Benefits Assessment for Tailored Arrivals

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1 Benefits Assessment for Tailored Arrivals A Year at San Francisco (Dec 3 rd 2007 Dec 31 st 2008) 2009 Environmental Working Group Operations Standing Committee July 28 29, 2009 Kevin Elmer BOEING is a trademark of Boeing Management Company. EOT_RT_Sub_Template.ppt 1/6/2009 1

2 Tailored Arrival Environmental Criterion 1. Data analysis included Tailored Arrivals flight candidates ANA8, ANZ8, JAL2, JAL880, QFA73, SIA16, UAL (1404, 34, 72, 74, 76, 78, 830, 838, 852, 856, 856D, 858, 862, 870, 872, 886, 888, 892, 9816, 9822) Flights that arrived via Woodside (OSI) or Point Reyes (PYE) 2. Primary data source: radar data from the SFO ANOMS8 system 6 days (1/03/08, 1/24/08-1/26/08, 2/23/08 and 11/01/08) were missing due to ANOMS8 outages 3. Flights sorted by Tailored Arrivals sort criteria using ATS clearances and ADS-C reports Analysis of ANOMS8 radar data to verify and refine the initial sorting 4. Fuel consumption calculations: For low speed performance below 10,000 ft altitude, using the Boeing Climbout Program (BCOP) Above 10,000 ft altitude, using the Boeing INFLT tool for cruise & descent. Vertical profile generated from BCOP and INFLT was matched to the mean descent paths of the collective ANOMS8 radar data Common start point at cruise EOT_RT_Sub_Template.ppt 2

3 Tailored Arrival Environmental Criterion, Cont. 5. Tailored Arrivals (TA) sort criteria, using ATS clearances and ADS-C data Non participating - Opted out of procedure or were ineligible Note: As ineligible flights are included in the above statistics, numbers should not be interpreted as pilot participation in Tailored Arrivals Partial Tailored Arrival Met SOME of the TA criteria Full Tailored Arrival Met ALL of the TA criteria 6. Environmental Criterion: Radar data shows no more than ONE Level Flight Segment and that is no more than ½ Nmi. 7. Evaluated all the ANOMS8 data to check if met Environmental Criterion including Non-Tailored Arrivals. EOT_RT_Sub_Template.ppt 3

4 SFO Tailored Arrival Environmental Statistics Data Collected Total Flights * % of Total Eligible Flights Non-TA ** % Partial TA % Tailored Arrival 391 9% Bad-Holding or 223 5% Wrong Runway Not Eligible (Routed through PYE) 1235 N/A * ANOMS8 Data collected for 5551 Total Flights from December 4, 2007 to December 31, 2008 ** Non-TA included non-participating flights and data collected prior to TA start date EOT_RT_Sub_Template.ppt 4

5 Airline Tailored Arrival Environmental Statistics Airline Airplane # Tailored Arrivals # Requested TA ** % ENV * Air New Zealand ER % United Airlines ER % United Airlines % Japan Airlines % Qantas % * Env Met Criterion for Environmental Performance ** Total of Full TA and Partial TA These are the total flights that requested the TA EOT_RT_Sub_Template.ppt 5

6 SFO Airport Noise Monitoring System (ANOMS 8) Data Lateral Tracks Altitude Profile Typical Level Flight (5-10 NM) Extended Level Flight ( NM) Ground Speed Baseline Arrivals RW28R RW28L RW19L Full TA Partial TA EOT_RT_Sub_Template.ppt 6

7 SFO Airport Noise Monitoring System (ANOMS 8) Data, Cont. Yf Lateral Tracks Increased Path Predictability Zf Altitude Profile Increased Altitude Assurance Xf Vk Ground Speed Extended Level Flight (10-60 NM) -1E Df Reduced Speed Variability Full TA Partial TA Partial TA RW19L 200-1E Df EOT_RT_Sub_Template.ppt 7

8 Low Altitude Level Flight (Mean & Std Dev) EOT_RT_Sub_Template.ppt st 6 months of data Full TA's Partial TA's Non TA's Holding or Go Around Env Non TA's Distance in Level Flight, NM Full Year of data Env Non TA's Distance in Level Flight, NM Full TA's Partial TA's Non TA's Holding or Go Around Non TA's From North through Pt Reyes to do...

9 Fuel Consumption (Cruise to Top of Descent to Landing) Non-TA 3,410 lbs 6,470 lbs Partial TA 2,900 lbs 5,650 lbs Full TA 1,980 lbs 3,670 lbs Fuel Saving from Tailored Arrival per Flight Full TA 1,430 lbs 2,800 lbs Partial TA 510 lbs 820 lbs Fuel consumption was calculated using the Boeing Climbout Program (BCOP) for low speed performance below 10,000 ft altitude. Fuel consumption above 10,000 ft altitude was calculated using the Boeing INFLT tool for cruise and descent. The vertical profile generated from BCOP and INFLT was matched to the mean descent paths of the collective ANOMS8 radar data. * Estimates derived from GE90-85B and PW4056 engine data EOT_RT_Sub_Template.ppt 9

10 Fuel Consumption (Cruise to Top of Descent to Landing), Cont Estimated Actual Fuel & CO2 Savings from SFO Tailored Arrivals Air New Zealand Airline Airplane Fuel / CO 2 Saved (lbs) ER United Airlines ER Fuel: 328,900 CO 2 : 1,037,680 Fuel: 509,080 CO 2 : 1,606,147 United Airlines Fuel: 915,600 CO 2 : 2,888,718 Japan Airlines Fuel: 86,800 CO 2 : 273,854 Qantas Fuel: 159,600 CO 2 : 503,538 Fuel / CO 2 Saved (kgs) Fuel: 162,785 CO 2 : 513,585 Fuel: 251,962 CO 2 : 794,941 Fuel: 453,164 CO 2 : 1,429,731 Fuel: 42,960 CO 2 : 135,540 Fuel: 78,992 CO 2 : 249,219 EOT_RT_Sub_Template.ppt 10

11 Trajectory Comparison from Boeing Performance Software Aircraft Height above Field Elevation, ft TA Non-TA Partial TA Distance from Threshold, ft EOT_RT_Sub_Template.ppt 11

12 Emissions Analysis - CREAN to the Runway Basic OTA Profile OTA w/ EDA Profile (11k) Min Congestion Avg Congestion Max Congestion CO2 (3.149*fuel) LBS CO(g) HC(g) NOX(g) EOT_RT_Sub_Template.ppt 12

13 Emissions Analysis - (10,000 to Landing) Total Reduction Relative to Non-TA Full TA Partial TA CO(g/10) HC(g) NOX(Kg) Local Emissions (below 10,000 ft) EOT_RT_Sub_Template.ppt 13

14 Noise Measurement Comparison- SEL (As Measured) Sound Exposure Level (as Measured), db (1688) (173) (263) Non TA's Full TA's Partial TA's (OSI) (665) (74) (168) (1217) Sample Size (2124) EOT_RT_Sub_Template.ppt 14

15 Noise Contour Comparison- 20 Flights per Scenario EOT_RT_Sub_Template.ppt 15

16 Full TA Scenario EOT_RT_Sub_Template.ppt 16

17 Full TA Scenario with Non TA Track Overlay EOT_RT_Sub_Template.ppt 17

18 Non TA Scenario EOT_RT_Sub_Template.ppt 18

19 Full TA / Non TA Comparison EOT_RT_Sub_Template.ppt 19

20 Summary First Year of Tailored Arrivals Operations at San Francisco Fuel Saved 1,999,980 lbs (989,863 kgs) CO2 Emissions Saved 6,309,937 lbs (3,123,016 kgs) Fuel Saved Noise Impact No Significant Change at a few temporary measurement sites Reduction in noise exposure area can be significant Air Quality Overall reduction CO, HC, and NOx (From TOD or 10,000 ) EOT_RT_Sub_Template.ppt 20

21 EOT_RT_Sub_Template.ppt 21

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