Title: Committee on Aviation Environmental Protection
1- Committee on Aviation Environmental Protection
- Sixth Meeting
- Montreal, Canada, 2-12 February 2004
- Economic Analysis of NOx Stringency Options
- Forecasting and Economic Support Group
2FESG Economic Analysis of NOx Stringency Options
- Models, Databases and Methods
- Assumptions
- LTO NOx Benefits Assessment
- Assessment of Costs
- Cost Benefit Results
3Models, Databases and Methods
- Models
- FAA Emissions Dispersion Modeling System (EDMS)
- Boeing Global Emissions Model (GEM)
- Spreadsheet model to aggregate costs developed by
Campbell-Hill - Databases
- FESG Fleet Forecast
- WG3 In-Production Airframe/Engine Database
- Methods
- WG3 Technology Level Matrix (TL1, TL2, TL5A, and
TL5B) - Discounting to allow costs and benefits to be
compared with one another even though they accrue
at different time periods
4FESG Economic Analysis of NOx Stringency Options
- Models, Databases and Methods
- Assumptions
- LTO NOx Benefits Assessment
- Assessment of Costs
- Cost Benefit Results
5Key Modelling Assumptions
- From FESG Fleet Forecast
- Time horizon 2002 to 2020
- Unconstrained demand
- No further improvement to airspace and airport
capacity and delay - Increased aircraft size and productivity
6Key Modelling Assumptions (continued)
- FESG Economic Analysis
- Applying to base case
- No change in NOx technology over forecast period
- Applying to options
- Engine technology is only developed to meet a
stringency increase - Technology development defined by level (TL1
through 5B) - Technology changes applied across engine family
- No impact to aircraft mission and payload
- No fuel burn penalty except for a TL5B solution
( 2) - Market-driven non-compliant engine cut-off
- Competition to maintain market share
7Number and Percentage of Types Failing Stringency
Levels
8Percentage New Engine Deliveries Affect by NOx
Stringency Options
Engine Deliveries from Implementation Date to
2020 FESG Fleet (Aircraft 20 to 650 seats)
9FESG Economic Analysis of NOx Stringency Options
- Models, Databases and Methods
- Assumptions
- LTO NOx Benefits Assessment
- Assessment of Costs
- Cost Benefit Results
10LTO NOx Benefits Assessment Scope and Limitations
- Benefits are NOx emitted over the landing and
take-off cycle using ICAO engine certification
data and ICAO times in mode - Analysis of environmental and health impact of
engine NOx emission has not been made - Results are not appropriate for
- Comparison with other sectors or other transport
modes - Comparison with Local Air Quality Modelling
results - Comparison with Climate Change Modelling results
11LTO NOx Benefits Assessment 2020
Percent Total LTO NOx Reduced
12FESG Economic Analysis of NOx Stringency Options
- Models, Databases and Methods
- Assumptions
- LTO NOx Benefits Assessment
- Assessment of Costs
- Cost Benefit Results
13Assessment of Costs
- Two types of cost of a new NOx certification
standard - Non-Recurring manufacturer technology
acquisition and - engine development costs
- Recurring incremental manufacturing and
airline - operational costs
- Methodology used ensured no double counting
- No projection of how costs might be translated
into engine or fare prices
14Assessment of Manufacturer Non-Recurring Costs
- Total non-recurring manufacturer cost
- TL1 10 million
- TL2 50 million
- TL5A 75 to 150 million
- TL5B 500 to 1,000 million
- __________________________________________________
___
Manufacturer Work Content Associated with Each
Technology Level Category
Technology Level (TL)____
1 2 5A 5B ________________________________________
_____________ Product design X X X X Certificat
ion analysis/ground test X X X X Product
development X X X Certification flight
test X X X Post certification product
improvement X X X Applied technology
development X X Post certification
redesign X X New Technology research X Pote
ntial engine architecture change X
15Assessment of Recurring Operator Manufacturing
Costs
- Incremental recurring manufacturing cost per
engine - TL1 No increase
- TL2 20 thousand
- TL5A 40 thousand
- TL5B 150 thousand
- __________________________________________________
______ - Combustor is approximately 5 of total engine
cost. Additional cost of technology enhancement
per engine based on - TL1 No incremental cost
- TL2 Incremental combustor cost 0.25
- TL5A Incremental combustor cost 0.50
- TL5B Incremental combustor cost 2.50
16Assessment of Recurring Operator Costs
- Maintenance
- up to 2 per engine flight hour
- Spare engine inventory associated with split
fleets - Inventory for unaffected engine fleet
- Inventory for technology enhanced engine fleet
- Costs associated with TL5B
- Additional fuel
- Additional MTOGW to carry the incremental fuel
- Landing fees due to additional weight
- Diminution of value of existing fleet
- TL1 No decrease
- TL2 - 250 thousand
- TL5A - 500 thousand
- TL5B - 1,000 thousand
17FESG Economic Analysis of NOx Stringency Options
- Models, Databases and Methods
- Assumptions
- LTO NOx Benefits Assessment
- Assessment of Costs
- Cost-Benefit Results
18Ranking of Cost per Tonne of NOx Central Analysis
19Qualifies to Economic Analysis
- Assessment of recent events places results two
years out - 2020 and 2030 absolute values would be 2 lower
- Relative ranking unchanged
- Assessment of longer-term benefits
- Effect of ICAO times in mode and aircraft
performance - Actual values of central estimates 20 lower
- Relative ranking unchanged
- Effect of no increased ticket price on demand
- FESG review of CAEP/5 CBA indicates demand effect
0.3-0.35 - Relative ranking unchanged
20Qualifies to Economic Analysis (continued)
- Effect of time period used
- Uncertainty of results increases rapidly for
projections beyond 2020 - Relative cost-benefit ranking for 2030 did not
change - Effect of no further stringency increase on
benefits results - Long-term benefits of CAEP/6 options are reduced
by future stringency - Effect on ranking not studied
- Effect of Discounting
- Relative ranking unchanged
21Qualifies to Economic Analysis (continued)
- Effect of the lead time for 2008 TL5B changes
- Cost-benefit results would be lower but would not
meet levels for options implemented in 2012 due
to earlier introduction of TL1, TL2 and TL5A
enhanced engines under 2008 options - Relative ranking unchanged
- Non-recurring high and low cost estimates
- Relative ranking unchanged
- Residual values
- Relative ranking unchanged
22Summary of Results of Central Analysis
- -10 option has the lowest cost per tonne of NOx
for a given implementation date ( 2008, 2012) - The relative ranking amongst the NOx stringency
options does not change under any of the major
assumptions tested - The relative ranking amongst the NOx stringency
options does not change for the duration of the
forecast period under study - A lesser NOx stringency increase implemented in
2008 could provide a similar NOx benefit to a
much higher stringency implemented in 2012, and
at lower cost, e.g. - - 10 in 2008 - 25 in 2012 - 15 in 2008
- LTO NOx Benefit 146,413 tonnes 156,880
tonnes 196,900 tonnes - Cost (low estimate) 24,709/tonne 247,545/tonne
49,966/tonne -
23Backup Slides
24Cost-Benefit Results of NOx Stringency Options
Central Analysis
Cumulative 2002-2020 Results 2008 Implementation
25Relative Ranking of NOx Stringency Options Do Not
Change with Adjustments to Some of FESG
Assumptions for Operator Costs
2008 Implementation, Discount Rate 0
A
- Without Loss Fleet Value (As shown
- in FESG report, WP19)
- Case A Plus Reducing Spares Inventory cost by 90
(Factor of 10 reduction) - Case A Plus Reducing fuel burn penalty assumption
of 2 for TL5B engines to 0
B
C
26Relative Ranking of NOx Stringency Options Do Not
Change with Adjustments to Some of FESG
Assumptions for Operator Costs
2008 Implementation, Discount Rate 0
A
- Without Loss Fleet Value (As shown
- in FESG report, WP19)
- D Case A Plus Reducing Spares Inventory cost by
90 (Factor of 10 reduction) Plus Reducing fuel
burn penalty assumption of 2 for TL5B engines to
0
D
27Cost-Benefit Results of NOx Stringency Options
Central Analysis
Cumulative 2002-2020 Results 2012 Implementation
28Relative Ranking of NOx Stringency Options Do Not
Change with Adjustments to Some of FESG
Assumptions for Operator Costs
2012 Implementation, Discount Rate 0
A
- Without Loss Fleet Value (As shown
- in FESG report, WP19)
- Case A Plus Reducing Spares Inventory cost by 90
(Factor of 10 reduction) - Case A Plus Reducing fuel burn penalty assumption
of 2 for TL5B engines to 0
B
C
29Relative Ranking of NOx Stringency Options Do Not
Change with Adjustments to Some of FESG
Assumptions for Operator Costs
2012 Implementation, Discount Rate 0
A
- Without Loss Fleet Value (As shown
- in FESG report, WP19)
- D Case A Plus Reducing Spares Inventory cost by
90 (Factor of 10 reduction) Plus Reducing fuel
burn penalty assumption of 2 for TL5B engines to
0
D
30LTO NOx Benefits Assessment Central Analysis
Base Case Results
Total and Percentage Departures and NOx Emissions
by Aircraft Category
31Percentage New Engine Deliveries Affect by NOx
Stringency Options
Engine Deliveries from Implementation Date to
2020 Aircraft greater than 100 seats
32LTO NOx Benefits Assessment Central Analysis
2030 Estimate Results
Cumulative Change in NOx and CO2 Engine Emissions
33Assessment of Total Costs of NOx Stringency
Increase
Incremental Cost Impacts of NOx Stringency
Options 2002-2020
34Cost-Benefit Ranking of NOx Stringency Options
Central Analysis
35Cost-Benefit Ranking of NOx Stringency Options
2002-2030
36Introduction
- Options Studied -5, -10, -15, -20, -25,
-30 below the ICAO CAEP/4 Standard - Implementation dates 2008 and 2012
- Costs are in 2002 U.S. dollars
- A base case in which ICAO does not implement any
of the options is established - The costs and benefits of each option are then
estimated and the results compared against the
base case
37Introduction
- Quantity of CO2 and the relationship between CO2
and NOx are reported - Relationship between noise and emissions
certification standards is discussed but not
addressed in the analysis