161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 1GE022 0.58 0.55 2.37 43.22 3 2 55.35 2.97 52.78 57.98 63.1 53.4 13757 2GE041 0.04 0.04 2.18 20.62 4 2 26.85 1.19 25.9 28.6 30.6 25.9 6681 1GE023 0.52 0.52 2.19 43.71 3 2 57.09 3.10 54.41 59.98 65.0 55.1 14493 1GE024 0.52 0.52 2.21 44.32 3 2 56.09 3.00 53.51 58.88 63.9 54.2 14270 2GE045 0.04 0.04 2.13 19.23 4 2 24.78 1.19 23.7 26.5 28.2 23.9 6317 1GE025 0.57 0.55 2.65 48.02 3 2 64.67 2.94 62.12 67.28 73.7 62.4 14929 2GE042 0.04 0.05 2.61 22.41 4 2 30.46 1.48 29.3 32.4 34.7 29.4 7024 1GE026 0.52 0.52 2.93 49.75 3 2 64.51 2.89 62.01 67.13 73.5 62.3 14928 2GE046 0.04 0.06 2.64 21.56 4 2 29.00 1.3 27.9 30.7 33.0 28.0 6717 1GE027 0.56 0.54 2.33 43.91 3 2 55.86 3.05 53.22 58.61 63.6 53.9 14193 2GE043 0.05 0.04 2.12 19.76 4 2 25.68 1.2 24.6 27.4 29.3 24.8 6538 1GE028 0.52 0.52 2.21 45.74 3 2 55.95 2.85 53.49 58.62 63.7 54.0 14251 2GE047 0.04 0.04 2.13 19.23 4 2 24.73 1.19 23.6 26.5 28.2 23.9 6317 3GE057 0.05 0.04 1.83 17.45 4 2 21.75   24.8 21.0 5931 1GE029 0.52 0.52 1.93 41.66 3 2 52.36 3.03 49.74 55.21 59.7 50.6 13970 2GE044 0.06 0.04 1.91 18.89 4 2 23.80 1.196 22.6 25.5 27.1 23.0 6367 1GE030 0.52 0.52 1.92 43.89 3 2 52.18 2.80 49.76 54.85 59.5 50.4 13931 2GE048 0.05 0.04 1.93 18.42 4 2 23.04 1.19 21.9 24.7 26.3 22.2 6166 2GE054 0.52 0.52 1.92 43.89 3 2 52.18 2.8 49.76 54.85 59.5 50.4 13931 2GE055 0.05 0.04 1.93 18.42 4 2 23.04 1.19 21.9 24.7 26.3 22.2 6166 3GE058 0.05 0.04 1.97 18.27 4 2 23.19   26.4 22.4 6185 1GE031 0.52 0.52 1.94 41.78 3 2 49.21 2.83 46.76 51.89 56.1 47.5 13279 2GE049 0.05 0.04 1.90 18.02 4 2 22.53 1.21 21.3 24.2 25.7 21.8 6093 1GE032 0.38 0.34 1.70 43.24 3 2 54.36 8.8 46.7 62.3 61.9 52.5 15678 2GE050 0.05 0.04 1.92 17.64 4 2 23.32 1.24 19.8 22.7 26.6 22.5 6565 1GE033 0.38 0.34 1.61 42.67 3 2 54.29 6.2 46.3 57.3 61.9 52.4 15602 2GE051 0.05 0.04 1.85 17.37 4 2 22.71 1.30 19.0 22.0 25.9 21.9 6517 5GE085 0.34 0.31 1.23 37.02 11 6 44.20   46.7 39.6 13473 4GE080 0.34 0.3 1.33 38.09 3 2 46.58   53.1 45.0 13860 4GE081 0.04 0.02 1.44 15.05 7 3 18.81   20.3 17.2 5598 2GE052 0.09 0.13 5.80 40.35 3 3 54.66  52.1 56.4 59.1 50.1 20020 3GE062 0.15 0.17 1.32 15.41 5 3 19.55  17.1 21.6 21.1 17.9 7048 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AV AW AX AY AZ BA BB BC BD BE BF BG BH BI BJ UID LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic Original CAEP 2 CAEP 4 Total mass ( g)

 Number

( g/ kg)

 EI NOx ( g/ kN)

 Dp/ Foo ( NOx) Characteristic as % of standards 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 1GE022 28.11 21.26 8.83 3.73 3 2 41.79 2.02 40.17 44.18 46.0 45.9 57.3 68.4 10400 2GE041 24.93 19.68 12.32 4.60 4 2 43.05 0.276 42.7 43.3 47.3 47.8 59.7 71.5 10719 1GE023 28.06 21.34 8.97 3.74 3 2 42.17 2.02 40.58 44.60 46.4 46.3 57.8 68.9 10718 1GE024 27.73 21.07 9.00 3.78 3 2 41.38 1.98 39.83 43.77 45.5 45.4 56.7 67.7 10528 2GE045 24.94 19.72 12.47 4.73 4 2 43.69 0.3 43.3 44.0 48.0 47.9 59.9 71.4 11113 1GE025 23.89 18.65 8.77 3.70 3 2 38.08 1.84 36.70 40.37 41.9 43.9 54.8 66.1 8796 2GE042 22.02 18.25 11.79 4.45 4 2 39.70 0.234 39.4 40.0 43.7 45.9 57.4 69.2 9169 1GE026 23.56 18.32 8.54 3.64 3 2 36.14 1.70 34.80 36.75 39.7 41.8 52.3 63.0 8361 2GE046 21.55 18.09 11.80 4.52 4 2 39.73 0.24 39.5 40.1 43.7 45.9 57.4 69.2 9192 1GE027 29.20 21.80 8.90 3.67 3 2 44.08 2.12 42.30 46.38 48.5 48.1 60.2 71.6 11211 2GE043 25.93 20.17 12.37 4.68 4 2 44.12 0.304 43.7 44.4 48.5 48.4 60.5 72.1 11226 1GE028 28.72 21.32 8.88 3.71 3 2 41.73 1.90 40.25 44.03 45.9 45.7 57.2 68.1 10635 2GE047 25.08 19.72 12.47 4.73 4 2 43.70 0.29 43.3 44.0 48.1 47.8 59.8 71.3 11137 3GE057 28.58 21.76 12.74 4.91 4 2 48.22   53.0 50.2 62.7 73.0 13142 1GE029 30.81 22.94 9.11 3.79 3 2 46.26 2.16 44.57 48.88 50.9 49.3 61.7 72.5 12362 2GE044 28.57 21.69 12.53 4.76 4 2 47.30 0.5 46.7 47.9 52.0 50.3 62.9 74.0 12640 1GE030 32.16 23.09 9.06 3.75 3 2 45.43 1.98 43.90 47.85 50.0 48.2 60.3 70.8 12134 2GE048 27.38 21.05 12.63 4.81 4 2 46.51 0.351 46.0 46.8 51.1 49.4 61.8 72.6 12420 2GE054 32.16 23.09 9.06 3.75 3 2 45.43 1.98 43.90 47.85 50.0 48.3 60.3 70.8 12134 2GE055 27.38 21.05 12.63 4.81 4 2 46.51 0.351 46.0 46.8 51.1 49.4 61.8 72.6 12420 3GE058 26.90 20.85 12.63 4.83 4 2 46.43   51.1 49.4 61.8 72.6 12400 1GE031 32.65 24.02 9.16 3.80 3 2 47.10 2.16 45.47 49.65 51.8 49.0 61.2 71.2 12714 2GE049 28.12 21.30 12.66 4.85 4 2 47.13 0.581 46.5 47.9 51.8 49.8 62.2 72.9 12724 1GE032 37.87 27.11 9.84 4.47 3 2 53.74 1.1 52.4 54.5 59.1 56.3 70.4 82.2 15429 2GE050 27.59 21.44 12.61 4.87 4 2 47.00 0.383 45.0 45.8 51.7 49.3 61.6 71.9 13232 1GE033 39.29 28.02 9.91 4.53 3 2 56.44 1.3 54.7 57.3 62.1 58.5 73.1 84.8 16203 2GE051 28.72 22.01 12.66 4.88 4 2 48.07 0.574 45.1 46.4 52.9 49.8 62.2 72.2 13796 5GE085 45.63 31.74 10.29 4.69 11 6 63.15   65.8 59.1 73.8 83.9 19254 4GE080 43.15 30.3 10.13 4.62 3 2 60.69   66.7 61.2 76.5 87.8 18055 4GE081 31.28 23.54 12.66 4.77 7 3 50.52   53.5 49.1 61.4 70.4 15027 2GE052 44.86 35.39 12.68 5.88 3 3 59.11  58.0 61.0 62.6 56.6 70.8 80.7 21342 3GE062 40.11 31.59 15.55 5.43 5 3 54.58  50.5 57.3 57.8 52.5 65.6 74.9 19680 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BK BL BM BN BO BP BQ BR BS BT BU BV UID Characteristic No T/ O C/ O App Idle Test Eng Max Sigma Range Characteristic % of Reg limit  Smoke Number

 Smoke Number  Number

161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 1GE022 7.1    3 2 7.1 1.1 5.7 7.6 8.3 45.2 2GE041 6.7 4.2 0.0 0.0 4 2 6.7 0.525 6.3 7.5 7.9 42.6 1GE023 7.1    3 2 7.1 1.1 5.7 7.5 8.3 45.4 1GE024 7.1    3 2 7.1 1.1 5.7 7.5 8.3 45.4 2GE045 6.9 4.5 0.0 0.0 4 2 6.9 0.62 6.2 7.7 8.1 44.1 1GE025 5.8    3 2 5.8 0.95 4.6 6.3 6.8 36.1 2GE042 5.6 3.1 0.0 0.0 4 2 5.6 0.608 5.0 6.4 6.6 34.9 1GE026 7.5 3.6 2.4 2.5 3 2 5.7 1.0 4.4 6.1 6.7 35.5 2GE046 5.7 3.1 0.0 0.0 4 2 5.7 0.61 5.0 6.4 6.7 35.5 1GE027 7.2    3 2 7.2 1.1 5.8 7.7 8.4 46.1 2GE043 6.9 4.5 0.0 0.0 4 2 6.9 0.624 6.2 7.7 8.1 44.2 1GE028 7.3 4.7 2.3 2.3 3 2 7.3 1.1 5.9 7.8 8.6 46.7 2GE047 6.9 4.5 0.0 0.0 4 2 6.9 0.64 6.2 7.7 8.1 44.2 3GE057 7.4 5.2 0 0 4 2 7.4   8.7 48.4 1GE029 7.8    3 2 7.8 1.3 6.1 8.4 9.1 50.6 2GE044 6.9 5.4 0.0 0.0 4 2 6.9 0.914 5.9 8.2 8.1 44.8 1GE030 8.2 5.4 2.3 3.4 3 2 8.2 1.4 6.3 8.9 9.6 53.2 2GE048 6.9 5.3 0.0 0.0 4 2 6.9 0.915 5.9 8.2 8.1 44.7 2GE054 8.2 5.4 2.3 3.40 3 2 8.20 1.4 6.3 8.9 9.6 53.1 2GE055 6.9 5.3 0.0 0.0 4 2 6.9 0.915 5.9 8.2 8.1 44.7 3GE058 7.2 5.2 0 0 4 2 7.2   8.4 46.4 1GE031 8.2 5.6 2.3 3.5 3 2 8.2 1.4 6.35 8.85 9.6 53.3 2GE049 7.0 5.5 0.0 0.0 4 2 7.0 0.908 6.1 8.3 8.2 45.5 1GE032 9.7 6.9 0 0 3 2 9.7 2.7 7.4 12.3 11.4 63.8 2GE050 6.9 6.2 0.0 0.0 4 2 6.9 1.07 6.5 8.7 8.1 45.4 1GE033 9.9 7.2 0 0 3 2 9.9 2.8 7.5 12.7 11.6 65.5 2GE051 6.8 6.5 0.0 0.0 4 2 6.8 1.26 6.1 8.9 8.0 44.9 5GE085 10.1 8.6 0.0 0.0 11 6 10.1   10.8 61.9 4GE080 10.09 8.06 0 0 3 2 10.09   11.8 67.4 4GE081 5.9 5.5 0 0 7 3 5.9   6.5 37.0 2GE052 < 3 < 3 < 3 9.90 3 3 10.22  9.4 10.2 11.2 67.5 3GE062     5 3 0.5  0.0 1.93 0.6 3.6 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BW BX BY BZ CA CB CC CD CE UID Fuel per No Spec H/ C Arom T/ O C/ O App Idle LTO cycle Ratio % ( kg)

 Fuel Flow

( kg/ sec)

 Fuel

161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 1GE022 Jet A 1.94 15.3 2.285 1.873 0.616 0.196 797 2GE041 Jet A 1.94 15.3 2.340 1.922 0.630 0.197 811 1GE023 Jet A 1.94 15.3 2.353 1.913 0.632 0.205 823 1GE024 Jet A 1.94 15.3 2.341 1.901 0.621 0.199 809 2GE045 Jet A 1.94 15.3 2.422 1.983 0.650 0.199 830 1GE025 Jet A 1.94 15.3 2.131 1.761 0.577 0.192 760 2GE042 Jet A 1.94 15.3 2.124 1.756 0.585 0.190 758 1GE026 Jet A 1.94 15.3 2.071 1.702 0.5585 0.1852 735 2GE046 Jet A 1.94 15.3 2.148 1.777 0.593 0.188 760 1GE027 Jet A 1.94 15.3 2.430 1.982 0.650 0.199 830 2GE043 Jet A 1.94 15.3 2.409 1.965 0.641 0.201 828 1GE028 Jet A 1.94 15.3 2.359 1.907 0.6138 0.1926 799 2GE047 Jet A 1.94 15.3 2.432 1.983 0.650 0.199 830 3GE057 Jet A 1.94 15.3 2.685 2.162 0.697 0.206 887 1GE029 Jet A 1.94 15.3 2.579 2.081 0.686 0.207 871 2GE044 Jet A 1.94 15.3 2.580 2.096 0.672 0.205 866 1GE030 Jet A 1.94 15.3 2.540 2.020 0.643 0.1963 834 2GE048 Jet A 1.94 15.3 2.594 2.104 0.682 0.203 867 2GE054 Jet A 1.94 15.3 2.54 2.02 0.64 0.20 834 2GE055 Jet A 1.94 15.3 2.594 2.104 0.682 0.203 867 3GE058 Jet A 1.94 15.3 2.605 2.117 0.688 0.205 874 1GE031 Jet A 1.94 15.3 2.596 2.065 0.657 0.196 845 2GE049 Jet A 1.94 15.3 2.629 2.126 0.688 0.205 876 1GE032 Jet A 1.89 16.4 2.702 2.199 0.714 0.226 928 2GE050 Jet A 1.94 15.3 2.702 2.199 0.714 0.226 928 1GE033 Jet A 1.89 16.4 2.767 2.245 0.724 0.228 942 2GE051 Jet A 1.94 15.3 2.767 2.245 0.724 0.228 942 5GE085 Jet A 1.94 15.3 2.989 2.387 0.755 0.227 976 4GE080 Jet A 1.94 15.3 2.904 2.337 0.744 0.227 963 4GE081 Jet A 1.94 15.3 2.904 2.337 0.744 0.227 963 2GE052 Jet A 1.91 1.92 15.9 18.6 2.83 2.33 0.78 0.30 1082 3GE062 Jet A 1.91 1.94 18.1 19.3 2.824 2.311 0.781 0.280 1048 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CF CG CH CI CJ CK CL CM UID No Baro Temp Humidity kW @ Power % CF @ Power kPa K kg/ kg  Ambient

 Loads

Power Extraction  Stage Bleed

161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 1GE022 0  0  97.40 97.82 287  296 .0084. 0140 2GE041 0  0  97.61 98.15 279 293 .00457. 00743 1GE023 0  0  97.40 97.82 287  296 .0084. 0140 1GE024 0  0  97.40 97.82 287  296 .0084. 0140 2GE045 0  0  97.61 98.15 279 293 .00457. 00743 1GE025 0  0  97.40 97.82 287  296 .0084. 0140 2GE042 0  0  97.61 98.15 279 293 .00457. 00743 1GE026 0  0  97.40 97.82 287  296 .0084. 0140 2GE046 0  0  97.61 98.15 279 293 .00457. 00743 1GE027 0  0  97.40 97.82 287  296 .0084. 0140 2GE043 0  0  97.61 98.15 279 293 .00457. 00743 1GE028 0  0  97.40 97.82 287  296 .0084. 0140 2GE047 0  0  97.61 98.15 279 293 .00457. 00743 3GE057 0  0  97.61 98.15 279 293 .0046. 0074 1GE029 0  0  97.40 97.82 287  296 .0084. 0140 2GE044 0  0  97.61 98.15 279 293 .00457. 00743 1GE030 0  0  97.40 97.82 287  296 .0084. 0140 2GE048 0  0  97.61 98.15 279 293 .00457. 00743 2GE054 0  0  97.40 97.82 287 296 .0084. 0140 2GE055 0  0  97.61 98.15 279 293 .00457. 00743 3GE058 0  0  97.61 98.15 279 293 .0046. 0074 1GE031 0  0  97.40 97.82 287  296 .0084. 0140 2GE049 0  0  97.61 98.15 279 293 .00457. 00743 1GE032 0  0  97.66 97.99 292  296 .012. 015 2GE050 0  0  97.61 98.15 279 293 .00457. 00743 1GE033 0  0  97.66 97.99 292  296 .012. 015 2GE051 0  0  97.61 98.15 279 293 .00457. 00743 5GE085 0  0  97.61  98.15 279  293 .00457  .00743 4GE080 0  0  97.61 98.15 279 293 .00457. 00743 4GE081 0  0  97.61 98.15 279 293 .00457. 00743 2GE052 0  0  97.38 98.59 274 299 .001. 00726 3GE062 0  0  97.52 98.62 283 301 .0036. 0151 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CN CO CP CQ CR CS UID  Test Dates

No Manufacturer Test Organisation Test Location From To 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 1GE022 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE041 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 1GE023 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 1GE024 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE045 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 1GE025 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE042 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 1GE026 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE046 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 1GE027 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE043 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 1GE028 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE047 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 3GE057 GE CF6 Ecval Engineering Site IIIB, PTO, Peebles, Ohio, USA 13 Jan 95 17 Jan 95 1GE029 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE044 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 1GE030 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE048 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 2GE054 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE055 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 3GE058 GE CF6 Ecval Engineering Site IIIB, PTO, Peebles, Ohio, USA 13 Jan 95 17 Jan 95 1GE031 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE049 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 1GE032 GE Aircraft Engines CF6 Evaluation Engineering Sites IIIC & IIID, Peebles Test Facility 8 Jun 92 4 Aug 92 2GE050 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 1GE033 GE Aircraft Engines CF6 Evaluation Engineering Sites IIIC & IIID, Peebles Test Facility 8 Jun 92 4 Aug 92 2GE051 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 5GE085 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 4GE080 GE CF6 Evaluation Engineering Site IIIB, PTO, Ohio 13 Jan 95 17 Jan 95 4GE081 GE CF6 Evaluation Engineering Site IIIB, PTO, Ohio 13 Jan 96 16 Mar 96 2GE052 GE GE90 Eval Engineering Site IVD and 6, PTO, Peebles 24 Feb 95 28 Jul 95 3GE062 GE GE90 Eval Engineering Site IIID, PTO, Peebles, Ohio, USA 24 Apr 97 19 Jun 97 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CT CU UID No Remarks 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 1GE022 1. Ref GE Report R84AEB152, Addendum 1 ( Dec 1986). 2. Engine S/ N's 690105 and 690005/ 2.

2GE041 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 1GE023 1. Ref GE Report R84AEB152. 2. Engine S/ N's 690105 and 690005/ 2.

1GE024 1. Ref GE Report R87AEB208 Rev A. ( Jan 88). 2. Engine S/ N's 690105 and 690005/ 2.

2GE045 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 1GE025 1. Ref GE Report R86AEB589. 2. Engine S/ N's 690105 and 690005/ 2.

2GE042 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 1GE026 1. Ref GE Report R88AEB277. 2. Engine S/ N's 690105 and 690005/ 2.

2GE046 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 1GE027 1. Ref GE Reports R84AEB152 and R86AEB144 ( Rev Aug 86). 2. Engine S/ N's 690105 and 690005/ 2.

2GE043 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 1GE028 1. Ref GE Report R88AEB277. 2. Engine S/ N's 690105 and 690005/ 2.

2GE047 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 3GE057 1. GE Report TM95 17. 2. Engine S/ N 704/ 223 & 704/ 234 3. 1862M39 combustor 1GE029 1. Ref GE Report R86AEB160. 2. Engine S/ N's 690105 and 690005/ 2.

2GE044 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 1GE030 1. Ref GE Report R88AEB277. 2. Engine S/ N's 690105 and 690005/ 2.

2GE048 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 2GE054 1. Ref GE Report R88AEB277. 2. Engine S/ N's 690105 and 690005/ 2.

2GE055 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 3GE058 1. GE Report TM95 17. 2. Engine S/ N 704/ 223 & 704/ 234 3. 1862M39 combustor 1GE031 1. Ref GE Report R88AEB266 Rev A ( Jan 91). 2. Engine S/ N's 690105 and 690005/ 2.

2GE049 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 1GE032 1. Ref GE Report R90AEB188. 2. Engine S/ N's 810 101/ 1 and 810 104/ 1.

2GE050 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 1GE033 1. Ref GE Report R90AEB188. 2. Engine S/ N's 810 101/ 1 and 810 104/ 1.

2GE051 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 5GE085 1. Ref. GE Reports R84AEB152, R90AEB188, R95AEB272 2 2. Standard combustor 4GE080 1. GE Report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. Standard combustor 4GE081 1. Ref GE Report TM95 17 & GEAE R95AEB272 2. 2. Engine S/ N 704/ 233, 704/ 234 & 704/ 378 3. Low emissions combustor 2GE052 1. Ref GE Report TM95 45. 2. Engine S/ N 900 108, 900 111 & 900 114. 3. Post certification/ as delivered to service. 4. Smoke < 3 below meas. capa 3GE062 1. GE Report R96AEB292. 2. Engine S/ S 900 173, 900 166 & 900 167 3. DAC II combustor Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CV CW CX CY CZ DA DB DC DD DE DF DG DH 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 pability. 5. DAC I combustor Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 DI DJ DK DL DM DN 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 A B C D E F G UID Engine Combustor Eng B/ P Press Rated No Identification Description Type Ratio Ratio Output kN 193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 5GE086 GE90 76B TF 8.53 34.88 360.6 6GE087 GE90 76B DAC II TF 8.53 34.88 360.6 3GE059 GE90 77B DAC I TF 8.6 35.2 363.42 3GE063 GE90 77B DAC II TF 8.58 35.3 363.42 6GE088 GE90 77B DAC II TF 8.52 35.11 363.4 2GE053 GE90 85B DAC I TF 8.4 38.10 395.31 3GE064 GE90 85B DAC II TF 8.44 38.0 395.31 6GE089 GE90 85B DAC II TF 8.41 37.7 395.3 3GE060 GE90 90B DAC I TF 8.4 39.7 418.13 3GE065 GE90 90B DAC II TF 8.36 39.8 418.13 6GE090 GE90 90B DAC II TF 8.36 39.38 418.1 3GE061 GE90 92B DAC I TF 8.4 40.4 426.72 3GE066 GE90 92B DAC II TF 8.33 40.6 426.72 6GE091 GE90 94B DAC II TF 8.33 40.53 432.8 International Aero Engines 1IA001 V2500 A1 TF 5.3 29.8 111.2 3IA006 V2522 A5 TF 4.88 25.6 102.66 3IA007 V2524 A5 TF 4.81 26.9 109.06 1IA002 V2525 D5 TF 4.82 27.2 111.2 1IA003 V2527 A5 TF 4.82 27.2 111.2 1IA004 V2528 D5 TF 4.66 30.0 124.5 1IA005 V2530 A5 TF 4.54 32.1 133.4 3IA008 V2533 A5 TF 4.46 33.44 140.56 KKBM 1KK001 NK 8 2U MTF 1.24 10.8 103 1KK002 NK 8 2U MTF 1.24 10.8 103 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 H I J K L M N O P Q R S T U UID Data Superseded Data No PR C R superseded by NME DTEPS Other Corr as Out of Date Out of Date UID No Annex 16 Production Service  Data Status  Current Engine Status

 Test Engine Status

193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 5GE086    x   x

6GE087  x    x   x

3GE059  x    x   x x

3GE063  x    x   x

6GE088  x    x   x

2GE053   x   x   x x

3GE064  x    x   x

6GE089  x    x   x

3GE060  x    x   x x

3GE065  x    x   x

6GE090  x    x   x

3GE061  x    x   x x

3GE066  x    x   x

6GE091  x    x   x

1IA001  x    x   x x

3IA006  x    x   x

3IA007  x    x   x

1IA002  x    x   x

1IA003  x    x   x

1IA004  x    x   x

1IA005  x    x   x

3IA008  x    x   x

1KK001   x     x  x

1KK002   x     x

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 V W X Y Z AA AB AC AD AE AF AG AH UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI HC  Number   Dp/ Foo ( HC)

( g/ kg) ( g/ kN)

193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 5GE086 0.04 0.03 0.06 0.52 3 1 0.68 0.058 0.061  0.071 1.1 5.4 241 6GE087 0.04 0.03 0.06 0.52 3 1 0.68 0.058 0.61 0.71 1.1 5.4 241 3GE059 0.07 0.06 0.80 3.83 3 3 5.33  4.58 5.92 6.2 31.6 1938 3GE063 0.04 0.04 0.07 0.56 5 3 0.75  0.44 1.07 0.9 4.6 276 6GE088 0.04 0.03 0.06 0.52 3 1 0.67 0.056 0.60 0.70 1.0 5.3 243 2GE053 0.08 0.07 1.52 3.05 3 3 4.52  4.27 4.79 5.3 26.9 1772 3GE064 0.04 0.04 0.07 0.45 5 3 0.60  0.30 0.92 0.7 3.6 238 6GE089 0.04 0.03 0.05 0.46 3 1 0.58 0.041 0.53 0.61 0.9 4.5 228 3GE060 0.08 0.07 1.34 2.77 3 3 4.01  3.82 4.22 4.7 24.0 1674 3GE065 0.04 0.04 0.07 0.39 5 3 0.52  0.25 0.84 0.6 3.1 218 6GE090 0.04 0.04 0.05 0.43 3 1 0.54 0.036 0.49 0.56 0.8 4.2 226 3GE061 0.09 0.07 1.17 2.64 3 3 3.74  3.58 3.94 4.4 22.4 1594 3GE066 0.04 0.04 0.07 0.37 5 3 0.50  0.24 0.81 0.6 3.1 212 6GE091 0.04 0.04 0.05 0.41 3 1 0.51 0.035 0.47 0.53 0.8 4.0 221 1IA001 0.10 0.11 0.15 0.22 3 1 0.65   1.0 5.1 73 3IA006 0.041 0.041 0.062 0.103 3 1 0.29   0.5 2.3 30 3IA007 0.042 0.042 0.061 0.100 3 1 0.28   0.4 2.2 31 1IA002 0.041 0.041 0.061 0.105 3 1 0.29   0.4 2.3 32 1IA003 0.041 0.041 0.061 0.105 3 1 0.29   0.4 2.3 32 1IA004 0.043 0.041 0.058 0.102 3 1 0.27   0.4 2.1 34 1IA005 0.045 0.041 0.056 0.100 3 1 0.26   0.4 2.0 35 3IA008 0.047 0.043 0.052 0.100 3 1 0.25   0.4 2.0 35 1KK001 0.45 0.55 5.00 103.80 2 2 388.2   505.1 2577.2 39677 1KK002 2.0 2.0 2.6 32.0 2 1 117.1   180.3 920.1 11824 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AI AJ AK AL AM AN AO AP AQ AR AS AT AU UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI CO  Number  Dp/ Foo ( CO)

( g/ kN)

( g/ kg)

193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 5GE086 0.12 0.15 1.58 15.66 3 1 19.08 0.476 18.53  19.39 23.4 19.8 6871 6GE087 0.12 0.15 1.58 15.66 3 1 19.08 0.476 18.53 19.39 23.4 19.8 6871 3GE059 0.09 0.13 6.39 43.32 3 3 58.21  55.7 60.1 63.0 53.4 21173 3GE063 0.15 0.17 1.30 15.26 5 3 19.28  16.9 21.3 20.9 17.7 7005 6GE088 0.12 0.15 1.55 15.52 3 1 18.85 0.47 18.30 19.15 23.1 19.6 6858 2GE053 0.08 0.12 25.35 37.83 3 3 58.54  55.8 60.2 63.3 53.7 22928 3GE064 0.15 0.16 1.10 13.67 5 3 16.51  14.4 18.4 17.9 15.2 6526 6GE089 0.12 0.13 1.30 14.10 3 1 16.47 0.414 16.00 16.75 20.2 17.1 6522 3GE060 0.08 0.11 23.48 35.79 3 3 53.84  51.0 55.7 58.2 49.3 22509 3GE065 0.15 0.15 0.98 12.70 5 3 14.91  13.0 16.7 16.1 13.6 6231 6GE090 0.12 0.13 1.16 13.21 3 1 15.05 0.379 14.62 15.31 18.5 15.7 6305 3GE061 0.08 0.10 21.87 34.70 3 3 51.31  48.4 53.3 55.5 47.0 21891 3GE066 0.15 0.15 0.94 12.35 5 3 14.40  12.5 16.1 15.6 13.2 6142 6GE091 0.12 0.12 1.07 12.69 3 1 14.24 0.358 13.83 14.49 17.5 14.8 6156 1IA001 0.55 0.55 0.77 7.76 3 1 14.8   18.2 15.4 1656 3IA006 0.57 0.67 2.60 13.42 3 1 26.90   33.0 28.0 2760 3IA007 0.54 0.63 2.37 12.64 3 1 24.80   30.4 25.8 2708 1IA002 0.53 0.62 2.44 12.43 3 1 24.9   30.6 25.9 2764 1IA003 0.53 0.62 2.44 12.43 3 1 24.9   30.6 25.9 2764 1IA004 0.47 0.56 2.03 11.53 3 1 21.5   26.4 22.4 2680 1IA005 0.45 0.52 1.81 10.95 3 1 19.7   24.2 20.5 2620 3IA008 0.463 0.515 1.65 9.317 3 1 16.00   19.6 16.6 2241 1KK001 5.5 6.0 21.0 116.0 2 2 466.9   532.0 450.8 47684 1KK002 5.0 6.0 13.0 64.0 2 1 248.5   305.0 258.5 25102 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AV AW AX AY AZ BA BB BC BD BE BF BG BH BI BJ UID LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic Original CAEP 2 CAEP 4 Total mass ( g)

 Number

( g/ kg)

 EI NOx ( g/ kN)

 Dp/ Foo ( NOx) Characteristic as % of standards 193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 5GE086 40.41 31.77 15.09 5.64 3 1 53.80 0.185 53.61  53.98 62.4 56.8 71.0 81.2 19393 6GE087 40.41 31.77 15.09 5.64 3 1 53.80 0.185 53.61 53.98 62.4 56.8 71.0 81.2 19394 3GE059 45.53 35.68 12.46 5.73 3 3 58.62  57.5 60.5 62.1 56.3 70.3 80.2 21308 3GE063 40.65 31.89 15.64 5.45 5 3 55.03  51.0 57.9 58.3 52.7 65.9 75.1 19995 6GE088 40.91 32.09 15.19 5.66 3 1 54.33 0.187 54.14 54.52 63.0 57.1 71.4 81.5 19743 2GE053 52.01 40.27 10.30 6.01 3 3 65.08  63.8 67.5 68.9 59.3 74.2 82.8 25703 3GE064 47.28 35.70 16.73 5.69 5 3 61.92  57.9 65.3 65.6 56.6 70.7 79.0 24478 6GE089 47.25 36.17 16.24 5.86 3 1 61.15 0.227 60.90 61.33 70.9 61.5 76.8 86.1 24177 3GE060 57.34 43.92 10.62 6.11 3 3 70.42  69.1 73.0 74.6 62.5 78.1 86.3 29448 3GE065 53.21 39.13 17.47 5.86 5 3 68.08  64.1 71.9 72.1 60.3 75.4 83.3 28459 6GE090 52.48 39.50 16.94 6.00 3 1 66.78 0.259 66.48 66.95 77.4 65.2 81.5 90.3 27923 3GE061 59.56 45.41 10.89 6.17 3 3 73.05  71.7 75.7 77.4 64.1 80.1 88.2 31175 3GE066 55.90 40.51 17.74 5.92 5 3 70.71  66.8 74.7 74.9 61.8 77.2 84.9 30172 6GE091 56.41 41.74 17.38 6.09 3 1 70.76 0.278 70.43 70.92 83.2 68.7 85.9 94.5 30617 1IA001 37.13 30.82 13.45 5.91 3 1 69.3   80.3 80.7 100.8 120.5 7716 3IA006 24.5 20.8 8.7 4.5 3 1 46   53.3 58.5 73.1 88.9 4720 3IA007 26.2 22 9 4.7 3 1 48.4   56.1 59.8 74.8 90.4 5278 1IA002 26.5 22.3 8.9 4.7 3 1 48.5   56.2 59.6 74.4 89.9 5382 1IA003 26.5 22.3 8.9 4.7 3 1 48.5   56.2 59.6 74.4 89.9 5382 1IA004 30.5 25.1 9.6 4.9 3 1 53.7   62.2 62.2 77.8 92.9 6686 1IA005 33.8 27.1 10.1 5.0 3 1 58.0   67.2 64.5 80.7 94.4 7732 3IA008 36.48 28.67 10.83 5.24 3 1 61.6   71.4 66.8 83.5 96.6 8646 1KK001 13.9 12.9 5.4 2.7 2 2 44.6   49.0 79.6 99.5 135.2 4776 1KK002

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BK BL BM BN BO BP BQ BR BS BT BU BV UID Characteristic No T/ O C/ O App Idle Test Eng Max Sigma Range Characteristic % of Reg limit  Smoke Number

 Smoke Number  Number

193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 5GE086 2.8 1.8 2.9 2.5 3 1 2.9 0.358 2.59  3.23 3.7 22.2 6GE087 2.8 1.8 2.9 2.5 3 1 2.9 0.358 2.59 3.23 3.7 22.4 3GE059 0 0 0 9.84 3 3 10.2  9.4 10.2 11.2 67.4 3GE063     5 3 0.5  0.0 1.92 0.6 3.6 6GE088 2.9 1.8 2.9 2.5 3 1 2.9 0.391 2.60 3.31 3.7 22.4 2GE053 < 3 < 3 < 3 9.60 3 3 9.80  9.2 9.8 10.8 66.4 3GE064     5 3 0.5  0.0 1.92 0.6 3.7 6GE089 3.3 2.4 3 2.5 3 1 3.3 0.648 2.73 4.01 4.2 26.1 3GE060 0 0 0 9.4 3 3 9.5  9.0 9.5 10.5 65.6 3GE065     5 3 0.5  0.0 2.03 0.6 3.8 6GE090 3.6 2.7 3.2 2.5 3 1 3.6 0.713 2.83 4.25 4.6 28.9 3GE061 0 0 0 9.3 3 3 9.5  8.9 9.5 10.5 66.0 3GE066     5 3 0.5  0.0 2.07 0.6 3.8 6GE091 3.7 2.9 3.2 2.5 3 1 3.7 0.726 2.89 4.29 4.8 30.0 1IA001     3 1 3.5   4.5 19.6 3IA006     3 1 9   11.6 49.4 3IA007     3 1 9   11.6 50.2 1IA002     3 1 9.0   11.6 50.4 1IA003     3 1 9.0   11.6 50.4 1IA004     3 1 9.0   11.6 52.0 1IA005     3 1 9.0   11.6 53.0 3IA008     3 1 9   11.6 53.8 1KK001       23.5   30.2 128.8 1KK002

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BW BX BY BZ CA CB CC CD CE UID Fuel per No Spec H/ C Arom T/ O C/ O App Idle LTO cycle Ratio % ( kg)

 Fuel Flow

( kg/ sec)

 Fuel

193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 5GE086 Jet A 1.92 17.4 2.781 2.280 0.763 0.267 1017 6GE087 Jet A 1.92 17.4 2.781 2.280 0.763 0.267 1017 3GE059 Jet A 1.94 17.2 2.837 2.321 0.774 0.295 1071 3GE063 Jet A 1.91 1.94 18.1 19.3 2.832 2.332 0.787 0.281 1054 6GE088 Jet A 1.92 17.4 2.806 2.301 0.768 0.269 1026 2GE053 Jet A 1.91 1.92 15.9 18.6 3.19 2.60 0.85 0.30 1149 3GE064 Jet A 1.91 1.94 18.1 19.3 3.169 2.583 0.852 0.292 1134 6GE089 Jet A 1.92 17.4 3.115 2.55 0.832 0.282 1107 3GE060 Jet A 1.94 17.2 3.419 2.756 0.884 0.313 1208 3GE065 Jet A 1.91 1.94 18.1 19.3 3.414 2.772 0.899 0.3 1193 6GE090 Jet A 1.92 17.4 3.348 2.733 0.878 0.291 1166 3GE061 Jet A 1.94 17.2 3.523 2.830 0.902 0.316 1231 3GE066 Jet A 1.91 1.94 18.1 19.3 3.515 2.844 0.917 0.304 1217 6GE091 Jet A 1.92 17.4 3.514 2.848 0.908 0.296 1203 1IA001 Jet A   1.113 0.924 0.334 0.124 442 3IA006 Jet A   0.971 0.817 0.311 0.118 407 3IA007 Jet A   1.042 0.868 0.328 0.123 429 1IA002 Jet A   1.053 0.880 0.319 0.128 437 1IA003 Jet A   1.053 0.880 0.319 0.128 437 1IA004 Jet A   1.209 0.996 0.353 0.134 476 1IA005 Jet A   1.331 1.077 0.377 0.138 504 3IA008 Jet A   1.426 1.1447 0.3901 0.1363 517 1KK001 TS 1 2 19 1.75 1.17 0.58 0.24 742 1KK002 TS 1 2 18 1.75 1.33 0.55 0.22 724 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CF CG CH CI CJ CK CL CM UID No Baro Temp Humidity kW @ Power % CF @ Power kPa K kg/ kg  Ambient

 Loads

Power Extraction  Stage Bleed

193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 5GE086 0  0  97.3  98.2 279.1  281.6 .0022  .0064 6GE087 0  0  97.3  98.2 279.1  281.6 .0022  .0064 3GE059 0  0  97.38 98.59 274 299 .001. 0073 3GE063 0  0  97.52 98.62 283 301 .0036. 0151 6GE088 0  0  97.3  98.2 279.1  281.6 .0022  .0064 2GE053 0  0  97.38 98.59 274 299 .001. 00726 3GE064 0  0  97.52 98.62 283 301 .0036. 0151 6GE089 0  0  97.3  98.2 279.1  281.6 .0022  .0064 3GE060 0  0  97.38 98.59 274 299 .001. 0073 3GE065 0  0  97.52 98.62 283 301 .0036. 0151 6GE090 0  0  97.3  98.2 279.1  281.6 .0022  .0064 3GE061 0  0  97.38 98.59 274 299 .001. 0073 3GE066 0  0  97.52 98.62 283 301 .0036. 0151 6GE091 0  0  97.3  98.2 279.1  281.6 .0022  .0064 1IA001 0  4.5 7% 101.3 286 0.0048 3IA006 0  6.2%/ 5.5% 7%/ 30% 101.0 101.8 288 296 .0086. 0114 3IA007 0  6.2%/ 5.5% 7%/ 30% 101.0 101.8 288 296 .0086. 0114 1IA002 0  4.5 7% 101.0 101.8 288  296 .0086. 0114 1IA003 0  4.5 7% 101.0 101.8 288  296 .0086. 0114 1IA004 0  4.5 7% 101.0 101.8 288  296 .0086. 0114 1IA005 0  4.5 7% 101.0 101.8 288  296 .0086. 0114 3IA008 0  4.5 7 101.0 101.8 288 296 .0086. 0114 1KK001 0  0  102.6 300 0.00876 1KK002 0  0  102.7 293 .00905 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CN CO CP CQ CR CS UID  Test Dates

No Manufacturer Test Organisation Test Location From To 193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 5GE086 GE GE90 Eval Engineering Site IIID, PTO, Peebles, Ohio, USA 9 Jan 00 12 Jan 00 6GE087 GE GE90 Eval Engineering Site IIID, PTO, Peebles, OH 9 Jan 00 12 Jan 00 3GE059 GE GE90 Eval Engineering Site IVD & 6, PTO, Peebles, Ohio, USA 24 Feb 95 28 Jul 95 3GE063 GE GE90 Eval Engineering Site IIID, PTO, Peebles, Ohio, USA 24 Apr 97 19 Jun 97 6GE088 GE GE90 Eval Engineering Site IIID, PTO, Peebles, OH 9 Jan 00 12 Jan 00 2GE053 GE GE90 Eval Engineering Site IVD and 6, PTO, Peebles 24 Feb 95 28 Jul 95 3GE064 GE GE90 Eval Engineering Site IIID, PTO, Peebles, Ohio, USA 24 Apr 97 19 Jun 97 6GE089 GE GE90 Eval Engineering Site IIID, PTO, Peebles, OH 9 Jan 00 12 Jan 00 3GE060 GE GE90 Eval Engineering Site IVD & 6, PTO, Peebles, Ohio, USA 24 Feb 95 28 Jul 95 3GE065 GE GE90 Eval Engineering Site IIID, PTO, Peebles, Ohio, USA 24 Apr 97 19 Jun 97 6GE090 GE GE90 Eval Engineering Site IIID, PTO, Peebles, OH 9 Jan 00 12 Jan 00 3GE061 GE GE90 Eval Engineering Site IVD & 6, PTO, Peebles, Ohio, USA 24 Feb 95 28 Jul 95 3GE066 GE GE90 Eval Engineering Site IIID, PTO, Peebles, Ohio, USA 24 Apr 97 19 Jun 97 6GE091 GE GE90 Eval Engineering Site IIID, PTO, Peebles, OH 9 Jan 00 12 Jan 00 1IA001 International Aero Engines Pratt & Whitney East Hartford, CT, USA 2 Jun 88 2 Jun 88 3IA006 International Aero Engines Pratt & Whitney East Hartford, CT, USA 12 Aug 92 13 Aug 92 3IA007 International Aero Engines Pratt & Whitney East Hartford, CT, USA 12 Aug 92 13 Aug 92 1IA002 International Aero Engines Pratt & Whitney East Hartford, CT, USA 12 Aug 92 13 Aug 92 1IA003 International Aero Engines Pratt & Whitney East Hartford, CT, USA 12 Aug 92 13 Aug 92 1IA004 International Aero Engines Pratt & Whitney East Hartford, CT, USA 12 Aug 92 13 Aug 92 1IA005 International Aero Engines Pratt & Whitney East Hartford, CT, USA 12 Aug 92 13 Aug 92 3IA008 International Aero Engines Pratt & Whitney East Hartford, CT, USA 12 Aug 92 13 Aug 92 1KK001 KKBM State Inst for Civ Aviation Sheremetjevo, Moscow 12 Jul 89

1KK002 KKBM State Inst for Civ Aviation Sheremetjevo, Moscow 14 Jun 90

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CT CU UID No Remarks 193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 5GE086 1. GE Report R97AEB298 2. Engine S/ N 900326 6GE087 1. Ref. GE Report R97AEB298, 2. Engine S/ N 900326 3. Turbomachinery incorporating 3D aero 3GE059 1. GE Report TM95 17. 2. Engine S/ N 704/ 223 & 704/ 234 3. DAC I combustor 3GE063 1. GE Report R96AEB292. 2. Engine S/ S 900 173, 900 166 & 900 167 3. DAC II combustor 6GE088 1. Ref. GE Report R97AEB298, 2. Engine S/ N 900326 3. Turbomachinery incorporating 3D aero 2GE053 1. Ref GE Report TM95 45. 2. Engine S/ N 900 108, 900 111 & 900 114. 3. Post certification/ as delivered to service. 4. Smoke < 3 below meas. capa 3GE064 1. GE Report R96AEB292. 2. Engine S/ S 900 173, 900 166 & 900 167 3. DAC II combustor 6GE089 1. Ref. GE Report R97AEB298, 2. Engine S/ N 900326 3. Turbomachinery incorporating 3D aero 3GE060 1. GE Report TM95 17. 2. Engine S/ N 704/ 223 & 704/ 234 3. DAC I combustor 3GE065 1. GE Report R96AEB292. 2. Engine S/ S 900 173, 900 166 & 900 167 3. DAC II combustor 6GE090 1. Ref. GE Report R97AEB298, 2. Engine S/ N 900326 3. Turbomachinery incorporating 3D aero 3GE061 1. GE Report TM95 17. 2. Engine S/ N 704/ 223 & 704/ 234 3. DAC I combustor 3GE066 1. GE Report R96AEB292. 2. Engine S/ S 900 173, 900 166 & 900 167 3. DAC II combustor 6GE091 1. Ref. GE Report R97AEB298, 2. Engine S/ N 900326 3. Turbomachinery incorporating 3D aero 1IA001 V2500 renamed V2500 A1 3IA006

3IA007

1IA002

1IA003

1IA004

1IA005

3IA008

1KK001 1. Data obtained on aircraft ( Tu 154A) 2. In service engine( s), tested after overhaul 1KK002 1. Data obtained on aircraft ( Tu 154A) 2. In service engine( s), tested after overhaul Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CV CW CX CY CZ DA DB DC DD DE DF DG DH 193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 pability. 5. DAC I combustor Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 DI DJ DK DL DM DN 193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 A B C D E F G UID Engine Combustor Eng B/ P Press Rated No Identification Description Type Ratio Ratio Output kN 225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 1KK003 NK 86 MTF 1.33 13.4 127.53 1KK004 NK 86A MTF 1.13 13.2 130.47 1KK005 NK 86MA MTF 1.13 13.2 130.47 Pratt & Whitney Aircraft Group 1PW035 JT15D 1 series TF 3.3 9.76 9.79 1PW036 JT15D 4 series TF 2.68 10.1 11.12 1PW037 JT15D 5,  5A,  5B TF 2.1 12.3 12.90 1PW038 JT15D 5C TF 2.1 13.3 14.19 1PW001 JT3D 3B TF 1.4 13.6 80.06 1PW003 JT3D 7 series Smoke fix 14 70KC TF 1.4 13.4 84.52 1PW002 JT3D 7 series 14 57D TF 1.4 13.4 84.52 1PW008 JT8D 11 MTF 1.00 17.17 66.72 1PW010 JT8D 15 Reduced emissions MTF 1.03 16.81 68.94 1PW009 JT8D 15 Smoke fix MTF 1.03 16.81 68.94 1PW011 JT8D 15A MTF 1.08 16.45 68.94 1PW013 JT8D 17 Reduced emissions MTF 1.02 17.01 71.17 1PW012 JT8D 17 Smoke fix MTF 1.01 17.01 71.17 1PW014 JT8D 17A MTF 1.05 16.87 71.17 1PW015 JT8D 17AR MTF 0.96 17.28 77.42 1PW016 JT8D 17R MTF 0.97 18.24 77.42 1PW017 JT8D 209 MTF 1.80 18.30 85.60 4PW068 JT8D 217 Environmental Kit ( E_ Kit) MTF 1.73 19.66 92.74 1PW018 JT8D 217 series MTF 1.73 19.66 92.74 4PW069 JT8D 217A Environmental Kit ( E_ Kit) MTF 1.73 19.66 92.74 4PW070 JT8D 217C Environmental Kit ( E_ Kit) MTF 1.70 19.05 92.74 4PW071 JT8D 219 Environmental Kit ( E_ Kit) MTF 1.70 20.27 96.52 1PW019 JT8D 219 MTF 1.70 20.27 96.52 1PW005 JT8D 7 series Reduced emissions MTF 1.05 15.82 62.27 1PW004 JT8D 7 series Smoke fix MTF 1.05 15.82 62.27 1PW007 JT8D 9 series Reduced emissions MTF 1.04 15.88 64.5 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 H I J K L M N O P Q R S T U UID Data Superseded Data No PR C R superseded by NME DTEPS Other Corr as Out of Date Out of Date UID No Annex 16 Production Service  Data Status  Current Engine Status

 Test Engine Status

225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 1KK003   x     x  x

1KK004   x     x x x

1KK005  x    x   x

1PW035 x      x  x x

1PW036 x      x  x x

1PW037  x     x  x x

1PW038  x     x  x x

1PW001 x      x  x x

1PW003 x      x  x x

1PW002 x      x  x x

1PW008 x     x   x x

1PW010  x     x  x x

1PW009 x     x   x x

1PW011  x     x  x x

1PW013  x     x  x x

1PW012 x     x   x x

1PW014  x     x  x x

1PW015  x     x  x x

1PW016  x     x  x x

1PW017  x     x  x x

4PW068  x     x  x x

1PW018  x     x  x x

4PW069  x     x  x x

4PW070  x     x  x

4PW071  x     x  x

1PW019  x     x  x x

1PW005  x     x  x x

1PW004 x       x x x

1PW007  x     x  x x

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 V W X Y Z AA AB AC AD AE AF AG AH UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI HC  Number   Dp/ Foo ( HC)

( g/ kg) ( g/ kN)

225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 1KK003 0.5 0.6 1.2 52.0 3 3 135   157.5 803.5 17379 1KK004 0.2 0.2 2.2 15.3 2 1 45.2   69.6 355.2 5988 1KK005 0.16 0.13 0.30 4.60 7 5 13.5 3.7 8.7 17.1 15.2 77.4 1773 1PW035 0.01 0.01 4.43 50.5 1 1 190.65   293.6 1498.1 1866 1PW036 0.09 0.19 5.15 40.0 1 1 152.83   235.4 1200.9 1706 1PW037 0 1.3 11.7 119.1 1 1 479.8   738.9 3769.9 5715 1PW038 0 0.67 16.0 96.67 1 1 312.8   481.7 2457.7 4439 1PW001 4.0 2.0 4.0 112.0  2 303.9   395.4 2017.6 24363 1PW003       143.0   220.2 1123.7 1PW002 0.50 0.40 2.10 123.00   293.9   452.6 2309.4 24838 1PW008 0.40 0.45 1.4 10.0 14 13 36.8   39.5 201.6 2455 1PW010 0.24 0.28 0.55 1.46 8 3 6.1   7.1 36.3 428 1PW009 0.25 0.25 1.65 11.0 8 7 39.3   43.4 221.2 2713 1PW011 0.25 0.33 0.65 1.86 7 2 7.2   9.4 47.8 497 1PW013 0.22 0.27 0.52 1.25 8 3 5.3   6.2 31.5 379 1PW012 0.69 0.79 1.96 10.2 8 7 37.2 9.3  41.0 209.4 2646 1PW014 0.25 0.30 0.64 6.6 7 2 6.6   8.6 43.8 1543 1PW015 0.21 0.27 0.55 1.33 8 3 5.2   6.1 31.0 403 1PW016 0.21 0.27 0.53 0.95 8 3 4.2   4.9 25.0 329 1PW017 0.35 0.50 1.69 4.03 3 1 12.2   18.8 95.9 1047 4PW068 0.00 0.00 0.00 0.00 3 1 0.00   0.0 0.0 0 1PW018 0.28 0.43 1.60 3.33 3 1 10.1   15.6 79.4 937 4PW069 0.00 0.00 0.00 0.00 3 1 0.00   0.0 0.0 0 4PW070 0.00 0.00 0.00 0.00 3 1 0.00   0.0 0.0 0 4PW071 0.00 0.00 0.00 0.00 3 1 0.00   0.0 0.0 0 1PW019 0.27 0.42 1.59 3.48 3 1 9.9   15.2 77.8 951 1PW005 0.25 0.25 0.4 3.8 7 2 13.2   17.2 87.6 830 1PW004 0.4 0.5 1.6 10.6 14 13 37.2   39.9 203.8 2315 1PW007 0.15 0.18 0.60 3.12 7 2 11.1   14.4 73.7 713 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AI AJ AK AL AM AN AO AP AQ AR AS AT AU UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI CO  Number  Dp/ Foo ( CO)

( g/ kN)

( g/ kg)

225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 1KK003 3.9 4.2 9.3 54.4 3 3 158.2   171.1 145.0 20396 1KK004 1.8 2.2 7.8 38.0 2 1 120.7   148.2 125.6 15703 1KK005 1.55 1.90 5.90 29.80 7 5 94.6 22.5 61.3 113 100.5 85.1 12334 1PW035 2.65 3.50 40.5 132 1 1 541.97   665.2 563.8 5306 1PW036 2.1 3.18 32 97 1 1 401.30   492.6 417.4 4478 1PW037 0 1.15 38.6 119.2 1 1 476.1   584.4 495.3 6142 1PW038 2.52 4.18 49.24 124.60 1 1 443.1   543.9 460.9 6288 1PW001 1.5 2.8 24.5 98.0  2 288.1   328.2 278.2 23092 1PW003       187.0   229.5 194.5 1PW002 0.89 1.90 19.50 138.99   353.5   433.9 367.7 29880 1PW008 1.2 1.9 9.4 35.0 14 13 134.7   139.8 118.4 8983 1PW010 1.03 1.15 2.77 11.0 8 3 42.6   46.1 39.0 2955 1PW009 0.7 1.0 9.6 35.2 8 7 130.6   137.4 116.4 9054 1PW011 1.08 1.2 2.9 12.93 8 3 46.8   50.6 42.9 3177 1PW013 0.95 1.10 2.67 10.46 8 3 39.4   42.6 36.1 2826 1PW012 0.74 1.00 8.54 31.00 8 7 112.5 12.4  118.3 100.3 8005 1PW014 1.07 1.16 2.88 12.46 8 3 43.8   47.4 40.1 3147 1PW015 0.93 1.08 2.68 10.7 8 3 37.2   40.2 34.1 2898 1PW016 0.95 1.03 2.54 9.43 8 3 34.8   37.6 31.9 2716 1PW017 1.03 1.4 4.37 14.1 3 1 40.6   49.8 42.2 3476 4PW068 0.42 0.47 3.54 15.31 3 1 39.8   48.9 41.4 3693 1PW018 0.80 1.23 4.17 12.27 3 1 34.8   42.7 36.2 3229 4PW069 0.42 0.47 3.54 15.31 3 1 39.8   48.9 41.4 3693 4PW070 0.42 0.49 3.79 17.89 3 1 45.8   56.2 47.6 4244 4PW071 0.42 0.46 3.57 17.19 3 1 41.7   51.2 43.4 4021 1PW019 0.73 1.20 4.07 12.63 3 1 33.5   41.1 34.8 3234 1PW005 0.9 1.1 2.2 14.3 7 2 50.9   52.9 44.8 3186 1PW004 1.5 2.0 10.5 35.5 14 13 130.9   135.8 115.1 8147 1PW007 1.04 1.11 2.14 14.14 7 2 50.2   57.2 48.5 3241 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AV AW AX AY AZ BA BB BC BD BE BF BG BH BI BJ UID LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic Original CAEP 2 CAEP 4 Total mass ( g)

 Number

( g/ kg)

 EI NOx ( g/ kN)

 Dp/ Foo ( NOx) Characteristic as % of standards 225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 1KK003 12.8 12.1 5.1 2.7 3 3 41.3   43.7 65.5 81.9 108.2 5440 1KK004 15.7 12.4 5.8 3.1 2 1 46.1   53.4 80.5 100.6 133.2 6106 1KK005 13.0 9.4 3.9 2.3 4 4 35.5 2.3 32 40.1 37.3 56.2 70.2 93.0 4633 1PW035 7.6 6.77 3.44 1.75 1 1 26.85   31.1 52.3 65.4 60.8 263 1PW036 9.23 8.56 5.29 2.63 1 1 36.77   42.6 70.8 88.5 82.9 409 1PW037 11.13 10.08 4.93 1.66 1 1 37.3   43.2 66.9 83.6 79.2 481 1PW038 9.93 9.79 5.23 1.08 1 1 32.0   37.1 55.7 69.6 66.4 454 1PW001 12.1 9.9 4.8 2.5  2 34.3   37.7 56.1 70.2 88.3 2740 1PW003       51.5   59.7 89.4 111.7 144.0 1PW002 12.69 9.59 5.30 2.20   34.4   39.9 59.7 74.6 96.2 2909 1PW008 18.9 14.6 5.8 2.75 14 13 56.1   57.6 77.5 96.9 112.6 3740 1PW010 19.4 15.1 6.9 3.2 5 2 59.6   65.5 89.0 111.3 130.7 4144 1PW009 19.1 15.0 5.9 3.0 8 7 57.9   60.1 81.6 102.0 119.9 3989 1PW011 18.1 13.9 6.6 3.1 5 2 51.4   56.5 77.5 96.9 114.0 3648 1PW013 20.6 15.7 8.0 3.2 5 2 63.7   70.0 94.6 118.3 140.1 4559 1PW012 19.20 15.23 6.10 3.3 8 7 60.2 7.2  62.5 84.4 105.5 125.0 4283 1PW014 19.1 14.3 6.7 3.2 5 2 55.1   60.6 82.2 102.7 121.7 3935 1PW015 24.5 16.0 8.0 3.2 5 2 64.6   71.0 95.3 119.1 144.6 5039 1PW016 25.3 17.6 8.4 3.3 5 2 72.3   79.5 104.0 129.9 156.9 5623 1PW017 22.8 19.0 8.8 3.5 3 1 59.3   68.7 89.7 112.2 140.1 5075 4PW068 17.54 13.54 7.66 4.57 3 1 49.4   57.3 72.2 90.3 113.6 4582 1PW018 25.7 20.6 9.1 3.7 3 1 64.6   74.9 94.4 118.0 148.4 5985 4PW069 17.54 13.54 7.66 4.57 3 1 49.4   57.3 72.2 90.3 113.6 4582 4PW070 16.49 13.02 7.65 4.05 3 1 45.5   52.7 67.5 84.3 106.5 4216 4PW071 18.72 13.73 7.65 4.16 3 1 47.7   55.3 68.7 85.8 107.5 4604 1PW019 27.0 20.8 9.13 3.6 3 1 63.3   73.4 91.1 113.9 142.7 6106 1PW005 17.2 14.0 6.3 3.15 4 2 52.3   57.5 80.3 100.3 115.1 3281 1PW004 17.1 13.5 5.5 2.7 14 13 49.5   50.9 71.0 88.7 101.8 3078 1PW007 19.3 14.5 6.0 2.9 4 2 54.2   59.6 83.1 103.8 120.2 3488 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BK BL BM BN BO BP BQ BR BS BT BU BV UID Characteristic No T/ O C/ O App Idle Test Eng Max Sigma Range Characteristic % of Reg limit  Smoke Number

 Smoke Number  Number

225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 1KK003     1 1 22.1   28.4 128.5 1KK004     10

1KK005     10 7 9.9 2.9 6 16 10.5 47.8 1PW035 15    1 1 15   19.3 43.2 1PW036 14.1    1 1 14.1   18.1 42.0 1PW037 18.5    1 1 18.5   24.1 58.1 1PW038 17.1 15.1   2 2 17.1 2.23 15.5 17.1 20.1 49.7 1PW001      2 54.5   63.9 254.1 1PW003       18   23.2 93.5 1PW002       52   66.9 270.0 1PW008     14 13 23   24.0 90.9 1PW010 15.7    5 3 15.7   17.3 65.9 1PW009     8 7 23.8   25.3 96.6 1PW011 15.7    4 3 15.7   17.3 65.9 1PW013 16.8    5 3 16.8   18.5 71.1 1PW012     8 7 24 3  25.5 98.2 1PW014 16.8    5 3 16.8   18.5 71.1 1PW015 19.6    5 3 19.6   21.6 84.9 1PW016 19.6    5 3 19.6   21.6 84.9 1PW017 11.1    3 1 11.1   14.3 57.8 4PW068 6.1    3 1 6.1   7.9 32.7 1PW018 13.2    3 1 13.3   17.1 70.8 4PW069 6.1    3 1 6.1   7.9 32.7 4PW070 6.1    3 1 6.1   7.9 32.7 4PW071 6.9    3 1 6.9   8.9 37.2 1PW019 14.3    3 1 14.5   18.7 78.1 1PW005 9.5    4 2 9.5   11.1 41.3 1PW004 22.2    14 13 22.2   23.2 86.1 1PW007 10.1    4 2 10.1   11.8 44.4 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BW BX BY BZ CA CB CC CD CE UID Fuel per No Spec H/ C Arom T/ O C/ O App Idle LTO cycle Ratio % ( kg)

 Fuel Flow

( kg/ sec)

 Fuel

225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 1KK003 TS 1 2 18.5 2.40 1.60 0.58 0.21 779 1KK004 TS 1 2 19 2.050 1.700 0.600 0.235 821 1KK005 TS 1 2 18.6 2.050 1.700 0.600 0.235 821 1PW035 Jet A 1 1.85 < 20 0.148 0.124 0.051 0.023 71 1PW036 Jet A 1 1.85 < 20 0.1697 0.143 0.059 0.0261 81 1PW037 Jet A 1 1.85  0.2054 0.1727 0.0660 0.0296 93 1PW038 Jet A 1 1.85  0.2151 0.1802 0.0678 0.0276 92 1PW001 Jet A   1.174 0.932 0.346 0.135 466 1PW003 Jet A   1.254 1.032 0.389 0.128 482 1PW002 Jet A   1.254 1.032 0.389 0.128 482 1PW008 Jet A   1.121 0.9136 0.3339 0.1455 475 1PW010 Jet A   1.178 0.9450 0.3402 0.1477 486 1PW009 Jet A   1.178 0.9450 0.3403 0.1477 486 1PW011 Jet A   1.115 0.8955 0.3120 0.1372 454 1PW013 Jet A   1.245 0.9970 0.3540 0.1474 499 1PW012 Jet A 1.89  1.245 0.997 0.354 0.147 498 1PW014 Jet A   1.173 0.9344 0.3304 0.1401 470 1PW015 Jet A   1.365 1.047 0.3574 0.1477 512 1PW016 Jet A   1.417 1.103 0.3755 0.1550 537 1PW017 Jet A  19.2 1.191 0.9828 0.3592 0.1303 469 4PW068 Jet A  18 1.320 1.078 0.3833 0.1372 504 1PW018 Jet A   1.320 1.078 0.3833 0.1372 504 4PW069 Jet A  18 1.320 1.078 0.3833 0.1372 504 4PW070 Jet A  18 1.282 1.045 0.363 0.137 493 4PW071 Jet A  18 1.354 1.085 0.3817 0.1344 501 1PW019 Jet A  19.2 1.354 1.085 0.3817 0.1344 501 1PW005 Jet A   0.9892 0.8113 0.2861 0.1291 419 1PW004 Jet A   0.9892 0.8113 0.2861 0.1291 419 1PW007 Jet A   1.040 0.8453 0.2977 0.1323 433 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CF CG CH CI CJ CK CL CM UID No Baro Temp Humidity kW @ Power % CF @ Power kPa K kg/ kg  Ambient

 Loads

Power Extraction  Stage Bleed

225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 1KK003 0  0  102.7 103.0 290  291 .00915 1KK004 0  0  102.3 270 .00238 1KK005 0  0  101.2 102.4 260  298 .00079. 0200 1PW035 0  0  100.526 290 0.0079 1PW036 0  0  103.146 257 0.0015 1PW037 0  0  99.42 280.3 .0036 1PW038 0  0  101.7 300 .010 1PW001 0  0

1PW003 0  0

1PW002 0  0

1PW008 0  0   262  300

1PW010 0  0   266  297

1PW009 0  0   269  302

1PW011 0  0   266  297

1PW013 0  0   266  297

1PW012 0  0   269  303 0.0029 0.0093 1PW014 0  0   266  297

1PW015 0  0   266  297

1PW016 0  0   266  297

1PW017 0  0   275  288

4PW068 0  0  98.8 103.1 271  281 .0009  .0047 1PW018 0  0   275  288

4PW069 0  0  98.8 103.1 271  281 .0009  .0047 4PW070 0  0  98.8 103.1 271  281 .0009  .0047 4PW071 0  0  98.8 103.1 271  281 .0009  .0047 1PW019 0  0   275  288

1PW005 0  0   270  311

1PW004 0  0  100 102 262  300 0.0005 0.0123 1PW007 0  0   270  311

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CN CO CP CQ CR CS UID  Test Dates

No Manufacturer Test Organisation Test Location From To 225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 1KK003 KKBM State Inst for Civ Aviation Sheremetjevo, Moscow 15 Jun 89

1KK004 KKBM KKBM Samara City 4 Oct 87

1KK005 KKBM KKBM Samara City 18 Jul 87 20 Jan 90 1PW035 Pratt & Whitney ( Canada) Pratt & Whitney ( Canada) Longueuil, Quebec 17 Aug 77

1PW036 Pratt & Whitney ( Canada) Pratt & Whitney ( Canada) Longueuil, Quebec 1 Feb 73

1PW037 Pratt & Whitney ( Canada) Pratt & Whitney ( Canada) Longueuil, Quebec 16 Apr 93 22 Apr 93 1PW038 Pratt & Whitney ( Canada) Pratt & Whitney ( Canada) Longueuil, Quebec 13 Jul 93 13 Jul 93 1PW001 Pratt & Whitney P& WA East Hartford, CT, USA. 8 Mar 72 12 Sep 74 1PW003 Pratt & Whitney P& WA East Hartford, CT, USA.

1PW002 Pratt & Whitney P& WA East Hartford, CT, USA.

1PW008 Pratt & Whitney P& WA E Hartford, CT, USA 26 Feb 80 18 Jun 80 1PW010 Pratt & Whitney P& WA E Hartford, CT, USA 7 Dec 79 19 Jun 80 1PW009 Pratt & Whitney P& WA E Hartford, CT, USA Apr 76 Mar 77 1PW011 Pratt & Whitney P& WA E Hartford, CT, USA 7 Dec 79 19 Jun 80 1PW013 Pratt & Whitney P& WA E Hartford, CT, USA 7 Dec 79 19 Jun 80 1PW012 Pratt & Whitney P& WA E Hartford, CT, USA Apr 76 Mar 77 1PW014 Pratt & Whitney P& WA E Hartford, CT, USA 7 Dec 79 19 Jun 80 1PW015 Pratt & Whitney P& WA E Hartford, CT, USA 7 Dec 79 19 Jun 80 1PW016 Pratt & Whitney P& WA E Hartford, CT, USA 7 Dec 79 19 Jun 80 1PW017 Pratt & Whitney P& WA E Hartford, CT, USA 7 Nov 83 30 Nov 83 4PW068 Pratt & Whitney P& WA East Hartford, CT 24 Feb 99 2 Mar 99 1PW018 Pratt & Whitney P& WA E Hartford, CT, USA 7 Nov 83 30 Nov 83 4PW069 Pratt & Whitney P& WA East Hartford, CT 24 Feb 99 2 Mar 99 4PW070 Pratt & Whitney P& WA East Hartford, CT 24 Feb 99 2 Mar 99 4PW071 Pratt & Whitney P& WA East Hartford, CT 24 Feb 99 2 Mar 99 1PW019 Pratt & Whitney P& WA E Hartford, CT, USA 7 Nov 83 30 Nov 83 1PW005 Pratt & Whitney P& WA E Hartford, CT, USA 26 Feb 80 18 Jun 80 1PW004 Pratt & Whitney P& WA E Hartford, CT, USA Apr 76 Mar 77 1PW007 Pratt & Whitney P& WA E Hartford, CT, USA 26 Feb 80 18 Jun 80 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CT CU UID No Remarks 225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 1KK003 1. Data obtained on aircraft ( Il 86) 2. In service engine( s), tested after overhaul 1KK004 1. For Il 86 aircraft. 2. In service engine( s), tested before overhaul.

1KK005 1. NK 86A with modified combustor. 2. For IL 86 aircraft.

1PW035 1. Not required to meet GASEOUS emissions regulations. 2. Applicable to JT15D 1,  1A,  1B.

1PW036 1. Not required to meet GASEOUS emissions regulations. 2. Applicable to JT15D 4,  4B,  4C,  4D 1PW037 1. Not required to meet GASEOUS emissions regulations.

1PW038 1. Not required to meet GASEOUS emissions regulations.

1PW001 Emissions data estimated from JT3D 7 engines using JT3D 3B performance data.

1PW003 1. Smoke fix combustor 14 70KC. 2. Applicable to JT3D 7,  7A.

1PW002 1. Combustor 14 57D. 2. Applicable to JT3D 7,  7A 1PW008 Reduced Emissions Combustor incorporated 1/ 1/ 84 1PW010 Reduced Emissions Combustor incorporated 1/ 1/ 84 1PW009 Smoke fix combustor in production prior to 1/ 1/ 84 1PW011 Reduced Emissions Combustor incorporated 1/ 1/ 84 1PW013 Reduced emissions combustor incorporated 1/ 1/ 84 1PW012 Smoke fix combustor in production prior to 1/ 1/ 84 1PW014 Reduced emissions combustor incorporated 1/ 1/ 84 1PW015 Reduced emissions combustor incorporated 1/ 1/ 84 1PW016 Reduced emissions combustor incorporated 1/ 1/ 84 1PW017 1. All measurements by traverse. 2. SCH 46 16B combustor.

4PW068 Environmental Kit ( E Kit) Combustor and Fuel Nozzles, incorporated 5/ 99 1PW018 1. All measurements by traverse. 2. SCH 46 16B combustor. 3. Applicable to JT8D 217,  217A,  217C.

4PW069 Environmental Kit ( E Kit) Combustor and Fuel Nozzles, incorporated 5/ 99 4PW070 Environmental Kit ( E Kit) Combustor and Fuel Nozzles, incorporated 5/ 99 4PW071 Environmental Kit ( E Kit) Combustor and Fuel Nozzles, incorporated 5/ 99 1PW019 1. All measurements by traverse. 2. SCH 46 16B combustor.

1PW005 1. Reduced emissions combustor. 2. Applicable to JT8D 7,  7A,  7B.

1PW004 1. Smoke fix combustor in production prior to 1/ 1/ 84. 2. Applicable to JT8D 7,  7A,  7B. 3. Tests performed on in service engine( s).

1PW007 1. Reduced Emissions Combustor incorporated 1/ 1/ 84. 2. Applicable to JT8D 9,  9A.

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CV CW CX CY CZ DA DB DC DD DE DF DG DH 225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 DI DJ DK DL DM DN 225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 A B C D E F G UID Engine Combustor Eng B/ P Press Rated No Identification Description Type Ratio Ratio Output kN 257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 1PW006 JT8D 9 series Smoke fix MTF 1.04 15.88 64.5 1PW031 JT9D 20 TF  20.3 205.3 1PW032 JT9D 20J TF 5.1 23.5 222.4 1PW033 JT9D 59A TF 4.9 24.5 235.8 1PW020 JT9D 7 TF  21.5 202.4 1PW034 JT9D 70A TF 4.9 24.5 235.8 1PW021 JT9D 7A TF  20.3 205.3 1PW022 JT9D 7F Mod V TF 5.1 22.8 213.5 1PW023 JT9D 7F Mod VI TF 5.1 22.8 213.5 1PW024 JT9D 7J TF 5.1 23.5 222.4 1PW025 JT9D 7Q TF 4.9 24.5 235.75 1PW026 JT9D 7R4D,  7R4D1 TF 5.0 23.40 213.5 1PW027 JT9D 7R4E,  7R4E1 TF 5.0 24.2 222.4 1PW028 JT9D 7R4E4,  E1( H) TF 5.0 24.2 222.41 1PW029 JT9D 7R4G2 TF 4.8 26.3 243.5 1PW030 JT9D 7R4H1 TF 4.8 26.7 249.1 1PW039 PW2037 TF 6.04 26.9 167.25 4PW072 PW2037 TF 5.71 26.7 166.35 1PW040 PW2040 TF  27.94 181.76 4PW073 PW2040 TF 5.54 29.4 182.02 7PW077 PW306A Annular TF 4.5 20 26.87 7PW078 PW306B Annular TF 4.5 20 26.91 7PW079 PW308A Annular TF 4.1 20.4 30.71 7PW080 PW308C Annular TF 4.1 20.7 31.15 1PW042 PW4056 Reduced emissions TF 4.7 29.3 249.1 1PW041 PW4056 TF 4.7 29.3 252.4 1PW043 PW4060 Reduced emissions TF 4.5 32.4 266.9 2PW060 PW4074 TF 6.8 32.2 333.2 3PW063 PW4074D TF 6.7 31.76 333.2 2PW061 PW4077 TF 6.7 33.2 343.0 3PW064 PW4077D TF 6.6 32.83 343.0 2PW062 PW4084 TF 6.4 36.2 369.6 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 H I J K L M N O P Q R S T U UID Data Superseded Data No PR C R superseded by NME DTEPS Other Corr as Out of Date Out of Date UID No Annex 16 Production Service  Data Status  Current Engine Status

 Test Engine Status

257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 1PW006 x     x   x x

1PW031 x       x x x

1PW032 x      x  x x

1PW033 x     x   x x

1PW020 x       x x x

1PW034 x     x   x x

1PW021 x       x x x

1PW022 x     x   x x

1PW023 x      x  x x

1PW024 x      x  x x

1PW025 x     x   x x

1PW026  x     x  x x

1PW027  x     x  x x

1PW028  x     x  x x

1PW029  x     x  x x

1PW030  x     x  x x

1PW039  x  x 4PW072 x   x x

4PW072   x   x   x

1PW040  x  x 4PW073 x   x x

4PW073   x   x   x

7PW077  x     x  x

7PW078  x     x  x

7PW079  x     x  x

7PW080  x     x  x

1PW042  x    x   x x

1PW041  x    x   x x

1PW043  x    x   x x

2PW060  x     x  x

3PW063  x    x   x x

2PW061  x     x  x

3PW064  x    x   x

2PW062  x     x  x

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 V W X Y Z AA AB AC AD AE AF AG AH UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI HC  Number   Dp/ Foo ( HC)

( g/ kg) ( g/ kN)

257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 1PW006 0.47 0.47 1.73 10.00 14 13 35.0 8.4  37.6 191.7 2256 1PW031 0.1 0.1 1.3 36.1 10 10 59   64.0 326.6 12108 1PW032 0 0 0.5 24.5 1 1 42.0   64.7 330.1 9178 1PW033 0.2 0.2 0.3 12.0 2 2 20.0 2.4  26.0 132.8 4559 1PW020 0.1 0.1 1.3 36.5 10 10 60.0 12.2 37.7 69.3 65.1 332.1 12179 1PW034 0.2 0.2 0.3 12.0 2 2 20.0 2.4  26.0 132.8 4559 1PW021 0.1 0.1 1.3 36.1 10 10 59   64.0 326.6 12108 1PW022 0.3 0.3 0.5 26.0 7 7 43.6 5.9  48.1 245.4 9055 1PW023 0 0 0.6 25.9 1 1 45.5   70.1 357.7 9464 1PW024 0 0 0.5 24.5 1 1 42.0   64.7 330.1 9178 1PW025 0.2 0.2 0.3 12.0 2 2 20.0 2.4  26.0 132.8 4559 1PW026 0.15 0.12 0.13 1.25 7 6 2.2   2.4 12.5 464 1PW027 0.16 0.13 0.13 1.11 7 6 2.1   2.3 11.9 447 1PW028 0.15 0.13 0.22 3.35 6 5 5.7   6.4 32.7 1231 1PW029 0.15 0.14 0.18 1.55 6 5 2.6   2.9 14.9 620 1PW030 0.15 0.14 0.18 1.48 6 5 2.7   3.0 15.5 651 1PW039 0.05 0.06 0.21 2.26 3 1 3.16   4.9 24.8 530 4PW072 0.02 0.02 0.11 1.92 4 2 2.8   3.6 18.4 472 1PW040 0.026 0.035 0.18 2.25 3 1 3.3   5.1 25.9 574 4PW073 0.01 0.02 0.10 1.65 4 2 2.3   3.0 15.3 426 7PW077 0 0 0.00 4.36 3 3 10.6  6.3  13.7 12.4 63.3 287 7PW078 0 0 0.00 4.36 3 3 10.6  6.3  13.7 12.4 63.3 287 7PW079 0 0 0.02 6.62 3 3 14.98  14.4  15.88 17.5 89.3 460 7PW080 0.09 0.1 0.14 5.94 3 3 13.63  12.5  15.2 15.9 81.1 425 1PW042 0.06 0.01 0.13 1.92 3 1 2.6   4.0 20.4 652 1PW041 0.11 0.17 0.25 0.66 3 1 1.2   1.8 9.4 288 1PW043 0.10 0.03 0.14 1.66 3 1 2.2   3.4 17.3 595 2PW060 0.1 0.1 0.2 3.2 3 1 3.7   5.7 29.1 1220 3PW063 0.03 0.05 0.08 5.07 3 1 5.76   8.9 45.4 1926 2PW061 0.1 0.1 0.2 3.0 3 1 3.4   5.2 26.5 1170 3PW064 0.03 0.04 0.07 4.66 3 1 5.26   8.1 41.3 1805 2PW062 0.1 0.1 0.2 2.7 3 1 2.9   4.5 23.0 1111 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AI AJ AK AL AM AN AO AP AQ AR AS AT AU UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI CO  Number  Dp/ Foo ( CO)

( g/ kN)

( g/ kg)

257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 1PW006 1.24 1.66 9.43 34.5 14 13 124.3 11.2  129.0 109.3 8018 1PW031 0 0 7.6 83.6 10 10 139.6   145.6 123.4 28647 1PW032 0.9 0.9 5.5 66.7 1 1 118.9   145.9 123.6 25974 1PW033 0.2 0.2 1.7 53.0   87.7 5.9  107.6 91.2 19946 1PW020 0 0 7.8 84.1 10 10 141.8 22.3 100.6 170.6 147.9 125.3 28691 1PW034 0.2 0.2 1.7 53.0   87.7 5.9  107.6 91.2 19946 1PW021 0 0 7.6 83.6 10 10 139.6   145.6 123.4 28647 1PW022 0.4 0.4 2.9 54.0 7 7 91.4 5.9  96.1 81.5 19012 1PW023 0.9 0.9 5.8 68.6 1 1 125.1   153.6 130.2 25989 1PW024 0.9 0.9 5.5 66.7 1 1 118.9   145.9 123.6 25974 1PW025 0.2 0.2 1.7 53.0   87.7 5.9  107.6 91.2 19946 1PW026 0.51 0.48 1.36 8.84 7 6 15.3   16.2 13.7 3231 1PW027 0.57 0.53 1.23 8.27 7 6 14.9   15.7 13.3 3215 1PW028 0.67 0.67 1.46 16.0 6 5 27.4   29.1 24.7 5952 1PW029 0.74 0.63 1.40 11.82 6 5 19.5   20.7 17.6 4582 1PW030 0.74 0.63 1.39 11.63 6 5 20.4   21.7 18.4 4938 1PW039 0.40 0.41 2.30 23.10 3 1 32.0   39.3 33.3 5396 4PW072 0.33 0.34 1.95 22.36 4 2 33.6   38.3 32.5 5597 1PW040 0.4 0.4 2.0 25.1 3 1 35.2   43.2 36.6 6412 4PW073 0.32 0.41 1.42 19.95 4 2 28.6   32.6 27.6 5219 7PW077 2.27 2.51 7.11 36.35 3 3 99.4  87.0  120.3 107.5 91.1 2677 7PW078 2.27 2.51 7.11 36.35 3 3 99.4  87.0  120.3 107.5 91.1 2677 7PW079 0.83 1.06 4.08 38.21 3 3 92.08  87.17  98.01 99.6 84.4 2828 7PW080 0.81 0.97 5.23 42.3 3 3 101.54  99.0  105.9 109.8 93.1 3163 1PW042 0.44 0.57 2.00 21.86 3 1 30.5   37.4 31.7 7597 1PW041 0.08 0.14 0.90 11.60 3 1 14.2   17.4 14.8 3587 1PW043 0.37 0.51 1.78 20.32 3 1 27.1   33.3 28.2 7234 2PW060 0.1 0.1 0.4 21.0 3 1 22.9   28.1 23.8 7589 3PW063 0.23 0.25 0.64 34.34 3 1 39.05   47.9 40.6 13036 2PW061 0.1 0.1 0.4 20.2 3 1 21.7   26.6 22.5 7434 3PW064 0.22 0.25 0.60 32.62 3 1 36.83   45.2 38.3 12648 2PW062 0.1 0.1 0.4 18.73 3 1 19.50   23.0 19.5 7205 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AV AW AX AY AZ BA BB BC BD BE BF BG BH BI BJ UID LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic Original CAEP 2 CAEP 4 Total mass ( g)

 Number

( g/ kg)

 EI NOx ( g/ kN)

 Dp/ Foo ( NOx) Characteristic as % of standards 257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 1PW006 17.92 14.21 5.64 2.90 14 14 52.3 5.7  53.7 74.8 93.5 108.3 3370 1PW031 38.7 28.5 7.6 3.1 10 10 59.9   61.8 76.7 95.8 120.0 12291 1PW032 44.9 34.9 9.4 3.3 1 1 68.7   79.6 91.5 114.4 140.6 15885 1PW033 31.6 25.6 7.8 3.0   54.4 3.0  63.1 70.9 88.6 108.3 12381 1PW020 37.9 27.7 7.6 3.1 10 10 58.8 6.9 46.6 66.1 60.7 73.1 91.3 113.6 11892 1PW034 31.6 25.6 7.8 3.0   54.4 3.0  63.1 70.9 88.6 108.3 12381 1PW021 38.7 28.5 7.6 3.1 10 10 59.9   61.8 76.7 95.8 120.0 12291 1PW022 46.0 34.4 7.8 3.1 7 7 69.4 4.0  72.0 84.2 105.2 129.8 14424 1PW023 41.7 31.5 9.1 3.2 1 1 63.1   73.1 85.4 106.7 131.8 13703 1PW024 44.9 34.9 9.4 3.3 1 1 68.7   79.6 91.5 114.4 140.6 15885 1PW025 31.6 25.6 7.8 3.0   54.4 3.0  63.1 70.9 88.6 108.3 12381 1PW026 38.5 30.0 9.8 4.1 6 5 61.9   64.7 74.5 93.2 114.6 13067 1PW027 41.6 34.2 10.4 4.1 6 5 67.3   70.3 79.6 99.5 121.9 14527 1PW028 36.9 29.7 8.5 3.5 6 5 60.3   63.0 71.3 89.1 109.2 13117 1PW029 41.3 29.5 8.8 3.8 6 5 60.5   63.2 68.3 85.4 103.5 14253 1PW030 45.2 30.0 8.9 3.8 6 5 65.2   68.2 73.0 91.2 110.4 15683 1PW039 31.1 24.8 10.3 4.4 3 1 48.1   55.8 59.4 74.3 89.9 8107 4PW072 29.41 23.96 9.77 4.1 4 2 48.8   53.7 57.5 71.9 87.0 8120 1PW040 34.3 27.3 10.6 4.2 3 1 55.1   63.9 66.6 83.3 100.3 10025 4PW073 35.04 26.62 10.49 4.37 4 2 54.9   60.4 61.1 76.4 91.5 9989 7PW077 20.08 19.26 11.87 4.26 3 3 55.6  52.7  58.0 58.9 73.6 92.0 92.1 1497 7PW078 20.08 19.26 11.87 4.26 3 3 55.6  52.7  58.0 58.9 73.6 92.0 92.1 1497 7PW079 16.74 14.06 8.03 3.65 3 3 42.33  41.21  42.94 44.8 55.4 69.3 70.2 1300 7PW080 18.45 15.99 7.83 3.63 3 3 45.38  45.0  45.92 48.1 59.1 73.9 74.9 1414 1PW042 28.1 22.9 11.6 4.8 3 1 48.1   55.8 56.5 70.7 84.6 11987 1PW041 32.5 24.6 11.6 5.0 3 1 51.7   59.9 60.8 76.0 91.0 13043 1PW043 32.8 24.7 12.0 4.9 3 1 52.7   61.1 58.3 72.9 85.1 14097 2PW060 38.1 31.5 11.0 4.2 3 1 54.2   62.8 60.2 75.2 88.0 18078 3PW063 42.35 34.48 11.88 3.81 3 1 59.93   69.5 67.1 83.9 98.6 19971 2PW061 39.8 32.5 11.3 4.2 3 1 56.3   65.3 61.4 76.7 89.0 19299 3PW064 44.74 35.82 12.10 3.83 3 1 62.76   72.8 68.9 86.1 100.2 21528 2PW062 45.0 35.5 12.0 4.4 3 1 62.8   72.8 64.8 81.0 91.7 23229 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BK BL BM BN BO BP BQ BR BS BT BU BV UID Characteristic No T/ O C/ O App Idle Test Eng Max Sigma Range Characteristic % of Reg limit  Smoke Number

 Smoke Number  Number

257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 1PW006     14 14 23 2  24.0 90.0 1PW031 12.3 9.5 2.5 0.7 10 10 12.3   14.5 74.4 1PW032       16.0   20.8 109.4 1PW033       8 1  10.3 55.0 1PW020 11.9 9.0 2.5 0.7 10 10 11.9 5.5 1.7 21.4 14.0 71.7 1PW034       8 1  10.3 55.0 1PW021 12.3 9.5 2.5 0.7 10 10 12.3   14.5 74.4 1PW022     7 7 4 1  4.3 22.1 1PW023 16.0      16.0   20.8 108.2 1PW024       16.0   20.8 109.4 1PW025       8 1  10.3 55.0 1PW026 4.6    5 4 4.6   5.0 26.0 1PW027 5.0    5 4 5.0   5.4 28.5 1PW028 4.3    3 3 4.3   4.7 24.9 1PW029 6.8    3 3 6.8   7.5 40.3 1PW030 7.6    3 3 7.6   8.4 45.4 1PW039     3 1 11.4   14.7 71.4 4PW072     4 2 10.5   12.3 59.7 1PW040     3 1 11.8   15.2 75.6 4PW073     4 2 10.7   12.5 62.2 7PW077     3 3 3.9  3.0  5.1 4.3 12.7 7PW078     3 3 3.9  3.0  5.1 4.3 12.7 7PW079     3 3 15.1  15.0  15.3 17.1 52.3 7PW080     3 3 7.6  5.3  9.4 8.3 25.5 1PW042 7.8    3 1 7.8   10.0 54.5 1PW041 14.3    3 1 14.3   18.4 100.2 1PW043 8.3    3 1 8.3   10.7 59.1 2PW060 6.4    3 1 6.4   8.2 48.2 3PW063     3 1 3.38   4.4 25.9 2PW061 7.4    3 1 7.4   9.5 56.3 3PW064     3 1 3.76   4.8 28.4 2PW062 10.5    3 1 10.5   13.5 81.6 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BW BX BY BZ CA CB CC CD CE UID Fuel per No Spec H/ C Arom T/ O C/ O App Idle LTO cycle Ratio % ( kg)

 Fuel Flow

( kg/ sec)

 Fuel

257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 1PW006 Jet A 1.89  1.040 0.846 0.298 0.132 433 1PW031 DERD2494   2.099 1.789 0.619 0.211 802 1PW032 Jet A   2.315 1.902 0.679 0.238 883 1PW033 Jet A 1.89  2.4419 1.9996 0.6804 0.2370 900 1PW020 DERD2494   2.083 1.764 0.609 0.210 794 1PW034 Jet A 1.89  2.4419 1.9996 0.6804 0.2370 900 1PW021 DERD2494   2.099 1.789 0.619 0.211 802 1PW022 Jet A 1.89  2.1672 1.7640 0.6237 0.2190 815 1PW023 Jet A   2.161 1.779 0.624 0.232 837 1PW024 Jet A   2.315 1.902 0.679 0.238 883 1PW025 Jet A 1.89  2.4419 1.9996 0.6804 0.2370 900 1PW026 Jet A   2.055 1.678 0.7593 0.2054 810 1PW027 Jet A   2.118 1.724 0.6529 0.2210 818 1PW028 Jet A   2.218 1.829 0.6400 0.2205 832 1PW029 Jet A   2.429 1.880 0.6590 0.2239 858 1PW030 Jet A   2.512 1.999 0.7227 0.2454 926 1PW039 Jet A   1.538 1.266 0.399 0.141 547 4PW072 Jet A   1.571 1.307 0.458 0.152 586 1PW040 Jet A   1.761 1.448 0.493 0.155 625 4PW073 Jet A   1.752 1.445 0.496 0.159 631 7PW077 Jet A 1 1.85  1.87 20.0  22.5 0.3171 0.2641 0.0974 0.0422 137 7PW078 Jet A 1 1.85  1.87 20.0  22.5 0.3171 0.2641 0.0974 0.0422 137 7PW079 Jet A 1 1.85  1.87 19.5  21.5 0.3604 0.2991 0.1235 0.0445 154 7PW080 Jet A 1 1.85  1.86 19.8  21.4 0.3669 0.3047 0.1237 0.0448 155 1PW042 Jet A 1.88 19.7 2.342 1.93 0.658 0.208 836 1PW041 Jet A 1.87 19.7 2.449 1.981 0.647 0.188 813 1PW043 Jet A 1.88 19.7 2.647 2.085 0.703 0.213 887 2PW060 Jet A 1.92 20.3 2.899 2.368 0.795 0.228 981 3PW063 Jet A   2.949 2.416 0.81 0.239 1010 2PW061 Jet A 1.92 20.3 3.019 2.452 0.816 0.232 1008 3PW064 Jet A   3.082 2.507 0.835 0.244 1041 2PW062 Jet A 1.92 20.3 3.411 2.689 0.875 0.242 1086 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CF CG CH CI CJ CK CL CM UID No Baro Temp Humidity kW @ Power % CF @ Power kPa K kg/ kg  Ambient

 Loads

Power Extraction  Stage Bleed

257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 1PW006 0  0  100 102 262 300 0.0005 0.0123 1PW031 0  0  97.9 101.7 276  300 0.0030 0.0149 1PW032 0  0

1PW033 0  0  97 100 280  285 0.0029 0.0050 1PW020 0  0  97.9 101.7 276  300 0.0030 0.0149 1PW034 0  0  97 100 280  285 0.0029 0.0050 1PW021 0  0  97.9 101.7 276  300 0.0030 0.0149 1PW022 0  0  99 103 266  290 0.0007 0.0068 1PW023 0  0

1PW024 0  0

1PW025 0  0  97 100 280  285 0.0029 0.0050 1PW026 0  0   276  304

1PW027 0  0   276  304

1PW028 0  0   271  299

1PW029 0  0   271  299

1PW030 0  0   271  299

1PW039 0  0  100.94 298

4PW072 0  0  100.61  100.94 283.4  298.2 .007  .008 1PW040 0  0  100.94 298

4PW073 0  0  100.61  100.94 283.4  298.2 .007  .008 7PW077 0  0  98.39  99.49 284  300 0.0054  0.0144 7PW078 0  0  98.39  99.49 284  300 0.0054  0.0144 7PW079 0  0  99.42  103.00 280  296 0.0028  0.0090 7PW080 0  0  98.94  100.73 296  301 0.0088  0.0122 1PW042 0  0  100.2 299 0.010 1PW041 0  0  101.63 290 0.00053 1PW043 0  0  100.2 299 0.010 2PW060 0  0  101.3 288 0.0063 3PW063 0  0  101.06 101.56 292.8 302.6 .0097. 0112 2PW061 0  0  101.3 288 0.0063 3PW064 0  0  101.06 101.56 292.8 302.6 .0097. 0112 2PW062 0  0  101.3 288 0.0063 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CN CO CP CQ CR CS UID  Test Dates

No Manufacturer Test Organisation Test Location From To 257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 1PW006 Pratt & Whitney P& WA E Hartford, CT, USA Apr 76 Mar 77 1PW031 Pratt & Whitney NGTE, Pyestock, UK British Airways Engine Overhaul Ltd, Wales Mar 76 Jul 77 1PW032 Pratt & Whitney P& WA E Hartford, CT, USA 16 Sep 80

1PW033 Pratt & Whitney P& WA E Hartford, CT, USA Apr 76 Apr 76 1PW020 Pratt & Whitney NGTE, Pyestock, UK British Airways Engine Overhaul Ltd, Wales Mar 76 Jul 77 1PW034 Pratt & Whitney P& WA E Hartford, CT, USA Apr 76 Apr 76 1PW021 Pratt & Whitney NGTE, Pyestock, UK British Airways Engine Overhaul Ltd, Wales Mar 76 Jul 77 1PW022 Pratt & Whitney P& WA E Hartford, CT, USA Nov 75 Dec 75 1PW023 Pratt & Whitney P& WA E Hartford, CT, USA 16 Sep 80

1PW024 Pratt & Whitney P& WA E Hartford, CT, USA 16 Sep 80

1PW025 Pratt & Whitney P& WA E Hartford, CT, USA Apr 76 Apr 76 1PW026 Pratt & Whitney P& WA E Hartford, CT, USA 6 Mar 80 3 Nov 81 1PW027 Pratt & Whitney P& WA E Hartford, CT, USA 6 Mar 80 3 Nov 81 1PW028 Pratt & Whitney P& WA E Hartford, CT, USA 26 Oct 81 10 Apr 83 1PW029 Pratt & Whitney P& WA E Hartford, CT, USA 26 Oct 81 10 Sep 83 1PW030 Pratt & Whitney P& WA E Hartford, CT, USA 26 Oct 81 10 Sep 83 1PW039 Pratt & Whitney P& WA X 8 Stand, PWA, East Hartford, CT 8 Aug 83 10 Aug 83 4PW072 Pratt & Whitney P& WA East Hartford, CT 8 Aug 83 20 Nov 98 1PW040 Pratt & Whitney   8 Aug 83 10 Aug 83 4PW073 Pratt & Whitney P& WA East Hartford, CT 8 Aug 83 20 Nov 98 7PW077 Pratt & Whitney Canada Inc. PW306 Development Engineering Mississauga, Ontario, Canada 8 May 00 20 Jul 00 7PW078 Pratt & Whitnet Canada Inc. PE306 Development Engineering Mississauga, Ontario, Canada 8 May 00 20 Jul 00 7PW079 Pratt & Whitney Canada Inc PW308 Development Engineering Mississauga, Ontario, Canada 15 Apr 00 5 Sep 00 7PW080 Pratt & Whitney Canada Inc. PW308 Development Engineering Mississauga, Ontario, Canada 7 Aug 01 31 Aug 01 1PW042 Pratt & Whitney   17 Aug 87 23 Aug 87 1PW041 Pratt & Whitney Pratt & Whitney P7 Stand, P& W, Middletown, CT 14 May 86 14 May 86 1PW043 Pratt & Whitney   17 Aug 87 23 Aug 87 2PW060 Pratt and Whitney Pratt and Whitney East Hartford, Ct, USA 26 Apr 94 2 May 94 3PW063 Pratt & Whitney Pratt & Whitney East Hartford, Conn, USA 15 Jun 96 16 Jun 96 2PW061 Pratt and Whitney Pratt and Whitney East Hartford, Ct, USA 26 Apr 94 2 May 94 3PW064 Pratt & Whitney Pratt & Whitney East Hartford, Conn, USA 15 Jun 96 16 Jun 96 2PW062 Pratt and Whitney Pratt and Whitney East Hartford, Ct, USA 26 Apr 94 2 May 94 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CT CU UID No Remarks 257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 1PW006 1. Smoke fix combustor in production prior to 1/ 1/ 84. 2. Applicable to JT8D 9,  9A.

1PW031 1. Emissions estimated from JT9D 7 engines using JT9D 7A performance data. 2. Tests performed on in service engine( s), after overhaul.

1PW032

1PW033

1PW020 Tests performed on in service engine( s), after overhaul.

1PW034

1PW021 1. Emissions estimated from JT9D 7 engines using JT9D 7A performance data. 2. Tests performed on in service engine( s), after overhaul.

1PW022 Mod V combustor 1PW023 Mod VI combustor 1PW024

1PW025

1PW026

1PW027

1PW028

1PW029

1PW030

1PW039

4PW072 Revision to add second engine test.

1PW040

4PW073 Revision to add second engine test.

7PW077 1, P& WC EC C2264A 2, Engines E9541/ 02, E9402/ 37, E9403/ 74 7PW078 1, P& WC EC C2264A 2, Engines E9541/ 02, E9402/ 37, E9403/ 74 7PW079 1, P& WC ER 3967 2, Engines E9608/ 01, E9606/ 04, E9609/ 01 7PW080 1, P& WC ER 5080 2, Engines E9633/ 01, E9631/ 07, CF0001/ 03 1PW042 Data from X698 5 with reduced smoke combustor.

1PW041

1PW043 Data from X698 5 with reduced smoke combustor.

2PW060 Data from X832 4 3PW063 Data from Report PWA 6678 2PW061 Data from X832 4 3PW064 Data from Report PWA 6678 2PW062 Data from X832 4 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CV CW CX CY CZ DA DB DC DD DE DF DG DH 257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 DI DJ DK DL DM DN 257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 A B C D E F G UID Engine Combustor Eng B/ P Press Rated No Identification Description Type Ratio Ratio Output kN 289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 3PW065 PW4084D TF 6.3 36.36 369.6 3PW066 PW4090 TF 6.1 39.16 395.0 5PW076 PW4098 TF  41.37 424.1 1PW045 PW4152 Reduced smoke TF 4.9 26.9 231.27 1PW044 PW4152 TF 4.9 26.9 231.3 1PW047 PW4156 Reduced smoke TF 4.7 29.3 249.1 1PW046 PW4156 TF 4.7 29.3 252.4 1PW048 PW4158 Reduced smoke TF 4.6 30.7 258.0 1PW049 PW4164 Floatwall TF 5.2 31.24 284.68 1PW050 PW4168 Floatwall TF 5.1 33.10 302.48 5PW075 PW4168 Talon II TF 5.1 31.84 302.5 4PW067 PW4168A Floatwall TF 5.1 33.1 302.48 1PW051 PW4256 TF 4.7 29.3 252.4 1PW052 PW4460 Reduced smoke TF 4.5 32.4 266.9 1PW053 PW4x50 Phase 3 TF 5.0 25.39 222.4 1PW054 PW4x52 Phase 3 TF 5.0 26.32 231.3 1PW055 PW4x56 Phase 3 TF 4.8 28.37 249.1 1PW056 PW4x58 Phase 3 TF 4.8 29.49 258.0 5PW074 PW4X58 Talon II TF 4.8 28.41 258.0 1PW057 PW4x60 Phase 3 TF 4.7 30.68 266.9 1PW059 PW4x62 Phase 3 TF 4.6 31.91 275.8 1PW058 PW4x62 Reduced smoke TF 4.4 33.4 275.8 Rolls Royce Ltd 1RR001 M45H 01 TF 3.0 16.5 32.4 1RR002 RB211 22B Package 1 TF 4.7 25.0 182.5 1RR003 RB211 22B Package 1 TF 4.7 25.0 182.5 1RR004 RB211 524B series Package 1 TF 4.5 28.0 218.5 1RR005 RB211 524B series Phase 2 TF 4.5 28.4 218.5 1RR006 RB211 524C2 Package 1 TF 4.5 29.1 224.8 1RR007 RB211 524D4 Package 1 TF 4.3 29.7 231.3 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 H I J K L M N O P Q R S T U UID Data Superseded Data No PR C R superseded by NME DTEPS Other Corr as Out of Date Out of Date UID No Annex 16 Production Service  Data Status  Current Engine Status

 Test Engine Status

289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 3PW065  x    x   x

3PW066  x    x   x

5PW076  x     x  x

1PW045  x    x   x x

1PW044  x    x   x x

1PW047  x    x   x x

1PW046  x    x   x x

1PW048  x    x   x x

1PW049  x     x  x

1PW050  x     x  x

5PW075  x     x  x

4PW067  x     x  x

1PW051  x    x   x x

1PW052  x    x   x x

1PW053  x     x  x x

1PW054  x     x  x

1PW055  x     x  x

1PW056  x     x  x

5PW074  x     x  x

1PW057  x     x  x

1PW059  x     x  x

1PW058  x    x   x x

1RR001 x      x  x x

1RR002 x     x   x x

1RR003 x     x x x

1RR004 x     x   x x

1RR005  x     x  x x

1RR006 x      x  x x

1RR007 x      x  x x

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 V W X Y Z AA AB AC AD AE AF AG AH UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI HC  Number   Dp/ Foo ( HC)

( g/ kg) ( g/ kN)

289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 3PW065 0.03 0.03 0.06 3.29 3 1 3.66   5.6 28.6 1353 3PW066 0.03 0.03 0.06 2.30 3 1 2.52   3.9 19.9 992 5PW076 0.00 0.00 0.00 0.00 3 1 0.00   0.0 0.0 0 1PW045 0.03 0.01 0.13 2.24 3 1 3.2   4.9 25.1 734 1PW044 0.13 0.16 0.15 0.74 3 1 1.3   2.0 10.2 275 1PW047 0.06 0.01 0.13 1.92 3 1 2.6   4.0 20.4 652 1PW046 0.11 0.17 0.25 0.66 3 1 1.2   1.8 9.4 288 1PW048 0.09 0.02 0.14 1.78 3 1 2.4   3.7 18.9 623 1PW049 0.03 0.04 0.16 4.46 3 1 5.3   8.2 41.6 1505 1PW050 0.03 0.04 0.15 3.29 3 1 3.9   6.0 30.6 1179 5PW075 0.0 0.0 0.0 0.2 3 1 0.3   0.5 2.3 78 4PW067 0.03 0.04 0.15 3.29 3 1 3.9   6.0 30.6 1179 1PW051 0.11 0.17 0.25 0.66 3 1 1.2   1.8 9.4 288 1PW052 0.10 0.03 0.14 1.66 3 1 2.2   3.4 17.3 595 1PW053 0.09 0.10 0.19 6.80 3 1 9.5   14.6 74.6 2104 1PW054 0.08 0.10 0.17 6.02 3 1 8.3   12.8 65.2 1914 1PW055 0.08 0.09 0.16 4.75 3 1 6.4   9.9 50.3 1597 1PW056 0.08 0.09 0.15 4.29 3 1 5.7   8.8 44.8 1481 5PW074 0.0 0.0 0.0 1.7 3 1 2.2   3.4 17.3 562 1PW057 0.08 0.08 0.15 3.73 3 1 5.0   7.7 39.3 1324 1PW059 0.08 0.08 0.15 3.26 3 1 4.3   6.6 33.8 1192 1PW058 0.10 0.06 0.14 1.53 3 1 2.0   3.1 15.7 571 1RR001 * 0.74 7.4 59.5 5 5 162.4 87.5 81.0 293.4 182.6 931.6 1RR002 0.36 0.39 7.73 65.37 4 3 132.8 8.23 122 140 154.9 790.4 29381 1RR003 0.15 0.25 5.96 67.75 7 7 134.8 5.6 169.8 204.1 148.7 758.7 24653 1RR004 0.52 0.40 4.98 50.60 4 3 106.3 6.61 97.7 112.0 124.0 632.7 22453 1RR005 0.39 0.26 0.70 1.95 3 1 4.25 0.1 4.2 4.4 6.5 33.4 934 1RR006 0.0 0.22 4.42 54.2   116.5   179.4 915.4 26209 1RR007 0.0 0.42 4.80 46.46 3 3 97.8   114.1 582.1 22707 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AI AJ AK AL AM AN AO AP AQ AR AS AT AU UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI CO  Number  Dp/ Foo ( CO)

( g/ kN)

( g/ kg)

289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 3PW065 0.18 0.24 0.48 25.74 3 1 28.60   35.1 29.7 10579 3PW066 0.19 0.23 0.44 20.63 3 1 22.38   27.5 23.3 8848 5PW076 0.160 0.210 0.700 6.480 3 1 8.35   10.2 8.6 3543 1PW045 0.5 0.62 2.29 23.67 3 1 34.8   42.7 36.2 8023 1PW044 0.12 0.17 1.09 12.76 3 1 17.0   20.9 17.7 3729 1PW047 0.44 0.57 2.00 21.86 3 1 30.5   37.4 31.7 7597 1PW046 0.08 0.14 0.90 11.60 3 1 14.2   17.4 14.8 3587 1PW048 0.40 0.54 1.88 20.99 3 1 28.7   35.2 29.9 7401 1PW049 0.69 0.79 1.86 26.67 3 1 33.0   40.5 34.3 9377 1PW050 0.72 0.74 1.75 23.51 3 1 28.9   35.5 30.1 8754 5PW075 0.1 0.2 2.4 15.9 3 1 22.3   27.4 23.2 6741 4PW067 0.72 0.74 1.75 23.51 3 1 28.9   35.5 30.1 8754 1PW051 0.08 0.14 0.90 11.60 3 1 14.2   17.4 14.8 3587 1PW052 0.37 0.51 1.78 20.32 3 1 27.1   33.3 28.2 7234 1PW053 0.53 0.62 2.33 36.91 3 1 52.2   64.1 54.3 11619 1PW054 0.52 0.60 2.15 34.54 3 1 48.2   59.2 50.1 11164 1PW055 0.48 0.56 1.89 29.96 3 1 41.0   50.3 42.6 10202 1PW056 0.44 0.53 1.82 28.08 3 1 38.0   46.6 39.5 9806 5PW074 0.2 0.3 3.8 24.3 3 1 33.9   41.6 35.3 8741 1PW057 0.40 0.52 1.74 25.83 3 1 34.7   42.6 36.1 9257 1PW059 0.38 0.51 1.68 23.96 3 1 31.9   39.2 33.2 8811 1PW058 0.35 0.49 1.69 19.51 3 1 25.6   31.4 26.6 7080 1RR001 6.2 7.9 51 178.4 5 5 526.0 99.5 374.3 633.8 558.6 473.4 17101 1RR002 2.48 4.14 26.38 93.17 4 3 205.3 8.01 197 212 222.0 188.2 44799 1RR003 0.78 1.68 20.65 88.99 7 7 188.5 13.1 169.8 204.1 198.3 168.0 34445 1RR004 1.83 2.82 20.0 82.2 4 3 182.9 7.15 175.6 189 197.8 167.6 39110 1RR005 0.70 0.33 1.56 12.39 3 1 22.9 0.68 22.3 23.6 28.1 23.8 5018 1RR006 0.66 1.63 18.9 81.0   185.4   227.6 192.9 41768 1RR007 0.51 1.18 16.9 73.8 3 3 163.4   176.7 149.7 37907 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AV AW AX AY AZ BA BB BC BD BE BF BG BH BI BJ UID LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic Original CAEP 2 CAEP 4 Total mass ( g)

 Number

( g/ kg)

 EI NOx ( g/ kN)

 Dp/ Foo ( NOx) Characteristic as % of standards 289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 3PW065 53.02 39.47 12.70 4.08 3 1 72.14   83.6 74.2 92.7 104.9 26662 3PW066 61.00 42.80 13.19 4.29 3 1 80.08   92.8 78.4 98.0 108.8 31629 5PW076 51.29 36.45 14.89 7.78 3 1 76.1   88.2 71.9 89.8 98.3 32265 1PW045 25.3 21.1 11.1 4.8 3 1 45.0   52.2 55.6 69.5 84.1 10381 1PW044 26.9 22.7 11.1 4.9 3 1 46.7   54.1 57.7 72.1 87.3 10741 1PW047 28.1 22.9 11.6 4.8 3 1 48.1   55.8 56.5 70.7 84.6 11987 1PW046 32.5 24.6 11.6 5.0 3 1 51.7   59.9 60.8 76.0 91.0 13043 1PW048 30.2 23.7 11.8 4.8 3 1 50.2   58.2 57.4 71.7 85.1 12928 1PW049 38.57 31.66 14.10 4.03 3 1 60.5   70.1 68.4 85.5 100.9 17232 1PW050 42.39 33.91 14.66 4.15 3 1 65.2   75.6 71.2 89.0 103.2 19704 5PW075 26.9 20.2 12.1 5.2 3 1 46.0   53.3 51.4 64.3 75.4 13936 4PW067 42.39 33.91 14.66 4.15 3 1 65.2   75.6 71.2 89.0 103.3 19704 1PW051 32.5 24.6 11.6 5.0 3 1 51.7   59.9 60.8 76.0 91.0 13043 1PW052 32.8 24.7 12.0 4.9 3 1 52.7   61.1 58.3 72.9 86.2 14097 1PW053 25.69 21.77 11.13 3.69 3 1 43.5   50.4 55.5 69.4 84.6 9681 1PW054 27.02 22.54 11.41 3.77 3 1 45.2   52.4 56.6 70.7 85.7 10449 1PW055 30.44 24.24 11.97 3.93 3 1 49.2   57.0 59.0 73.7 88.6 12246 1PW056 32.51 25.22 12.25 3.99 3 1 51.6   59.8 60.4 75.5 90.4 13305 5PW074 22.5 18.0 11.1 4.3 3 1 39.9   46.3 47.8 59.8 71.8 10297 1PW057 34.89 26.34 12.53 4.07 3 1 54.4   63.1 62.2 77.8 92.2 14505 1PW059 37.65 27.55 12.78 4.14 3 1 57.5   66.7 64.2 80.2 94.1 15864 1PW058 36.3 25.7 12.2 4.9 3 1 56.0   64.9 60.8 76.0 88.0 15470 1RR001 11.5 9.3 3.6 1.5 5 5 31.2 3.8 26.4 35.9 32.6 44.7 55.8 57.0 1001 1RR002 34.32 25.63 8.05 2.70 4 3 54.3 4.4 48 57 57.5 63.9 79.9 97.5 10142 1RR003 37.33 26.89 8.18 2.86 7 7 57.8 3.1 52.2 60.7 60.0 66.7 83.3 101.7 10545 1RR004 47.0 33.0 9.75 3.53 4 3 73.9 6.0 64.9 77.6 78.3 81.5 101.9 122.7 16270 1RR005 52.3 38.2 9.8 4.2 3 1 77.3 0.8 76.5 78.1 89.6 92.6 115.7 139.0 16935 1RR006 41.9 32.3 10.4 3.37   72.9   84.5 86.1 107.6 128.9 16401 1RR007 56.9 41.0 9.65 4.11 3 3 88.6   93.8 94.4 118.0 141.0 20514 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BK BL BM BN BO BP BQ BR BS BT BU BV UID Characteristic No T/ O C/ O App Idle Test Eng Max Sigma Range Characteristic % of Reg limit  Smoke Number

 Smoke Number  Number

289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 3PW065     3 1 5.36   6.9 41.7 3PW066     3 1 7.12   9.2 56.6 5PW076     3 1 9.3   12.0 75.3 1PW045 7.0    3 1 7.0   9.0 47.9 1PW044 12.7    3 1 12.7   16.3 86.9 1PW047 7.8    3 1 7.8   10.0 54.5 1PW046 14.3    3 1 14.3   18.4 100.2 1PW048 8.1    3 1 8.1   10.4 57.1 1PW049 3.3    3 1 3.3   4.2 23.9 1PW050 4.0    3 1 4.0   5.1 29.5 5PW075     3 1 12.7   16.4 93.5 4PW067 4.0    3 1 4.0   5.1 29.2 1PW051 14.3    3 1 14.3   18.4 100.2 1PW052 8.3    3 1 8.3   10.7 59.1 1PW053 6.8    3 1 6.8   8.8 46.0 1PW054 7.3    3 1 7.3   9.4 50.0 1PW055 8.5    3 1 8.5   10.9 59.4 1PW056 9.1    3 1 9.1   11.7 64.2 5PW074     3 1 11.6   14.9 81.6 1PW057 9.6    3 1 9.6   12.4 68.3 1PW059 10.1    3 1 10.1   13.0 72.5 1PW058 8.4    3 1 8.4   10.8 60.3 1RR001 46.3 38.4 10.9 2.7 5 5 46.3 3.87 42 54.5 49.8 154.5 1RR002 14.7 12.9 8.0 3.1 1 1 14.7   18.9 94.3 1RR003 7 7 22.6 6.5 14.6 33.4 24.0 119.7 1RR004 17.9 13.5 2.7 0.9 4 3 17.9 0.5 17.3 18.4 19.7 103.0 1RR005     3 1 12.3 0.2 12.1 12.6 15.8 82.9 1RR006       14.5   18.7 98.4 1RR007     3 3 12.2   13.4 71.2 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BW BX BY BZ CA CB CC CD CE UID Fuel per No Spec H/ C Arom T/ O C/ O App Idle LTO cycle Ratio % ( kg)

 Fuel Flow

( kg/ sec)

 Fuel

289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 3PW065 Jet A   3.511 2.771 0.907 0.258 1133 3PW066 Jet A   3.898 2.977 0.957 0.268 1204 5PW076 Jet A 1.9 15.5 4.138 3.245 1.075 0.321 1361 1PW045 Jet A 1.88 19.7 2.129 1.783 0.613 0.203 789 1PW044 Jet A 1.87 19.7 2.177 1.785 0.593 0.177 745 1PW047 Jet A 1.88 19.7 2.342 1.93 0.658 0.208 836 1PW046 Jet A 1.87 19.7 2.449 1.981 0.647 0.188 813 1PW048 Jet A 1.88 19.7 2.481 2.004 0.682 0.211 862 1PW049 Jet A 1.89 21.85 2.626 2.179 0.754 0.210 906 1PW050 Jet A 1.89 21.85 2.836 2.327 0.798 0.221 963 5PW075 Jet A 1.94 15.5 2.884 2.363 0.809 0.25 1017 4PW067 Jet A 1.89 21.85 2.836 2.327 0.798 0.221 963 1PW051 Jet A 1.87 19.7 2.449 1.981 0.647 0.188 813 1PW052 Jet A 1.88 19.7 2.647 2.085 0.703 0.213 887 1PW053 Jet A 1.91 21.0 2.027 1.683 0.579 0.193 747 1PW054 Jet A 1.91 21.0 2.127 1.757 0.600 0.198 774 1PW055 Jet A 1.91 21.0 2.351 1.912 0.643 0.208 830 1PW056 Jet A 1.91 21.0 2.482 1.993 0.665 0.213 859 5PW074 Jet A 1.9 20.6 2.496 1.999 0.663 0.212 859 1PW057 Jet A 1.91 21.0 2.623 2.075 0.686 0.218 889 1PW059 Jet A 1.91 21.0 2.767 2.166 0.708 0.223 920 1PW058 Jet A 1.88 19.7 2.858 2.161 0.725 0.217 918 1RR001 DERD 2494 1.94 19 0.498 0.416 0.146 0.053 194 1RR002 DERD 2494 1.94 20 1.866 1.542 0.553 0.277 847 1RR003 DERD 2494 1.877 1.546 0.566 0.225 770 1RR004 DERD 2494 1.94 20 2.383 1.939 0.693 0.272 947 1RR005 AVTUR 1.91 20 2.21 1.79 0.63 0.24 855 1RR006 AVTUR 1.91 20 2.48 2.02 0.74 0.30 1016 1RR007 AVTUR 1.91 20 2.51 2.01 0.74 0.30 1016 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CF CG CH CI CJ CK CL CM UID No Baro Temp Humidity kW @ Power % CF @ Power kPa K kg/ kg  Ambient

 Loads

Power Extraction  Stage Bleed

289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 3PW065 0  0  101.06 101.56 292.8 302.6 .0097. 0112 3PW066 0  0  101.06 101.56 292.8 302.6 .0097. 0112 5PW076 0  0  101.7  102.5 284  289 .00274  .00608 1PW045 0  0  100.2 299 .010 1PW044 0  0  101.63 290 0.00053 1PW047 0  0  100.2 299 0.010 1PW046 0  0  101.63 290 0.00053 1PW048 0  0  100.2 299 0.010 1PW049 0  0  101.3 273.5 .0018 1PW050 0  0  101.3 273.5 .0018 5PW075 0  0  101.4  102.3 279  282 .00210  .00355 4PW067 0  0  101.3 273.5 0.0018 1PW051 0  0  101.63 290 0.00053 1PW052 0  0  100.2 299 0.010 1PW053 0  0  102.0 270 .0015 1PW054 0  0  102.0 270 .0015 1PW055 0  0  102.0 270 .0015 1PW056 0  0  102.0 270 .0015 5PW074 0  0  100.0  101.3 277  281 .00268  .00342 1PW057 0  0  102.0 270 .0015 1PW059 0  0  102.0 270 .0015 1PW058 0  0  100.2 299 0.010 1RR001 0  6 7% 98.6 102.1 281  293 0.00456 0.00749 1RR002 0  0  99.3 100.3 287  291 0.008 1RR003 0  0  99.6 102.2 275  287 .0033. 0077 1RR004 0  0  99.3 100.3 287  291 0.008 1RR005 0  0  103 283  286 0.005 1RR006 0  0  102 288 0.005 1RR007 0  0  101 277 0.006 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CN CO CP CQ CR CS UID  Test Dates

No Manufacturer Test Organisation Test Location From To 289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 3PW065 Pratt & Whitney Pratt & Whitney East Hartford, Conn, USA 15 Jun 96 16 Jun 96 3PW066 Pratt & Whitney Pratt & Whitney East Hartford, Conn, USA 15 Jun 96 16 Jun 96 5PW076 Pratt and Whitney Pratt and Whitney East Hartford, Conn. USA 3 Jan 98 4 Jan 98 1PW045 Pratt & Whitney   17 Aug 87 23 Aug 87 1PW044 Pratt & Whitney Pratt& Whitney P7 Stand, P& W, Middletown, CT 14 May 86 14 May 86 1PW047 Pratt & Whitney   17 Aug 87 23 Aug 87 1PW046 Pratt & Whitney Pratt & Whitney P7 Stand, P& W, Middletown, CT 14 May 86 14 May 86 1PW048 Pratt & Whitney   17 Aug 87 23 Aug 87 1PW049 Pratt & Whitney Pratt & Whitney East Hartford, CT 14 Feb 93 17 Feb 93 1PW050 Pratt & Whitney Pratt & Whitney East Hartford, CT 14 Feb 93 17 Feb 93 5PW075 Pratt and Whitney Pratt and Whitney East Hartford, Conn. USA 10 Apr 00 4PW067 Pratt & Whitney Pratt & Whitney East Hartford, CT 14 Feb 93 17 Feb 93 1PW051 Pratt & Whitney Pratt & Whitney P7 Stand, P& W, Middletown, CT 14 May 86 14 May 86 1PW052 Pratt & Whitney   17 Aug 87 23 Aug 87 1PW053 Pratt & Whitney Pratt & Whitney Middletown, CT 15 Jan 93 19 Jan 93 1PW054 Pratt & Whitney Pratt & Whitney Middletown, CT 15 Jan 93 19 Jan 93 1PW055 Pratt & Whitney Pratt & Whitney Middletown, CT 15 Jan 93 19 Jan 93 1PW056 Pratt & Whitney Pratt & Whitney Middletown, CT 15 Jan 93 19 Jan 93 5PW074 Pratt and Whitney Pratt and Whitney East Hartford, Conn. USA 3 Nov 99 4 Nov 99 1PW057 Pratt & Whitney Pratt & Whitney Middletown, CT 15 Jan 93 19 Jan 93 1PW059 Pratt & Whitney Pratt & Whitney Middletown, CT 15 Jan 93 19 Jan 93 1PW058 Pratt & Whitney   17 Aug 87 23 Aug 87 1RR001 Rolls Royce Ltd Rolls Royce Ltd Bristol 1971 1977 1RR002 Rolls Royce Ltd Rolls Royce Ltd Derby Jun 79 Aug 79 1RR003 Rolls Royce Ltd NGTE, Pyestock, UK British Airways Test Facility, Heathrow Mar 79 Apr 80 1RR004 Rolls Royce Ltd Rolls Royce Ltd Derby Jun 79 Aug 79 1RR005 Rolls Royce Ltd Rolls Royce Ltd SINFIN Derby Sep 86 Sep 86 1RR006 Rolls Royce Ltd Rolls Royce Ltd SINFIN Derby Sep 86

1RR007 Rolls Royce Ltd Rolls Royce Ltd SINFIN Derby Nov 82

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CT CU UID No Remarks 289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 3PW065 Data from Report PWA 6678 3PW066 Data from Report PWA 6678 5PW076 1. Data from Report PWA 6726 01 1PW045 Data from X698 5 with reduced smoke combustor.

1PW044

1PW047 Data from X698 5 with reduced smoke combustor.

1PW046

1PW048 Data from X698 5 with reduced smoke combustor.

1PW049 Data from X821 3 with Floatwall Combustor 1PW050 Data from X821 3 with Floatwall Combustor 5PW075 1. Data from Report PWA 7138. 2. TALON II Combustor 4PW067 Data from X821 3 with Floatwall Combustor 1PW051

1PW052 Data from X698 5 with reduced smoke combustor.

1PW053 Data from X693 20 with Phase 3 reduced pressure loss combustor 1PW054 Data from X693 20 with Phase 3 reduced pressure loss combustor 1PW055 Data from X693 20 with Phase 3 reduced pressure loss combustor 1PW056 Data from X693 20 with Phase 3 reduced pressure loss combustor 5PW074 1. Data from Report PWA 7312. 2. TALON II Combustor 1PW057 Data from X693 20 with Phase 3 reduced pressure loss combustor 1PW059 Data from X693 20 with Phase 3 reduced pressure loss combustor 1PW058 Data from X698 5 with reduced smoke combustor.

1RR001 Stage bleed on 2 engines 1RR002 Package 1 combustor.

1RR003 1. Package 1 combustor. 2. Tests performed on in service engine( s), after overhaul.

1RR004 1. Package 1 Combustor. 2. Applicable to RB211 524B, B2, B3, B4.

1RR005 1. Data from certification report CRR60515. 2. Phase 2 combustor. 3. Applicable to engines manufactured after Feb 87. 4. Applicable to RB211 524B 1RR006 Package 1 combustor 1RR007 Package 1 combustor Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CV CW CX CY CZ DA DB DC DD DE DF DG DH 289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 4B, B2, B3, B4.

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 DI DJ DK DL DM DN 289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 A B C D E F G UID Engine Combustor Eng B/ P Press Rated No Identification Description Type Ratio Ratio Output kN 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 1RR008 RB211 524D4 Phase 2 TF 4.3 30.22 231.3 1RR009 RB211 524G MTF 4.25 32.1 253 1RR010 RB211 524G MTF 4.25 32.1 253 4RR036 RB211 524G T MTF 4.25 32.1 253 1RR011 RB211 524H MTF 4.2 34.0 264.4 4RR037 RB211 524H T MTF 4.2 34.0 264 1RR012 RB211 535C TF 4.5 21.5 163.3 1RR013 RB211 535E4 TF 4.1 25.4 176.1 1RR014 RB211 535E4 TF 4.1 25.4 176.1 3RR028 RB211 535E4 TF 4.1 25.8 178.4 5RR038 RB211 535E4 Phase 5 MTF 4.1 26.0 178.4 3RR034 RB211 535E4B TF 4.1 27.65 191.73 5RR039 RB211 535E4B Phase 5 MTF 4.1 27.9 191.7 4RR035 Spey 555 Transply IIF MTF 1.0 15.9 44 1RR015 SPEY Mk511 MTF 0.64 19.9 50.7 1RR016 SPEY Mk511 Transply IIH MTF 0.64 18.7 50.7 1RR017 SPEY Mk555 MTF 1.0 16.1 43.8 1RR018 SPEY Mk555 Transply IIF MTF 1.0 15.9 44 3RR031 TAY 650 Pedhead MTF 3.0 15.9 67.2 3RR032 TAY 651 Pedhead MTF 3.0 16.4 68.5 3RR033 TAY 651 Transply MTF 3.0 16.4 68.5 1RR019 TAY Mk611 8 MTF 3.0 16.1 61.6 6RR042 TAY 611 8C Transply IIJ TF 3.2 15.75 61.61 1RR020 TAY Mk620 15 MTF 3.0 16.1 61.6 1RR021 TAY Mk650 15 MTF 3.0 16.4 67.2 6RR041 Trent 556 61 Phase 5 tiled TF 7.5 36.71 261.5 2RR022 Trent 768 TF 5.15 34.04 298.7 3RR029 Trent 768 Improved traverse TF 5.15 34 300.3 2RR023 Trent 772 TF 5.03 35.79 315.9 3RR030 Trent 772 Improved traverse TF 5.03 35.8 316.3 2RR024 Trent 875 TF 6.08 35.42 351.85 2RR025 Trent 877 TF 6.02 36.30 361.64 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 H I J K L M N O P Q R S T U UID Data Superseded Data No PR C R superseded by NME DTEPS Other Corr as Out of Date Out of Date UID No Annex 16 Production Service  Data Status  Current Engine Status

 Test Engine Status

321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 1RR008  x     x  x x

1RR009  x  x 1RR010  x  x x

1RR010   x    x  x x

4RR036  x     x  x

1RR011       x  x x

4RR037  x     x  x

1RR012  x    x   x x

1RR013  x  x 1RR014  x  x x

1RR014   x x 3RR028  x  x x

3RR028   x    x  x x

5RR038  x     x  x

3RR034   x    x  x x

5RR039  x     x  x

4RR035  x     x  x x

1RR015 x     x x  x x

1RR016  x     x  x x

1RR017 x      x  x x

1RR018  x    x x  x

3RR031  x     x  x

3RR032  x     x  x

3RR033  x     x  x x

1RR019  x    x   x

6RR042  x     x  x

1RR020  x    x   x x

1RR021  x     x  x x

6RR041  x    x   x

2RR022  x    x   x x  x

3RR029  x     x  x

2RR023  x    x   x x  x

3RR030  x     x  x

2RR024  x     x  x

2RR025  x     x  x

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 V W X Y Z AA AB AC AD AE AF AG AH UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI HC  Number   Dp/ Foo ( HC)

( g/ kg) ( g/ kN)

321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 1RR008 0.59 0.26 0.70 1.41 3 1 3.44 0.08 3.3 3.5 5.3 27.0 805 1RR009 2.28 1.46 1.14 3.28 3 1 8.62 0.34 8.24 8.92 13.3 67.7 2174 1RR010 0.39 0.27 0.37 0.89 3 2 2.14 0.28 1.87 2.44 2.8 14.2 540 4RR036 0.00 0.03 0.00 3.95 3 1 6.24  5.29 7.11 9.6 49.0 1610 1RR011 0.34 0.33 0.36 0.74 3 2 1.93 0.28 1.61 2.14 2.5 12.8 495 4RR037 0 0.02 0 3.31 3 1 5.17  4.39 5.89 8.0 40.6 1348 1RR012 0.25 0.14 0.44 1.44 3 3 3.4 0.4 3.0 3.8 4.0 20.2 552 1RR013 0.69 0.94 1.33 2.85 5 2 7.12 0.45 6.6 7.7 9.3 47.3 1268 1RR014 0.04 0.01 0.04 1.00 3 1 1.69 0.09 1.59 1.77 2.6 13.3 307 3RR028 0 0.01 0.04 0.37 3 1 0.6  0.57 0.66 0.9 4.6 111 5RR038 0.03 0.00 0.04 0.27 3 1 0.46  0.32  0.7 0.7 3.6 83 3RR034 0.01 0.00 0.03 0.28 3 1 0.45  0.41 0.49 0.7 3.6 88 5RR039 0.07 0.00 0.05 0.14 3 1 0.28  0.16  0.54 0.4 2.2 54 4RR035 0.15 0.22 0.33 3.41 3 1 12.54  10.4 15.9 19.3 98.5 552 1RR015 0.98 1.32 7.23 56.73 15 14 217 82.8 109 360 232.4 1185.5 11179 1RR016 0.09 0.12 0.18 3.69 3 2 15.0 1.9 12.9 16.8 19.5 99.6 758 1RR017 0.88 1.60 6.97 92.74 2 2 392 82.1 334 450 510.1 2602.5 17160 1RR018 0.29 0.15 0.29 1.86 3 3 7.1 2.2 5.8 9.7 8.3 42.3 315 3RR031 0.11 0.22 0.11 1.23 1 1 3.90  3.90 6.0 30.6 261 3RR032 0.09 0.19 0.12 1.32 1 1 4.08  4.08 6.3 32.1 276 3RR033 0.56 0.37 0.85 3.1 4 2 10.2  9.9 10.4 13.3 67.9 689 1RR019 0.8 0.3 0.9 3.4 6 2 10.7 1.4 9.11 12.97 13.9 71.0 684 6RR042 0.02 0 0 1.11 3 1 2.96 0 2.56 3.37 4.6 23.2 182.4404 1RR020 0.8 0.3 0.9 3.4 6 2 10.7 1.4 9.11 12.97 13.9 71.0 684 1RR021 0.37 0.41 0.88 3.29 4 2 10.7 0.63 10.2 11.1 13.9 71.0 717 6RR041 0 0 0 0.1 4 2 0.1 0.14 0  0.2 0.2 1.0 36 2RR022 0.25 0.38 0.84 1.08 3 1 2.52  1.53  3.52 3.9 19.8 752 3RR029 0 0.01 0.01 1.89 3 1 2.7  2.29 3.13 4.2 21.4 801 2RR023 0.33 0.35 0.81 0.97 3 1 2.29  1.23  3.18 3.5 18.0 735 3RR030 0 0 0.01 1.46 3 1 2.06  1.74 2.37 3.2 16.3 640 2RR024 0 0 0 1.78 3 1 2.20  1.85 2.52 3.4 17.3 778 2RR025 0 0 0 1.55 3 1 1.90  1.60 2.18 2.9 14.9 677 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AI AJ AK AL AM AN AO AP AQ AR AS AT AU UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI CO  Number  Dp/ Foo ( CO)

( g/ kN)

( g/ kg)

321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 1RR008 1.24 0.34 1.56 9.30 3 1 18.07 0.64 17.6 18.8 22.2 18.8 4223 1RR009 0.59 0.43 1.01 13.74 3 1 23.49 0.34 23.13 23.81 28.8 24.4 5926 1RR010 0.59 0.43 1.01 13.74 3 1 23.49 0.34 23.13 23.81 28.8 24.4 5926 4RR036 0.16 0.14 1.17 28.82 3 1 46.37  43.60 50.58 56.9 48.2 11954 1RR011 0.87 0.38 0.99 11.75 3 1 19.35 0.37 18.9 19.6 23.8 20.1 5143 4RR037 0.18 0.14 1.05 26.17 3 1 41.67  39.21 45.02 51.2 43.3 10871 1RR012 0.70 0.27 0.48 18.79 3 3 37.3 2.6 35.5 40.3 40.3 34.2 6030 1RR013 1.01 1.23 1.71 15.44 5 2 28.6 3.5 24.6 33.4 32.6 27.6 5134 1RR014 1.01 1.23 1.71 15.44 5 2 28.6 3.5 24.6 33.4 32.6 27.6 5134 3RR028 0.77 0.5 1.14 13.31 3 1 22.3  22.0 22.6 27.4 23.2 4040 5RR038 0.26 0.29 2.72 20.33 3 1 33.6  33.3  33.8 41.2 34.9 6126 3RR034 0.94 0.60 1.05 11.76 3 1 19.67  19.35 19.92 24.1 20.5 3837 5RR039 0.33 0.26 2.43 18.24 3 1 29.7  29.45  29.91 36.5 30.9 5812 4RR035 1.54 2.08 5.78 31.16 3 1 118.08  116.5 120.0 144.9 122.8 5203 1RR015 1.81 2.06 20.30 97.96 15 14 382 66.5 233 522 395.8 335.4 19810 1RR016 0.12 0.63 2.65 31.77 3 2 128.9 8.3 119.5 135.3 146.9 124.5 6536 1RR017 0.44 0.0 22.22 88.23 2 2 388 148.9 283 493 442.1 374.6 17026 1RR018 0.3 0.7 3.7 29.3 3 3 106.3 16.3 88.7 120.8 115.0 97.4 4648 3RR031 0.69 0.48 1.76 22.36 4 1 65.16  62.4 67.9 80.0 67.8 4361 3RR032 0.75 0.51 1.64 23.26 4 1 66.93  64.2 69.8 82.2 69.6 4532 3RR033 1.68 1.93 6.11 32.68 4 2 99.7  91.6 107.8 113.6 96.3 6744 1RR019 0.7 0.8 3.9 24.1 6 2 69.3 4.1 65.5 74.8 79.0 66.9 4440 6RR042 1.12 1.27 4.99 28.55 3 1 82.78 0 78.58 86.04 101.6 86.1 5103 1RR020 0.7 0.8 3.9 24.1 6 2 69.3 4.1 65.5 74.8 79.0 66.9 4440 1RR021 1.74 2.01 6.54 33.77 4 2 102.9 11.8 94.6 111.3 117.2 99.4 6921 6RR041 0.02 0.25 0.46 10.3 4 2 14.6 0.99 13.9  15.3 16.6 14.1 3826 2RR022 0.18 0.13 0.86 10.52 3 1 15.10  13.83 15.92 18.5 15.7 4496 3RR029 0.18 0.15 1.02 20.22 3 1 29.7  27.6 31.4 36.5 30.9 8786 2RR023 0.18 0.15 0.78 9.36 3 1 13.32  12.29 14.00 16.4 13.9 4175 3RR030 0.2 0.16 0.89 17.94 3 1 26  24.2 27.4 31.9 27.0 8099 2RR024 0.19 0.16 0.86 19.66 3 1 24.93  23.17 26.31 30.6 25.9 8848 2RR025 0.20 0.16 0.80 18.42 3 1 23.26  21.62 24.46 28.6 24.2 8302 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AV AW AX AY AZ BA BB BC BD BE BF BG BH BI BJ UID LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic Original CAEP 2 CAEP 4 Total mass ( g)

 Number

( g/ kg)

 EI NOx ( g/ kN)

 Dp/ Foo ( NOx) Characteristic as % of standards 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 1RR008 59.35 43.01 10.63 4.41 3 1 86.54 0.55 85.9 86.9 100.3 99.9 124.8 148.7 20124 1RR009 58.71 40.54 9.56 4.63 3 1 83.57 1.39 82.34 85.08 96.9 93.0 116.2 136.1 21075 1RR010 58.71 40.54 9.56 4.63 3 1 83.57 1.39 82.34 85.08 96.9 93.0 116.2 136.1 21075 4RR036 28.43 21.80 9.68 4.00 3 1 49.42  48.0 50.3 57.3 55.0 68.7 80.5 12513 1RR011 65.84 46.31 10.26 4.78 3 1 92.83 1.79 91.1 94.6 107.6 99.6 124.5 143.5 24501 4RR037 31.19 23.19 9.91 4.16 3 1 53.09  51.6 54.1 61.5 57.0 71.2 82.1 13995 1RR012 33.71 24.89 6.37 3.44 3 3 57.0 2.0 54.1 58.7 60.4 72.7 90.9 113.1 9277 1RR013 52.7 36.2 7.5 4.3 5 2 76.9 1.3 75.0 78.9 84.6 93.1 116.4 141.8 13633 1RR014 52.7 36.2 7.5 4.3 5 2 76.9 1.3 75.0 78.9 84.6 93.1 116.4 141.8 13633 3RR028 44.88 32.06 6.78 3.46 3 1 65.6  64.4 66.9 76.0 83.0 103.7 126.1 11714 5RR038 22.31 17.56 8.38 4.4 3 1 41.8  40.3  43.6 48.5 52.7 65.8 80.0 7492 3RR034 54.46 36.82 7.35 3.52 3 1 76.97  75.9 77.9 89.2 93.6 117.0 141.0 14791 5RR039 25.88 19.3 8.65 4.58 3 1 46.4  44.9  48.0 53.8 56.1 70.2 84.5 8927 4RR035 17.33 13.06 5.05 2.23 3 1 49.02  46.7 52.8 56.8 79.1 98.9 105.5 2160 1RR015 23.27 19.18 7.94 1.48 14 13 69.1 7.39 52.5 81.4 71.0 89.0 111.2 120.6 3513 1RR016 22.7 17.3 7.2 3.6 3 2 73.0 4.8 67.8 77.2 80.3 103.7 129.6 140.9 3701 1RR017 18.92 14.64 5.92 1.83 2 2 50.75 12.48 41.9 59.6 55.8 77.3 96.6 102.9 2354 1RR018 21.9 16.5 6.8 3.7 3 3 65.5 1.7 64.5 67.5 69.4 96.6 120.8 128.8 2880 3RR031 16.45 12.94 5.26 2.50 4 1 38.75  38.1 39.5 44.9 62.6 78.2 91.6 2591 3RR032 17.56 13.77 5.42 2.52 4 1 40.45  39.7 41.1 46.9 64.4 80.5 94.6 2760 3RR033 20.31 17.13 4.77 1.72 4 2 43.9  40.9 46.8 48.3 66.3 82.9 97.4 2990 1RR019 21.1 16.8 5.7 2.5 6 2 45.6 0.7 44.9 46.7 50.1 69.5 86.8 99.2 2814 6RR042 18.42 15.01 5.6 2.76 3 1 41.59 0 40.99 41.92 48.2 67.4 84.3 96.6 2562 1RR020 21.1 16.8 5.7 2.5 6 2 45.6 0.7 44.9 46.7 50.1 69.5 86.8 99.2 2814 1RR021 19.81 16.47 4.55 1.70 4 2 42.8 3.92 40.2 45.6 47.1 64.6 80.8 94.4 2875 6RR041 44.91 32.76 11.78 6.19 4 2 61.1 0.42 60.8  61.4 67.2 59.2 74.1 83.6 16113 2RR022 39.11 30.01 10.34 5.60 3 1 62.52  62.1  62.8 72.5 67.1 83.8 96.5 18672 3RR029 31.25 24.66 10.01 4.52 3 1 52.2  51.0 53.1 60.5 56.0 70.0 80.7 15658 2RR023 43.60 32.66 10.68 5.74 3 1 68.09  67.7  68.4 78.9 70.7 88.4 100.4 21462 3RR030 34.38 26.44 10.3 4.71 3 1 56.3  55.0 57.4 65.3 58.5 73.1 83.1 17784 2RR024 33.32 26.55 10.43 4.64 3 1 49.88  48.7 50.8 57.8 52.2 65.2 74.3 17575 2RR025 34.76 27.59 10.59 4.75 3 1 51.82  50.5 52.8 60.1 53.3 66.7 75.5 18736 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BK BL BM BN BO BP BQ BR BS BT BU BV UID Characteristic No T/ O C/ O App Idle Test Eng Max Sigma Range Characteristic % of Reg limit  Smoke Number

 Smoke Number  Number

321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 1RR008     3 1 12.3 0.31 12.1 12.7 15.8 84.2 1RR009     3 1 3.9 0.37 3.7 4.3 5.0 27.3 1RR010     3 1 3.9 0.37 3.7 4.3 5.0 27.3 4RR036     3 1 5.34  4.7 6.0 6.9 37.4 1RR011     3 1 3.9 0.37 3.7 4.3 5.0 27.7 4RR037     3 1 5.34  4.7 6.0 6.9 37.9 1RR012      3 8.0 3.0 4.6 10.1 8.8 42.5 1RR013     5 2 1.7 0.3 1.5 2.3 2.0 9.8 1RR014     5 2 1.7 0.3 1.5 2.3 2.0 9.8 3RR028     3 1 1.8  1.5 2.2 2.3 11.4 5RR038     3 1 7.3  6.9  7.9 9.4 46.5 3RR034     3 1 1.84  1.5 2.2 2.4 12.1 5RR039     3 1 7.3  6.9  7.9 9.4 47.5 4RR035     3 1 27.97  26.9 28.8 36.0 121.5 1RR015 66.2 < 66.2 < 66.2 < 66.2 10 10 66.2 7.2 50.4 71.3 77.9 273.1 1RR016     3 2 21.9 3.1 19.9 25.4 25.7 90.1 1RR017 N/ A N/ A N/ A N/ A N/ A N/ A N/ A N/ A N/ A

1RR018     3 3 25.8 1.7 24.0 27.4 28.4 95.7 3RR031     4 1 9.87  9.3 10.4 12.7 48.1 3RR032     4 1 9.87  9.3 10.4 12.7 48.4 3RR033     4 2 17.5  16.1 18.9 20.5 78.1 1RR019     6 2 21.3 1.6 18.9 22.8 25.0 92.4 6RR042 3.93 2.24 0.23 0.13 3 1 3.93 0 3.53 4.35 5.06 18.7 1RR020     6 2 21.3 1.6 18.9 22.8 25.0 92.4 1RR021     4 2 17.6 1.98 16.2 19.0 20.6 78.2 6RR041 2.24 2.09 1.02 0.76 4 2 3.1 1.13 2.3  3.9 3.7 20.3 2RR022     3 1 1.26  1.1  1.5 1.6 9.2 3RR029     3 1 2  1.6 2.5 2.6 14.8 2RR023     3 1 1.26  1.1  1.5 1.6 9.4 3RR030     3 1 2  1.6 2.5 2.6 15.1 2RR024     3 1 5.34  4.7 6.0 6.9 41.0 2RR025     3 1 5.34  4.7 6.0 6.9 41.3 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 BW BX BY BZ CA CB CC CD CE UID Fuel per No Spec H/ C Arom T/ O C/ O App Idle LTO cycle Ratio % ( kg)

 Fuel Flow

( kg/ sec)

 Fuel

321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 1RR008 AVTUR 1.91 20 2.34 1.91 0.65 0.26 912 1RR009 AVTUR 1.91 20 2.62 2.08 0.70 0.26 958 1RR010 AVTUR 1.91 20 2.62 2.08 0.70 0.26 958 4RR036 AVTUR 1.95 16 2.62 2.10 0.74 0.26 970 1RR011 AVTUR 1.91 20 2.73 2.17 0.71 0.26 977 4RR037 AVTUR 1.95 16 2.81 2.22 0.77 0.26 1001 1RR012 AVTUR 1.91 20 1.80 1.47 0.54 0.20 711 1RR013 AVTUR 1.91 20 1.86 1.51 0.57 0.19 711 1RR014 AVTUR 1.91 20 1.86 1.51 0.57 0.19 711 3RR028 AVTUR 1.9 18.2 1.86 1.51 0.52 0.18 683 5RR038 AVTUR 1.931 17.6 1.85 1.5 0.52 0.18 681 3RR034 AVTUR 1.90 18.2 2.08 1.65 0.55 0.19 734 5RR039 AVTUR 1.931 17.6 2.07 1.64 0.55 0.19 732 4RR035 AVTUR 1.87 1.95 15 20 0.735 0.593 0.221 0.0964 313 1RR015 DERD 2494 1.94 20 0.889 0.726 0.279 0.119 386 1RR016 DERD 2494 1.91 20 0.891 0.726 0.278 0.127 398 1RR017 DERD 2494 1.94 20 0.720 0.589 0.222 0.115 341 1RR018 DERD 2494 1.91 20 0.735 0.592 0.221 0.096 312 3RR031 AVTUR 1.95 16.1 0.86 0.71 0.25 0.12 377 3RR032 AVTUR 1.95 16.1 0.87 0.72 0.26 0.12 381 3RR033 AVTUR 1.91 20 0.87 0.72 0.26 0.12 381 1RR019 AVTUR 1.91 20 0.76 0.63 0.23 0.11 342 6RR042  1.986 17.5 0.741 0.612 0.241 0.105 334 1RR020 AVTUR 1.91 20 0.76 0.63 0.23 0.11 342 1RR021 AVTUR 1.91 20 0.874 0.715 0.254 0.119 378 6RR041  1.97 17.6 2.24 1.83 0.62 0.23 843 2RR022 AVTUR 1.94 16 2.94 2.42 0.80 0.26 1041 3RR029 AVTUR 1.95 16 2.97 2.43 0.81 0.27 1061 2RR023 AVTUR 1.94 16 3.15 2.58 0.84 0.27 1096 3RR030 AVTUR 1.95 16 3.2 2.58 0.85 0.28 1116 2RR024 AVTUR 1.95 16 3.10 2.57 0.88 0.28 1117 2RR025 AVTUR 1.95 16 3.21 2.66 0.90 0.28 1139 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CF CG CH CI CJ CK CL CM UID No Baro Temp Humidity kW @ Power % CF @ Power kPa K kg/ kg  Ambient

 Loads

Power Extraction  Stage Bleed

321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 1RR008 0  0  103 283  286 0.005 1RR009 0  0  101 283  286 0.006 1RR010 0  0  101 283  286 0.006 4RR036 0  0  100.2 287 .0053. 0089 1RR011 0  0  101 283  286 0.006 4RR037 0  0  100.2 287 .0053. 0089 1RR012 0  0   281  287 0.004 0.005 1RR013 0  0  100.8 101.2 285  298 0.0058 0.0087 1RR014 0  0  100.8 101.2 285  298 0.0058 0.0087 3RR028 0  0  98.8 282 0.0037 5RR038 0  0  100.7  101.2 281  287 .0058  .0064 3RR034 0  0  98.8 282 0.0037 5RR039 0  0  100.7  101.2 281  287 .0058  .0064 4RR035 0  0  100.2 287 .0068. 0088 1RR015 0  0    0.0035 0.0126 1RR016 0  0  99 102 285  289 0.006 0.009 1RR017 0  0  102 279 N/ A 1RR018 0  0  99 102 280  290 0.006 0.010 3RR031 0  0   283 .0068. 0081 3RR032 0  0   283 .0068. 0081 3RR033 0  0  99 101 280 289 .005. 008 1RR019 0  0  100 288 0.005 6RR042 0  0  99.9  100 281.4  282.7 0.00475 1RR020 0  0  100 288 0.005 1RR021 0  0  99 101 280  289 .005. 008 6RR041 0  0  100.04  102.91 275.5  280.3 0.0038  0.0062 2RR022 0  0  100.6 293 .0073  .0084 3RR029 0  0  100.2 287 .0053. 0089 2RR023 0  0  100.6 293 .0073  .0084 3RR030 0  0  100.2 287 .0053. 0089 2RR024 0  0  100.2 287 .00527  .00886 2RR025 0  0  100.2 287 .00527  .00886 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CN CO CP CQ CR CS UID  Test Dates

No Manufacturer Test Organisation Test Location From To 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 1RR008 Rolls Royce Ltd Rolls Royce Ltd SINFIN Derby Sep 86 Sep 86 1RR009 Rolls Royce Ltd Rolls Royce Ltd SINFIN Derby Apr 87 May 87 1RR010 Rolls Royce Ltd Rolls Royce Ltd SINFIN Derby Apr 87 Oct 92 4RR036 Rolls Royce plc Rolls Royce plc SINFIN, Derby Sep 94 1RR011 Rolls Royce Ltd Rolls Royce Ltd SINFIN Derby Apr 87 Oct 92 4RR037 Rolls Royce plc Rolls Royce plc SINFIN, Derby Sep 94 1RR012 Rolls Royce Ltd Rolls Royce Ltd SINFIN Derby Apr 84 May 84 1RR013 Rolls Royce Ltd Rolls Royce Ltd SINFIN Derby 2 Jul 84 25 Oct 84 1RR014 Rolls Royce Ltd Rolls Royce Ltd SINFIN Derby 2 Jul 84 Apr 91 3RR028 Rolls Royce plc Rolls Royce plc SINFIN, Derby Apr 91

5RR038 Rolls Royce plc Rolls Royce plc Hucknall May 99 3RR034 Rolls Royce plc Rolls Royce plc SINFIN, Derby Apr 91

5RR039 Rolls Royce plc Rolls Royce plc Hucknall May 99 4RR035 Rolls Royce plc Rolls Royce plc SINFIN, Derby 1987 1RR015 Rolls Royce Ltd Rolls Royce Ltd Derby 1970 1975 1RR016 Rolls Royce Ltd Rolls Royce Ltd Derby Sep 84 Aug 85 1RR017 Rolls Royce Ltd Rolls Royce Ltd Derby 1973 1975 1RR018 Rolls Royce Ltd   Aug 83 Nov 84 3RR031 Rolls Royce plc Rolls Royce plc SINFIN, Derby Jun 97 3RR032 Rolls Royce plc Rolls Royce plc SINFIN, Derby Jun 97 3RR033 Rolls Royce plc Rolls Royce plc SINFIN, Derby Mar 88 Oct 89 1RR019 Rolls Royce Ltd   Oct 86 Nov 86 6RR042 Rolls Royce Rolls Royce Dahlewitz 21 Jan 02 22 Jan 02 1RR020 Rolls Royce Ltd   Oct 86 Nov 86 1RR021 Rolls Royce Ltd Rolls Royce Ltd Derby Mar 88 Oct 89 6RR041 Rolls Royce Rolls Royce Derby 7 Jan 02 18 Jan 02 2RR022 Rolls Royce plc Rolls Royce plc SINFIN, Derby Jul 94

3RR029 Rolls Royce plc Rolls Royce plc SINFIN, Derby Sep 94

2RR023 Rolls Royce plc Rolls Royce plc SINFIN, Derby Jul 94

3RR030 Rolls Royce plc Rolls Royce plc SINFIN, Derby Sep 94

2RR024 Rolls Royce plc Rolls Royce plc SINFIN, Derby Sep 94

2RR025 Rolls Royce plc Rolls Royce plc SINFIN, Derby Sep 94

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CT CU UID No Remarks 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 1RR008 1. Data from certification report CRR60515. 2. Phase 2 combustor. 3. Applicable to engines manufactured after Feb 87.

1RR009 Data from certification report CRR60560 1RR010 HC data remeasured.

4RR036 Data from Certification Report DNS38044 1RR011

4RR037 Data from Certification Report DNS38044 1RR012 Data from certification report CRR58085 1RR013 Ref RR report CRR58095 1RR014 HC data remeasured.

3RR028 Data from Certification Report DNS21233 5RR038 1. Data from certification report DNS63281. 2. Phase 5 combustor 3RR034 Data from Certification Report DNS21233 5RR039 1. Data from certification report DNS63281. 2. Phase 5 combustor 4RR035 1. Ref RR report CRR10165 2. Transply IIF combustors with standard fuel pump 1RR015

1RR016 1. Data from RR report CRR10149. 2. Transply IIH combustors.

1RR017

1RR018 1. Ref RR report CRR10145. 2. Transply IIF combustors with H. P. fuel pump.

3RR031 Pedhead combustor 3RR032 Pedhead combustor 3RR033 Transply combustor 1RR019 Data from certification report CRR19019 6RR042 1. Certification report E TR164/ 02 2. New airspray fuel injector 1RR020 Data from certification report CRR19019 1RR021 Data from certification report CRR19057 6RR041 1. Certification report DNS 85728 2. Phase 5 tiled combustor 2RR022 Data from certification report DNS 12859 3RR029 1. Data from certification report DNS 19234. 2. Improved traverse combustor.

2RR023 Data from certification report DNS 12859 3RR030 1. Data from certification report DNS 19234. 2. Improved traverse combustor.

2RR024 Data from certification report DNS 14445 2RR025 Data from certification report DNS 14445 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 CV CW CX CY CZ DA DB DC DD DE DF DG DH 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 New airspray fuel injector Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 DI DJ DK DL DM DN 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 A B C D E F G UID Engine Combustor Eng B/ P Press Rated No Identification Description Type Ratio Ratio Output kN 353 354 355 356 357 358 359 360 361 362 363 364 365 366 2RR026 Trent 884 TF 5.87 38.96 390.10 2RR027 Trent 892 TF 5.7 41.38 411.48 5RR040 Trent 895 TF 5.7 41.52 413.05 Textron Lycoming 1TL001 ALF 502L 2 TF 5.1 13.15 33.4 1TL002 ALF 502R 3 TF 5.7 11.4 29.8 1TL003 ALF 502R 5 TF 5.6 12.0 31.0 1TL004 LF507 1F,  1H TF 5.1 13.0 31.0 ZMKB 1ZM001 D 36 TF 5 19.9 63.765 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 H I J K L M N O P Q R S T U UID Data Superseded Data No PR C R superseded by NME DTEPS Other Corr as Out of Date Out of Date UID No Annex 16 Production Service  Data Status  Current Engine Status

 Test Engine Status

353 354 355 356 357 358 359 360 361 362 363 364 365 366 2RR026  x     x  x

2RR027  x     x  x

5RR040  x     x  x

1TL001  x    x   x x

1TL002  x    x   x x

1TL003  x    x   x x

1TL004  x    x   x

1ZM001  x    x   x x

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 V W X Y Z AA AB AC AD AE AF AG AH UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI HC  Number   Dp/ Foo ( HC)

( g/ kg) ( g/ kN)

353 354 355 356 357 358 359 360 361 362 363 364 365 366 2RR026 0 0 0 1.00 3 1 1.21  1.03 1.40 1.9 9.5 484 2RR027 0.01 0 0 0.7 3 1 0.79  0.67 0.93 1.2 6.1 329 5RR040 0.02 0.00 0.00 0.89 3 1 1.10  0.95  1.24 1.7 8.6 462 1TL001 0.02 0.023 0.183 6.65 3 3 15.3 2.59 13.2 18.2 17.8 90.8 501 1TL002 0.056 0.053 0.287 6.51 3 3 15.0 3.25 11.9 18.4 17.5 89.3 449 1TL003 0.060 0.053 0.217 5.39 3 3 11.7   13.6 69.4 351 1TL004 0.01 0.01 0.12 4.72 3 1 10.8   16.7 85.2 337 1ZM001 0 0 0 5.4 7 3 12 0.8 11.2 13 14.0 71.4 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AI AJ AK AL AM AN AO AP AQ AR AS AT AU UID Characteristic LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic % of Total mass Reg limit ( g)

 EI CO  Number  Dp/ Foo ( CO)

( g/ kN)

( g/ kg)

353 354 355 356 357 358 359 360 361 362 363 364 365 366 2RR026 0.24 0.18 0.65 15.19 3 1 19.02  17.64 19.78 23.4 19.8 7602 2RR027 0.28 0.2 0.57 13.07 3 1 15.34  13.98 16.27 18.8 15.9 6381 5RR040 0.27 0.19 0.54 14.71 3 1 18.80  17.71  19.67 23.1 19.6 7834 1TL001 0.40 0.30 3.97 45.63 3 3 107.3 6.47 101.5 114.3 116.1 98.4 3527 1TL002 0.433 0.500 8.43 44.67 3 3 109.0 10.62 100.2 120.8 117.9 99.9 3244 1TL003 0.300 0.250 7.10 40.93 3 3 90.4   97.8 82.9 2796 1TL004 0.20 0.30 4.43 37.83 3 1 90.10   110.6 93.7 2803 1ZM001 0.5 0.4 2.7 20.7 7 3 48.8 3 46.2 52 52.8 44.7 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 AV AW AX AY AZ BA BB BC BD BE BF BG BH BI BJ UID LTO No T/ O C/ O App Idle Test Eng Average Sigma Range Characteristic Original CAEP 2 CAEP 4 Total mass ( g)

 Number

( g/ kg)

 EI NOx ( g/ kN)