### COMMITTEE ON AVIATION ENVIRONMENTAL PROTECTION (CAEP)
STEERING GROUP MEETING Beijing, 12 to 16 September 2011 Agenda Item 3: Performance and Em issions

– WG3
U.S. POSITION ON THE DEVELOPMENT OF ICAO’S AIRCRAFT CO 2 STANDARD (Presented by the United States)

SUMMARY The purpose of this paper is to : 1 ) provide the U.S. position on the development of ICAO’s aircraft CO 2 Standard; 2 ) recommend a purp ose of the CO 2 Standard to provide the CO 2 TG policy guidance to complete its work; 3 ) identify major points of disagreement requiring resolution in order to move the work forward; and 4 ) suggest possible next steps to ensure the work is completed in an expediti ous manner. Action by the CAEP

- SG is in paragraph 4.

1

. INTRODUCTION
1

. 1 Since the meeting of the Steering Group in 2010, the WG3 has focused the majority of their resources on CO 2 TG assigned remits, specifically to develop an aircraft CO 2 Certification Requirement. A concentrated schedule of teleconferences , workshops, and meetings was followed to accomplish this work, which focused mainly on conducting technical analyses to select a certification framework as a basis for the development of the certification requirement. Such a certification framework histor ically consists of a metric (e.g. DP/F00 for NO x , EPNdB for noise), correlating parameter (e.g. overall pressure ratio for NO x , MTOW for noise), and evaluation option (i.e. representative landing and takeoff (LTO) cycle for NO x , combination of flyover, la teral, and approach measurement for noise).
1

. 2 The CO 2 TG initially attempted to target each specific part of the certification framework separately. However, the CO 2 TG recently concluded that the analysis of metrics, correlating parameters (CPs), and evalu ation options (EOs) form a highly complex and interdependent system (i.e. Metric System). As a result, the CO 2 TG agreed that further work must assess metrics, CPs, and EOs as a whole

International Civil Aviation Organization 

### WORKING PAPER CAEP

- SG/2011 2

- WP/25 22/8/11 English onlyCAEP

- SG/2011 2

- WP/25

- 2

-

rather than individually. The analysis of metric systems ought to help re cognize interdependencies and potential consequences, isolate effects, and aid the understanding of differences of opinions within the working group. The CO 2 TG also constructed a set of Key Criteria (KC) to be used in the process as a guide to identify and select candidate metric systems for aircraft certification purposes.
1

. 3 At the conclusion of the sixth and most recent meeting of WG3/CO 2 TG, on July 18 to 22 , 2011 in Hartford, Connecticut , the group narrowed down to four favoured metric systems (MS) 1 . The se metrics systems are listed in the Table I below, and include metrics based on both mission fuel and Specific Air Range (SAR).
Table I : Favoured CO 2 M etric S ystem S ubmissions 2

Metric Sys tem # Metric Correlating Parameter(s) Evaluation option MS #1 1/SAR MTOW 75% (MTOW

- MinW)+MinW 3 MS #2 1/SAR (MTOW+MZFW)/2 (MTOW+MZFW)/2 MS #3 1/SAR TBD TBD MS #4

Mission Fuel Payload (MZFW

- SAEW) and Distance 3 test points at ZFW = SAEW + 0.7 (MZFW

- SAEW) with fuel mass of: i) 1/3(MTOW

- MZFW) ii) 1/2(MTOW

- MZFW) iii) 2/3(MTOW

- MZFW) >1500ft flight phases

2

. DISCUSSION
2

. 1 While progress has been made by the CO 2 TG to down

- select to three well defined metric systems (and one to be determined), significant differences in opinion exist and have prevented the group from identifying a single metric system as the basis for a CO 2 certification requirement. Discussions regarding the appropriateness of the metric systems have been focused on how the metric systems relate to t he CO 2 TG KC, however, the differences in opinion persist as to the true ability of each MS to meet several of these criteria. In particular, the considerations include:
2

. 1

. 1 The purpose of the CO 2 S tandard so as to inform the development of the aircraft CO2 Cer tification Requirement;
2

. 1

. 2 Whether the metric needs to explicitly represent fuel efficiency across all relevant phases of flight (i.e. Mission

- based) or if it is sufficient to represent fuel efficiency at a cruise condition (1/SAR);
2

. 1

. 3 How to determine if a met ric system is transport capability neutral;
2

. 1

. 4 Whether empty weight reductions need to be explicitly rewarded, through increased margin to a notional limit line, and also whether empty weight increases should be penalized through decreased margin to a notiona l limit line, similar to aerodynamic or propulsive efficiency changes;
2

. 1

. 5 Whether the evaluation options should be based on day to day operational patterns versus measuring the performance at maximum capability; and

1 CAEP9_WG3_CO2

- - 4

- 6_WP13 2 Where SAR is specific air range, MTOW is maximum takeoff weight, MZFW is maximum zero fuel weight, and MinW is minimum weight 3 Possible use of SAEW instead of MinW , where SAEW is standard aircraft empty weightCAEP

- SG/2011 2

- WP/25

- 3

-

2

. 1

. 6 The complexity and extent of the burden r equired from certification authorities to certify new parameters and promulgate national regulations, develop processes to implement the regulations, and train certification engineers to oversee implementation and verification.
2

. 2 Some of the divergence of op inions cannot be answered solely through technical analyses, but may require policy direction. The CO 2 TG requires guidance from CAEP on policy questions in order to successfully carry out its technical work. The U.S. believes that CAEP should provide the CO 2 TG direction on an agreed purpose of the CO 2 Standard. The U.S. believes that the purpose of the CO 2 S tandard is to achieve CO 2 emission reductions from the aviation sector beyond expected ―business as usual‖

– i.e., a standard that achieves CO 2 emiss ion reductions from the aviation sector beyond reductions that would otherwise be achieved in the absence of the standard. This would be analysed using the ICAO criteria of technical feasibility, environmental benefit, cost effectiveness, and impacts of i nterdependencies. Similarly, in anticipation of the next phase of CO 2 TG work involving the CO 2 S tandard’s applicability and stringency, the U.S. believes that CAEP should reaffirm the importance of analysing the potential applicability of a CO 2 Standard to new in

- production aircraft as well as new types.
2

. 3 To address all of the criteria and these considerations the U.S. believes that the CO 2 S tandard metric system should be feasible to implement and demonstrated by data and rigorous quantitative analysis.
2

. 4 To address considerations 2.1.1 and 2.1.4, the U.S. believes that the CO 2 S tandard metric system should reflect all relevant phases of flight and real

- world operations of aircraft as much as possible.
2

. 5 Consensus within the group has not been reached because some believe that technical evidence evaluating the degree to which the three well defined MS meet the KC has not been presented by the members that support the different systems. This has been expressed in particular with respect to the mission

- based appr oach. Therefore, the U.S. believes it is important to direct the CO 2 TG to focus future data gathering and analysis on the most robust metric system that reflects all relevant phases of flight and real

- world operations as much as possible, is feasible to im plement, and is demonstrated by data and rigorous quantitative analysis. This work should be performed without prejudice toward a final metric system selection. Furthermore, there is not yet technical consensus on all of the evidence that has been provid ed within the task group; the aforementioned differences in opinion appear to be preventing a technical consensus in several aspects.
2

. 6 A specific area of disagreement that distinctively surfaced is whether changes in transport capability, in absence of cha nges in technology, could be explicitly rewarded by the metric system via an increased margin to any assumed notional limit line. Any metric systems that are determined to not be transport capability neutral for any assumed notional limit line should requ ire an analysis for a comprehensive assessment of potential consequences before down

- selecting to the final metric system.
2

. 7 It should be noted that some metric systems that are not neutral to transport capability for any assumed notional limit line could dr ive the design and development of aircraft in unintended directions, such as influencing the design based on transport capabilities, which may result in responses to a notional limit line without promoting technology improvements. This could have potential implications on the air transportation system and its stakeholders, including airline purchases, aircraft utilization, operations and routing, air transportation system congestion and delay, safety, and system

- wide fuel burn, local air quality, and noise. The U.S. believes that the CO 2 TG should eliminate any non

- transportCAEP

- SG/2011 2

- WP/25

- 4

-

capability neutral metric systems, as inappropriate for consideration at this point given all the uncertainties of this approach.
2

. 8 The U.S. believes that CAEP should maintain a schedule fo r the CO 2 S tandard that will produce international agreement on a standard in 2014. As part of this approach, WG3 needs to decide on a metric system at the November WG3 meeting, and CO 2 TG should work on an aggressive schedule to do the necessary analytica l work in advance of that meeting. If further work by CO 2 TG members concludes that it is not feasible to down

- select to a single metric system within a reasonable amount of time, the working group and CO 2 TG should clearly state to Steering Group its reaso ning with identification of pros/cons, existing gaps in technical opinions, and basis for the technical gaps

. WG3 should also work with MDG and FESG to identify schedule efficiencies to recover from delays, including moving forward with the sample problem.

3

. CONCLUSION
3

. 1 The CO 2 TG has conducted a significant amount of work toward achieving its remits; however there are still major points of technical disagreement that prevent the CO 2 TG from reaching a consensus on one single metric system.
3

. 2 The CO 2 TG should iden tify a clear plan to work on the development of an aircraft CO 2 certification requirement to achieve a down

- select of one metric system by the end of their next scheduled meeting in November. This work plan should include key points that must be addressed in order to resolve disagreements and subsequently down

- select to a single metric system to take forward to a sample problem analysis.

4

. ACTION BY THE CAEP
- SG
4

. 1 The CAEP

- SG is invited to:

a ) agree that the purpose of the CO 2 S tandard is to achieve CO 2 emission r eductions from the aviation sector beyond expected ―business as usual‖

– i.e., a standard that achieves CO 2 emission reductions from the aviation sector beyond reductions that would otherwise be achieved in the absence of the standard. This would be analys ed using ICAO criteria of technical feasibility, environmental benefit, cost effectiveness, and impacts of interdependencies

. b ) r eaffirm the importance of analysing the potential applicability of a CO 2 S tandard to new in

- production aircraft as well as new types;

c ) a gree that the CO 2 metric system should reflect all relevant phases of flight and real

- world operations of ai rcraft as much as possible;
d ) a gree that the CO 2 metric system should be feasible to implement and demonstrated by data and r igorous quantitat ive analysis;

e ) a gree to eliminate from consideration any non

- transport capability neutral metric systems at this point given all the uncertainties of this approach;CAEP

- SG/2011 2

- WP/25

- 5

-

f ) r equest an action plan by 5 October 2011 from WG3 CO 2 TG to deliver one down

selected metric system by the end of their next scheduled meeting in November;
g ) a gree to maintain a schedule for the CO 2 S tandard that will produce international agreement on a S tandard in 2014; and
h ) a gree that WG3 should work with MDG and FESG to identify schedule effici encies to recover from delays, including moving forward with the sample problem.

— END

—