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GM32 Annex I Definitions
ED Decision 2022/012/R
EFVSs — DIFFERENCES WITH ENHANCED VISION SYSTEMS (EVSs)
(a)Introduction to EVSs
EVSs use sensing technology to improve a pilot’s ability to detect objects and topographical features ahead of the aircraft. Different types of sensing technology are used on different aircraft installations. Sensing technologies used include forward-looking infrared, millimetre wave radiometry, millimetre wave radar or low-light level intensification; additional technologies may be developed in the future. The image from sensors may be displayed to the pilot in a number of different ways including ‘head-up’ and ‘head-down’ displays.
(b)EVSs and EFVSs
An EFVS is an EVS that is integrated with a flight guidance system, which presents the image from sensors to the pilot on a head-up display (HUD) or equivalent display. If EFVS equipment is certified according to the applicable airworthiness requirements and an operator holds the necessary specific approval, then an EFVS may be used for EFVS operations. An EFVS operation is an operation with an operational credit which allows operating in visibility conditions lower than those in which operations without the use of EFVS are permitted.
(c)Functions of EVSs
Depending on the capabilities of the particular system, EVSs may be useful during operations at night or in reduced visibility for the following:
(1)improving visibility of airport features and other traffic during ground operations;
(2)displaying terrain and obstructions in flight;
(3)displaying weather in flight;
(4)improving visibility of the runway environment during approach operations; and
(5)improving visibility of obstructions on a runway (e.g. aircraft, vehicles or animals) during take-off and approach operations.
(d)Limitations of EVSs
EVSs are a useful tool for enhancing situational awareness; however, each EVS installation has its own specific limitations. These may include:
(1)Performance variations depend on conditions including ambient temperature and lighting and weather phenomena. A system may provide very different image qualities in the same visibility depending on the particular phenomena causing restricted visibility, e.g. haze, rain, fog, snow, dust, etc.
(2)An EVS may not be able to detect certain types of artificial lighting. Light emitting diode (LED) lights have a much lower infrared signature than incandescent lights and therefore may not be detected by some types of EVSs. LED lighting is used for runway, taxiway and approach lighting at many airports.
(3)Monochrome display. EVSs will generally not be able to detect and display the colour of airport lighting. This means that colour coding used on airport lighting will not be visible to the pilot using an EVS.
(4)Many EVS installations do not have redundancy, so a single failure may lead to loss of EVS image.
(5)The location of the sensor on the airframe may mean that in certain conditions it could be susceptible to ice accretion or obscuration from impact damage from objects such as insects or birds.
(6)Where an EVS image is presented on a HUD or an equivalent display, the image needs to be consistent with the pilot’s external view through the display. Particular installations may have limitations on the conditions under which this consistent image can be generated (e.g. crosswind conditions during approach).
(7)Imaging sensor performance can be variable and unpredictable. Pilots should not assume that a flightpath is free of hazards because none are visible in an EVS image.
(e)Considerations for the use of EVSs
EVSs may be used in all phases of flight and have significant potential to enhance the pilot’s situational awareness. No specific approval is required for the use of an EVS; however, the operator is responsible for ensuring that the flight crew members have received training on the equipment installed on their aircraft in accordance with ORO.FC.120. In addition, the operator is responsible for evaluating the risks associated with system limitations and for implementing suitable mitigation measures in accordance with ORO.GEN.200(a)(3) before using the EVS.
The use of EVSs does not permit the use of different operating minima, and EVS images cannot replace natural vision for the required visual reference in any phase of flight including take-off, approach or landing.
An EVS that is not an EFVS cannot be used for EFVS operations and therefore does not obtain an operational credit.
GM33 Annex I Definitions
ED Decision 2022/012/R
INSTRUMENT APPROACH OPERATIONS
(a)Depending on the instrument approach procedure (IAP) in use, the lateral and vertical navigation guidance for an instrument approach operation may be provided by:
(1)a ground-based radio navigation aid; or
(2)computer-generated navigation data from ground-based, space-based or self-contained navigation aids or a combination of these.
(b)A non-precision approach (NPA) procedure flown as CDFA with vertical path guidance calculated by on-board equipment is considered to be a 3D instrument approach operation. Depending on the limitations of the equipment and information sources used to generate vertical guidance, it may be necessary for the pilot to cross-check this guidance against other navigational sources during the approach and to ensure that the minimum altitude/height over published step-down fixes is observed. CDFAs with manual calculation of the required rate of descent are considered 2D operations.
(c)Further guidance on the classification of an instrument approach operation based on the designed lowest operating minima is contained in Appendix J to ICAO Doc 9365 Manual of All-Weather Operations, Fourth Edition, 2017.
GM34 Annex I Definitions
ED Decision 2022/012/R
DECISION ALTITUDE (DA) OR DECISION HEIGHT (DH)
(a)Decision altitude (DA) is referenced to mean sea level and decision height (DH) is referenced to the threshold elevation.
(b)For operations using DA, the aircraft altimeters are set to QNH. For operations using a barometric DH, the aircraft altimeters are set to QFE.
(c)For SA CAT I, SA CAT II, CAT II/III operations, the DH is based on the use of a radio altimeter or other devices capable of providing equivalent performance. The DH is determined with reference to threshold elevation, but the value of the DH set for the approach will be based on the height of the aircraft above the pre-threshold terrain, which may be higher or lower than the threshold.
(d)For convenience, when both expressions are used, they may be written in the form ‘decision altitude/height’ and abbreviated ‘DA/H’.
GM35 Annex I Definitions
ED Decision 2022/012/R
MINIMUM DESCENT ALTITUDE (MDA) OR MINIMUM DESCENT HEIGHT (MDH)
(a)Minimum descent altitude (MDA) is referenced to mean sea level and minimum descent height (MDH) is referenced to the aerodrome elevation or to the threshold elevation if that is more than 7 ft below the aerodrome elevation. An MDH for a circling approach is referenced to the aerodrome elevation.
(b)For operations using MDA, the aircraft altimeters are set to QNH. For operations using a barometric MDH, the aircraft altimeters are set to QFE.
(c)For convenience, when both expressions are used, they may be written in the form ‘minimum descent altitude/height’ and abbreviated ‘MDA/H’.
GM36 Annex I Definitions
ED Decision 2025/008/R
GROUND SUPERVISION
(a)Ground supervision may be contracted by an operator as an individual service. It is usually associated with ground administration services provided by a GH organisation on behalf of the operator.
(b)This service includes the supervision and/or coordination of one or more ground handling activities on behalf of an operator, which may be performed by one or more providers of ground handling services.
(c)Ground supervision comprises activities such as:
(1)providing official representation for the contracting aircraft operator in relation to the aerodrome authorities or other organisations operating at that aerodrome, issuing disbursements on behalf of the aircraft operator, and ensuring the provision of office space for representatives of the operator;
(2)setting key performance indicators for operational performance;
(3)organising workflows and conducting operational planning;
(4)reporting incidents, accidents and near misses;
(5)activating and coordinating emergency responses, in accordance with the operator’s procedures;
(6)communicating with the operator;
(7)handling, storing and administering ULDs;
(8)supervising operational functions in the areas of:
(i)passenger and baggage handling,
(ii)ramp handling,
(iii)load control;
(9)any other administrative services requested by the aircraft operator.
(d)Ground supervision does not include a ground handling organisation’s self-management of its own activities.
(e)Ground supervision does not imply that the individual performing this function will replace, when necessary, an individual performing a ground handling operation.
(f)A person responsible for ground supervision may act on behalf of more than one operator to ensure the safe delivery of the services by ground handling organisations.
[applicable from 29 March 2028 — ED Decision 2025/008/R]
GM37 Annex I (Definitions)
ED Decision 2025/010/R
VEMS OPERATING SITE (Definition (139))
Operating sites used in VEMS training are considered VEMS operating sites.
GM38 Annex I (Definitions)
ED Decision 2025/010/R
VERTIPORT (Definition (140))
A vertiport is considered a type of aerodrome.