ft)
Note: Fuelling equipment does not include equipment and outlet points of an installation
located below ground level when the equipment is stowed and covering hatches are in place.
5.2 The operator of an aircraft shall ensure that all persons who may be required to
start the engine of the aircraft are familiar with the method of operation of any
installed engine nacelle fire extinguishing equipment.
5.3 The pilot in command and the operator shall ensure that passengers do not
embark or disembark or that freight is not loaded or unloaded from the aircraft
whilst an engine of the aircraft is operating unless the passengers and/or the
loading personnel have been given instruction and guidance to protect them
from injury as a consequence of engine operation.
6 GROUND OPERATION OF AIRCRAFT RADAR EQUIPMENT
6.1 The requirement of this subsection shall apply to all radar equipment with a
nominal peak power output rating in excess of 25 kW.
6.2 During all ground operation, including testing and maintenance of aircraft
radar equipment, the operator and person in charge of such equipment shall
ensure that:
6.2.1 The equipment is not energised in its normal mode (antenna rotating) unless
the sector area scanned by the radar beam is clear of the following objects to a
distance of 37 metres (120 ft) from the antenna:
(a) aircraft being refuelled or defuelled;
(b) fuel tankers, fuel tanks or fuel storage areas;
(c) persons or cargo;
(d) any other aircraft or aircraft hangar.
Note: For each radar installation the sector area should be defined in terms of readily
distinguishable dimensions preferably related to some feature of the aircraft and should
appear in the Aircraft Maintenance Manual.
Issue 7: 8 December 2004
Amdt No. 213
-9- SECTION 20.9
Issue 7
6.2.2 The equipment is not energised with the antenna stationary and the beam
directed towards any of the objects specified in paragraph 6.2.1 unless the
distance separating them from the antenna is in excess of 60 metres (200 ft).
6.2.3 The distance specified in paragraphs 6.2.1 and 6.2.2 may be reduced by 75 per
cent when an approved beam attenuating device is used between the antenna
and any object specified in paragraph 6.2.1.
6.2.4 The equipment is not energised in any radiating mode of operation when the
aircraft in which the equipment is fitted is in a hangar or other enclosure unless
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