Introduction ICAO ENGINE EXHAUST EMISSIONS DATA BANK SUBSONIC ENGINES Introduction This workbook contains a combined version of the ICAO Exhaust Emissions Data Bank There are five worksheets. The first sheet is the Introduction sheet, which is this sheet.

A record of the issue number and changes to the databank is held in Record of Changes.

The Record of Changes sheet is followed by a background description of the databank ( Background).

The Data spreadsheet contains all the data for all the engines with one engine per row. Engines are grouped by manufacturer.

In this version the engines of each manufacturer are grouped alphabetically so that for each engine e. g. PW4056, all versions appear together.

Column Description describes the contents of each column in the Data worksheet.

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Introduction, Page 1 of 149 Record of Changes Issue Date Detail of Changes 17 Mar 04 Issue 12 implemented on Website.

9 Mar 04 New engine data added, CFM56 5C2/ P, 5C3/ P, 5C4/ P, 5B8/ P, 5B9/ P, 5B9/ 2P 1CM006 engine identification changed from CFM56 3C ( rerated) to CFM56 3C 1 ( rerated) 1CM004, 005, 006  additional note, number 4, added.

27 Feb 04 New engine data, PW306A, PW306B, PW308A, PW308C added.

23 Dec 03 New engine data added BR700 710 C4 11 28 Nov 03 Issue 11 implemented on Website.

27 Nov 03 New engine data added  Tay 611 8C 11 2 Sep 03 Correction to engine identifier for UID 1RR001, M54H corrected to M45H Correction to data for engines UID's 3GE067 to 3GE079 to include note showing idle data calculated at normal idle setting rather than 7%. 1 Sep 03 New engine data added  CF34 8C1 Block 1 10 19 May 03 Issue 10 implemented on Website. No new data at this time. 12 Feb 03 Data in columns CR and CS changed to date format ( previously a mixture of date and text formats). 4 Feb 03 New engine data added  CF34 8C5,  8E2,  8E5,  8E5A1 New engine data added  CFM56 5B7/ P CF6 80E series UID No's 2GE050, 2GE051 and 4GE081 not currently produced with low emissions combustor ( 1862M39), marked as out of production. 28 Nov 02 New engine data added  AE3007 family, 20 new entries.

9 31 Jul 02 New engine data added  Trent 556 61 with Phase 5 tiled combustor 17 Jul 02 New engine data added  GE90 76B,  77B,  85B,  90B,  94B with turbomachinery incorporating 3D aero 2 Jul 02 Further format changes. No new data at this time. 27 Mar 02 Rolls Royce Corporation AE3007C1 added 8 19 Dec 01 New engine data added  GE90 76B 27 Nov 01 New engine data added  CF34 3B, CF34 8C1, CF6 80E1A3 Changes to background notes, column descriptions and data base format ( data requirements and associated data)

7 14 Nov 00 New engine data added  PW4098 27 Oct 00 New engine data added  PW4168 with TALON II combustor.

6 2 May 00 New engine data added  PW4X58 with TALON II combustor.

5 29 Feb 00 New engine data added  Trent 895 New engine data added  RB211 535E4 and  535E4B with phase 5 combustor 4 31 Dec 99 New engine data added  AE3007A, AE3007A1 series ( A1, A1/ 1, A1/ 2) New engine data added  PW2037 and PW2040  revised to add second engine test New engine data added  BR700 710A1 10,  710A2 20.

3 16 Nov 99 New engine data added  BR700 715A1 30,  715B1 30 and 715C1 30 with improved fuel injectors. New engine data added  JT8D 217,  217A,  217C,  219 with E Kit combustors.

2 8 Feb 99 Engine UID 2PW062, CO idle EI and Dp/ Foo average were reversed. This has been corrected. New engine data added. Spey 555, standard fuel pump. RB211 524G T and  524 H T, BR700 715A1 30,  715B1 30 and  715C1 30 New engine data added. CFM56 5A4,  5A5. CFM56 5B2/ 2P,  5B3/ 2P CFM56 7B20/ 2,  7B22/ 2,  7B24/ 2,  7B26/ 2,  7B27/ 2. CF6 80E1A4 standard combustor, CF6 80E1A4 low emissions combustor PW4168A 1 10 Mar 98 First full issue of the databank on the internet Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Record of Changes, Page 2 of 150 Background Double click on the icon to open the file in Microsoft Word.

Databank supporting text Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Background, Page 3 of 150 Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 A B C D E F G UID Engine Combustor Eng B/ P Press Rated No Identification Description Type Ratio Ratio Output kN Allied Signal 1AS001 TFE731 2 2B TF 2.64 13.9 15.6 1AS002 TFE731 3 TF 2.64 14.3 16.5 Allison Engine Company / Rolls Royce Corporation 4AL003 AE3007A TF 5.23 18.08 33.73 4AL002 AE3007A1 series TF 4.76 17.81 33.73 3AL001 AE3007C TF 5.3 16.2 28.6 6AL004 AE3007C1 TF 5.1 16.6 31.5 6AL005 AE3007A1 Type 1 TF 4.77 17.97 34.91 6AL006 AE3007A1 Type 2 TF 4.77 17.97 34.91 6AL007 AE3007A1 Type 3 ( reduced emissions) TF 4.77 17.97 34.91 6AL008 AE3007A1/ 1 Type 1 TF 4.77 17.9 34.74 6AL009 AE3007A1/ 1 Type 2 TF 4.77 17.9 34.74 6AL010 AE3007A1/ 1 Type 3 ( reduced emissions) TF 4.77 17.9 34.74 6AL011 AE3007A1/ 3 Type 1 TF 4.81 17.22 33.05 6AL012 AE3007A1/ 3 Type 2 TF 4.81 17.22 33.05 6AL013 AE3007A1/ 3 Type 3 ( reduced emissions) TF 4.81 17.22 33.05 6AL014 AE3007A1P Type 1 TF 4.77 17.9 34.74 6AL015 AE3007A1P Type 2 TF 4.77 17.9 34.74 6AL016 AE3007A1P Type 3 ( reduced emissions) TF 4.77 17.9 34.74 6AL017 AE3007A3 Type 1 TF 4.72 17.2 33 6AL018 AE3007A3 Type 2 TF 4.72 17.2 33 6AL019 AE3007A3 Type 3 ( reduced emissions) TF 4.72 17.2 33 6AL020 AE3007A1E Type 3 TF 4.72 19.06 37.16 6AL021 AE3007C Type 1 TF 5.2 15.8 29.62 6AL022 AE3007C Type 2 TF 5.2 15.8 29.62 6AL023 AE3007C1 Type 1 TF 5.1 16.58 31.46 6AL024 AE3007C1 Type 2 TF 5.1 16.58 31.46 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 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 1AS001 x     x    x

1AS002 x     x    x

4AL003  x     x  x

4AL002  x  x   x  x

3AL001  x  x   x  x

6AL004  x  x 6AL023  x  x

6AL005   x    x  x

6AL006  x     x  x

6AL007  x     x  x

6AL008  x     x  x

6AL009  x     x  x

6AL010  x     x  x

6AL011  x     x  x

6AL012  x     x  x

6AL013  x     x  x

6AL014  x     x  x

6AL015  x     x  x

6AL016  x     x  x

6AL017  x     x  x

6AL018  x     x  x

6AL019  x     x  x

6AL020  x     x  x

6AL021  x     x  x

6AL022  x     x  x

6AL023  x     x  x

6AL024  x     x  x

 Data Status  Current Engine Status

 Test Engine Status

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 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)

1AS001 0.114 0.128 4.26 20.04 3 3 53.4  50 58 62.3 317.8 823 1AS002 0.062 0.072 1.41 9.04 4 4 24.0  19 25 27.4 139.7 393 4AL003 0.25 0.29 0.64 2.51 3 2 6.65   8.7 44.1 226 4AL002 0.26 0.30 0.72 3.10 3 2 8.33   10.8 55.3 279 3AL001 0.29 0.33 0.83 5.84 3 2 13.46   17.5 89.3 387 6AL004 0.24 0.28 0.66 4.84 3 2 10.95   14.25 55.9 346 6AL005 0.221 0.257 0.655 3.818 3 2 8.78   11.42 58.3 307 6AL006 0 0 0.18 5.04 3 1 10.51   16.19 82.6 367 6AL007 0.03 0.03 0.03 3.85 3 1 8.01   12.34 63.0 279 6AL008 0.222 0.258 0.658 3.92 3 2 9.01   11.72 59.8 313 6AL009 0 0 0.18 5.1 3 1 10.67   16.43 83.8 370 6AL010 0.03 0.03 0.03 3.88 3 1 8.08   12.44 63.5 280 6AL011 0.233 0.269 0.689 4.64 3 2 10.8   14.05 71.7 357 6AL012 0 0 0.21 5.23 3 1 11.25   17.33 88.4 372 6AL013 0.03 0.03 0.03 3.81 3 1 8.15   12.55 64.0 269 6AL014 0.222 0.258 0.658 3.85 3 2 8.88   11.55 58.9 308 6AL015 0 0 0.19 5.06 3 1 10.61   16.34 83.4 368 6AL016 0.03 0.03 0.03 3.86 3 1 8.06   12.41 63.3 280 6AL017 0.233 0.27 0.69 4.705 3 2 10.93   14.22 72.6 361 6AL018 0 0 0.23 5.65 3 1 12.14   18.7 95.4 401 6AL019 0.03 0.03 0.03 4.1 3 1 8.75   13.48 68.8 289 6AL020 0.03 0.03 0.03 3.52 3 1 7.1   10.93 55.8 264 6AL021 0.254 0.291 0.696 4.953 3 2 10.79   14.04 71.6 320 6AL022 0 0.01 0.23 5.75 3 1 11.59   17.85 91.1 344 6AL023 0.24 0.277 0.661 4.837 3 2 10.95   14.25 72.7 344 6AL024 0 0.01 0.21 5.88 3 1 12.36   19.04 97.1 389  EI HC  Number   Dp/ Foo ( HC)

( g/ kg) ( g/ kN)

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 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)

1AS001 1.394 2.03 22.38 58.6 3 3 169.4  161 177 183.2 155.3 2612 1AS002 1.13 1.62 15.56 47.7 4 4 137.7  133 147 147.3 124.8 2254 4AL003 0.75 0.92 3.28 17.35 3 2 43.15   49.2 41.7 1468 4AL002 0.79 0.97 3.80 22.43 3 2 57.03   65.0 55.1 1910 3AL001 0.97 1.19 4.5 29.88 3 2 68   77.5 65.7 1964 6AL004 0.87 1.07 3.96 26.04 3 2 58.61   66.78 56.6 1850 6AL005 0.77 0.96 3.91 23.73 3 2 53.38   60.82 51.5 1865 6AL006 0.12 0.01 1.36 32.59 3 1 68.2   83.71 70.9 2383 6AL007 0.75 0.56 6.72 39.91 3 1 88.38   108.48 91.9 3088 6AL008 0.77 0.97 3.93 23.95 3 2 53.94   61.46 52.1 1874 6AL009 0 0 1.4 32.84 3 1 68.8   84.45 71.6 2389 6AL010 0.74 0.55 6.8 40.07 3 1 88.9   109.12 92.5 3088 6AL011 0.83 1.03 4.21 25.58 3 2 59.1   67.34 57.1 1954 6AL012 0 0 1.83 32.4 3 1 70.08   86.02 72.9 2317 6AL013 0.5 0.5 7.62 38.47 3 1 88.3   108.38 91.8 2919 6AL014 0.77 0.97 3.93 23.8 3 2 53.75   61.24 51.9 1867 6AL015 0 0 1.51 32.68 3 1 68.7   84.33 71.5 2386 6AL016 0.74 0.55 6.79 39.97 3 1 88.88   109.1 92.5 3087 6AL017 0.83 1.03 4.22 25.73 3 2 59.41   67.69 57.4 1960 6AL018 0 0 2 34.86 3 1 75.39   92.54 78.4 2488 6AL019 0.5 0.5 7.65 41.29 3 1 94.25   115.69 98.0 3111 6AL020 0.77 0.64 5.63 37.97 3 1 81.18   99.64 84.4 3018 6AL021 0.94 1.16 4.28 26.32 3 2 57.18   65.15 55.2 1695 6AL022 0 0 2.02 35.07 3 1 71.08   87.25 73.9 2108 6AL023 0.87 1.07 3.96 26.04 3 2 58.61   66.78 56.6 1842 6AL024 0 0 1.62 36.04 3 1 76   93.29 79.1 2389  EI CO  Number  Dp/ Foo ( CO)

( g/ kN)

( g/ kg)

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 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)

1AS001 15.25 13.08 5.90 2.82 3 3 40.5  39 43 42.9 63.3 79.1 75.8 630 1AS002 19.15 16.02 6.92 3.72 4 4 51.4  47 55 54.0 78.7 98.4 94.7 845 4AL003 20.54 17.47 7.79 3.83 3 2 46.30   50.9 66.8 83.6 85.6 1563 4AL002 19.78 16.84 7.22 3.52 3 2 44.61   49.1 64.9 81.1 83.1 1502 3AL001 16.92 14.56 6.63 3.24 3 2 34.73   38.2 52.8 66.0 66.4 991 6AL004 17.90 15.35 7.05 3.37 3 2 37.36   41.08 56.1 70.2 71.3 1175 6AL005 19.66 16.63 7.1 3.47 3 2 41.71   45.87 60.4 75.5 77.6 1456 6AL006 22.41 19.58 7.2 3.19 3 1 46.02   53.34 70.2 87.8 90.3 1607 6AL007 16.17 14.07 7.13 4.17 3 1 38.49   44.62 58.8 73.4 75.5 1344 6AL008 19.57 16.55 7.07 3.46 3 2 41.53   45.67 60.3 75.3 77.4 1442 6AL009 22.31 19.49 7.16 3.19 3 1 45.84   53.14 70.1 87.6 90.1 1592 6AL010 16.10 14.01 7.12 4.17 3 1 38.38   44.49 58.7 73.4 75.4 1333 6AL011 18.55 15.81 6.83 3.39 3 2 39.93   43.91 59.0 73.7 75.4 1319 6AL012 21.26 18.62 6.84 3.29 3 1 44.34   51.4 69.0 86.3 88.2 1465 6AL013 15.42 13.49 6.93 4.27 3 1 37.66   43.65 58.6 73.3 74.9 1245 6AL014 19.57 16.56 7.07 3.47 3 2 41.57   45.71 60.3 75.4 77.9 1444 6AL015 22.02 19.16 6.89 3.19 3 1 45.12   52.3 69.0 86.2 88.3 1567 6AL016 16.10 14.01 7.12 4.17 3 1 38.41   44.52 58.7 73.4 75.2 1334 6AL017 18.52 15.79 6.83 3.38 3 2 39.87   43.84 58.9 73.7 75.3 1316 6AL018 20.93 18.27 6.56 3.18 3 1 43.31   50.2 67.5 84.3 86.2 1429 6AL019 15.40 13.48 6.93 4.12 3 1 37.32   43.26 58.1 72.7 74.3 1232 6AL020 17.17 14.91 7.42 4.26 3 1 40.38   46.81 59.9 74.9 77.6 1501 6AL021 16.88 14.57 6.78 3.36 3 2 35.47   39 54.5 68.1 68.8 1050 6AL022 19.36 17.01 6.62 3.2 3 1 38.83   45.01 62.9 78.6 79.4 1150 6AL023 17.90 15.35 7.05 3.37 3 2 37.36   41.08 56.2 70.2 71.4 1175 6AL024 20.20 17.6 6.71 3.14 3 1 40.16   46.55 63.6 79.5 80.9 1262  Number

( g/ kg)

 EI NOx ( g/ kN)

 Dp/ Foo ( NOx) Characteristic as % of standards Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 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 1AS001

1AS002

4AL003 1 0 0 0 3 2 1   1.2 3.7 4AL002 1 0 0 0 3 2 1   1.2 3.7 3AL001 1 0 0 0 3 2 1   1.2 3.6 6AL004 1.00 0.00 0.00 0.00 3 2 1.00   1.17 3.6 6AL005 1.00 0.01 0.01 0.01 3 2 1.00   1.17 3.7 6AL006 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0 6AL007 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0 6AL008 1.00 0.01 0.01 0.01 3 2 1.00   1.17 3.7 6AL009 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0 6AL010 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0 6AL011 1.00 0.01 0.01 0.01 3 2 1.00   1.17 3.6 6AL012 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0 6AL013 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0 6AL014 1.00 0.01 0.01 0.01 3 2 1.00   1.17 3.7 6AL015 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0 6AL016 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0 6AL017 1.00 0.01 0.01 0.01 3 2 1.00   1.17 3.6 6AL018 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0 6AL019 <. 01 <. 01 <. 01 <. 01 3 1 <. 01   0.01 0.0 6AL020 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0 6AL021 1.00 0.01 0.01 0.01 3 2 0.00   1.17 3.5 6AL022 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0 6AL023 1.00 0.01 0.01 0.01 3 2 1.00   1.17 3.6 6AL024 0.01 0.01 0.01 0.01 3 1 0.01   0.01 0.0  Smoke Number

 Smoke Number  Number

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 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)

1AS001 ASTM D1655 73T  17 0.205 0.173 0.067 0.024 85 1AS002 ASTM D1655 73T  17 0.225 0.186 0.072 0.026 92 4AL003 Jet A/ JP 8 1.899 16.5 0.377 0.315 0.117 0.049 162 4AL002 Jet A/ JP 8 1.899 16.5 0.380 0.319 0.117 0.050 164 3AL001 Jet A/ JP 8 1.899 16.5 0.28 0.234 0.091 0.039 125 6AL004 Jet A / JP8 1.899 16.5 0.322 0.269 0.099 0.042 138 6AL005 Jet A 1.9 16  20 0.3826 0.318 0.113 0.0461 157 6AL006 Jet A 1.9 16  20 0.3826 0.318 0.113 0.0461 157 6AL007 Jet A 1.9 16  20 0.3826 0.318 0.113 0.0461 157 6AL008 Jet A 1.9 16  20 0.3805 0.3163 0.1125 0.0459 156 6AL009 Jet A 1.9 16  20 0.3805 0.3163 0.1125 0.0459 156 6AL010 Jet A 1.9 16  20 0.3805 0.3163 0.1125 0.0459 156 6AL011 Jet A 1.9 16  20 0.3589 0.2999 0.1077 0.0449 151 6AL012 Jet A 1.9 16  20 0.3589 0.2999 0.1077 0.0449 151 6AL013 Jet A 1.9 16  20 0.3589 0.2999 0.1077 0.0449 151 6AL014 Jet A 1.9 16  20 0.3806 0.3163 0.1126 0.046 157 6AL015 Jet A 1.9 16  20 0.3806 0.3163 0.1126 0.046 157 6AL016 Jet A 1.9 16  20 0.3806 0.3163 0.1126 0.046 157 6AL017 Jet A 1.9 16  20 0.3583 0.2995 0.1076 0.0448 150 6AL018 Jet A 1.9 16  20 0.3583 0.2995 0.1076 0.0448 150 6AL019 Jet A 1.9 16  20 0.3583 0.2995 0.1076 0.0448 150 6AL020 Jet A 1.9 16  20 0.4122 0.3425 0.12 0.0475 165 6AL021 Jet A 1.9 16  20 0.301 0.2527 0.0943 0.0377 127 6AL022 Jet A 1.9 16  20 0.301 0.2527 0.0943 0.0377 127 6AL023 Jet A 1.9 16  20 0.3222 0.2689 0.0991 0.0418 138 6AL024 Jet A 1.9 16  20 0.3222 0.2689 0.0991 0.0418 138  Fuel Flow

( kg/ sec)

 Fuel

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 CF CG CH CI CJ CK CL CM UID No Baro Temp Humidity kW @ Power % CF @ Power kPa K kg/ kg 1AS001 0  0  96.7 98.1 285  288 .0066. 0087 1AS002 0  0  97.0 97.3 294  313 .0039. 0073 4AL003 0  0  101.3 288 0.0063 4AL002 0  0  101.3 288 0.0063 3AL001 0  0  101.3 288 0.0063 6AL004 0  0  101.3 288 0.0063 6AL005 0  0

6AL006 0  0  99.6  99.7 297  301 0.0115  0.0141 6AL007 0  0  98.9  99.0 291  301 0.009  0.012 6AL008 0  0

6AL009 0  0  99.6  99.7 297  301 0.0115  0.0141 6AL010 0  0  98.9  99.0 291  301 0.009  0.012 6AL011 0  0

6AL012 0  0  99.6  99.7 297  301 0.0115  0.0141 6AL013 0  0  98.9  99.0 291  301 0.009  0.012 6AL014 0  0

6AL015 0  0  99.6  99.7 297  301 0.0115  0.0141 6AL016 0  0  98.9  99.0 291  301 0.009  0.012 6AL017 0  0

6AL018 0  0  99.6  99.7 297  301 0.0115  0.0141 6AL019 0  0  98.9  99.0 291  301 0.009  0.012 6AL020 0  0  98.9  99.0 291  301 0.009  0.012 6AL021 0  0

6AL022 0  0  99.6  99.7 297  301 0.0115  0.0141 6AL023 0  0

6AL024 0  0  99.6  99.7 297  301 0.0115  0.0141  Ambient

 Loads

Power Extraction  Stage Bleed

Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 CN CO CP CQ CR CS UID  Test Dates

No Manufacturer Test Organisation Test Location From To 1AS001 Allied Signal Allied Signal Phoenix Dec 75 Apr 76 1AS002 Allied Signal Allied Signal Phoenix Feb 76 Aug 76 4AL003 Allison Engine Company Allison Engine Company Indianapolis, Indiana, USA 3 Mar 94 19 Apr 95 4AL002 Allison Engine Company Allison Engine Company Indianapolis, Indiana, USA 3 Mar 94 19 Apr 95 3AL001 Allison Engine Company Allison Engine Company Indianapolis, Indiana, USA 3 Mar 94 19 Apr 95 6AL004 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 3 Mar 94 19 Apr 95 6AL005 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 3 Mar 94 19 Apr 95 6AL006 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 28 Aug 02 29 Aug 02 6AL007 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 9 Jun 01 11 Jun 01 6AL008 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 3 Mar 94 19 Apr 95 6AL009 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 28 Aug 02 29 Aug 02 6AL010 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 9 Jun 01 11 Jun 01 6AL011 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 3 Mar 94 19 Apr 95 6AL012 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 28 Aug 02 29 Aug 02 6AL013 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 9 Jun 01 11 Jun 01 6AL014 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 3 Mar 94 19 Apr 95 6AL015 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 28 Aug 02 29 Aug 02 6AL016 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 9 Jun 01 11 Jun 01 6AL017 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 3 Mar 94 19 Apr 95 6AL018 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 28 Aug 02 29 Aug 02 6AL019 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 9 Jun 01 11 Jun 01 6AL020 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 9 Jun 01 11 Jun 01 6AL021 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 3 Mar 94 19 Apr 95 6AL022 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 28 Aug 02 29 Aug 02 6AL023 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 3 Mar 94 19 Apr 95 6AL024 Rolls Royce Corporation Rolls Royce Corporation Indianapolis, Indiana, USA 28 Aug 02 29 Aug 02 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 CT CU UID No Remarks 1AS001 Not required to meet GASEOUS regulations 1AS002 Not required to meet GASEOUS regulations 4AL003 4AL002 For AE3007A1, A1/ 1, A1/ 2 3AL001 6AL004 Results based on Rolls Royce report EDR 15171B 6AL005 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Results are based on Rolls Royce report EDR 15171B 3. AE3007A1 data i 6AL006 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007A1 egines fitted with PAB fuel nozzles 3. Resu 6AL007 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007A1 engine fitted with reduced emissions comb 6AL008 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Results based on Rolls Royce report EDR 15171B 6AL009 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for A3007A1/ 1 fitted with PAB fuel nozzles 3. Results bas 6AL010 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007A1/ 1 engine fitted with reduced emissions com 6AL011 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Results based on Rolls Royce report EDR 15171B 6AL012 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007A1/ 3 engine fitted with PAB fuel nozzles 3. Re 6AL013 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007A1/ 3 engine fitted with reduced emissions com 6AL014 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Results based on Rolls Royce report EDR 15171B 6AL015 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007A1P engine fitted with PAB fuel nozzles 3. Re 6AL016 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007A1P engine fitted with reduced emissions com 6AL017 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Results based on Rolls Royce report EDR 15171B 6AL018 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007A3 engine fitted with PAB fuel nozzles 3. Resu 6AL019 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007A3 engine fitted with reduced emissions comb 6AL020 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007A1E engine fitted with reduced emissions com 6AL021 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Results based on Rolls Royce report EDR 15171B 6AL022 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007C engine fitted with PAB fuel nozzles 3. Resul 6AL023 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Results based of Rolls Royce report EDR 15171B 6AL024 1. For effectivity see Rolls Royce Notice to Operators No. AE3007A 076 2. Data in this form for AE3007C1 engine fitted with PAB fuel nozzles 3. Resu Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 CV CW CX CY CZ DA DB DC DD DE DF DG DH a in this report replace data reported in ICAO databank under ID No. 4AL002, Rev 9 sults based on Rolls Royce report EDR 19972 bustor and PAB fuel nozzles 3. Results based on Rolls Royce report EDR 19587 ased on Rolls Royce report EDR 19972 mbustor & PAB fuel nozzles 3. Results based on Rolls Royce report EDR 19587 Results based on Rolls Royce report EDR 19972 mbustor & PAB fuel nozzles 3. Results based on Rolls Royce report EDR 19587 esults based on Roll Royce report EDR 19972 mbustor & PAB fuel nozzles 3. Results based on Rolls Royce report EDR 19587 sults based on Rolls Royce report EDR 19972 bustor & PAB fuel nozzles 3. Results based on Rolls Royce report EDR 19587 mbustor & PAB fuel nozzles 3. Results based on Rolls Royce report EDR 19587 ults based on Rolls Royce report EDR 19972 sults based on Rolls Royce report EDR 19972 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 DI DJ DK DL DM DN 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 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 AO ' Aviadgatel'

1AA001 D 30 ( Il series) MTF 0.85 18.4 66.64 1AA002 D 30KP 2 MTF 2.2 19.45 117.6 1AA003 D 30KU MTF 2.35 17.4 112.7 1AA004 D 30KU 154 MTF 2.3 17 107.5 1AA005 PS 90A MTF 5 30.85 156.9 BMW Roll Royce 3BR001 BR700 710A1 10 TF 4.2 24.31 65.61 4BR008 BR700 710A1 10 TF 4.20 24.23 65.61 4BR009 BR700 710A2 20 TF 4.19 24.16 65.61 6BR010 BR700 710 C4 11 Annular TF 4.05 24.95 68.77 4BR002 BR700 715A1 30 TF 4.66 28.98 84.16 4BR005 BR700 715A1 30 Improved fuel injector TF 4.68 28.75 83.23 4BR003 BR700 715B1 30 TF 4.60 30.47 89.68 4BR006 BR700 715B1 30 Improved fuel injector TF 4.60 30.58 89.68 4BR004 BR700 715C1 30 TF 4.55 32.01 95.33 4BR007 BR700 715C1 30 Improved fuel injector TF 4.54 32.15 95.33 CFM International 1CM001 CFM56 2A series TF 6 25.2 106.76 1CM002 CFM56 2B 1 TF 6 23.5 97.86 1CM003 CFM56 2 C5 TF 6 23.5 97.86 1CM004 CFM56 3 B1 TF 5.1 22.44 89.41 1CM005 CFM56 3B 2 TF 5.1 24.10 98.30 1CM006 CFM56 3C 1 ( Rerated) TF 5.1 21.3 82.29 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

36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 1AA001   x     x  x

1AA002   x     x  x

1AA003   x     x  x

1AA004   x     x  x

1AA005  x    x   x x

3BR001  x     x  x x

4BR008  x     x  x

4BR009  x     x  x

6BR010  x     x  x

4BR002  x     x  x x

4BR005  x     x  x

4BR003  x     x  x x

4BR006  x     x  x

4BR004  x     x  x x

4BR007  x     x  x

1CM001  x    x   x x

1CM002  x    x   x x

1CM003  x    x   x x

1CM004   x   x   x x

1CM005   x   x   x x

1CM006   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)

36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 1AA001 0.12 0.14 1.50 43.60 2 1 134.9   207.8 1060.0 8992 1AA002 0.7 0.8 2.7 13.3 7 4 41.4 8.6  47.2 241.0 4874 1AA003 0.3 0.4 1.2 10.5 5 5 33.3 6.55  37.4 191.0 3753 1AA004 0.4 0.5 1.9 12.7 2 2 40.8 5.0  53.1 270.9 4389 1AA005 0.12 0.12 0.20 0.30 3 1 0.9   1.4 7.1 138 3BR001 0 0.03 0.04 1.98 3 1 4.29  3.83 5.03 6.6 33.7 279 4BR008 0.02 0.02 0.05 1.09 3 1 2.37  2.13 2.63 3.7 18.6 156 4BR009 0.02 0.02 0.05 1.12 3 1 2.44  2.19 2.70 3.8 19.2 160 6BR010 0.02 0.02 0.05 2.29 3 1 4.36  4.19  4.47 6.7 34.2 301 4BR002 0.00 0.02 0.01 0.21 3 1 0.39  0.32 0.47 0.6 3.1 34 4BR005 0.05 0.06 0.02 0.11 3 1 0.32  0.03 0.66 0.5 2.5 25 4BR003 0.00 0.01 0.00 0.17 3 1 0.30  0.24 0.37 0.5 2.3 27 4BR006 0.03 0.06 0.02 0.07 3 1 0.23  0.03 0.45 0.4 1.8 20 4BR004 0.00 0.00 0.00 0.14 3 1 0.23  0.17 0.29 0.4 1.8 22 4BR007 0.01 0.06 0.02 0.06 3 1 0.18  0.02 0.34 0.3 1.4 18 1CM001 0.04 0.04 0.08 1.13 3 1 2.26 0.41 1.82 2.63 3.5 17.8 242 1CM002 0.04 0.05 0.08 1.83 3 1 3.87 0.41 3.40 4.15 6.0 30.4 378 1CM003 0.04 0.05 0.08 1.83 3 1 3.87 0.41 3.40 4.15 6.0 30.4 378 1CM004 0.04 0.05 0.08 2.28 3 1 4.67 0.53 4.17 5.22 7.2 36.7 418 1CM005 0.036 0.047 0.073 1.75 3 1 3.44 0.37 3.01 3.67 5.3 27.0 337 1CM006 0.05 0.05 0.08 2.86 3 1 6.18 1.05 5.47 7.38 9.5 48.6 507 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)

36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 1AA001 2.7 3.2 14.5 60.3 2 1 209.9   257.6 218.3 13989 1AA002 2.2 2.8 15.4 62.4 7 4 195.0 11.1  208.6 176.8 22932 1AA003 2.8 3.7 11.8 54.0 5 5 180.5 33.4  191.7 162.5 20341 1AA004 3.0 3.6 18.2 77.7 2 2 257.0 21.8  292.8 248.1 27627 1AA005 0.35 0.40 0.90 6.90 3 1 13.6   16.7 14.1 2123 3BR001 0.52 0.66 4.24 26.09 3 1 59.85  57.89 63.69 73.5 62.3 3913 4BR008 1.04 0.93 4.78 27.82 3 1 64.26  63.75 65.02 78.9 66.8 4212 4BR009 1.04 0.93 4.81 28.00 3 1 64.82  64.31 65.59 79.6 67.4 4239 6BR010 1.04 0.92 4.92 31.57 3 1 64.37  63.78 64.19 79.0 67.0 4449 4BR002 0.78 0.75 3.76 16.27 3 1 32.64  31.93 33.86 40.1 33.9 2753 4BR005 0.66 0.63 4.05 19.72 3 1 40.83  40.21 41.37 50.1 42.5 3390 4BR003 0.78 0.76 3.38 15.56 3 1 30.08  29.44 31.21 36.9 31.3 2693 4BR006 0.72 0.63 3.59 18.60 3 1 36.85  36.28 37.42 45.2 38.3 3300 4BR004 0.75 0.78 3.06 14.86 3 1 27.77  27.22 28.85 34.1 28.9 2655 4BR007 0.80 0.64 3.23 17.85 3 1 34.04  33.51 34.63 41.8 35.4 3236 1CM001 0.9 0.9 3.4 23.5 3 1 48.5 2.5 47.0 51.4 59.5 50.5 5176 1CM002 0.9 0.9 4.2 30.7 3 1 67.2 4.1 63.5 71.7 82.5 69.9 6578 1CM003 0.9 0.9 4.2 30.7 3 1 67.2 4.1 63.5 71.7 82.5 69.9 6578 1CM004 0.9 0.95 3.8 34.4 3 1 72.9 5.1 68.5 78.5 89.5 75.8 6517 1CM005 0.9 0.9 3.4 30.1 3 1 61.0 3.8 57.6 65.1 74.9 63.5 5988 1CM006 0.9 1.0 4.2 38.1 3 1 85.2 6.4 79.7 92.2 104.6 88.6 7002 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 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 1AA001 19.1 16.3 7.0 3.6 2 1 65.1   75.5 98.3 122.8 141.9 4338 1AA002 16.5 13.5 6.3 3.3 7 4 47.1 6.6  49.5 62.7 78.4 98.8 5510 1AA003 16.3 12.6 5.1 2.7 5 5 41.9 3.15  43.8 58.6 73.2 93.5 4720 1AA004 14.5 11.6 5.1 2.9 2 2 36.7 2.5  40.4 54.5 68.2 87.4 4000 1AA005 37.0 31.5 11.8 5.8 3 1 74.2   86.0 84.6 105.7 125.2 11648 3BR001 17.07 13.93 8.20 4.00 3 1 39.32  38.09 40.51 45.6 51.5 64.3 72.6 2576 4BR008 18.79 15.07 7.68 4.69 3 1 42.52  41.84 42.94 49.3 55.7 69.7 78.6 2790 4BR009 18.73 15.03 7.67 4.67 3 1 42.49  41.81 42.91 49.3 55.8 69.7 78.7 2784 6BR010 19.52 15.43 7.71 4.5 3 1 41.41  40.63 41.90 48.0 53.4 66.7 76.0 2850 4BR002 23.97 18.65 11.19 5.37 3 1 47.54  47.19 48.08 55.1 56.3 70.3 82.9 4002 4BR005 20.97 16.43 8.75 3.95 3 1 40.17  39.09 41.16 46.6 47.8 59.7 70.3 3340 4BR003 27.21 20.34 11.38 5.54 3 1 51.10  50.79 51.54 59.2 58.7 73.3 87.2 4583 4BR006 24.28 18.27 9.01 4.14 3 1 44.14  43.00 45.23 51.2 50.6 63.2 75.1 3958 4BR004 31.39 22.41 11.55 5.72 3 1 55.71  55.26 56.04 64.6 62.1 77.6 90.9 5314 4BR007 27.92 20.05 9.23 4.28 3 1 48.13  46.96 49.29 55.8 53.5 66.9 78.2 4588 1CM001 20.4 17.3 8.7 4.3 3 1 42.8 0.8 42.3 43.7 49.6 54.9 68.6 83.6 4571 1CM002 18.5 16.0 8.2 4.0 3 1 39.9 0.6 39.4 40.5 46.3 53.2 66.5 81.7 3906 1CM003 18.5 16.0 8.2 4.0 3 1 39.9 0.6 39.4 40.5 46.3 53.2 66.5 81.7 3906 1CM004 17.7 15.5 8.3 3.9 3 1 40.3 0.8 39.6 41.2 46.7 55.0 68.8 85.1 3595 1CM005 19.4 16.7 8.7 4.1 3 1 42.9 0.81 42.4 43.9 49.7 56.4 70.5 86.4 4213 1CM006 16.6 14.7 8.0 3.8 3 1 39.0 0.78 38.2 40.0 45.2 54.7 68.4 82.9 3210 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

36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 1AA001 33 35 27 8 1 1 35   45.1 170.3 1AA002 17.5 19.5 16.0 6.5 1 1 19.5   25.1 110.9 1AA003     1 1 22.9   29.5 128.7 1AA004

1AA005     3 1 13   16.7 80.0 3BR001 11.03 8.69 0 0.17 3 1 11.03  10.18 11.87 14.2 53.4 4BR008 13.99 11.92 0.29 0.56 3 1 13.99  12.64 15.18 18.0 67.8 4BR009 13.96 11.87 0.27 0.57 3 1 13.96  12.60 15.15 18.0 67.6 6BR010 14.34 12.36 0.35 0.45 3 1 14.34  13.08 14.37 18.46 70.4 4BR002 3.24 2.73 0.97 0.91 3 1 3.24  3.04 3.40 4.2 16.8 4BR005 4.33 3.96 0.77 0.11 3 1 4.33  3.85 4.74 5.6 22.4 4BR003 3.55 2.90 1.03 0.89 3 1 3.55  3.24 3.80 4.6 18.9 4BR006 4.56 4.13 0.96 0.07 3 1 4.56  4.16 5.00 5.9 24.1 4BR004 3.98 3.09 1.09 0.87 3 1 3.98  3.61 4.26 5.1 21.3 4BR007 4.86 4.26 1.12 0.04 3 1 4.86  4.62 5.28 6.3 26.1 1CM001 7.9 4.2 2.5 2.0 3 1 7.9 0.6 7.3 8.5 10.2 43.7 1CM002 6.0 3.0 2.6 2.2 3 1 6.0 0.8 5.4 6.9 7.7 32.4 1CM003 6.0 3.0 2.6 2.2 3 1 6.0 0.8 5.4 6.9 7.7 32.4 1CM004 4.0 2.5 2.5 2.2 3 1 4.0 0.6 3.4 4.5 5.1 21.1 1CM005 6.0 3.0 2.5 2.2 3 1 6.0 0.8 5.4 6.9 7.7 32.5 1CM006 3.0 2.4 2.5 2.1 3 1 3.0 0.4 2.5 3.2 3.9 15.5 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 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

36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 1AA001 TS 1 2 19.3 1.150 0.975 0.350 0.130 464 1AA002 TS 1 2 19 1.67 1.42 0.49 0.210 703 1AA003 TS 1 2 18.6 1.520 1.300 0.500 0.215 691 1AA004 TS 1 2 18 1.420 1.100 0.420 0.207 629 1AA005 TS 1 2 19 1.739 1.431 0.489 0.178 657 3BR001 AVTUR 1.94 16.5 0.707 0.588 0.220 0.089 299 4BR008 AVTUR 1.89 1.92 16.4 18.0 0.713 0.594 0.214 0.089 299 4BR009 AVTUR 1.89 1.92 16.4 18.0 0.714 0.595 0.214 0.089 299 6BR010 AVTUR 1.89 16.4  18.0 0.747 0.617 0.215 0.083 294 4BR002 AVTUR 1.89 17.7 0.836 0.690 0.245 0.096 335 4BR005 AVTUR 1.93 16.6 0.831 0.686 0.240 0.100 339 4BR003 AVTUR 1.89 17.7 0.905 0.743 0.259 0.098 351 4BR006 AVTUR 1.93 16.6 0.910 0.750 0.257 0.103 360 4BR004 AVTUR 1.89 17.7 0.980 0.799 0.273 0.101 370 4BR007 AVTUR 1.93 16.6 0.984 0.805 0.272 0.105 377 1CM001 Jet A 1.93 16.0 1.114 0.911 0.318 0.130 446 1CM002 Jet A 1.93 16.0 0.985 0.819 0.311 0.128 424 1CM003 Jet A 1.93 16.0 0.985 0.819 0.311 0.128 424 1CM004 Jet A 1.93 16.0 0.946 0.792 0.290 0.114 392 1CM005 Jet A 1.93 16.0 1.056 0.878 0.314 0.119 421 1CM006 Jet A 1.93 16.0 0.872 0.732 0.273 0.111 372 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

36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 1AA001 0  0  103 293 .01048 1AA002 0  0  102.7 103.1 284  289 .00748 1AA003 0  0  102.6 102.7 292  294 .00788 1AA004 0  0  102.3 102.6 289  291 .01119 1AA005 0  0  102.9 104 281  285 .00348. 00607 3BR001 0  0  101.5 102.1 291.2 300.3 .0074. 0087 4BR008 0  0  100.9 101.2 282.9 286.7 .0064. 0087 4BR009 0  0  100.9 101.2 282.9 286.7 .0064. 0087 6BR010 0  0  100.9  101.2 282.9  286.7 0.0064  0.0087 4BR002 0  0  101.3 101.9 288.8 294.4 0.0066. 0079 4BR005 0  0  100.9 101.3 294.4 297.2 .0072. 0075 4BR003 0  0  101.3 101.9 288.8 294.4 0.0066. 0079 4BR006 0  0  100.9 101.3 294.4 297.2 .0072. 0075 4BR004 0  0  101.3 101.9 288.8 294.4 0.0066. 0079 4BR007 0  0  100.9 101.3 294.4 297.2 .0072. 0075 1CM001 0  0  95.98 97.49 279  286 .002. 009 1CM002 0  0  95.98 97.49 279  286 .002. 009 1CM003 0  0  95.98 97.49 279  286 .002. 009 1CM004 0  0  95.98 97.49 279  286 .002. 009 1CM005 0  0  95.98 97.49 279  286 .002. 009 1CM006 0  0  95.98 97.49 279  286 .002. 009 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 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 1AA001 AO ' Aviadgatel' State Inst for Civ Aviation Sheremetjevo, Moscow 3 Aug 90

1AA002 AO ' Aviadgatel' State Inst for Civ Aviation Sheremetjevo, Moscow 28 Jun 90

1AA003 AO ' Aviadgatel' State Inst for Civ Aviation Sheremetjevo, Moscow 19 Jul 89

1AA004 AO ' Aviadgatel' State Inst for Civ Aviation Sheremetjevo, Moscow 4 Jul 89

1AA005 AO ' Aviadgatel' AO ' Aviadgatel' Perm City 17 Apr 89 18 Apr 89 3BR001 BMW Rolls Royce GmbH BMW Rolls Royce GmbH BMW Rolls Royce GmbH, Dahlewitz, German 5 Jun 96 6 Jun 96 4BR008 BMW Rolls Royce GmbH BMW Rolls Royce GmbH BMW Rolls Royce GmbH, Dahlewitz, German 19 Oct 96 20 Oct 96 4BR009 BMW Rolls Royce GmbH BMW Rolls Royce GmbH BMW Rolls Royce GmbH, Dahlewitz, German 19 Oct 96 20 Oct 96 6BR010 Rolls Royce Rolls Royce Dahlewitz 19 Oct 96 20 Oct 96 4BR002 BMW Rolls Royce GmbH BMW Rolls Royce GmbH BMW Rolls Royce GmbH, Dahlewitz, German 7 May 98 8 May 98 4BR005 BMW Rolls Royce GmbH BMW Rolls Royce GmbH BMW Rolls Royce GmbH, Dahlewitz, German 29 Jun 99 4BR003 BMW Rolls Royce GmbH BMW Rolls Royce GmbH BMW Rolls Royce GmbH, Dahlewitz, German 7 May 98 8 May 98 4BR006 BMW Rolls Royce GmbH BMW Rolls Royce GmbH BMW Rolls Royce GmbH, Dahlewitz, German 29 Jun 99 4BR004 BMW Rolls Royce GmbH BMW Rolls Royce GmbH BMW Rolls Royce GmbH, Dahlewitz, German 7 May 98 8 May 98 4BR007 BMW Rolls Royce GmbH BMW Rolls Royce GmbH BMW Rolls Royce GmbH, Dahlewitz, German 29 Jun 99 1CM001 CFMI CFM56 Evaluation Engineering Peebles Site IVD 11 Nov 83 14 Nov 83 1CM002 CFMI CFM56 Evaluation Engineering Peebles Site IVD 11 Nov 83 14 Nov 83 1CM003 CFMI CFM56 Evaluation Engineering Peebles Site IVD 11 Nov 83 14 Nov 83 1CM004 CFMI CFM56 Evaluation Engineering Peebles Site IVD 11 Nov 83 14 Nov 83 1CM005 CFMI CFM56 Evaluation Engineering Peebles Site IVD 11 Nov 83 14 Nov 83 1CM006 CFMI CFM56 Evaluation Engineering Peebles Site IVD 11 Nov 83 14 Nov 83 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 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 1AA001 1. Data obtained on aircraft ( Tu 134B) 2. In service engine( s), tested after overhaul 1AA002 1. Data obtained on aircraft ( Il 76TD) 2. In service engine( s), tested before overhaul 1AA003 1. Data obtained on aircraft ( Il 62M) 2. In service engine( s), tested after overhaul 1AA004 1. Data obtained on aircraft ( Tu 154M) 2. In service engine( s), tested before overhaul 1AA005 For aircraft Il 96 and Tu 204 3BR001 Data from certification report E TR403/ 96( FR) ISS02 4BR008 1. Data from Certification report E TR825/ 96( FR) ISS01. 2. For Gulfstream V application 4BR009 1. Data from Certification report E TR853/ 96( FR) ISS01. 2. For Canadair Global Express application 6BR010 1. Certification report E TR554/ 01  ( FR)  01 2. For Gulfstream G550 appliaction 4BR002 Data from Certification Report E TR484/ 98 ( FR) ISS00 4BR005 1. Data from certification report E TR346/ 99 ( FR) ISS00. 2. Incorporating improved fuel injector.

4BR003 Data from Certification Report E TR484/ 98 ( FR) ISS00 4BR006 1. Data from certification report E TR346/ 99 ( FR) ISS00. 2. Incorporating improved fuel injector.

4BR004 Data from Certification Report E TR484/ 98 ( FR) ISS00 4BR007 1. Data from certification report E TR346/ 99 ( FR) ISS00. 2. Incorporating improved fuel injector.

1CM001 1. Ref GE Report R83AEB631. 2. Engine S/ N 692441. 3. Applicable to CFM56 2A2 and  2A3.

1CM002 1. Ref GE Report R83AEB631. 2. Engine S/ N 692441.

1CM003 1. Ref GE Report R83AEB631. 2. Engine S/ N 692441.

1CM004 1. Ref GE Report R84AEB245. 2. Engine S/ N 692441. 3. Revised based on 3/ 89 production cycle. 4. Data also apply to CFM56 3C 1 and  3B 2 engines rerated to 89.4 kN ( 20,100 Lb) thrust for B737 300 aircraft.

1CM005 1. Ref GE Report R84AEB245. 2. Engine S/ N 692441. 3. Revised based on 3/ 89 production cycle. 4. Data also apply to CFM56 3C 1 engines rerated to 98.3 kN ( 22,100 Lb.) thrust for B737 300 and  400 aircraft.

1CM006 1. Ref GE Report R84AEB579. 2. Engine S/ N 692441. 3. Revised based on 3/ 89 production status cycle. 4. Data also apply to CFM56 3 B1 engines rerated to 82.3 kN ( 18,500 Lb.) thrust for B737 500 aircraft.

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 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 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 DI DJ DK DL DM DN 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 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 A B C D E F G UID Engine Combustor Eng B/ P Press Rated No Identification Description Type Ratio Ratio Output kN 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 1CM007 CFM56 3C 1 TF 5.1 25.5 104.60 1CM008 CFM56 5 A1 TF 6.0 26.6 111.2 1CM009 CFM56 5A3 TF 6.0 27.9 117.88 4CM035 CFM56 5A4 TF 6 23.8 97.89 4CM036 CFM56 5A5 TF 6 25.1 104.53 2CM012 CFM56 5B1 TF 5.7 30.2 133.45 2CM016 CFM56 5B1/ 2 DAC TF 5.7 30.2 133.45 3CM020 CFM56 5B1/ 2P DAC II TF 5.7 30.5 133.5 3CM023 CFM56 5B1/ P TF 5.7 30.47 133.45 2CM013 CFM56 5B2 TF 5.6 31.3 137.9 2CM017 CFM56 5B2/ 2 DAC TF 5.7 31.2 137.9 4CM037 CFM56 5B2/ 2P DAC II TF 5.6 31.6 137.9 3CM024 CFM56 5B2/ P TF 5.6 31.57 137.90 4CM038 CFM56 5B3/ 2P DAC II TF 5.6 32.8 142.4 3CM025 CFM56 5B3/ P TF 5.6 32.78 142.35 2CM014 CFM56 5B4 TF 5.9 27.1 117.9 2CM018 CFM56 5B4/ 2 DAC TF 5.7 27.1 117.9 3CM021 CFM56 5B4/ 2P DAC II TF 5.9 27.7 120.1 3CM026 CFM56 5B4/ P TF 5.9 27.69 120.11 3CM027 CFM56 5B5/ P TF 5.9 23.33 97.89 2CM019 CFM56 5B6/ 2 DAC TF 5.7 24.8 104.5 3CM022 CFM56 5B6/ 2P DAC II TF 6.0 24.6 104.5 3CM028 CFM56 5B6/ P TF 6.0 24.64 104.53 6CM044 CFM56 5B7/ P TF 5.9 27.69 120.11 7CM048 CFM56 5B8/ P SAC TF 5.9 22.6 94.7 7CM050 CFM56 5B9/ 2P DAC TF 5.9 24.4 102.2 7CM049 CFM56 5B9/ P SAC TF 5.9 24.0 102.2 1CM010 CFM56 5C2 TF 6.8 28.8 138.78 7CM045 CFM56 5C2/ P SAC MTF 6.8 28.2 137.61 1CM011 CFM56 5C3 TF 6.7 29.9 144.57 7CM046 CFM56 5C3/ P SAC MTF 6.7 29.2 143.33 2CM015 CFM56 5C4 TF 6.6 31.15 151.25 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

65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 1CM007   x   x   x x

1CM008   x   x   x

1CM009  x    x   x

4CM035  x    x   x

4CM036  x    x   x

2CM012  x    x   x x

2CM016  x    x   x x

2CM020  x     x  x

3CM023  x    x   x

2CM013  x    x   x x

2CM017  x    x   x x

4CM037  x     x  x

3CM024  x    x   x

4CM038  x     x  x

3CM025  x    x   x

2CM014  x    x   x x

2CM018  x    x   x x

2CM021  x     x  x

3CM026  x    x   x

3CM027  x    x   x

2CM019  x    x   x x

2CM022  x     x  x

3CM028  x    x   x

6CM044  x    x   x

7CM048  x    x   x

7CM050  x     x  x

7CM049  x    x   x

1CM010  x    x   x

7CM045  x    x   x

1CM011  x    x   x

7CM046  x    x   x

2CM015  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)

65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 1CM007 0.03 0.04 0.07 1.42 3 1 2.76 0.38 2.33 3.06 4.3 21.7 287 1CM008 0.23 0.23 0.40 1.4 3 1 2.6 0.5 2.3 3.2 4.0 20.4 285 1CM009 0.2 0.2 0.3 1.3 3 1 2.3 0.5 1.8 2.8 3.5 18.1 268 4CM035 0.23 0.23 0.50 1.75 3 1 3.3   5.1 25.9 322 4CM036 0.23 0.23 0.45 1.53 3 1 2.8   4.3 22.0 297 2CM012 0.10 0.10 0.12 3.21 3 1 4.60 0.29 4.28 4.86 7.1 36.1 617 2CM016 0.1 0.1 9.1 1.7 3 2 8.7  8.1 9.4 11.3 57.7 1168 3CM020 0.1 0.1 3.7 2.9 4 2 6.8  6.2 7.4 8.8 44.9 891 3CM023 0.10 0.20 0.50 3.70 3 1 5.29   8.2 41.8 710 2CM013 0.10 0.10 0.12 3.04 3 1 4.31 0.24 4.05 4.53 6.6 33.9 596 2CM017 0.1 0.1 8.4 1.7 3 2 8.1  7.9 8.9 10.5 53.6 1128 4CM037 0.1 0.1 3.3 2.7 4 2 6.13  5.6 6.7 8.0 40.7 877 3CM024 0.10 0.20 0.50 3.60 3 1 5.13   7.9 40.3 712 4CM038 0.1 0.1 2.9 2.5 4 2 5.57  5.1 6.0 7.3 37.0 807 3CM025 0.10 0.20 0.50 3.50 3 1 5.00   7.7 39.3 708 2CM014 0.10 0.10 0.13 3.87 3 1 5.70 0.40 5.26 6.04 8.8 44.8 674 2CM018 0.1 0.1 11.4 2.2 3 2 11.2  10.4 12.0 14.6 74.5 1350 3CM021 0.1 0.2 5.3 3.6 4 2 9.2  8.2 10.1 12.0 61.2 1136 3CM026 0.20 0.20 0.50 4.60 3 1 6.77   10.4 53.1 818 3CM027 0.20 0.20 0.70 6.20 3 1 9.96   15.3 78.1 980 2CM019 0.1 0.2 0.2 3.4 9 4 5.84  4.58 8.45 6.7 34.0 630 3CM022 0.2 0.2 0.4 4.6 4 2 7.9  7.6 8.2 10.3 52.6 849 3CM028 0.20 0.20 0.60 5.50 3 1 8.61   13.3 67.9 901 6CM044 0.20 0.20 0.50 4.60 3 1 6.77   10.4 53.2 818 7CM048 0.1 0.1 0.9 6.5 3 1 10.8   16.6 84.7 1023 7CM050 0.2 0.3 0.4 4.4 4.00 2 7.6  7.4  7.8 9.9 50.5 789 7CM049 0.1 0.1 0.8 5.9 3 1 9.4   14.4 73.5 970 1CM010 0.008 0.008 0.082 5.68 3 1 7.56 0.59 6.90 8.01 11.6 59.4 1050 7CM045 0 0 0 5.8 3 1 7.2   11.1 56.6 986 1CM011 0.008 0.008 0.074 5.35 3 1 7.00 0.49 6.45 7.41 10.8 55.0 1012 7CM046 0 0 0 5.4 3 1 6.6   10.2 52.0 943 2CM015 0.008 0.008 0.065 5.00 3 1 6.40 0.44 5.95 6.83 9.9 50.5 975 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)

65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 1CM007 0.9 0.9 3.1 26.8 3 1 53.5 2.85 51.2 56.7 65.7 55.7 5591 1CM008 0.9 0.9 2.5 17.6 3 1 27.9 0.7 27.0 28.4 34.2 29.0 3093 1CM009 0.9 0.9 2.4 16.2 3 1 25.1 0.6 24.2 25.5 30.8 26.1 2968 4CM035 1.1 1.1 3.1 20.3 3 1 34.1   41.9 35.5 3352 4CM036 1.1 1.1 2.8 18.5 3 1 30.3   37.2 31.5 3175 2CM012 0.50 0.50 1.57 28.40 3 1 40.5 0.34 40.1 40.8 49.7 42.1 5423 2CM016 0.6 2.5 38.4 34.0 3 2 79.5  73.9 85.2 90.6 76.8 10641 3CM020 0.8 1.9 23.1 36.5 4 2 70.5  66.2 74.7 80.3 68.1 9197 3CM023 0.90 0.90 2.00 19.80 3 1 28.05   34.4 29.2 3738 2CM013 0.50 0.50 1.40 27.40 3 1 38.6 0.21 38.3 38.7 47.4 40.2 5319 2CM017 0.4 1.7 35.8 33.7 3 2 75.4  70.0 80.9 85.9 72.8 10404 4CM037 0.7 1.6 21.4 35.5 4 2 66.47  62.6 70.3 75.7 64.2 9478 3CM024 0.80 0.90 1.90 19.50 3 1 27.18   33.4 28.3 3776 4CM038 0.6 1.3 19.9 34.5 4 2 62.79  59.3 66.3 71.5 60.6 9141 3CM025 0.80 0.90 1.70 19.20 3 1 26.48   32.5 27.5 3777 2CM014 0.50 0.50 2.33 31.90 3 1 47.3 0.38 47.0 47.7 58.1 49.2 5595 2CM018 1.6 4.9 43.8 37.1 3 2 93.5  87.6 99.3 106.5 90.3 11234 3CM021 1.4 3.6 29.1 40.1 4 2 84.7  79.0 90.4 96.5 81.8 10400 3CM026 0.90 0.90 2.30 23.40 3 1 34.30   42.1 35.7 4123 3CM027 0.90 1.00 3.40 30.00 3 1 48.31   59.3 50.3 4743 2CM019 4.48 12.18 17.75 46.10 9 4 103.35  97.66 109.78 110.6 93.7 10842 3CM022 3.1 7.4 21.5 44.8 4 2 96.7  95.2 98.2 110.2 93.4 10205 3CM028 0.90 1.00 2.90 27.70 3 1 43.27   53.1 45.0 4525 6CM044 0.90 0.90 2.30 23.40 3 1 34.33   42.1 35.7 4123 7CM048 0.8 0.8 3.9 32.9 3 1 54.4   66.8 56.6 5176 7CM050 2.9 8.1 21 44.1 4 2 94.3  92.9  95.8 107.5 91.1 9687 7CM049 0.8 0.8 3.7 30.4 3 1 48.7   59.7 50.6 5012 1CM010 0.93 0.80 1.75 34.0 3 1 47.2 1.71 45.4 48.8 57.9 49.1 6546 7CM045 0.8 0.7 2.1 35.1 3 1 45.7   56.2 47.6 6278 1CM011 0.98 0.82 1.57 32.6 3 1 44.5 1.69 42.7 46.1 54.6 46.3 6436 7CM046 0.8 0.7 1.9 33.4 3 1 42.8   52.6 44.6 6142 2CM015 1.00 0.85 1.40 30.93 3 1 41.6 1.37 39.7 42.4 51.1 43.3 6308 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 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 1CM007 20.7 17.8 9.1 4.3 3 1 45.8 0.82 45.3 46.8 53.1 58.3 72.9 88.8 4810 1CM008 24.6 19.6 8.0 4.0 3 1 40.5 0.6 39.9 40.9 46.9 50.4 63.0 76.3 4506 1CM009 26.4 21.1 8.3 4.1 3 1 43.4 0.7 42.7 44.2 50.3 52.5 65.6 79.0 5110 4CM035 22.64 19.11 8.51 4.04 3 1 39.3   45.6 52.0 65.0 79.8 3851 4CM036 24.79 19.98 8.94 4.29 3 1 41.8   48.5 53.7 67.1 81.9 4367 2CM012 35.1 27.2 10.8 4.6 3 1 58.4 0.7 58.0 59.2 67.7 67.4 84.3 100.4 7783 2CM016 27.75 14.91 7.02 4.73 3 2 39.8  38.8 40.8 43.8 43.6 54.5 65.0 5314 3CM020 23.3 16.4 7.3 4.1 4 2 37.9  37.5 38.3 41.7 41.3 51.6 61.3 5024 3CM023 33.00 26.20 10.70 4.50 3 1 53.38   61.9 61.3 76.7 91.1 7112 2CM013 37.8 28.5 11.0 4.7 3 1 61.5 0.5 61.2 62.2 71.3 69.5 86.9 102.4 8485 2CM017 29.57 15.86 7.24 4.82 3 2 41.8  40.7 42.8 46.0 44.9 56.2 66.3 5756 4CM037 29.4 17.5 7.6 4.2 4 2 42.12  41.4 42.9 46.3 44.9 56.1 66.0 5844 3CM024 35.10 27.40 10.90 4.60 3 1 56.00   64.9 62.9 78.7 92.5 7723 4CM038 32.0 18.6 7.8 4.3 4 2 44.93  44.3 45.5 49.4 46.8 58.5 68.1 6420 3CM025 37.30 28.50 11.20 4.70 3 1 58.81   68.2 64.6 80.8 94.0 8360 2CM014 28.7 23.3 10.0 4.3 3 1 49.7 0.5 49.3 50.2 57.6 61.1 76.4 92.4 5861 2CM018 16.61 12.58 6.13 4.49 3 2 31.5  31.0 31.9 34.6 36.7 45.9 55.5 3783 3CM021 18.4 13.6 6.5 3.9 4 2 31.7  31.1 32.4 34.9 36.6 45.7 55.1 3847 3CM026 28.00 23.20 10.00 4.30 3 1 47.06   54.6 57.2 71.6 86.3 5641 3CM027 21.90 18.50 8.70 3.80 3 1 38.23   44.3 51.1 63.9 78.6 3732 2CM019 13.51 10.41 10.32 3.90 9 4 30.2  29.37 31.42 31.7 35.4 44.2 54.0 3158 3CM022 14.2 11.0 8.7 3.6 4 2 28.8  28.4 29.2 31.7 35.5 44.4 54.3 3020 3CM028 23.60 19.60 9.20 4.00 3 1 40.49   46.9 52.5 65.7 80.3 4232 6CM044 28.00 23.20 10.00 4.30 3 1 47.06   54.6 57.2 71.5 86.2 5641 7CM048 19.7 16.7 8.4 3.4 3 1 35.4   41.0 48.1 60.2 74.4 3358 7CM050 13.9 10.7 7.6 3.2 4 2 26.9  26.5  27.2 29.5 33.2 41.5 51 2754 7CM049 21.4 17.9 8.8 3.6 3 1 37.9   43.9 49.9 62.4 76.5 3875 1CM010 32.6 25.8 10.0 4.19 3 1 50.9 0.04 50.89 50.96 59.0 60.5 75.6 90.7 7077 7CM045 29.7 23.8 9.3 3.9 3 1 45.4   52.6 54.6 68.2 82.1 6240 1CM011 34.7 27.1 10.4 4.26 3 1 53.8 0.22 53.5 53.9 62.4 62.5 78.1 93.3 7770 7CM046 31.6 25.1 9.6 4.0 3 1 47.8   55.4 56.3 70.4 84.3 6858 2CM015 37.67 29.05 10.67 4.28 3 1 57.5 0.33 57.2 57.9 66.7 65.2 81.5 96.2 8702 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

65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 1CM007 7.7 3.9 2.5 2.3 3 1 7.7 0.76 6.8 8.3 9.9 42.4 1CM008 15.8 14.0 4.4 2.3 3 1 15.8 2.00 13.5 17.3 20.3 88.5 1CM009 16.8 14.6 4.8 2.7 3 1 16.8 2.0 14.6 18.8 21.6 95.6 4CM035 13.9    3 1 13.9   17.9 75.1 4CM036 14.3    3 1 14.3   18.4 78.7 2CM012 8.6 10.5 0 0 3 1 10.5 1.4 8.9 11.4 13.5 61.7 2CM016     3 2 4.75  4.5 5.0 5.6 25.6 3CM020 0.5 0.3 0.5 2.1 4 2 2.1  2.0 2.3 2.5 11.4 3CM023     3 1 5.4   7.0 32.0 2CM013 8.2 10.1 0 0 3 1 10.1 1.3 8.6 11.0 13.0 60.0 2CM017     3 2 4.75  4.5 5.0 5.6 25.8 4CM037 0.5 0.3 0.5 2.2 4 2 2.15  2.0 2.3 2.5 11.6 3CM024     3 1 5.4   7.0 32.3 4CM038 0.5 0.3 0.5 2.3 4 2 2.25  2.1 2.4 2.6 12.3 3CM025     3 1 5.4   7.0 32.6 2CM014 10.0 11.7 0 0 3 1 11.7 1.3 10.2 12.7 15.1 66.7 2CM018     3 2 4.75  4.5 5.0 5.6 24.8 3CM021 0.3 0.3 0.5 2.0 4 2 2.0  1.8 2.2 2.3 10.2 3CM026     3 1 5.4   7.0 31.1 3CM027     3 1 5.4   7.0 29.4 2CM019     9 4 3.7  3.1 4.2 4.0 17.1 3CM022 0.3 0.3 6.7 1.8 4 2 6.7  6.2 7.1 7.9 33.8 3CM028     3 1 5.4   7.0 29.9 6CM044     3 1 5.4   6.9 30.7 7CM048 5.4    3 1 5.4   6.9 28.7 7CM050 6.6    4 2 6.6   7.8 33.1 7CM049 5.4    3 1 5.4   6.9 29.3 1CM010 11.1 8.5 1.0 1.1 3 1 11.1 1.6 9.3 12.1 14.3 66.0 7CM045 10.7    3 1 10.7   13.8 63.6 1CM011 11.8 9.1 1.0 1.1 3 1 11.8 1.6 9.9 12.8 15.2 71.0 7CM046 11.6    3 1 11.6   14.9 69.5 2CM015 12.58 9.80 1.03 1.10 3 1 12.6 1.4 10.7 13.6 16.2 76.7 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 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

65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 1CM007 Jet A 1.93 16.0 1.154 0.954 0.336 0.124 448 1CM008 Jet A 1.95 18.0 1.051 0.862 0.291 0.1011 385 1CM009 Jet A 1.95 18.0 1.131 0.925 0.307 0.1044 406 4CM035 Jet A 1.95 18 0.897 0.74 0.261 0.095 346 4CM036 Jet A 1.95 18 0.972 0.799 0.276 0.098 365 2CM012 Jet A 1.93 16.8 1.359 1.113 0.364 0.117 474 2CM016 Jet A 1.93 16.8 1.345 1.104 0.369 0.129 492 3CM020 Jet A 1.93 17.33 1.32 1.07 0.37 0.12 473 3CM023 Jet A 1.92 19.0 1.295 1.058 0.345 0.11 448 2CM013 Jet A 1.93 16.8 1.426 1.158 0.376 0.119 489 2CM017 Jet A 1.93 16.8 1.406 1.132 0.377 0.131 503 4CM037 Jet A 1.93 17.33 1.39 1.11 0.39 0.13 501 3CM024 Jet A 1.92 19.0 1.361 1.099 0.356 0.113 464 4CM038 Jet A 1.93 17.33 1.47 1.15 0.4 0.13 512 3CM025 Jet A 1.92 19.0 1.430 1.141 0.366 0.115 478 2CM014 Jet A 1.93 16.8 1.166 0.961 0.326 0.107 421 2CM018 Jet A 1.93 16.8 1.180 0.975 0.335 0.121 447 3CM021 Jet A 1.93 17.33 1.14 0.95 0.34 0.12 442 3CM026 Jet A 1.92 19.0 1.132 0.935 0.312 0.104 408 3CM027 Jet A 1.92 19.0 0.891 0.742 0.260 0.094 344 2CM019 Jet A 1.92 18.1 0.998 0.827 0.315 0.111 400 3CM022 Jet A 1.93 17.33 0.970 0.81 0.31 0.11 394 3CM028 Jet A 1.92 19.0 0.961 0.799 0.275 0.097 363 6CM044 Jet A 1.92 19.0 1.132 0.935 0.312 0.104 408 7CM048 Jet A 1.92 19 0.875 0.729 0.262 0.094 342 7CM050 Jet A 1.93 17.33 0.961 0.799 0.296 0.105 381 7CM049 Jet A 1.92 19 0.954 0.794 0.280 0.098 365 1CM010 Jet A 1.95 17.3 1.308 1.076 0.3558 0.1175 466 7CM045 Jet A 1.95 17.3 1.252 1.035 0.342 0.109 441 1CM011 Jet A 1.95 17.3 1.373 1.131 0.370 0.1203 483 7CM046 Jet A 1.95 17.3 1.316 1.085 0.355 0.112 458 2CM015 Jet A 1.95 17.3 1.456 1.195 0.386 0.124 505 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

65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 1CM007 0  0  95.98 97.49 279  286 .002. 009 1CM008 0  0  94.70 95.60 280  291 .0026. 0034 1CM009 0  0  94.70 95.60 280  291 .0026. 0034 4CM035 0  0  94.70 95.60 280 291 .0026. 0034 4CM036 0  0  94.70 95.60 280 291 .0026. 0034 2CM012 0  0  97.49  98.18 283.4  293.9 .0067  .0076 2CM016 0  0  100.67 101.01 293 299 .0114. 0129 3CM020 0  0  98.5 99.74 284.6 292.4 .0081. 0115 3CM023 0  0  98.2 99.6 281.5 283.6 .0065. 0075 2CM013 0  0  97.49  98.18 283.4  293.9 .0067  .0076 2CM017 0  0  100.67 101.01 293 299 .0114. 0129 4CM037 0  0  98.5 99.74 284.6 292.4 .0081. 0115 3CM024 0  0  98.2 99.6 281.5 283.6 .0065. 0075 4CM038 0  0  98.5 99.74 284.6 292.4 .0081. 0115 3CM025 0  0  98.2 99.6 281.5 283.6 .0065. 0075 2CM014 0  0  97.49  98.18 283.4  293.9 .0067  .0076 2CM018 0  0  100.67 101.01 293 299 .0114. 0129 3CM021 0  0  98.5 99.74 284.6 292.4 .0081. 0115 3CM026 0  0  98.2 99.6 281.5 283.6 .0065. 0075 3CM027 0  0  98.2 99.6 281.5 283.6 .0065. 0075 2CM019 0  0  99.29 101.01 288 298 .0100. 0146 3CM022 0  0  98.5 99.74 284.6 292.4 .0081. 0115 3CM028 0  0  98.2 99.6 281.5 283.6 .0065. 0075 6CM044 0  0  98.2  99.6 281.5  283.6 .0065  .0075 7CM048 0  0  98.2  99.6 281.5  283.6 0.0065  0.0075 7CM050 0  0  98.5  99.74 284.6  292.4 0.0081  0.0115 7CM049 0  0  98.2  99.6 281.5  283.6 0.0065  0.0075 1CM010 0  0  97.77 98.11 286  295 .0061. 0074 7CM045 0  0  97.77  98.11 286  295 0.0061  0.0074 1CM011 0  0  97.77 98.11 286  295 .0061. 0074 7CM046 0  0  97.77  98.11 286  295 0.0061  0.0074 2CM015 0  0  97.77 98.11 286  295 .0061. 0074 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 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 1CM007 CFMI CFM56 Evaluation Engineering Peebles Site IVD 11 Nov 83 14 Nov 83 1CM008 CFMI CFM56 Evaluation Engineering Peebles Site IIIC 19 Nov 86 20 Nov 86 1CM009 CFMI CFM56 Evaluation Engineering Peebles Site IIIC 19 Nov 86 20 Nov 86 4CM035 CFMI CFM56 Evaluation Engineering Peebles Site IIIC 19 Nov 86 20 Nov 86 4CM036 CFMI CFM56 Evaluation Engineering Peebles Site IIIC 19 Nov 86 20 Nov 86 2CM012 CFMI CFM56 Evaluation Engineering Peebles Site IIIB 7 Oct 92 8 Oct 92 2CM016 CFMI CFM56 Evaluation Engineering PTO Site IIIC 15 Jun 94 1 Jul 94 3CM020 CFM International GEAE Peebles Testing Facility + Techspace APeebles Ohio, USE + Liers, Belgium Aug 96 Sep 96 3CM023 GE CFM56 5B Eval Engineering Techspace Aero Facility, Liege, Belgium Nov 95 2CM013 CFMI CFM56 Evaluation Engineering Peebles Site IIIB 7 Oct 92 8 Oct 92 2CM017 CFMI CFM56 Evaluation Engineering PTO Site IIIC 15 Jun 94 1 Jul 94 4CM037 CFM International GEAE Peebles Testing Facility + Techspace APeebles, Ohio, USA + Liers, Belgium Aug 96 Sep 96 3CM024 GE CFM56 5B Eval Engineering Techspace Aero Facility, Liege, Belgium Nov 95 4CM038 CFM International GEAE Peebles Testing Facility + Techspace APeebles, Ohio, USA + Liers, Belgium Aug 96 Sep 96 3CM025 GE CFM56 5B Eval Engineering Techspace Aero Facility, Liege, Belgium Nov 95 2CM014 CFMI CFM56 Evaluation Engineering Peebles Site IIIB 7 Oct 92 8 Oct 92 2CM018 CFMI CFM56 Evaluation Engineering PTO Site IIIC 15 Jun 94 1 Jul 94 3CM021 CFM International GEAE Peebles Testing Facility + Techspace APeebles Ohio, USE + Liers, Belgium Aug 96 Sep 96 3CM026 GE CFM56 5B Eval Engineering Techspace Aero Facility, Liege, Belgium Nov 95 3CM027 GE CFM56 5B Eval Engineering Techspace Aero Facility, Liege, Belgium Nov 95 2CM019 CFMI SNECMA, Villaroche, France Techspace Aero, Liege, Belgium 19 Jun 95 28 Jul 95 3CM022 CFM International GEAE Peebles Testing Facility + Techspace APeebles Ohio, USE + Liers, Belgium Aug 96 Sep 96 3CM028 GE CFM56 5B Eval Engineering Techspace Aero Facility, Liege, Belgium Nov 95 6CM044 GE CFM56 5B Eval Engineering Techspace Aero, Liege, Belgium Nov 95 Nov 95 7CM048 CFM International CFM56 Evaluation Engineering Techspace Aero, Liege, Belgium Nov 95 Nov 95 7CM050 CFM International CFM56 Evaluation Engineering GEAE PTO and Techspace Aero, Liege, Belgi 1 Aug 96 30 Sep 96 7CM049 CFM International CFM56 Evaluation Engineering Techspace Aero, Liege, Belgium 13 Non 95 Nov 95 1CM010 CFMI CFM56 Evaluation Engineering PTO Site IVD 4 Jun 91 5 Jun 91 7CM045 CFM International CFM56 Evaluation Engineering PTO Site IV D 4 Jun 91 5 Jun 91 1CM011 CFMI CFM56 Evaluation Engineering PTO Site IVD 4 Jun 91 5 Jun 91 7CM046 CFM International CFM56 Evaluation Engineering PTO Site IV D Jun 91 Jun 91 2CM015 CFMI CFM56 Evaluation Engineering PTO Site IVD 4 Jun 91 5 Jun 91 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 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 1CM007 1. Ref GE Report R84AEB579. 2. Engine S/ N 692441. 3. Revised based on 3/ 89 production status cycle.

1CM008 1. Ref GE Report R87AEB368. 2. Engine S/ N 730002/ 2. 3. Data revised and corrected April 93.

1CM009 1. Ref GE Reports R89AEB316 and R87AEB386. 2. Engine S/ N 730002/ 2.

4CM035 1. Ref GE Reports R89AEB316 and R87AEB386 2. Engine S/ N 730002/ 2 4CM036 1. Ref GE Reports R89AEB316 and R87AEB386 2. Engine S/ N 730002/ 2 2CM012 1. Ref GE Report R92AEB262. 2. Engine S/ N 779101 2CM016 1. Ref GE Report CR 797/ 2. 2. Engine S/ N 779131/ 001 & 779132/ 001 3. DAC combustor 3CM020 DAC II Combustor P/ N 1968M99G04 3CM023 1. FAA Certification Report CR 797/ P, June 95. 2. Engine S/ N 779 194/ 1 2CM013 1. Ref GE Report R92AEB262. 2. Engine S/ N 779101 2CM017 1. Ref GE Report CR 797/ 2. 2. Engine S/ N 779131/ 001 & 779132/ 001 3. DAC combustor 4CM037 DAC II Combustor P/ N 1968M99G04 3CM024 1. FAA Certification Report CR 797/ P, June 95. 2. Engine S/ N 779 194/ 1 4CM038 DAC II Combustor P/ N 1968M99G04 3CM025 1. FAA Certification Report CR 797/ P, June 95. 2. Engine S/ N 779 194/ 1 2CM014 1. Ref GE Report R92AEB262. 2. Engine S/ N 779101 2CM018 1. Ref GE Report CR 797/ 2. 2. Engine S/ N 779131/ 001 & 779132/ 001 3. DAC combustor 3CM021 DAC II Combustor P/ N 1968M99G04 3CM026 1. FAA Certification Report CR 797/ P, June 95. 2. Engine S/ N 779 194/ 1 3CM027 1. FAA Certification Report CR 797/ P, June 95. 2. Engine S/ N 779 194/ 1 2CM019 1. Ref GE Report CR 797/ 2 Supplement 1. 2. Engine S/ N 779172/ 001, 779174/ 001, 779175/ 001, & 779178/ 001 3. DAC combustor 3CM022 DAC II Combustor P/ N 1968M99G04 3CM028 1. FAA Certification Report CR 797/ P, June 95. 2. Engine S/ N 779 194/ 1 6CM044 1. FAA Certification Report CR0797/ P, June 95. 2. Engine S/ N 779 194/ 1 7CM048 1. FAA Certificiaction Report CR 0797/ P, June 1995 and Certification Report CR 700 S3, October 2001 2. Engine S/ N 779 194/ 1 7CM050 1. FAA Certification Report CR 700 S3, October 2001 2. DAC II combustor P/ N 196M99G04 7CM049 1. FAA Certifiaction Report CR 0797/ P, June 1995 and Certification Report CR 700 S3, October 2001 2. Engine S/ N 779 194/ 1 1CM010 1. Ref GE Report R91AEB471. 2. Engine S/ N 740 105.

7CM045 1. Ref GE Report R91AEB471 and FAA Certification Report CR 897/ P, July 2003 2. Engine S/ N 740/ 105 1CM011 1. Ref GE Report R91AEB471. 2. Engine S/ N 740 105.

7CM046 1. Ref GE Report R91AEB471 and FAA Certification Report CR 897/ P, July 2003 2. Engine S/ N 740 105 2CM015 1. Ref GE Report R91AEB471 2. Engine S/ N 740 105 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 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 Engine S/ N 779 194/ 1 0 0 DAC II Combustor P/ N 1 0 0 Engine S/ N 779 194/ P 0 0 Engine S/ N 740 105 0 0 Ebgine S/ N 740 105 0 0 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 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 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 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 7CM047 CFM56 5C4/ P SAC MTF 6.6 30.5 149.9 3CM029 CFM56 7B18 TF 5.5 21.59 86.74 3CM030 CFM56 7B20 TF 5.4 22.61 91.63 4CM039 CFM56 7B20/ 2 TF 5.4 22.77 91.63 3CM031 CFM56 7B22 TF 5.3 24.41 100.97 4CM040 CFM56 7B22/ 2 TF 5.3 24.61 100.97 3CM032 CFM56 7B24 TF 5.2 25.78 107.65 4CM041 CFM56 7B24/ 2 TF 5.2 25.95 107.65 3CM033 CFM56 7B26 TF 5.1 27.61 116.99 4CM042 CFM56 7B26/ 2 TF 5.1 27.80 116.99 3CM034 CFM56 7B27 TF 5.0 28.63 121.44 4CM043 CFM56 7B27/ 2 TF 5.0 28.84 121.44 General Electric 1GE034 CF34 3A LEC II TF 6.25 19.7 41.01 1GE035 CF34 3A1 LEC II TF 6.25 19.7 41.01 5GE084 CF34 3B TF 6.25 19.3 41.01 5GE083 CF34 8C1 TF 5.13 23.03 56.36 6GE096 CF34 8C1 Block 1 LEC TF 5.13 22.15 56.36 6GE092 CF34 8C5 LEC TF 5.13 23.09 59.42 6GE093 CF34 8E2 LEC TF 5.13 21.71 55.19 6GE094 CF34 8E5 LEC TF 5.13 23.18 59.68 6GE095 CF34 8E5A1 LEC TF 5.13 24.12 62.49 3GE067 CF6 45A Low emissions fuel nozzle TF 4.3 25.38 202.8 1GE005 CF6 45A2 TF 4.3 25.9 202.8 3GE068 CF6 45A2 Low emissions fuel nozzle TF 4.3 25.38 202.8 3GE069 CF6 50A Low emissions fuel nozzle TF 4.3 26.88 215.3 1GE006 CF6 50C TF 4.3 28.8 224.2 3GE070 CF6 50C Low emissions fuel nozzle TF 4.3 27.76 224.2 3GE073 CF6 50C1 Low emissions fuel nozzle TF 4.3 28.44 230.4 1GE007 CF6 50C1,  C2 TF 4.3 29.8 230.4 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 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

97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 7CM047  x    x   x

3CM029  x    x   x

3CM030  x    x   x

4CM039  x    x   x

3CM031  x    x   x

4CM040  x    x   x

3CM032  x    x   x

4CM041  x    x   x

3CM033  x    x   x

4CM042  x    x   x

3CM034  x    x   x

4CM043  x    x   x

1GE034  x    x   x

1GE035  x    x   x

5GE084  x    x   x

5GE083  x    x   x

6GE096  x    x   x

6GE092  x    x   x

6GE093  x    x   x

6GE094  x    x   x

6GE095  x    x   x

3GE067  x    x   x x

1GE005 x     x   x x

3GE068  x    x   x x

3GE069  x    x   x x

1GE006 x     x   x x

3GE070  x    x   x x

3GE073  x    x   x x

1GE007 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)

97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 7CM047 0 0 0 5.0 3 1 6   9.3 47.4 897 3CM029 0.10 0.10 0.10 3.50 3 1 6.32   9.7 49.5 549 3CM030 0.10 0.10 0.10 3.10 3 1 5.44   8.4 42.9 504 4CM039 0.07 0.23 0.36 8.11 3 3 14.61  13.8 15.9 17.0 86.9 1340 3CM031 0.10 0.10 0.10 2.50 3 1 4.22   6.4 32.7 432 4CM040 0.06 0.10 6.06 7.26 3 3 16.31  14.6 18.2 19.0 97.1 1643 3CM032 0.10 0.10 0.10 2.40 3 1 3.91   6.0 30.6 432 4CM041 0.05 0.07 6.01 6.55 3 3 14.66  13.4 15.9 17.1 87.2 1576 3CM033 0.10 0.10 0.10 1.90 3 1 3.06   4.7 24.0 361 4CM042 0.03 0.06 4.73 5.88 3 3 12.21  11.1 13.4 14.2 72.7 1425 3CM034 0.10 0.10 0.10 1.70 3 1 2.76   4.3 21.9 335 4CM043 0.05 0.06 4.21 5.56 3 3 11.21  10.1 12.3 13.1 66.7 1363 1GE034 0.06 0.06 0.13 3.95 3 1 7.63 0.20 7.41 7.78 11.8 60.0 313 1GE035 0.06 0.06 0.13 3.95 3 1 7.63 0.20 7.41 7.78 11.8 60.0 313 5GE084 0.06 0.05 0.13 4.69 3 1 8.9   13.7 69.9 366 5GE083 0.02 0.02 0.06 0.08 3 1 0.20 0.00 0.2  0.2 0.3 1.5 13 6GE096 0.02 0.03 0.07 0.13 3 1 0.30  0.3  0.4 0.5 2.6 20 6GE092 0.02 0.02 0.06 0.13 3 1 0.31   0.5 2.6 18 6GE093 0.02 0.03 0.07 0.16 3 1 0.38   0.6 3.1 21 6GE094 0.02 0.02 0.06 0.13 3 1 0.31   0.5 2.6 18 6GE095 0.02 0.02 0.06 0.13 3 1 0.29   0.4 2.0 18 3GE067 0.09 0.14 0.35 2.72* 3 1 3.88 0.14 3.76 4.04 6.0 30.6 780 1GE005 0.7 0.7 1.1 26.0 6 6 39.7 3.8  44.2 225.3 8485 3GE068 0.09 0.14 0.35 2.72* 3 1 3.88 0.14 3.76 4.04 6.0 30.6 780 3GE069 0.15 0.14 0.31 2.72* 3 1 3.66 0.14 3.53 3.81 5.6 28.6 785 1GE006 0.6 0.7 1.0 23.0 6 6 35.2 3.8  39.2 199.8 7998 3GE070 0.14 0.14 0.29 2.72* 3 1 3.47 0.09 3.38 3.56 5.3 27.0 784 3GE073 0.14 0.15 0.28 2.72* 3 1 3.42 0.15 3.28 3.58 5.3 27.0 788 1GE007 0.6 0.7 1.0 21.8 6 6 33.5 3.8  37.3 190.1 7715 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)

97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 7CM047 0.8 0.7 1.6 31.6 3 1 39.9   48.9 41.4 5964 3CM029 0.60 0.40 3.60 28.30 3 1 52.45   64.4 54.6 4566 3CM030 0.60 0.50 3.20 25.90 3 1 47.21   58.0 49.2 4324 4CM039 4.26 11.38 11.37 49.71 3 3 108.63  102.1 114.9 117.5 99.6 9963 3CM031 0.50 0.60 2.50 22.80 3 1 39.58   48.6 41.2 4002 4CM040 2.18 6.58 30.87 45.35 3 3 104.18  96.9 111.7 112.7 95.5 10492 3CM032 0.40 0.60 2.20 22.00 3 1 37.11   45.6 38.6 3998 4CM041 1.38 4.30 30.32 42.72 3 3 94.03  88.4 100.0 101.7 86.2 10117 3CM033 0.20 0.60 1.60 18.80 3 1 30.33   37.2 31.5 3533 4CM042 0.77 2.51 26.07 39.93 3 3 81.39  77.1 85.9 88.0 74.6 9495 3CM034 0.20 0.50 1.40 17.90 3 1 28.30   34.7 29.4 3436 4CM043 0.54 1.97 24.28 38.73 3 3 76.46  72.7 80.4 82.7 70.1 9291 1GE034 0 0 1.9 42.6 3 1 81.8 3.25 79.2 85.5 100.4 85.1 3350 1GE035 0 0 1.9 42.6 3 1 81.8 3.25 79.2 85.5 100.4 85.1 3350 5GE084 0 0 1.88 47.59 3 1 89.7   110.1 93.3 3683 5GE083 0.41 0.50 2.91 24.92 3 1 51.30 1.04 50.1  52.0 63.0 53.4 2845 6GE096 0.59 0.57 4.67 19.73 3 1 42.80  41.5  44.5 52.5 44.5 2406 6GE092 0.64 0.57 4.24 18.25 3 1 34.86   42.8 36.3 2070 6GE093 0.59 0.58 4.52 20.01 3 1 39.28   48.2 40.8 2169 6GE094 0.64 0.57 4.23 18.16 3 1 34.62   42.5 36.0 2065 6GE095 0.71 0.57 4.05 17.3 3 1 32.43   39.8 33.7 2027 3GE067 0.43 0.54 5.01 24.04* 3 1 34.43 0.56 33.90 34.38 42.3 35.8 6980 1GE005 0.5 0.5 7.5 66.0 6 6 102.0 4.6  107.7 91.3 21798 3GE068 0.43 0.54 5.01 24.04* 3 1 34.43 0.56 33.90 34.38 42.3 35.8 6980 3GE069 0.43 0.49 4.35 24.04* 3 1 32.16 0.50 31.72 32.71 39.5 33.5 6920 1GE006 0.5 0.5 5.2 62.3 6 6 95.1 4.6  100.5 85.1 21583 3GE070 0.44 0.46 3.99 24.04* 3 1 30.73 0.48 30.32 31.25 37.7 31.9 6883 3GE073 0.45 0.45 3.71 24.04* 3 1 29.80 0.44 29.42 30.28 36.6 31.0 6863 1GE007 0.5 0.5 4.3 61.8 6 6 93.7 4.6  99.0 83.9 21591 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 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 7CM047 34.1 26.7 9.9 4.1 3 1 50.9   59.0 58.4 73.0 86.8 7641 3CM029 19.20 16.60 9.10 4.30 3 1 39.99   46.4 55.8 69.7 85.8 3472 3CM030 20.50 17.40 9.50 4.30 3 1 41.83   48.5 56.9 71.1 87.9 3829 4CM039 13.25 10.81 9.39 3.75 3 3 30.58  30.4 30.8 32.4 37.9 47.3 58.4 2802 3CM031 23.10 19.00 10.00 4.50 3 1 45.16   52.4 59.0 73.7 90.3 4560 4CM040 15.08 12.16 6.37 3.94 3 3 30.63  30.4 30.9 32.4 36.4 45.4 55.6 3091 3CM032 25.30 20.50 10.10 4.40 3 1 47.83   55.4 60.5 75.6 92.0 5149 4CM041 16.63 13.23 6.72 4.08 3 3 32.86  32.7 33.2 34.8 37.9 47.3 57.5 3534 3CM033 28.80 22.50 10.80 4.70 3 1 52.64   62.2 65.3 81.7 98.5 6149 4CM042 19.20 14.77 7.26 4.27 3 3 36.24  36.0 36.8 38.4 40.2 50.2 60.5 4233 3CM034 30.90 23.70 11.00 4.80 3 1 55.27   64.1 65.9 82.4 98.9 6719 4CM043 20.81 15.59 7.53 4.36 3 3 38.23  37.9 38.8 40.5 41.5 51.8 62.2 4648 1GE034 11.61 10.14 6.86 3.82 3 1 27.8 1.61 26.0 29.0 32.2 40.6 50.7 53.2 1137 1GE035 11.61 10.14 6.86 3.82 3 1 27.8 1.61 26.0 29.0 32.2 40.6 50.7 53.2 1137 5GE084 11.28 9.68 6.63 3.72 3 1 26.3   30.5 38.8 48.5 50.9 1078 5GE083 14.67 12.82 11.10 4.31 3 1 37.20 0.74 36.6  38.0 43.1 50.1 62.6 68.7 2120 6GE096 13.82 12.00 9.85 4.03 3 1 35.20  35.0  35.7 40.9 48.5 60.6 71.3 1956 6GE092 14.69 12.6 10.75 4.6 3 1 37.12   43.0 49.9 62.4 69.2 2205 6GE093 13.6 11.82 10.29 4.45 3 1 35.14   40.7 48.8 61.0 66.9 1939 6GE094 14.77 12.65 10.77 4.61 3 1 37.25   43.2 50.0 62.5 69.4 2222 6GE095 15.81 13.15 11.06 4.7 3 1 38.71   44.9 50.9 63.6 71.1 2419 3GE067 25.45 21.61 9.36 3.4* 3 1 44.90 2.94 42.69 48.24 52.0 57.3 71.6 87.2 9105 1GE005 31.0 26.2 8.4 3.3 6 6 54.3 0.5  56.5 61.6 77.0 93.5 10819 3GE068 25.45 21.61 9.36 3.4* 3 1 44.90 2.94 42.69 48.24 52.0 57.3 71.6 87.2 9105 3GE069 27.17 23.27 9.72 3.4* 3 1 47.86 2.96 45.72 51.24 55.5 59.2 74.0 89.5 10286 1GE006 35.0 29.0 9.4 3.5 6 6 60.2 0.5  62.7 64.2 80.3 96.3 13436 3GE070 28.03 24.30 10.09 3.4* 3 1 49.59 2.93 47.66 52.96 57.5 60.2 75.2 90.7 11116 3GE073 28.97 25.50 10.16 3.4* 3 1 51.58 2.80 49.71 54.80 59.8 61.7 77.2 92.7 11884 1GE007 36.3 29.7 9.5 3.6 6 6 61.8 0.5  64.3 64.6 80.7 96.5 14247 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

97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 7CM047 12    3 1 12   15.4 72.7 3CM029     3 1 10.7   13.8 56.1 3CM030     3 1 11.4   14.7 60.6 4CM039     3 3 1.52  0  3.4 1.7 6.9 3CM031     3 1 12.0   15.4 65.2 4CM040     3 3 0.69  0.1 1.8 0.8 3.2 3CM032     3 1 12.6   16.2 69.8 4CM041     3 3 0.65  0.2 1.5 0.7 3.1 3CM033     3 1 14.7   18.9 83.4 4CM042     3 3 0.71  0.3 1.6 0.7 3.1 3CM034     3 1 15.7   20.2 90.0 4CM043     3 3 0.75  0.3 1.6 0.8 3.7 1GE034 21.9 9.2 3.1 3.1 3 1 21.9 0.25 21.7 22.2 28.2 93.3 1GE035 21.9 9.2 3.1 3.1 3 1 21.9 0.25 21.7 22.2 28.2 93.3 5GE084 18.3 9.2 3.1 3.1 3 1 18.3   23.6 78.1 5GE083 5.33 1.48 0 0 3 1 5.33 1.0 4.6  6.5 6.9 24.9 6GE096 5.20 1.25 0.00 0.00 3 1 5.20  2.5  7.2 6.7 24.2 6GE092 8.32 2.52 0 0 3 1 8.32   10.7 39.2 6GE093 4.58 0.96 0 0 3 1 4.58   5.9 21.2 6GE094 8.63 2.64 0 0 3 1 8.63   11.1 40.7 6GE095 13.64 3.9 0 0 3 1 13.64   17.6 65.4 3GE067 11.61 11.98 1.25 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 82.6 1GE005 2.9 2.2 2.9 4.6 6 6 4.6 1.5  4.9 25.2 3GE068 11.61 11.98 1.25 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 82.6 3GE069 11.53 12.03 1.49 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 83.9 1GE006 3.9 2.6 2.8 4.5 6 6 4.5 1.5  4.8 25.3 3GE070 11.41 11.83 1.61 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 84.9 3GE073 10.95 11.72 1.62 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 85.5 1GE007 4.1 2.7 2.7 4.5 6 6 4.5 1.5  4.8 25.5 Filename DCTM_ ARP. xls Printed on 5/ 20/ 05 Check website for latest version www. QinetiQ. com/ aviation_ emissions_ databank Data 1 2 3 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

97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 7CM047 Jet A 1.95 17.3 1.395 1.143 0.370 0.115 478 3CM029 Jet A 1.86 1.97 16.9 17.7 0.854 0.714 0.260 0.097 344 3CM030 Jet A 1.86 1.97 16.9 17.7 0.913 0.761 0.274 0.100 361 4CM039 Jet A 1.93 1.94 18.0 19.2 0.903 0.754 0.278 0.102 363 3CM031 Jet A 1.86 1.97 16.9 17.7 1.021 0.844 0.298 0.105 390 4CM040 Jet A 1.93 1.94 18.0 19.2 1.008 0.837 0.303 0.105 389 3CM032 Jet A 1.86 1.97 16.9 17.7 1.103 0.910 0.316 0.109 412 4CM041 Jet A 1.93 1.94 18.0 19.2 1.089 0.902 0.313 0.109 410 3CM033 Jet A 1.86 1.97 16.9 17.7 1.221 0.999 0.338 0.113 441 4CM042 Jet A 1.93 1.94 18.0 19.2 1.203 0.989 0.334 0.113 438 3CM034 Jet A 1.86 1.97 16.9 17.7 1.284 1.043 0.349 0.116 456 4CM043 Jet A 1.93 1.94 18.0 19.2 1.265 1.033 0.351 0.115 453 1GE034 JP 5 1.92 20.3 0.4070 0.3343 0.1190 0.0496 167 1GE035 JP 5 1.92 20.3 0.4070 0.3343 0.1190 0.0496 167 5GE084 Jet A 1.92 20.30 0.3991 0.3288 0.1160 0.0489 164 5GE083 Jet A 1.93 16.87 0.6042 0.4941 0.1681 0.0690 239 6GE096 Jet A 1.937 18 0.6080 0.4790 0.1702 0.0703 239 6GE092 Jet A 1.937 18 0.6481 0.5297 0.1793 0.0643 240 6GE093 Jet A 1.937 18 0.5906 0.4850 0.1680 0.0620 226 6GE094 Jet A 1.937 18 0.6518 0.5326 0.1800 0.0644 241 6GE095 Jet A 1.937 18 0.6914 0.5632 0.1876 0.066 251 3GE067 Jet A 1.935 16.3 2.027 1.663 0.592 0.163 701 1GE005 Jet A 1.92 17.1 2.058 1.716 0.583 0.200 765 3GE068 Jet A 1.935 16.3 2.027 1.663 0.592 0.163 701 3GE069 Jet A 1.935 16.3 2.168 1.787 0.625 0.163 731 1GE006 Jet A 1.92 17.1 2.379 1.915 0.643 0.212 838 3GE070 Jet A 1.935 16.3 2.281 1.875 0.641 0.163 751 3GE073 Jet A 1.935 16.3 2.361 1.940 0.663 0.163 769 1GE007 Jet A 1.92 17.1 2.487 1.975 0.660 0.215 859 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

97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 7CM047 0  0  97.77  98.11 286  295 0.0061  0.0074 3CM029 0  0  97.8 98.0 294 297 .0100. 0157 3CM030 0  0  97.8 98.0 294 297 .0100. 0157 4CM039 0  0  97.9 98.0 292.8 296.7 .00814. 0131 3CM031 0  0  97.8 98.0 294 297 .0100. 0157 4CM040 0  0  97.9 98.0 292.8 296.7 .00814. 0131 3CM032 0  0  97.8 98.0 294 297 .0100. 0157 4CM041 0  0  97.9 98.0 292.8 296.7 .00814. 0131 3CM033 0  0  97.8 98.0 294 297 .0100. 0157 4CM042 0  0  97.9 98.0 292.8 296.7 .00814. 0131 3CM034 0  0  97.8 98.0 294 297 .0100. 0157 4CM043 0  0  97.9 98.0 292.8 296.7 .00814. 0131 1GE034 0  0  101.6 102.9 275.5 281.1 .0016. 0039 1GE035 0  0  101.6 102.9 275.5 281.1 .0016. 0039 5GE084 0  0  101.6 102.9 275.5 281.1 .0016. 0039 5GE083 0  0  96.87  97.62 287  296.4 .0056  .00656 6GE096 0  0  97.1  98.1 284  292 0.00470  0.00727 6GE092 0  0  97.1  98.1 284  292 .00470  .00727 6GE093 0  0  97.1  98.1 284  292 .00470  .00727 6GE094 0  0  97.1  98.1 284  292 .00470  .00727 6GE095 0  0  97.1  98.1 284  292 .00470  .00727 3GE067 0  0  97.73 97.91 292.3 301.3 .0127. 0216 1GE005 0  0  98.3 100.4 270  296 .0027. 0103 3GE068 0  0  97.73 97.91 292.3 301.3 .0127. 0216 3GE069 0  0  97.73 97.91 292.3 301.3 .0127. 0216 1GE006 0  0  98.3 100.4 270  296 .0027. 0103 3GE070 0  0  97.73 97.91 292.3 301.3 .0127. 0216 3GE073 0  0  97.73 97.91 292.3 301.3 .0127. 0216 1GE007 0  0  98.3 100.4 270  296 .0027. 0103 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 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 7CM047 CFM International CFM56 Evaluation Engineering PTO Site IV D Jun 91 Jun 91 3CM029 GE CFM56 7B Eval Engineering Peebles Test Operation, Peebles, Ohio, USA Jul 96 3CM030 GE CFM56 7B Eval Engineering Peebles Test Operation, Peebles, Ohio, USA Jul 96 4CM039 GE CFM56 7B Eval Engineering Peebles Test Operation ( PTO) Peebles, OH 30 Aug 97 12 Sep 97 3CM031 GE CFM56 7B Eval Engineering Peebles Test Operation, Peebles, Ohio, USA Jul 96 4CM040 GE CFM56 7B Eval Engineering Peebles Test Operation ( PTO) Peebles, OH 30 Aug 97 12 Sep 97 3CM032 GE CFM56 7B Eval Engineering Peebles Test Operation, Peebles, Ohio, USA Jul 96 4CM041 GE CFM56 7B Eval Engineering Peebles Test Operation ( PTO) Peebles, OH 30 Aug 97 12 Sep 97 3CM033 GE CFM56 7B Eval Engineering Peebles Test Operation, Peebles, Ohio, USA Jul 96 4CM042 GE CFM56 7B Eval Engineering Peebles Test Operation ( PTO) Peebles, OH 30 Aug 97 12 Sep 97 3CM034 GE CFM56 7B Eval Engineering Peebles Test Operation, Peebles, Ohio, USA Jul 96 4CM043 GE CFM56 7B Eval Engineering Peebles Test Operation ( PTO) Peebles, OH 30 Aug 97 12 Sep 97 1GE034 GE Aircraft Engines GE Aircraft Engines, Lynn, MA Lynn Cell 121 21 Mar 91 23 Mar 91 1GE035 GE Aircraft Engines GE Aircraft Engines, Lynn, MA Lynn Cell 121 21 Mar 91 23 Mar 91 5GE084 GE GE Aircraft Engines, Lynn, MA Lynn Cell 121 21 Mar 91 25 Mar 91 5GE083 GE Peebles Test Opeation Peebles, Ohio 6GE096 GE Aircraft Engines Peebles Test Operation Peebles, Ohio 27 Jan 02 28 Jan 02 6GE092 GE Aircraft Engines Peebles Test Operation Peebles, Ohio 27 Jan 02 28 Jan 02 6GE093 GE Aircraft Engines Peebles Test Organisation Peebles, Ohio 27 Jan 02 28 Jan 02 6GE094 GE Aircraft Engines Peebles Test Organisation Peebles, Ohio 27 Jan 02 28 Jan 02 6GE095 GE Aircraft Engines Peebles Test Organisation Peebles, Ohio 27 Jan 02 28 Jan 02 3GE067 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 1GE005 GE Aircraft Engines Production Engine Test Production Test Cells M34 & M35 12 Oct 79 5 Dec 79 3GE068 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 3GE069 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 1GE006 GE Aircraft Engines Production Engine Test Production Test Cells M34 & M35 12 Oct 79 5 Dec 79 3GE070 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 3GE073 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 1GE007 GE Aircraft Engines Production Engine Test Production Test Cells M34 & M35 12 Oct 79 5 Dec 79 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 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 7CM047 1. Ref GE Report R91AEB471 and FAA Certification Report CR 897/ P, July 2003 2. Engine S/ N 740 105 3. Data also applies to CFM56 5C4/ 1P 3CM029 1. FAA Certification Report CR 997, Dec 96. 2. Engine S/ N 874 101/ 01 3CM030 1. FAA Certification Report CR 997, Dec 96. 2. Engine S/ N 874 101/ 01 4CM039 1. FAA Certification Report CR 997/ 2, 14 Nov 97 2. Engine S/ N 874 136/ 01, 874 141/ 01, 874 146/ 01 3CM031 1. FAA Certification Report CR 997, Dec 96. 2. Engine S/ N 874 101/ 01 4CM040 1. FAA Certification Report CR 997/ 2, 14 Nov 97 2. Engine S/ N 874 136/ 01, 874 141/ 01, 874 146/ 01 3CM032 1. FAA Certification Report CR 997, Dec 96. 2. Engine S/ N 874 101/ 01 4CM041 1. FAA Certification Report CR 997/ 2, 14 Nov 97 2. Engine S/ N 874 136/ 01, 874 141/ 01, 874 146/ 01 3CM033 1. FAA Certification Report CR 997, Dec 96. 2. Engine S/ N 874 101/ 01 4CM042 1. FAA Certification Report CR 997/ 2, 14 Nov 97 2. Engine S/ N 874 136/ 01, 874 141/ 01, 874 146/ 01 3CM034 1. FAA Certification Report CR 997, Dec 96. 2. Engine S/ N 874 101/ 01 4CM043 1. FAA Certification Report CR 997/ 2, 14 Nov 97 2. Engine S/ N 874 136/ 01, 874 141/ 01, 874 146/ 01 1GE034 1. Ref GE Report R91AEB051 ( 1/ 92 rev). 2. Engine S/ N 807 005. 3. LEC II combustor.

1GE035 1. Ref GE Report R91AEB051 ( 1/ 92 rev). 2. Engine S/ N 807 005. 3. LEC II combustor.

5GE084 1. Ref. GE Report R95AEB012 2. Engine S/ N 807 005 5GE083 1. Ref. GE Report R99AEB031. 2. Engine S/ S 965202.

6GE096 1. GE Report R2001AE078 2. Engine S/ N 193111 6GE092 1. GE Report R2001AE078 2. Engine S/ N 193111 3. LEC combustor 6GE093 1. GE Report R2001AE078 2. Engine S/ N 193111 3. LEC combustor 6GE094 1. GE Report R2001AE078 2. Engine S/ N 193111 3. LEC combustor 6GE095 1. GE Report R2001AE078 2. Engine S/ N 193111 3. LEC combustor 3GE067 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 1GE005 Ref Report no FAA EE 80 27 ( GE Report R80AEG420)

3GE068 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 3GE069 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 1GE006 Ref Report no FAA EE 80 27 ( GE Report R80AEG420)

3GE070 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 3GE073 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 1GE007 Ref Report no FAA EE 80 27 ( GE Report R80AEG420)

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 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 Engine S/ N 740 105 Data also a 0 ted at normal idle setting rather than 7%.

ted at normal idle setting rather than 7%.

ted at normal idle setting rather than 7%.

ted at normal idle setting rather than 7%.

ted at normal idle setting rather than 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 DI DJ DK DL DM DN 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 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 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 3GE074 CF6 50C2 Low emissions fuel nozzle TF 4.3 28.44 230.4 3GE078 CF6 50C2B Low emissions fuel nozzle TF 4.3 29.06 236.7 1GE008 CF6 50C2R TF 4.3 28.8 224.2 3GE072 CF6 50C2R Low emissions fuel nozzle TF 4.3 27.76 224.2 3GE071 CF6 50CA Low emissions fuel nozzle TF 4.3 27.76 224.2 3GE075 CF6 50E Low emissions fuel nozzle TF 4.3 28.44 230.4 3GE076 CF6 50E1 Low emissions fuel nozzle TF 4.3 28.44 230.4 1GE009 CF6 50E2 TF 4.3 29.8 230.4 3GE077 CF6 50E2 Low emissions fuel nozzle TF 4.3 28.44 230.4 3GE079 CF6 50E2B Low emissions fuel nozzle TF 4.3 29.06 236.7 1GE001 CF6 6D TF 5.9 24.7 174.8 1GE002 CF6 6D1A TF 5.9 25.4 181.9 1GE003 CF6 6K TF 5.9 24.7 174.8 1GE004 CF6 6K2 TF 5.9 25.4 181.9 1GE010 CF6 80A TF 5 29.0 208.8 1GE011 CF6 80A1 TF 5 29.0 209.0 1GE012 CF6 80A2 TF 5 30.1 216.5 1GE013 CF6 80A3 TF 5 30.1 217.8 1GE014 CF6 80C2A1 TF 5.1 30.96 257.4 2GE036 CF6 80C2A1 1862M39 TF 5.1 30.53 257.40 1GE015 CF6 80C2A2 TF 5.1 28 233.35 1GE016 CF6 80C2A2 TF 5.1 28.0 233.35 2GE037 CF6 80C2A2 1862M39 TF 5.1 27.79 233.35 1GE017 CF6 80C2A3 TF 5.1 31.64 262.22 1GE018 CF6 80C2A3 TF 5.1 31.64 262.22 2GE038 CF6 80C2A3 1862M39 TF 5.1 31.09 262.22 1GE019 CF6 80C2A5 TF 5.1 31.58 267.3 1GE020 CF6 80C2A5 TF 5.1 31.58 267.3 2GE039 CF6 80C2A5 1862M39 TF 5.1 31.66 267.34 3GE056 CF6 80C2A5F 1862M39 TF 5.1 32.88 271.88 1GE021 CF6 80C2A8 TF 5.1 31.0 257.4 2GE040 CF6 80C2A8 1862M39 TF 5.1 30.45 257.37 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

129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 3GE074  x    x   x x

3GE078  x    x   x x

1GE008 x     x   x x

3GE072  x    x   x x

3GE071  x    x   x x

3GE075  x    x   x x

3GE076  x    x   x x

1GE009 x     x   x x

3GE077  x    x   x x

3GE079  x    x   x x

1GE001 x     x   x x

1GE002 x     x   x x

1GE003 x     x   x x

1GE004 x     x   x x

1GE010 x     x   x x

1GE011 x     x   x x

1GE012 x     x   x x

1GE013 x     x   x x

1GE014  x    x   x x

2GE036  x    x   x

1GE015  x  x 1GE016 x   x x

1GE016   x   x   x x

2GE037  x    x   x

1GE017  x  x 1GE018 x   x x

1GE018   x   x   x x

2GE038  x    x   x

1GE019  x  x 1GE020 x   x x

1GE020   x   x   x x

2GE039  x    x   x

3GE056  x    x   x

1GE021  x    x   x x

2GE040  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)

129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 3GE074 0.14 0.15 0.28 2.72* 3 1 3.42 0.15 3.28 3.58 5.3 27.0 788 3GE078 0.13 0.15 0.26 2.72* 3 1 3.33 0.15 3.19 3.48 5.1 26.0 786 1GE008 0.6 0.7 1.0 23.0 6 6 35.2 3.8  39.2 199.8 7998 3GE072 0.14 0.14 0.29 2.72* 3 1 3.47 0.09 3.38 3.56 5.3 27.0 784 3GE071 0.14 0.14 0.29 2.72* 3 1 3.47 0.09 3.38 3.56 5.3 27.0 784 3GE075 0.14 0.15 0.28 2.72* 3 1 3.42 0.15 3.28 3.58 5.3 27.0 788 3GE076 0.14 0.15 0.28 2.72* 3 1 3.42 0.15 3.28 3.58 5.3 27.0 788 1GE009 0.6 0.7 1.0 21.8 6 6 33.5 3.8  37.3 190.1 7715 3GE077 0.14 0.15 0.28 2.72* 3 1 3.42 0.15 3.28 3.58 5.3 27.0 788 3GE079 0.13 0.15 0.26 2.72* 3 1 3.33 0.15 3.19 3.48 5.1 26.0 786 1GE001 0.3 0.3 0.7 21.0 7 7 33.3 3.5  36.7 187.4 5821 1GE002 0.3 0.3 0.6 19.9 7 7 30.9 3.5  34.1 173.9 5617 1GE003 0.3 0.3 0.7 21.0 7 7 33.3 3.5  36.7 187.4 5821 1GE004 0.3 0.3 0.6 19.9 7 7 30.9 3.5  34.1 173.9 5617 1GE010 0.29 0.29 0.47 6.29 3 1 7.84 0.95 7.17 8.93 12.1 61.7 1636 1GE011 0.29 0.29 0.47 6.29 3 1 7.83 0.95 7.16 8.92 12.1 61.7 1636 1GE012 0.30 0.37 0.45 6.28 3 1 7.58 0.96 6.91 8.69 11.7 59.7 1659 1GE013 0.30 0.37 0.45 6.28 3 1 7.53 0.96 6.87 8.64 11.6 59.2 1659 1GE014 0.08 0.09 0.20 9.19 3 2 11.32 1.27 10.24 12.65 14.7 75.2 2915 2GE036 0.05 0.05 0.12 1.59 4 2 2.07 0.234 1.94 2.45 2.7 13.7 536 1GE015 0.14 0.11 0.25 10.74 3 2 13.86 1.25 12.42 14.60 18.0 92.0 3239 1GE016 0.08 0.10 0.23 10.48 3 2 13.50 1.25 12.42 14.60 17.6 89.6 3152 2GE037 0.05 0.05 0.12 1.90 4 2 2.58 0.293 2.37 2.99 3.4 17.1 602 1GE017 0.08 0.10 0.21 9.21 3 2 11.30 1.29 9.85 12.32 14.7 75.0 2970 1GE018 0.06 0.08 0.19 8.94 3 2 10.94 1.29 9.85 12.32 14.2 72.6 2874 2GE038 0.04 0.05 0.11 1.54 4 2 1.99 0.22 1.85 2.34 2.6 13.2 523 1GE019 0.07 0.08 0.20 8.99 3 2 11.12 1.30 10.02 12.49 14.5 73.8 2966 1GE020 0.07 0.08 0.20 8.99 3 2 11.12 1.30 10.02 12.49 14.5 73.8 2966 2GE039 0.04 0.05 0.11 1.48 4 2 1.90 0.209 1.76 2.24 2.5 12.6 509 3GE056 0.05 0.04 0.11 1.18 4 2 1.63   2.1 10.7 440 1GE021 0.08 0.09 0.20 9.2 3 2 11.6 1.31 10.52 13.00 15.1 77.0 3005 2GE040 0.05 0.05 0.12 1.59 4 2 2.08 0.233 1.94 2.45 2.7 13.8 536 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)

129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 3GE074 0.45 0.45 3.71 24.04* 3 1 29.80 0.44 29.42 30.28 36.6 31.0 6863 3GE078 0.46 0.44 3.42 24.04* 3 1 28.88 0.407 28.50 29.31 35.4 30.0 6823 1GE008 0.5 0.5 5.2 62.3 6 6 95.1 4.6  100.5 85.1 21583 3GE072 0.44 0.46 3.99 24.04* 3 1 30.73 0.48 30.32 31.25 37.7 31.9 6883 3GE071 0.44 0.46 3.99 24.04* 3 1 30.73 0.48 30.32 31.25 37.7 31.9 6883 3GE075 0.45 0.45 3.71 24.04* 3 1 29.80 0.44 29.42 30.28 36.6 31.0 6863 3GE076 0.45 0.45 3.71 24.04* 3 1 29.80 0.44 29.42 30.28 36.6 31.0 6863 1GE009 0.5 0.5 4.3 61.8 6 6 93.7 4.6  99.0 83.9 21591 3GE077 0.45 0.45 3.71 24.04* 3 1 29.80 0.44 29.42 30.28 36.6 31.0 6863 3GE079 0.46 0.44 3.42 24.04* 3 1 28.88 0.407 28.50 29.31 35.4 30.0 6823 1GE001 0.5 0.5 6.5 54.2 7 7 88.7 6.9  93.3 79.1 15496 1GE002 0.5 0.5 5.5 52.0 7 7 82.8 6.9  87.1 73.8 15066 1GE003 0.5 0.5 6.5 54.2 7 7 88.7 6.9  93.3 79.1 15496 1GE004 0.5 0.5 5.5 52.0 7 7 82.8 6.9  87.1 73.8 15066 1GE010 1.0 1.1 3.1 28.2 3 1 35.5 0.4 35.0 35.9 43.6 36.9 7407 1GE011 1.0 1.1 3.1 28.2 3 1 35.5 0.4 35.0 35.9 43.6 36.9 7407 1GE012 1.0 1.1 2.8 28.2 3 1 34.2 0.4 33.8 34.5 42.0 35.6 7398 1GE013 1.0 1.1 2.8 28.2 3 1 34.0 0.4 33.6 34.3 41.7 35.3 7398 1GE014 0.56 0.54 2.19 42.24 3 2 53.04 3.04 50.41 55.78 60.4 51.2 13643 2GE036 0.05 0.04 2.05 19.76 4 2 25.37 1.18 24.3 27.1 28.9 24.5 6532 1GE015 0.58 0.56 3.04 46.65 3 2 61.53 3.08 57.97 63.34 70.1 59.4 14358 1GE016 0.57 0.55 2.94 46.01 3 2 60.64 3.08 57.97 63.34 69.1 58.6 14152 2GE037 0.04 0.05 2.56 21.97 4 2 29.81 1.33 28.7 31.5 34.0 28.8 6958 1GE017 0.59 0.57 2.15 42.18 3 2 52.67 3.03 49.18 54.56 60.0 50.9 13838 1GE018 0.58 0.56 2.07 41.51 3 2 51.80 3.03 49.18 54.56 59.0 50.0 13611 2GE038 0.06 0.04 1.98 19.32 4 2 24.58 1.19 23.4 26.3 28.0 23.7 6450 1GE019 0.52 0.52 1.93 41.65 3 2 52.35 3.03 49.73 55.20 59.6 50.5 13967 1GE020 0.52 0.52 1.93 41.65 3 2 52.35 3.03 49.73 55.20 59.6 50.5 13967 2GE039 0.06 0.04 1.91 18.89 4 2 23.78 1.96 22.6 25.5 27.1 23.0 6367 3GE056 0.05 0.04 1.92 16.96 4 2 22.68   25.8 21.9 6156 1GE021 0.52 0.52 2.05 42.3 3 2 54.4 3.09 51.75 57.31 62.0 52.5 14039 2GE040 0.05 0.04 2.05 19.76 4 2 25.35 1.18 24.3 27.1 28.9 24.5 6532 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 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 3GE074 28.97 25.50 10.16 3.4* 3 1 51.58 2.80 49.71 54.80 59.8 61.7 77.2 92.7 11884 3GE078 29.59 26.34 10.49 3.4* 3 1 52.87 2.73 51.06 56.10 61.3 62.5 78.1 93.6 12482 1GE008 35.0 29.0 9.4 3.5 6 6 60.2 0.5  62.7 64.2 80.3 96.3 13436 3GE072 28.03 24.30 10.09 3.4* 3 1 49.59 2.93 47.66 52.96 57.5 60.2 75.2 90.7 11116 3GE071 28.03 24.30 10.09 3.4* 3 1 49.59 2.93 47.66 52.96 57.5 60.2 75.2 90.7 11116 3GE075 28.97 25.50 10.16 3.4* 3 1 51.58 2.80 49.71 54.80 59.8 61.7 77.2 92.7 11884 3GE076 28.97 25.50 10.16 3.4* 3 1 51.58 2.80 49.71 54.80 59.8 61.7 77.2 92.7 11884 1GE009 36.3 29.7 9.5 3.6 6 6 61.8 0.5  64.3 64.6 80.7 96.5 14247 3GE077 28.97 25.50 10.16 3.4* 3 1 51.58 2.80 49.71 54.80 59.8 61.7 77.2 92.7 11884 3GE079 29.59 26.34 10.49 3.4* 3 1 52.87 2.73 51.06 56.10 61.3 62.5 78.1 93.6 12482 1GE001 40.0 32.6 11.4 4.5 7 7 66.4 2.3  68.9 77.1 96.4 117.8 11611 1GE002 41.6 33.9 11.8 4.6 7 7 69.0 2.3  71.6 78.9 98.6 120.1 12549 1GE003 40.0 32.6 11.4 4.5 7 7 66.4 2.3  68.9 77.1 96.4 117.8 11611 1GE004 41.6 33.9 11.8 4.6 7 7 69.0 2.3  71.6 78.9 98.6 120.1 12549 1GE010 29.8 25.6 10.3 3.4 3 1 53.1 3.0 49.6 55.4 61.6 62.9 78.6 94.2 11066 1GE011 29.8 25.6 10.3 3.4 3 1 53.0 3.0 49.6 55.3 61.4 62.7 78.3 93.9 11066 1GE012 29.6 26.6 10.8 3.4 3 1 55.5 2.9 52.4 58.1 64.3 64.2 80.2 95.7 11878 1GE013 29.6 26.6 10.8 3.4 3 1 55.2 2.9 52.1 57.7 64.0 63.9 79.8 95.2 11878 1GE014 32.22 24.85 9.76 3.99 3 2 48.12 0.53 47.41 48.43 52.9 51.9 64.9 76.8 12382 2GE036 26.55 20.45 12.43 4.68 4 2 44.72 0.31 44.3 45.0 49.2 48.7 60.8 72.3 11514 1GE015 27.90 20.71 9.52 3.91 3 2 41.70 0.42 41.31 42.14 45.9 47.8 59.7 71.9 9729 1GE016 27.93 20.69 9.44 3.95 3 2 41.68 0.42 41.31 42.14 45.8 47.7 59.7 71.8 9728 2GE037 22.35 18.37 11.86 4.49 4 2 40.01 0.236 39.7 40.3 44.0 46.0 57.5 69.3 9339 1GE017 34.44 25.45 10.01 3.96 3 2 49.91 0.40 49.63 50.42 54.9 53.1 66.4 78.1 13090 1GE018 34.50 25.46 9.93 3.92 3 2 49.84 0.44 49.63 50.42 54.8 53.1 66.3 78.0 13074 2GE038 27.68 21.05 12.48 4.72 4 2 46.03 0.56 45.5 46.8 50.6 49.5 61.9 73.2 12074 1GE019 30.85 22.86 9.11 3.79 3 2 46.31 2.16 44.62 48.92 50.9 49.4 61.7 72.6 12353 1GE020 34.38 22.86 9.11 3.79 3 2 49.25 2.23 46.22 49.73 54.2 52.5 65.6 77.2 12735 2GE039 28.57 21.69 12.53 4.76 4 2 47.28 0.5 46.7 47.9 52.0 50.3 62.9 73.9 12640 3GE056 28.11 21.27 12.64 4.90 4 2 47.07   51.8 49.0 61.2 71.2 12796 1GE021 33.5 22.0 9.0 3.7 3 2 45.8 1.75 44.33 47.72 50.4 49.4 61.7 73.0 11797 2GE040 26.42 20.45 12.43 4.68 4 2 44.63 0.312 44.2 44.9 49.1 48.6 60.8 72.3 11491 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

129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 3GE074 10.95 11.72 1.62 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 85.5 3GE078 11.17 11.62 1.58 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 86.1 1GE008 3.9 2.6 2.8 4.5 6 6 4.5 1.5  4.8 25.3 3GE072 11.41 11.83 1.61 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 84.9 3GE071 11.41 11.83 1.61 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 84.9 3GE075 10.95 11.72 1.62 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 85.5 3GE076 10.95 11.72 1.62 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 85.5 1GE009 4.1 2.7 2.7 4.5 6 6 4.5 1.5  4.8 25.5 3GE077 10.95 11.72 1.62 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 85.5 3GE079 11.17 11.62 1.58 1.4* 3 1 12.52 1.79 10.68 14.00 16.1 86.1 1GE001 4 3 3 4 7 7 4 2.2  4.3 20.9 1GE002 4 3 3 4 7 7  2.2

1GE003 4 3 3 4 7 7 4 2.2  4.3 20.9 1GE004 4 3 3 4 7 7  2.2

1GE010 12 10 2 2 1 1 12   15.6 80.6 1GE011 12 10 2 2 1 1 12   15.6 80.7 1GE012 12 10 2 2 1 1 12   15.6 81.4 1GE013 12 10 2 2 1 1 12   15.6 81.6 1GE014 8.2    3 2 8.2 1.2 6.0 8.2 9.6 52.6 2GE036 7.0 4.7 0.0 0.0 4 2 7.0 0.74 6.1 7.8 8.2 44.9 1GE015 6.5    3 2 6.5 1.0 5.4 7.3 7.6 40.6 1GE016 6.5    3 2 6.5 1.0 5.4 7.3 7.6 40.6 2GE037 5.8 3.2 0.0 0.0 4 2 5.8 0.63 5.1 6.6 6.8 36.2 1GE017 7.8    3 2 7.8 1.3 6.3 8.6 9.1 50.3 1GE018 7.8    3 2 7.8 1.3 6.3 8.6 9.1 50.3 2GE038 6.9 5.0 0.0 0.0 4 2 6.9 0.91 5.8 8.0 8.1 44.5 1GE019 7.8    3 2 7.8 1.3 6.1 8.4 9.1 50.6 1GE020 7.8    3 2 7.8 1.3 6.1 8.4 9.1 50.6 2GE039 6.94 5.36 0.0 0.0 4 2 6.9 0.91 5.9 8.2 8.1 44.8 3GE056 7.4 5.2 0 0 4 2 7.4   8.7 48.3 1GE021 8.2    3 2 8.2   9.6 52.6 2GE040 6.97 4.70 0.0 0.0 4 2 7.0 0.739 6.0 7.8 8.2 44.9 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

129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 3GE074 Jet A 1.935 16.3 2.361 1.940 0.663 0.163 769 3GE078 Jet A 1.935 16.3 2.410 1.997 0.667 0.163 779 1GE008 Jet A 1.92 17.1 2.379 1.915 0.643 0.212 838 3GE072 Jet A 1.935 16.3 2.281 1.875 0.641 0.163 751 3GE071 Jet A 1.935 16.3 2.281 1.875 0.641 0.163 751 3GE075 Jet A 1.935 16.3 2.361 1.940 0.663 0.163 769 3GE076 Jet A 1.935 16.3 2.361 1.940 0.663 0.163 769 1GE009 Jet A 1.92 17.1 2.487 1.975 0.660 0.215 859 3GE077 Jet A 1.935 16.3 2.361 1.940 0.663 0.163 769 3GE079 Jet A 1.935 16.3 2.410 1.997 0.667 0.163 779 1GE001 Jet A 1.93 18.7 1.736 1.431 0.4839 0.1728 648 1GE002 Jet A 1.93 18.7 1.812 1.502 0.494 0.176 667 1GE003 Jet A 1.93 18.7 1.736 1.431 0.4839 0.1728 648 1GE004 Jet A 1.93 18.7 1.812 1.502 0.494 0.176 667 1GE010 Jet A 1.93 17.1 2.145 1.795 0.615 0.150 709 1GE011 Jet A 1.93 17.1 2.145 1.795 0.615 0.150 709 1GE012 Jet A 1.93 17.1 2.254 1.885 0.641 0.150 731 1GE013 Jet A 1.93 17.1 2.254 1.885 0.641 0.150 731 1GE014 Jet A 1.94 15.3 2.400 1.953 0.636 0.199 822 2GE036 Jet A 1.94 15.3 2.453 1.989 0.651 0.201 835 1GE015 Jet A 1.94 15.3 2.117 1.745 0.580 0.189 753 1GE016 Jet A 1.94 15.3 2.117 1.745 0.580 0.189 753 2GE037 Jet A 1.94 15.3 2.152 1.771 0.590 0.192 765 1GE017 Jet A 1.94 15.3 2.457 2.003 0.649 0.202 838 1GE018 Jet A 1.94 15.3 2.457 2.003 0.649 0.202 838 2GE038 Jet A 1.94 15.3 2.516 2.041 0.662 0.203 851 1GE019 Jet A 1.94 15.3 2.581 2.082 0.687 0.207 871 1GE020 Jet A 1.94 15.3 2.581 2.082 0.687 0.207 871 2GE039 Jet A 1.94 15.3 2.580 2.096 0.672 0.205 866 3GE056 Jet A 1.94 15.3 2.630 2.106 0.691 0.22 897 1GE021 Jet A 1.94 15.3 2.507 1.953 0.655 0.205 840 2GE040 Jet A 1.94 15.3 2.444 1.989 0.651 0.201 835 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

129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 3GE074 0  0  97.73 97.91 292.3 301.3 .0127. 0216 3GE078 0  0  97.73 97.91 292.3 301.3 .0127. 0216 1GE008 0  0  98.3 100.4 270  296 .0027. 0103 3GE072 0  0  97.73 97.91 292.3 301.3 .0127. 0216 3GE071 0  0  97.73 97.91 292.3 301.3 .0127. 0216 3GE075 0  0  97.73 97.91 292.3 301.3 .0127. 0216 3GE076 0  0  97.73 97.91 292.3 301.3 .0127. 0216 1GE009 0  0  98.3 100.4 270  296 .0027. 0103 3GE077 0  0  97.73 97.91 292.3 301.3 .0127. 0216 3GE079 0  0  97.73 97.91 292.3 301.3 .0127. 0216 1GE001 0  0  99.15 100.46 280  301 .003. 015 1GE002 0  0  99.15 100.46 280  301 .003. 015 1GE003 0  0  99.15 100.46 280  301 .003. 015 1GE004 0  0  99.15 100.46 280  301 .003. 015 1GE010 0  0  99.08 99.78 275  277 .002 1GE011 0  0  99.08 99.78 275  277 .002 1GE012 0  0  99.08 99.78 275  277 .002 1GE013 0  0  99.08 99.78 275  277 .002 1GE014 0  0  97.40 97.82 287  296 .0084. 0140 2GE036 0  0  97.61 98.15 279 293 .00457. 00743 1GE015 0  0  97.40 97.82 287  296 .0084. 0140 1GE016 0  0  97.40 97.82 287  296 .0084. 0140 2GE037 0  0  97.61 98.15 279 293 .00457. 00743 1GE017 0  0  97.40 97.82 287  296 .0084. 0140 1GE018 0  0  97.40 97.82 287  296 .0084. 0140 2GE038 0  0  97.61 98.15 279 293 .00457. 00743 1GE019 0  0  97.40 97.82 287  296 .0084. 0140 1GE020 0  0  97.40 97.82 287  296 .0084. 0140 2GE039 0  0  97.61 98.15 279 293 .00457. 00743 3GE056 0  0  97.61 98.15 279 293 .0046. 0074 1GE021 0  0  97.40 97.82 287  296 .0084. 0140 2GE040 0  0  97.61 98.15 279 293 .00457. 00743 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 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 3GE074 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 3GE078 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 1GE008 GE Aircraft Engines Production Engine Test Production Test Cells M34 & M35 12 Oct 79 5 Dec 79 3GE072 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 3GE071 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 3GE075 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 3GE076 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 1GE009 GE Aircraft Engines Production Engine Test Production Test Cells M34 & M35 12 Oct 79 5 Dec 79 3GE077 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 3GE079 GE GE Development/ Production Test Operation Site IVD, Peebles, Ohio 28 Jul 87 29 Jul 87 1GE001 GE Aircraft Engines Production Engine Test Production Test Cells M34 & M35 16 Aug 79 19 Nov 79 1GE002 GE Aircraft Engines Production Engine Test Production Test Cells M34 & M35 16 Aug 79 19 Nov 79 1GE003 GE Aircraft Engines Production Engine Test Production Test Cells M34 & M35 16 Aug 79 19 Nov 79 1GE004 GE Aircraft Engines Production Engine Test Production Test Cells M34 & M35 16 Aug 79 19 Nov 79 1GE010 GE Aircraft Engines Production Engine Test Production Test Cells M35 11 Nov 83 12 Nov 83 1GE011 GE Aircraft Engines Production Engine Test Production Test Cells M35 11 Nov 83 12 Nov 83 1GE012 GE Aircraft Engines Production Engine Test Production Test Cells M35 11 Nov 83 12 Nov 83 1GE013 GE Aircraft Engines Production Engine Test Production Test Cells M35 11 Nov 83 12 Nov 83 1GE014 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE036 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 1GE015 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 1GE016 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE037 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 1GE017 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 1GE018 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE038 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 1GE019 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 1GE020 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE039 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 3GE056 GE CF6 Ecval Engineering Site IIIB, PTO, Peebles, Ohio, USA 13 Jan 95 17 Jan 95 1GE021 GE Aircraft Engines CF6 Evaluation Engineering Site IIIC, PTO, Peebles, Ohio 29 May 85 3 Jun 85 2GE040 GE CF6 Eval Engineering Site IIIB, PTO Peebles 13 Jan 95 17 Jan 95 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 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 3GE074 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 3GE078 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 1GE008 Ref Report no FAA EE 80 27 ( GE Report R80AEG420)

3GE072 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 3GE071 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 3GE075 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 3GE076 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 1GE009 Ref Report no FAA EE 80 27 ( GE Report R80AEG420)

3GE077 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 3GE079 1. Engine equipped with low emissions fuel nozzle config. 2. GE Report R87AEB559. 3. Engine 530375/ 001. 4. Asterisked idle emissions calculate 1GE001 Ref Report no FAA EE 80 27 ( GE Report R80AEG420)

1GE002 Ref Report no FAA EE 80 27 ( GE Report R80AEG420)

1GE003 Ref Report no FAA EE 80 27 ( GE Report R80AEG420)

1GE004 Ref Report no FAA EE 80 27 ( GE Report R80AEG420)

1GE010 1. Ref GE Report no R83AEB635. 2. Engine S/ N 580214. 3. Smoke from Engine S/ N 580005, report R81AEG513. 4. With approval of US FAA, idle p 1GE011 1. Ref GE Report no R83AEB635. 2. Engine S/ N 580214. 3. Smoke from Engine S/ N 580005, report R81AEG513. 4. With approval of US FAA, idle p 1GE012 1. Ref GE Report no R83AEB635. 2. Engine S/ N 580214. 3. Smoke from Engine S/ N 580005, report R81AEG513. 4. With approval of US FAA, idle p 1GE013 1. Ref GE Report no R83AEB635. 2. Engine S/ N 580214. 3. Smoke from Engine S/ N 580005, report R81AEG513. 4. With approval of US FAA, idle p 1GE014 1. Ref GE Report R84AEB152. 2. Engine S/ N's 690105 and 690005/ 2.

2GE036 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 1GE015 1. Ref GE Report R85AEB486. 2. Engine S/ N's 690105 and 690005/ 2.

1GE016 1. Ref GE Report R85AEB486. 2. Engine S/ N's 690105 and 690005/ 2.

2GE037 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 1GE017 1. Ref GE Report R86AEB143. 2. Engine S/ N's 690105 and 690005/ 2.

1GE018 1. Ref GE Report R86AEB143. 2. Engine S/ N's 690105 and 690005/ 2.

2GE038 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 1GE019 1. Ref GE Report R84AEB152. 2. Engine S/ N's 690105 and 690005/ 2.

1GE020 1. Ref GE Report R84AEB152. 2. Engine S/ N's 690105 and 690005/ 2.

2GE039 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 combustor 3GE056 1. GE Report TM95 17. 2. Engine S/ N 704/ 223 & 704/ 234 3. 1862M39 combustor 1GE021 1. Ref GE Report R90AEB379. Engine S/ N's 690105 and 690005/ 2.

2GE040 1. Ref GE report TM95 17. 2. Engine S/ N 704/ 233 & 704/ 234 3. 1862M39 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 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 ted at normal idle setting rather than 7%.

ted at normal idle setting rather than 7%.

ted at normal idle setting rather than 7%.

ted at normal idle setting rather than 7%.

ted at normal idle setting rather than 7%.

ted at normal idle setting rather than 7%.

ted at normal idle setting rather than 7%.

ted at normal idle setting rather than 7%.

e power data were only acquired at the engine design setting of 3.69%.

e power data were only acquired at the engine design setting of 3.69%.

e power data were only acquired at the engine design setting of 3.69%.

e power data were only acquired at the engine design setting of 3.69%.

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 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 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 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 CF6 80C2B1 TF 5.1 30.08 249.0 2GE041 CF6 80C2B1 1862M39 TF 5.1 29.53 249.01 1GE023 CF6 80C2B1F TF 5.1 30.13 254.3 1GE024 CF6 80C2B1F TF 5.1 30.13 254.3 2GE045 CF6 80C2B1F 1862M39 TF 5.1 30.13 254.26 1GE025 CF6 80C2B2 TF 5.1 27.74 231.1 2GE042 CF6 80C2B2 1862M39 TF 5.1 27.53 231.08 1GE026 CF6 80C2B2F TF 5.1 27.52 231.35 2GE046 CF6 80C2B2F 1862M39 TF 5.1 27.6 231.35 1GE027 CF6 80C2B4 TF 5.1 30.36 254.35 2GE043 CF6 80C2B4 1862M39 TF 5.1 30.14 254.35 1GE028 CF6 80C2B4F TF 5.1 30.17 254.79 2GE047 CF6 80C2B4F 1862M39 TF 5.1 30.22 254.79 3GE057 CF6 80C2B5F 1862M39 TF 5.1 32.82 272.53 1GE029 CF6 80C2B6 TF 5.1 31.56 267.2 2GE044 CF6 80C2B6 1862M39 TF 5.1 31.66 267.20 1GE030 CF6 80C2B6F TF 5.1 31.79 267.03 2GE048 CF6 80C2B6F 1862M39 TF 5.1 31.72 267.03 2GE054 CF6 80C2B7F TF 5.1 31.79 267.03 2GE055 CF6 80C2B7F 1862M39 TF 5.1 31.72 267.03 3GE058 CF6 80C2B8FA 1862M39 TF 5.1 31.71 267.02 1GE031 CF6 80C2D1F TF 5.1 32.86 269.96 2GE049 CF6 80C2D1F 1862M39 TF 5.1 32.05 269.96 1GE032 CF6 80E1A1 TF 5.1 32.44 281.5 2GE050 CF6 80E1A1 1862M39 TF 5.1 32.46 281.53 1GE033 CF6 80E1A2 TF 5.1 33.08 287.0 2GE051 CF6 80E1A2 1862M39 TF 5.1 33.1 287.04 5GE085 CF6 80E1A3 Standard TF 5.1 35.7 304.8 4GE080 CF6 80E1A4 Standard TF 5.1 34.5 297.44 4GE081 CF6 80E1A4 Low emissions TF 5.1 34.5 297.44 2GE052 GE90 76B DAC I TF 8.5 35.30 360.62 3GE062 GE90 76B DAC II TF 8.59 35.1 360.62 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

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  x    x   x x

2GE041  x    x   x

1GE023  x  x 1GE024 x   x x

1GE024   x   x   x x

2GE045  x    x   x

1GE025  x    x   x x

2GE042  x    x   x

1GE026  x    x   x x

2GE046  x    x   x

1GE027  x    x   x x

2GE043  x    x   x

1GE028  x    x   x x

2GE047  x    x   x

3GE057  x    x   x

1GE029  x    x   x x

2GE044  x    x   x

1GE030  x    x   x x

2GE048  x    x   x

2GE054  x    x   x x

2GE055  x    x   x

3GE058  x    x   x

1GE031  x    x   x x

2GE049  x    x   x

1GE032  x    x   x

2GE050  x    x   x x

1GE033  x    x   x

2GE051  x    x   x x

5GE085  x    x   x

4GE080  x    x   x

4GE081  x    x   x x

2GE052   x   x   x x

3GE062  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)

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 0.08 0.09 0.21 9.46 3 2 11.89 1.31 10.77 13.2 15.5 78.9 2953 2GE041 0.05 0.05 0.12 1.71 4 2 2.25 0.22 2.12 2.65 2.9 14.9 561 1GE023 0.08 0.09 0.20 9.68 3 2 12.43 1.30 11.31 13.70 16.2 82.5 3157 1GE024 0.08 0.09 0.20 9.88 3 2 12.30 1.25 11.22 13.48 16.0 81.7 3127 2GE045 0.05 0.05 0.11 1.54 4 2 2.01 0.223 1.87 2.36 2.6 13.3 513 1GE025 0.08 0.10 0.22 11.17 3 2 14.75 1.25 13.68 16.01 19.2 97.9 3407 2GE042 0.05 0.05 0.12 1.97 4 2 2.67 0.34 2.43 3.15 3.5 17.7 617 1GE026 0.08 0.09 0.23 11.80 3 2 14.99 1.24 13.96 16.37 19.5 99.5 3467 2GE046 0.05 0.05 0.12 1.86 4 2 2.49 0.279 2.3 2.89 3.2 16.5 579 1GE027 0.08 0.09 0.21 9.74 3 2 12.15 1.27 11.05 13.37 15.8 80.7 3088 2GE043 0.05 0.05 0.12 1.59 4 2 2.10 0.235 1.96 2.48 2.7 13.9 535 1GE028 0.08 0.09 0.20 10.37 3 2 12.47 1.19 11.44 13.52 16.2 82.8 3176 2GE047 0.05 0.05 0.11 1.54 4 2 2.00 0.223 1.86 2.36 2.6 13.3 513 3GE057 0.05 0.05 0.11 1.31 4 2 1.67   2.2 11.2 459 1GE029 0.07 0.08 0.20 8.99 3 2 11.12 1.30 10.02 12.49 14.5 73.8 2966 2GE044 0.04 0.05 0.11 1.48 4 2 1.90 0.209 1.76 2.24 2.5 12.6 509 1GE030 0.07 0.08 0.19 9.74 3 2 11.40 1.19 10.37 12.53 14.8 75.7 3041 2GE048 0.05 0.05 0.11 1.43 4 2 1.83 0.207 1.68 2.16 2.4 12.1 490 2GE054 0.07 0.08 0.19 9.74 3 2 11.4 1.19 10.37 12.53 14.8 75.5 3041 2GE055 0.05 0.05 0.11 1.43 4 2 1.83 0.207 1.68 2.16 2.4 12.1 490 3GE058 0.05 0.05 0.11 1.41 4 2 1.83   2.4 12.2 489 1GE031 0.07 0.08 0.20 9.03 3 2 10.46 1.21 9.43 11.73 13.6 69.4 2822 2GE049 0.04 0.05 0.11 1.38 4 2 1.76 0.196 1.62 2.07 2.3 11.7 478 1GE032 0.05 0.07 0.14 9.68 3 2 12.07 5.0 7.5 16.4 15.7 80.1 3463 2GE050 0.05 0.04 0.11 1.30 4 2 1.76 0.186 1.44 1.88 2.3 11.7 494 1GE033 0.05 0.07 0.14 9.37 3 2 11.78 4.8 7.4 16.0 15.3 78.2 3384 2GE051 0.04 0.04 0.11 1.25 4 2 1.68 0.187 1.36 1.80 2.2 11.2 480 5GE085 0.07 0.07 0.18 9.53 11 6 11.28   12.6 64.3 3438 4GE080 0.06 0.07 0.18 10.35 3 2 12.52   16.3 83.1 3726 4GE081 0.04 0.04 0.09 0.92 7 3 1.20   1.4 7.1 359 2GE052 0.07 0.06 0.67 3.42 3 3 4.78  4.18 5.28 5.6 28.5 1753 3GE062 0.04 0.04 0.07 0.57 5 3 0.77  0.45 1.08 0.9 4.6 279 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)