ANNEX II
METHODOLOGY FOR ESTIMATING FLIGHT EMISSIONS
This Annex lays down the methodology and the necessary steps that the Agency shall follow for the estimation of flight emissions.
1. CALCULATION OF FLIGHT EMISSIONS
(1)
Flight emissions shall be calculated by multiplying the estimated consumption of aviation fuels for the flight in question by the weighted average of lifecycle emissions of the aviation fuels uplifted at the departure airport. At the same time, flight emissions are equal to the sum of cabin and freight emissions.
where:
E
=
flight emissions, in tonnes of carbon dioxide equivalent (t CO 2 eq),
E c
=
cabin emissions, in t CO 2 eq,
E f
=
freight emissions, in t CO 2 eq,
E WTT
=
fraction of the flight emissions corresponding to well-to-tank, in t CO 2 eq,
E TTW
=
fraction of the flight emissions corresponding to tank-to-wheel, in t CO 2 eq,
V fuel
=
consumption of aviation fuels of the flight, in tonnes,
EC fuel
=
energy content of aviation fuels, in megajoule per kilogramme (MJ/kg),
LCE fuel
=
weighted average lifecycle emissions of the aviation fuels uplifted at the departure airport, in grammes of carbon dioxide equivalent per megajoule (g CO 2 eq/MJ).
(2)
The average lifecycle emissions of the aviation fuels uplifted at the departure airport shall be the weighted average of the aviation fuel life cycle emissions of all batches ( b ) of aviation fuels uplifted at that airport, taking into account Article 5(6):
where:
LCE b
=
aviation fuels lifecycle emissions of a batch ‘b’ of aviation fuels, in g CO 2 eq/MJ. For conventional aviation fuels, this value shall be 89 g CO 2 eq/MJ;
V b
=
mass of a batch ‘b’ of aviation fuels, in tonnes.
(3)
The estimated aviation fuels consumption of a flight shall be calculated using either of the following methods:
(a)
Using past operations
When primary data is available for the operations of the previous corresponding scheduling periods and tallies with the operating conditions of the scheduled flight, the estimation of aviation fuels consumption shall be calculated as the weighted average of the reported aviation fuels consumption in the flights ( a ) operated on the route in question:
where:
F a
=
total block aviation fuel for all flights relevant to each label, in the reporting period;
N a
=
total number of flights operated relevant to each label, in the reporting period.
(b)
Based on the Breguet-Range equation
If primary data for the scheduled flights reported under Article 3(3) does not exist, is insufficient, cannot be verified or exists only for operating conditions significantly differing from those reported under Article 3(4), the estimated aviation fuels consumption shall be calculated by approximation using the Breguet-Range equation.
This equation estimates the overall cruise performance as follows:
where:
R
=
distance travelled, in kilometres,
V
=
speed of the aircraft, in kilometres per hour,
c
=
thrust-specific aviation fuels consumption, in kilogrammes per Newton-hour,
L
=
lift force acting on the aircraft, in Newtons,
D
=
aerodynamic drag force acting on the aircraft, in Newtons,
ln
=
natural logarithm function,
W 1
=
aircraft mass at the beginning of the cruise, in tonnes,
W 2
=
aircraft mass at the end of the cruise, in tonnes.
By rearranging the Breguet-Range equation, a ratio between an aircraft’s initial and final mass can be derived, representing the aviation fuels consumption of the flight in question:
In the absence of information on each flight’s landing mass, engine performance and the aerodynamic performance of the aircraft, these factors are not computed directly. The equation is further refined by regressing the factors to correlate them with observations of the information reported under Article 3(4) and, at least, the aircraft type. This refined equation shall be applied for each aircraft:
where:
a
=
aircraft mass when landing at the airport of arrival, in tonnes,
,
.
and where:
W 0
=
aircraft empty mass, in tonnes,
W 1
=
aircraft mass after climbing to 3 000 ft (or 914,4 metres), in tonnes,
W 2
=
aircraft mass after climbing to cruise, cruising, and descending to 3 000 ft (or 914,4 metres), in tonnes,
W 3
=
aircraft mass when landing at the arrival airport, in tonnes.
The coefficients a , b and r shall be determined using regression analysis, to minimise the estimated difference (L2-Norm) between the observed aviation fuels consumption and the estimated value.
2. ALLOCATION OF FLIGHT EMISSIONS TO CABIN AND FREIGHT
(1)
Flight emissions shall be attributed to the cabin (cabin emissions, Ec ) and to freight (freight emissions, Ef ) on the basis of the respective apportionment of cabin and freight mass, as follows:
(a)
cabin emissions ( E c
)
where:
, share of the payload of the aircraft attributed to the cabin,
C w
=
mass corresponding to the cabin (passengers and their baggage), in tonnes,
F w
=
mass corresponding to the freight on board of the aircraft, in tonnes.
(b)
freight emissions ( E f
)
where:
, share of the payload of the aircraft attributed to the freight.
(2)
Where information on the number of passengers is not reported because the conditions of the scheduled operations are different to those of previous flights, such as for new aircraft operators or new aircraft configurations, an estimated number of passengers shall be calculated on the basis of the following factors (to be given on the website established under Article 8):
where:
N
=
number of seats available in the aircraft type, per cabin class,
L
=
estimated load factor of the flight, calculated taking into account the average load factor of the aircraft operator per cabin class particularly in flights (i) on the same route; (ii) on comparable routes; and (iii) on any other route,
P m
=
mass attributed to a passenger including their baggage, which shall be 100 kg.
3. GENERATION OF EMISSIONS FOOTPRINT AND EFFICIENCY
(1)
Flight emissions allocated to the cabin and freight are then used to generate its emissions footprint and emissions efficiency, and shall be calculated as follows:
(a)
Cabin emissions footprint and efficiency
Cabin emissions per passenger ( C ef
)
, in kg CO 2 eq/pax
Cabin emissions per passenger-kilometre ( C ei
)
, in g CO 2 eq/pkm
where,
, flight range determined using the great circle distance method (GCD), in km.
(b)
Freight emissions footprint and efficiency
Freight emissions per tonne of freight ( F ef
)
, in kg CO 2 eq/t
Freight emissions per tonne-kilometre ( F ee
)
, in g CO 2 eq/tkm
4. ALLOCATION OF CABIN EMISSIONS TO EACH CABIN CLASS
(1)
Where an aircraft is operated with more than one cabin class, the cabin emissions shall be allocated to each cabin class.
(2)
Where the aircraft operator reports the seating area of every configuration of each aircraft type, that seating area (SA) shall be used in the first instance to calculate what cabin class factor to apply.
where:
CCF =
cabin class factor representing the allocation of cabin emissions per passenger in each cabin class estimated based on the seating area allocated in an aircraft to the lowest class,
SA c =
floor area per seat in each cabin class (‘c’), in square metres,
SA l =
floor area per seat of the lowest cabin class (‘l’), in square metres.
(3)
If the information referred to in the previous point is not available, the CCF shall be estimated based on the weighted averages of the seating area reported under Article 3(4)(a). The weighted averages shall be based, where possible, on operator specific data and shall be, at least, by cabin class.
(4)
Where the information to estimate CCF is insufficient, the default CCF set out in Table 1 shall be used.
Table 1
CCF calculations based on seating area and default values
Cabin class (c)
CCF based on seating area
Default CCF
Wide-body ( CCF c-w
)
Narrow-body ( CCF c-n
)
Economy (e)
Premium Economy (pe)
Business (b)
First (f)
(5)
As cabin emissions include all passengers on a flight regardless of the cabin class they are seated in, cabin emissions shall be allocated to each passenger based on their respective cabin class factor. This allocation shall be made using a theoretical number of passengers (LCeq) using as a common equivalent the lowest cabin class.
where:
LC eq
=
theoretical number of passengers calculated for the purpose of allocating cabin emissions to passengers in each cabin class,
pax c
=
number of passengers in each cabin class.
(6)
The emissions of the lowest cabin class equivalent passenger are then allocated to each passenger proportionally to their respective cabin class factor:
Cabin class emissions per passenger ( CC ef
)
, in kg CO 2 eq/pax
Cabin class emissions per passenger-kilometre ( CC ei
)
, in g CO 2 eq/pkm.