. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 MACT proposal 2003 Region: System Page: 2. 29 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.            TVA CT 0612 000000 00 4. 4. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 TVA CT 0614 000000 00 291. 291. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 TVA CT 0622 000000 00 3741. 3741. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 TVA CT 0623 000000 00 1500. 1500. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 TVA MSCT 1612 000000 00 20. 20. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 TVA MSCT 1614 000000 00 9. 9. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 TVA MSCT 1622 000000 00 1903. 1903. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SOU CT 0611 000000 00 3. 3. 0. 0.0 91.0 2. 14.1 94.1 2. 5.9 92.3 SOU CT 0613 000000 00 3. 3. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SOU CT 0614 000000 00 81. 81. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SOU CT 0622 000000 00 7042. 7042. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SOU CT 0623 000000 00 2277. 2277. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SOU CT 0624 000000 00 673. 673. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SOU MSCT 1613 000000 00 20. 20. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SOU MSCT 1614 000000 00 80. 80. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SOU MSCT 1622 000000 00 640. 640. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SOU MSCT 1624 000000 00 153. 153. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 ENTG CT 1012 000000 00 66. 66. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 ENTG CT 1014 000000 00 78. 78. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 ENTG CT 1022 000000 00 1476. 1476. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 ENTG CT 1023 000000 00 216. 216. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 ENTGMSCT 1614 000000 00 11. 11. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 ENTGMSCT 1622 000000 00 613. 613. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 ENTGMOCT 0513 000000 00 45. 45. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 ENTGMOCT 0522 000000 00 290. 290. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPN CT 1711 000000 00 17. 17. 0. 0.0 91.0 3. 4.8 94.1 3. 2.0 92.3 SPPN CT 1712 000000 00 214. 214. 0. 0.0 91.0 37. 4.7 94.1 37. 2.0 92.3 SPPN CT 1713 000000 00 90. 90. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPN CT 1714 000000 00 493. 493. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPN CT 1722 000000 00 353. 353. 0. 0.0 91.0 61. 4.7 94.1 61. 2.0 92.3 SPPN CT 1723 000000 00 637. 637. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPN CT 1724 000000 00 81. 81. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPNMOCT 0511 000000 00 2. 2. 0. 0.0 91.0 0. 4.7 94.1 0. 2.0 92.3 SPPNMOCT 0512 000000 00 103. 103. 0. 0.0 91.0 18. 4.7 94.1 18. 2.0 92.3 SPPNMOCT 0513 000000 00 11. 11. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPNMOCT 0514 000000 00 309. 309. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPNMOCT 0522 000000 00 1320. 1320. 0. 0.0 91.0 127. 2.6 94.1 127. 1.1 92.3 SPPNMOCT 0523 000000 00 733. 733. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPNMOCT 0524 000000 00 288. 288. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPS CT 0812 000000 00 6. 6. 0. 0.0 91.0 1. 4.7 94.1 1. 2.0 92.3 SPPS CT 0814 000000 00 35. 35. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPS CT 0823 000000 00 66. 66. 0. 0.0 91.0 11. 4.7 94.1 11. 2.0 92.3 SPPS CT 0824 000000 00 244. 244. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPS CT 1012 000000 00 9. 9. 0. 0.0 91.0 2. 4.7 94.1 2. 2.0 92.3 SPPS CT 1014 000000 00 76. 76. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPS CT 1022 000000 00 457. 457. 0. 0.0 91.0 79. 4.7 94.1 79. 2.0 92.3 SPPS CT 3612 000000 00 11. 11. 0. 0.0 91.0 2. 4.7 94.1 2. 2.0 92.3 SPPS CT 3614 000000 00 161. 161. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPS CT 3622 000000 00 512. 512. 0. 0.0 91.0 88. 4.7 94.1 88. 2.0 92.3 SPPS CT 3623 000000 00 53. 53. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPS CT 3624 000000 00 162. 162. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPSMSCT 1614 000000 00 15. 15. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPSTXCT 2214 000000 00 40. 40. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPSTXCT 2322 000000 00 100. 100. 0. 0.0 91.0 17. 4.7 94.1 17. 2.0 92.3 SPPSTXCT 2512 000000 00 3. 3. 0. 0.0 91.0 1. 4.7 94.1 1. 2.0 92.3 SPPSTXCT 2513 000000 00 5. 5. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPSTXCT 2514 000000 00 47. 47. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 MACT proposal 2003 Region: System Page: 2. 30 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.            SPPSTXCT 2524 000000 00 48. 48. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 SPPSTXCT 2722 000000 00 95. 95. 0. 0.0 91.0 16. 4.7 94.1 16. 2.0 92.3 SPPSTXCT 3513 000000 00 2. 2. 0. 0.0 91.0 0. 4.7 94.1 0. 2.0 92.3 SPPSTXCT 3514 000000 00 43. 43. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 CALI CT 0812 000000 00 3. 3. 0. 0.0 91.0 1. 4.7 94.1 1. 2.0 92.3 CALI CT 0813 000000 00 203. 203. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 CALI CT 0814 000000 00 550. 550. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 CALI CT 0821 000000 00 48. 48. 167. 68.2 91.0 124. 70.6 94.1 291. 69.2 92.3 CALI CT 0822 000000 00 2209. 2209. 189. 1.7 91.0 380. 4.7 94.1 570. 2.9 92.3 CALI CT 0823 000000 00 927. 927. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 CALI CT 0824 000000 00 542. 542. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 PNW CT 0714 000000 00 0. 0. 0. N/ A 91.0 0. N/ A 94.1 0. N/ A 92.3 PNW CT 0722 000000 00 1151. 1151. 2881. 49.2 91.0 3978. 94.1 94.1 6859. 68.0 92.3 PNW CT 0724 000000 00 0. 0. 0. N/ A 91.0 0. N/ A 94.1 0. N/ A 92.3 PNW CT 0812 000000 00 3. 3. 14. 91.0 91.0 10. 94.1 94.1 24. 92.3 92.3 PNW CT 0814 000000 00 0. 0. 0. N/ A 91.0 0. N/ A 94.1 0. N/ A 92.3 PNW CT 0822 000000 00 371. 371. 1717. 91.0 91.0 1282. 94.1 94.1 3000. 92.3 92.3 AZNM CT 0813 000000 00 16. 16. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 AZNM CT 0814 000000 00 288. 288. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 AZNM CT 0822 000000 00 1747. 1747. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 AZNM CT 0823 000000 00 752. 752. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 AZNM CT 0824 000000 00 722. 722. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 AZNMTXCT 3523 000000 00 69. 69. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 RMPA CT 0713 000000 00 68. 68. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 RMPA CT 0714 000000 00 10. 10. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 RMPA CT 0722 000000 00 48. 48. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 RMPA CT 0723 000000 00 42. 42. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 RMPA CT 0812 000000 00 10. 10. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 RMPA CT 0814 000000 00 121. 121. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 RMPA CT 0822 000000 00 1444. 1444. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 RMPA CT 0823 000000 00 84. 84. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 RMPA CT 0824 000000 00 235. 235. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 RMPANECT 1412 000000 00 4. 4. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 RMPANECT 1414 000000 00 11. 11. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 NWPE CT 0712 000000 00 0. 0. 0. N/ A 91.0 0. N/ A 94.1 0. N/ A 92.3 NWPE CT 0714 000000 00 0. 0. 0. N/ A 91.0 0. N/ A 94.1 0. N/ A 92.3 NWPE CT 0722 000000 00 160. 160. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 NWPE CT 0811 000000 00 14. 14. 0. 0.0 91.0 2. 4.7 94.1 2. 2.0 92.3 NWPE CT 0812 000000 00 53. 53. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 NWPE CT 0814 000000 00 0. 0. 0. N/ A 91.0 0. N/ A 94.1 0. N/ A 92.3 NWPE CT 0822 000000 00 928. 928. 0. 0.0 91.0 0. 0.0 94.1 0. 0.0 92.3 NWPE CT 0824 000000 00 0. 0. 0. N/ A 91.0 0. N/ A 94.1 0. N/ A 92.3 NENG CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENGCTCT 32 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENGCTCT 32 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENGCTACT 32 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENGCTACT 32 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACT proposal 2003 Region: System Page: 2. 31 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.            DSNY ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NYC CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NYC CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NYC ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NYC ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 LILC CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 LILC CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 LILC ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 LILC ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPPMOCT 5 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPPMOCT 5 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPPMOACT 5 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPPMOACT 5 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS CT 8 ( a) 143. 143. 0. 0.0 92.3 24. 4.6 92.3 24. 1.9 92.3 WUMS CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANOMOCT 5 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANOMOCT 5 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANOMOACT 5 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANOMOACT 5 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPNMOCT 5 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPNMOCT 5 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPNMOACT 5 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPNMOACT 5 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXCT 19 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXCT 19 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXACT 19 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXACT 19 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACT proposal 2003 Region: System Page: 2. 32 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.            RMPA CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACE CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACE CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACE ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACE ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACS CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACS CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACS ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACS ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 FRCC CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 FRCC CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 FRCC ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 FRCC ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACANCCT 6 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACANCCT 6 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACANCACT 6 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACANCACT 6 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACT proposal 2003 Region: System Page: 2. 33 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.            TVA CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTGMOCT 5 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTGMOCT 5 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTGMOACT 5 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTGMOACT 5 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU CT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU CT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU ACT 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU ACT 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU CT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU CT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU ACT 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU ACT 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0            Turbine 11 130486. 130486. 7706. 1.2 91.0 11648. 2.4 94.1 19354. 1.7 92.3 MECS BIOMS00 42 000000 00 161. 161. 698. 85.2 85.2 539. 91.2 91.2 1237. 87.7 87.7 ECAO BIOMS00 42 000000 00 84. 84. 364. 85.2 85.2 281. 91.2 91.2 645. 87.7 87.7 MACE BIOMS00 44 000000 00 8. 8. 35. 85.2 85.2 27. 91.2 91.2 61. 87.7 87.7 MACW BIOMS00 44 000000 00 17. 17. 74. 85.2 85.2 57. 91.2 91.2 131. 87.7 87.7 WUMS BIOMS00 45 000000 00 12. 12. 52. 85.2 85.2 40. 91.2 91.2 92. 87.7 87.7 MANO BIOMS00 45 000000 00 1. 1. 4. 85.2 85.2 3. 91.2 91.2 8. 87.7 87.7 MAPP BIOMS00 46 000000 00 163. 163. 644. 77.7 85.2 409. 68.4 91.2 1054. 73.8 87.7 UPNY BIOMS00 47 000000 00 18. 18. 78. 85.2 85.2 60. 91.2 91.2 138. 87.7 87.7 NENG BIOMS00 48 000000 00 309. 309. 962. 61.2 85.2 155. 13.7 91.2 1117. 41.3 87.7 FRCC BIOMS00 49 000000 00 54. 54. 234. 85.2 85.2 181. 91.2 91.2 415. 87.7 87.7 VACA BIOMS00 50 000000 00 47. 47. 204. 85.2 85.2 157. 91.2 91.2 361. 87.7 87.7 TVA BIOMS00 50 000000 00 1. 1. 4. 85.2 85.2 3. 91.2 91.2 8. 87.7 87.7 ENTG BIOMS00 51 000000 00 10. 10. 43. 85.2 85.2 33. 91.2 91.2 77. 87.7 87.7 CALI BIOMS00 54 000000 00 432. 432. 1872. 85.2 85.2 1447. 91.2 91.2 3319. 87.7 87.7 PNW BIOMS00 52 000000 00 6. 6. 26. 85.2 85.2 20. 91.2 91.2 46. 87.7 87.7 AZNM BIOMS00 53 000000 00 18. 18. 78. 85.2 85.2 60. 91.2 91.2 138. 87.7 87.7 RMPA BIOMS00 53 000000 00 1. 1. 4. 85.2 85.2 1. 13.7 91.2 5. 55.2 87.7 NWPE BIOMS00 52 000000 00 5. 5. 22. 85.2 85.2 13. 68.4 91.2 34. 78.1 87.7 NENG BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NYC BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 LILC BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXBIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACT proposal 2003 Region: System Page: 2. 34 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.            MECS BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACE BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACS BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 FRCC BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU BIOCC0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0            Biomass 12 1347. 1347. 5398. 78.8 85.2 3488. 70.5 91.2 8886. 75.3 87.7 CALI GEO 00 000000 00 2665. 2665. 11344. 83.7 83.7 8966. 91.6 91.6 20310. 87.0 87.0 PNW GEO 00 000000 00 8. 8. 34. 83.7 83.7 27. 91.6 91.6 61. 87.0 87.0 AZNM GEO 00 000000 00 29. 29. 123. 83.7 83.7 98. 91.6 91.6 221. 87.0 87.0 NWPE GEO 00 000000 00 241. 241. 1026. 83.7 83.7 811. 91.6 91.6 1837. 87.0 87.0 RMPA GEOR 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE GEOJ10 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE GEOJ20 ( a) 0. 0. 0. N/ A 87.2 0. N/ A 87.2 0. N/ A 87.2 NWPE GEOJ30 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE GEOJ40 ( a) 0. 0. 0. N/ A 87.2 0. N/ A 87.2 0. N/ A 87.2 NWPE GEOJ50 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM GEOA 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM GEOA20 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW GEOP 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW GEOP20 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW GEOP30 ( a) 0. 0. 0. N/ A 87.2 0. N/ A 87.2 0. N/ A 87.2 CALI GEOC 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI GEOC20 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI GEOC30 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0            Geothermal 13 2943. 2943. 12528. 83.7 83.7 9901. 91.6 91.6 22429. 87.0 87.0 MECS LFGAS00 000000 00 5. 5. 22. 87.9 87.9 17. 92.9 92.9 39. 90.0 90.0 ECAO LFGAS00 000000 00 12. 12. 54. 87.9 87.9 41. 92.9 92.9 95. 90.0 90.0 ERCT LFGAS00 000000 00 67. 67. 300. 87.9 87.9 229. 92.9 92.9 528. 90.0 90.0 MACE LFGAS00 000000 00 24. 24. 107. 87.9 87.9 82. 92.9 92.9 189. 90.0 90.0 MACW LFGAS00 000000 00 1. 1. 4. 87.9 87.9 3. 92.9 92.9 8. 90.0 90.0 MACS LFGAS00 000000 00 4. 4. 18. 87.9 87.9 14. 92.9 92.9 32. 90.0 90.0 WUMS LFGAS00 000000 00 14. 14. 63. 87.9 87.9 48. 92.9 92.9 110. 90.0 90.0 MANO LFGAS00 000000 00 38. 38. 170. 87.9 87.9 130. 92.9 92.9 300. 90.0 90.0 MAPP LFGAS00 000000 00 11. 11. 49. 87.9 87.9 38. 92.9 92.9 87. 90.0 90.0 UPNY LFGAS00 000000 00 6. 6. 27. 87.9 87.9 20. 92.9 92.9 47. 90.0 90.0 NENG LFGAS00 000000 00 18. 18. 81. 87.9 87.9 61. 92.9 92.9 142. 90.0 90.0 FRCC LFGAS00 000000 00 2. 2. 9. 87.9 87.9 7. 92.9 92.9 16. 90.0 90.0 VACA LFGAS00 000000 00 25. 25. 112. 87.9 87.9 85. 92.9 92.9 197. 90.0 90.0 TVA LFGAS00 000000 00 2. 2. 9. 87.9 87.9 7. 92.9 92.9 16. 90.0 90.0 SOU LFGAS00 000000 00 9. 9. 40. 87.9 87.9 31. 92.9 92.9 71. 90.0 90.0 ENTG LFGAS00 000000 00 6. 6. 27. 87.9 87.9 20. 92.9 92.9 47. 90.0 90.0 SPPS LFGAS00 000000 00 9. 9. 40. 87.9 87.9 31. 92.9 92.9 71. 90.0 90.0 CALI LFGAS00 000000 00 216. 216. 966. 87.9 87.9 737. 92.9 92.9 1703. 90.0 90.0 PNW LFGAS00 000000 00 21. 21. 94. 87.9 87.9 72. 92.9 92.9 166. 90.0 90.0 AZNM LFGAS00 000000 00 11. 11. 49. 87.9 87.9 38. 92.9 92.9 87. 90.0 90.0 RMPA LFGAS00 000000 00 1. 1. 4. 87.9 87.9 3. 92.9 92.9 8. 90.0 90.0 NENG LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACT proposal 2003 Region: System Page: 2. 35 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.            MAPP LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS LG 0 ( a) 0. 0. 0. N/ A 85.0 0. N/ A 85.0 0. N/ A 85.0 MANO LG 0 ( a) 0. 0. 0. N/ A 85.0 0. N/ A 85.0 0. N/ A 85.0 SPPS LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXLG 19 ( a) 0. 0. 0. N/ A 85.0 0. N/ A 85.0 0. N/ A 85.0 RMPA LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM LG 0 ( a) 0. 0. 0. N/ A 85.0 0. N/ A 85.0 0. N/ A 85.0 PNW LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS LG 0 ( a) 0. 0. 0. N/ A 85.0 0. N/ A 85.0 0. N/ A 85.0 MACE LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW LG 0 ( a) 0. 0. 0. N/ A 85.0 0. N/ A 85.0 0. N/ A 85.0 MACS LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 FRCC LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA LG 0 ( a) 0. 0. 0. N/ A 85.0 0. N/ A 85.0 0. N/ A 85.0 TVA LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG LG 0 ( a) 0. 0. 0. N/ A 85.0 0. N/ A 85.0 0. N/ A 85.0 SOU LG 0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0            Landfill Gas 14 502. 502. 2245. 87.9 87.9 1712. 92.9 92.9 3958. 90.0 90.0 MECS WIND 00 000000 00 0. 1. 2. 30.7 78.0 1. 23.9 85.2 2. 27.8 81.0 ECAO WIND 00 000000 00 105. 105. 164. 30.7 78.0 92. 23.9 85.2 256. 27.8 81.0 ERCT WIND 00 000000 00 628. 703. 1465. 41.0 78.0 823. 31.9 85.2 2288. 37.1 81.0 MACE WIND 00 000000 00 14. 14. 20. 27.9 78.0 11. 21.7 85.2 31. 25.3 81.0 MACW WIND 00 000000 00 3. 10. 17. 33.5 78.0 10. 26.0 85.2 27. 30.4 81.0 WUMS WIND 00 000000 00 0. 13. 20. 30.7 78.0 11. 23.9 85.2 32. 27.8 81.0 MANO WIND 00 000000 00 52. 52. 88. 33.1 78.0 49. 25.7 85.2 137. 30.0 81.0 MAPP WIND 00 000000 00 569. 857. 1443. 33.1 78.0 809. 25.7 85.2 2252. 30.0 81.0 UPNY WIND 00 000000 00 183. 194. 87. 8.8 78.0 49. 6.9 85.2 136. 8.0 81.0 DSNY WIND 00 000000 00 64. 64. 29. 8.8 78.0 16. 6.9 85.2 45. 8.0 81.0 NYC WIND 00 000000 00 59. 59. 27. 8.8 78.0 15. 6.9 85.2 41. 8.0 81.0 LILC WIND 00 000000 00 36. 36. 16. 8.8 78.0 9. 6.9 85.2 25. 8.0 81.0 NENG WIND 00 000000 00 30. 31. 14. 8.8 78.0 8. 6.9 85.2 22. 8.0 81.0 VACA WIND 00 000000 00 14. 14. 20. 27.9 78.0 11. 21.7 85.2 31. 25.3 81.0 TVA WIND 00 000000 00 1. 2. 2. 19.5 78.0 1. 15.2 85.2 3. 17.7 81.0 ENTG WIND 00 000000 00 37. 57. 57. 19.5 78.0 32. 15.2 85.2 88. 17.7 81.0 SPPS WIND 00 000000 00 66. 66. 66. 19.5 78.0 37. 15.2 85.2 102. 17.7 81.0 CALI WIND 00 000000 00 995. 1931. 4635. 47.2 78.0 2599. 36.7 85.2 7234. 42.8 81.0 PNW WIND 00 000000 00 398. 412. 185. 8.8 78.0 104. 6.9 85.2 290. 8.0 81.0 AZNM WIND 00 000000 00 49. 49. 102. 41.0 78.0 57. 31.9 85.2 159. 37.1 81.0 RMPA WIND 00 000000 00 212. 270. 648. 47.2 78.0 363. 36.7 85.2 1011. 42.8 81.0 NWPE WIND 00 000000 00 134. 138. 62. 8.8 78.0 35. 6.9 85.2 97. 8.0 81.0 NENG WIN610 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG WIN620 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG WIN630 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACT proposal 2003 Region: System Page: 2. 36 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.            UPNY WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXWIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXWIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXWIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA WIN610 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA WIN620 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA WIN630 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE WIN610 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE WIN620 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE WIN630 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM WIN610 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM WIN620 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM WIN630 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW WIN610 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW WIN620 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW WIN630 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACT proposal 2003 Region: System Page: 2. 37 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.            PNW WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI WIN610 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI WIN620 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI WIN630 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACE WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACE WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACE WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACS WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACS WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACS WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA WIN610 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA WIN620 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA WIN630 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA WIN610 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA WIN620 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA WIN630 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU WIN610 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU WIN620 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACT proposal 2003 Region: System Page: 2. 38 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.            SOU WIN630 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU WIN510 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU WIN520 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU WIN530 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU WIN410 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU WIN420 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU WIN430 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0            Wind 15 3649. 5078. 9168. 35.5 78.0 5143. 27.6 85.2 14310. 32.2 81.0 MACE FCELL00 000000 00 15. 15. 0. 0.0 89.3 8. 13.9 92.7 8. 5.8 90.7 UPNY FCELL00 000000 00 1. 1. 0. 0.0 89.3 0. 4.6 92.7 0. 1.9 90.7 NENG FCELL00 000000 00 1. 1. 0. 4.5 89.3 1. 13.9 92.7 1. 8.4 90.7 NENG FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NENG FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NYC FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NYC FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 LILC FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 LILC FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS FC 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS FC 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN FC 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN FC 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPNMOFC 5 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPNMOFC 5 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXFC 19 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXFC 19 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA FC 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA FC 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE FC 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE FC 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM FC 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM FC 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW FC 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW FC 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI FC 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI FC 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACE FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACE FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACS FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACS FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACT proposal 2003 Region: System Page: 2. 39 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.            FRCC FC 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 FRCC FC 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG FC 8 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG FC 8 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU FC 1 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU FC 1 ( b) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0            Fuel Cell 16 17. 17. 0. 0.3 89.3 8. 13.3 92.7 9. 5.7 90.7 ERCT SOLAR00 000000 00 0. 1. 0. 5.5 78.0 0. 5.5 85.2 0. 5.5 81.0 CALI SOLAR00 000000 00 165. 324. 516. 31.3 78.0 274. 23.0 85.2 790. 27.8 81.0 AZNM SOLAR00 000000 00 61. 61. 17. 5.5 78.0 12. 5.5 85.2 29. 5.5 81.0 RMPA SOLAR00 000000 00 3. 3. 5. 31.3 78.0 3. 23.0 85.2 7. 27.8 81.0 NWPE SOLAR00 000000 00 24. 24. 38. 31.3 78.0 20. 23.0 85.2 59. 27.8 81.0 NENG SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 UPNY SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 DSNY SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NYC SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 LILC SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP SLRTH0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MAPP SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 WUMS SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO SLRTH0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MANO SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS SLRTH0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPS SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN SLRTH0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SPPN SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXSLRTH0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ERCTTXSLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA SLRTH0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 RMPA SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE SLRTH0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 NWPE SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM SLRTH0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 AZNM SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW SLRTH0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 PNW SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 CALI SLRTH0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ECAO SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MECS SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACE SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACW SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 MACS SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 FRCC SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 VACA SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 TVA SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG SLRTH0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 ENTG SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0 SOU SLRPV0 ( a) 0. 0. 0. N/ A 0.0 0. N/ A 0.0 0. N/ A 0.0            Solar 17 253. 413. 577. 27.4 78.0 309. 20.4 85.2 886. 24.5 81.0 MACT proposal 2003 Region: System Page: 2. 40 Resource, Purchases and Sales by Season and Plant Year: 2005 Capacity WINTER SUMMER Total Plant Name R. M. Dispatch [ GWh] C. F. Avail . [ GWh] C. F. Avail. [ GWh] C. F. Avail.


[Federal Register Volume 77, Number 59 (Tuesday, March 27, 2012)]
[Rules and Regulations]
[Pages 18099-18102]
[FR Doc No: 2012-7280]

========================================================================
Rules and Regulations
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by the Superintendent of Documents.
Prices of new books are listed in the first FEDERAL REGISTER issue of each
week.

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Federal Register / Vol. 77, No. 59 / Tuesday, March 27, 2012 / Rules
and Regulations

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 25

[Docket No. FAA-2012-0344; Special Conditions No. 25-461-SC]

Special Conditions: Dassault Aviation, Model Falcon 7X Airplanes;
Seats With Inflatable Shoulder Straps

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final special conditions; request for comments.

-----------------------------------------------------------------------

SUMMARY: These special conditions are issued for the Dassault Aviation
Model Falcon 7X airplane. This airplane will have a novel or unusual
design feature associated with seats with inflatable shoulder straps.
The applicable airworthiness regulations do not contain adequate or
appropriate safety standards for this design feature. These special
conditions contain the additional safety standards that the
Administrator considers necessary to establish a level of safety
equivalent to that established by the existing airworthiness standards.

DATES: The effective date of these special conditions is March 19,
2012. We must receive your comments by May 11, 2012.

ADDRESSES: Send comments identified by docket number FAA-2012-0344
using any of the following methods:
     Federal eRegulations Portal: Go to http://www.regulations.gov and follow the online instructions for sending your
comments electronically.
     Mail: Send comments to Docket Operations, M-30, U.S.
Department of Transportation (DOT), 1200 New Jersey Avenue SE., Room
W12-140, West Building Ground Floor, Washington, DC, 20590-0001.
     Hand Delivery or Courier: Take comments to Docket
Operations in Room W12-140 of the West Building Ground Floor at 1200
New Jersey Avenue SE., Washington, DC, between 8 a.m. and 5 p.m.,
Monday through Friday, except federal holidays.
     Fax: Fax comments to Docket Operations at<PHONE_NUMBER>.
    Privacy: The FAA will post all comments it receives, without
change, to http://www.regulations.gov/, including any personal
information the commenter provides. Using the search function of the
docket web site, anyone can find and read the electronic form of all
comments received into any FAA docket, including the name of the
individual sending the comment (or signing the comment for an
association, business, labor union, etc.). DOT's complete Privacy Act
Statement can be found in the Federal Register published on April 11,
2000 (65 FR 19477-19478), as well as at http://DocketsInfo.dot.gov.
    Docket: Background documents or comments received may be read at
http://www.regulations.gov at any time. Follow the online instructions
for accessing the docket or go to the Docket Operations in Room W12-140
of the West Building Ground Floor at 1200 New Jersey Avenue SE.,
Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday,
except federal holidays.

FOR FURTHER INFORMATION CONTACT: Dan Jacquet, FAA, Airframe and Cabin
Safety Branch, ANM-115, Transport Airplane Directorate, Aircraft
Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057-
3356; telephone<PHONE_NUMBER>; facsimile<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: The FAA has determined that notice of, and
opportunity for prior public comment on, these special conditions are
impracticable because these procedures would significantly delay
issuance of the design approval and thus delivery of the affected
aircraft. In addition, the substance of these special conditions has
been subject to the public comment process in several prior instances
with no substantive comments received. The FAA therefore finds that
good cause exists for making these special conditions effective upon
issuance.

Comments Invited

    We invite interested people to take part in this rulemaking by
sending written comments, data, or views. The most helpful comments
reference a specific portion of the special conditions, explain the
reason for any recommended change, and include supporting data.
    We will consider all comments we receive by the closing date for
comments. We may change these special conditions based on the comments
we receive.

Background

    On March 15, 2011, Dassault Aviation applied for a change to Type
Certificate No. A59NM to install an inflatable restraint system on side
facing divans in Dassault Aviation Model Falcon 7X airplanes (hereafter
referred to as ``Falcon 7X''). The Falcon 7X is a 19-passenger,
transport category airplane powered by three aft-mounted Pratt &
Whitney PW307A high-bypass-ratio turbofan engines. Maximum takeoff
weight is 69,000 pounds, and maximum certified altitude is 51,000 feet
with a range of 5,700 nautical miles.
    The inflatable restraint system is designed to limit occupant
forward excursion in the event of an accident. This will reduce the
potential for head injury, thereby reducing the Head Injury Criteria
(HIC) measurement. The inflatable restraint system behaves similarly to
an automotive inflatable airbag, but in this case the airbag is
integrated into the shoulder strap and inflates away from the seated
occupant. While inflatable airbags are now standard in the automotive
industry, the use of an inflatable shoulder strap is novel for
commercial aviation.
    Title 14, Code of Federal Regulations (14 CFR) 25.785 requires that
occupants be protected from head injury by either the elimination of
any injurious object within the striking radius of the head, or by
padding. Traditionally, this has required a setback of 35 inches from
any bulkhead or other rigid interior feature or, where not practical,
specified types of padding. The relative effectiveness of these means
of injury protection was not quantified. With the adoption of Amendment
25-64 to part 25, specifically Sec.  25.562, a new standard that
quantifies required head injury protection was created.
    Section 25.562 specifies that each seat type design approved for
crew or passenger occupancy during takeoff and landing must
successfully complete dynamic tests or be shown to be compliant by
rational analysis based on dynamic tests of a similar type seat. In
particular, the regulations require that

persons not suffer serious head injury under the conditions specified
in the tests, and that protection must be provided or the seat be
designed so that the head impact does not exceed a HIC of 1000 units.
While the test conditions described for HIC are detailed and specific,
it is the intent of the requirement that an adequate level of head
injury protection be provided for passengers in a severe crash.
    Because Sec. Sec.  25.562 and 25.785 and associated guidance do not
adequately address seats with inflatable shoulder straps, the FAA
recognizes that appropriate pass/fail criteria need to be developed
that do fully address the safety concerns specific to occupants of
these seats.

Type Certification Basis

    Under the provisions of 14 CFR 21.101, Dassault Aviation must show
that the Falcon 7X, as changed, continues to meet the applicable
provisions of the regulations incorporated by reference in Type
Certificate No. A59NM or the applicable regulations in effect on the
date of application for the change. The regulations incorporated by
reference in the type certificate are commonly referred to as the
``original type certification basis.'' The regulations incorporated by
reference in Type Certificate No. A59NM are as follows: 14 CFR part 25,
effective February 1, 1965, including Amendments 25-1 through 25-111 in
entirety, and in accordance with 14 CFR part 11, Special Conditions No.
25-346-SC: High Intensity Radiated Fields (HIRF) Protection.
    The U.S. type certification basis for the Falcon 7X is established
in accordance with 14 CFR 21.29 and 21.17 and the type certification
application date. The U.S. type certification basis is listed in Type
Certification Data Sheet No. A59NM.
    If the Administrator finds that the applicable airworthiness
regulations (i.e., 14 CFR part 25) do not contain adequate or
appropriate safety standards for the Falcon 7X because of a novel or
unusual design feature, special conditions are prescribed under the
provisions of Sec.  21.16.
    Special conditions are initially applicable to the model for which
they are issued. Should the type certificate for that model be amended
later to include any other model that incorporates the same novel or
unusual design feature, the special conditions would also apply to the
other model.
    In addition to the applicable airworthiness regulations and special
conditions, the Falcon 7X must comply with the fuel vent and exhaust
emission requirements of 14 CFR part 34 and the noise certification
requirements of 14 CFR part 36.
    The FAA issues special conditions, as defined in 14 CFR 11.19, in
accordance with Sec.  11.38, and they become part of the type
certification basis under Sec.  21.101.

Novel or Unusual Design Features

    The Falcon 7X will incorporate the following novel or unusual
design feature: Dassault Aviation is proposing to install inflatable
shoulder straps on side facing divans to reduce the potential for head
injury in the event of an accident. The inflatable shoulder strap works
similarly to an automotive airbag, except that the airbag is integrated
with the shoulder strap of the restraint system.
    Part 25 states the performance criteria for head injury protection
in objective terms. However, none of these criteria are adequate to
address the specific issues raised concerning seats with inflatable
shoulder straps. The FAA has therefore determined that, in addition to
the requirements of part 25, special conditions are needed to address
requirements particular to installation of seats with inflatable
shoulder straps.
    Accordingly, in addition to the passenger injury criteria specified
in Sec.  25.785, these special conditions are adopted for Falcon 7X
airplanes equipped with inflatable shoulder straps. Other conditions
may be developed, as needed, based on further FAA review and
discussions with the manufacturer and civil aviation authorities.

Discussion

    From the standpoint of a passenger safety system, the inflatable
shoulder strap is unique in that it is both an active and entirely
autonomous device. While the automotive industry has good experience
with airbags, the conditions of use and reliance on the inflatable
shoulder strap as the sole means of injury protection are quite
different. In automobile installations, the airbag is a supplemental
system and works in conjunction with an upper torso restraint. In
addition, the crash event is more definable and of typically shorter
duration, which can simplify the activation logic. The airplane
operating environment is also quite different from automobiles and
includes the potential for greater wear and tear and unanticipated
abuse conditions (due to galley loading, passenger baggage, etc.).
Airplanes also operate where exposure to high intensity electromagnetic
fields could affect the activation system.
    The inflatable shoulder strap has two potential advantages over
other means of head impact protection. First, it can provide
significantly greater protection than would be expected with energy-
absorbing pads; and second, it can provide essentially equivalent
protection for occupants of all stature. These are significant
advantages from a safety standpoint, since such devices will likely
provide a level of safety that exceeds the minimum standards of the
federal aviation regulations. Conversely, inflatable shoulder straps in
general are active systems and must be relied upon to activate properly
when needed, as opposed to an energy-absorbing pad or upper torso
restraint that is passive and always available. Therefore, the
potential advantages must be balanced against this and other potential
disadvantages in order to develop standards for this design feature.
    The FAA has considered the installation of inflatable shoulder
straps to have two primary safety concerns: First, that they perform
properly under foreseeable operating conditions, and second, that they
do not perform in a manner or at such times as would constitute a
hazard to the airplane or occupants. This latter point has the
potential to be the more rigorous of the requirements, owing to the
active nature of the system.
    The inflatable shoulder strap will rely on electronic sensors for
signaling and a stored gas canister for inflation. These same devices
could be susceptible to inadvertent activation, causing deployment in a
potentially unsafe manner. The consequences of inadvertent deployment,
as well as failure to deploy, must be considered in establishing the
reliability of the system. Dassault Aviation must substantiate that the
effects of an inadvertent deployment in flight either would not cause
injuries to occupants or that such deployment(s) meet the requirement
of Sec.  25.1309(b). The effect of an inadvertent deployment on a
passenger or crewmember that might be positioned close to the
inflatable shoulder strap should also be considered. The person could
be either standing or sitting. A minimum reliability level will have to
be established for this case, depending upon the consequences, even if
the effect on the airplane is negligible.
    The potential for an inadvertent deployment could be increased as a
result of conditions in service. The installation must take into
account wear and tear so that the likelihood of an inadvertent
deployment is not increased to an unacceptable level. In this context,
an appropriate inspection interval and self-test capability are
considered

necessary. Other outside influences are lightning and high intensity
radiated fields (HIRF). Existing HIRF special conditions for the
Dassault Aviation Model Falcon 7X airplanes, Special Conditions No. 25-
346-SC, are applicable. Finally, the inflatable shoulder strap
installation should be protected from the effects of fire, so that an
additional hazard is not created by, for example, a rupture of the
pyrotechnic squib.
    In order to be an effective safety system, the inflatable shoulder
strap must function properly and must not introduce any additional
hazards to occupants as a result of its functioning. There are several
areas where the inflatable shoulder strap differs from traditional
occupant protection systems, and requires special conditions to ensure
adequate performance.
    Because the inflatable shoulder strap is essentially a single use
device, there is the potential that it could deploy under crash
conditions that are not sufficiently severe as to require head injury
protection from the inflatable shoulder strap. Since an actual crash is
frequently composed of a series of impacts before the airplane comes to
rest, this could render the inflatable shoulder strap useless if a
larger impact follows the initial impact. This situation does not exist
with energy absorbing pads or upper torso restraints, which tend to
provide continuous protection regardless of severity or number of
impacts in a crash event. Therefore, the inflatable shoulder strap
installation should provide protection, when it is required, by not
expending its protection during a less severe impact. Also, it is
possible to have several large impact events during the course of a
crash, but there is no requirement for the inflatable shoulder strap to
provide protection for multiple impacts.
    Since each occupant's restraint system provides protection for that
occupant only, the installation must address seats that are unoccupied.
It will be necessary to show that the required protection is provided
for each occupant regardless of the number of occupied seats, and
considering that unoccupied seats may have shoulder straps that are
active.
    The inflatable shoulder straps should be effective for a wide range
of occupants. The FAA has historically considered the range from the
fifth percentile female to the ninety-fifth percentile male as the
range of occupants that must be taken into account. In this case, the
FAA is proposing consideration of a broader range of occupants, due to
the nature of the shoulder straps installation and its close proximity
to the occupant. In a similar vein, these persons could have assumed
the brace position, for those accidents where an impact is anticipated.
Test data indicate that occupants in the brace position do not require
supplemental protection, and so it would not be necessary to show that
the inflatable shoulder straps will enhance the brace position.
However, the inflatable shoulder straps must not introduce a hazard in
the case of deploying into the seated, braced occupant.
    Another area of concern is the use of seats, so equipped, by
children whether lap-held, in approved child safety seats, or occupying
the seat directly. Similarly, if the seat is occupied by a pregnant
woman, the installation should address such usage, either by
demonstrating that it will function properly, or by adding appropriate
limitation on usage.
    Since the inflatable shoulder strap will be electrically powered,
there is the possibility that the system could fail due to a separation
in the fuselage. Since this system is intended as crash/post-crash
protection means, failure to deploy due to fuselage separation is not
acceptable. As with emergency lighting, the system should function
properly if such a separation occurs at any point in the fuselage.
    Since the inflatable shoulder strap is likely to have a large
volume displacement, the inflated bag could potentially impede egress
of passengers. Since the bag deflates to absorb energy, it is likely
that an inflatable shoulder strap would be deflated at the time that
persons would be trying to leave their seats. Nonetheless, it is
considered appropriate to specify a time interval after which the
inflatable shoulder strap may not impede rapid egress. Ten seconds has
been chosen as a reasonable time, since this corresponds to the maximum
time allowed for an exit to be openable (Sec.  25.809). In actuality,
it is unlikely that an exit would be prepared by a flight attendant
this quickly in an accident severe enough to warrant deployment of the
inflatable shoulder strap, and the inflatable shoulder strap is
expected to deflate much quicker than ten seconds.
    Part I of appendix F to part 25 specifies the flammability
requirements for interior materials and components. There is no
reference to inflatable restraint systems in appendix F, because such
devices did not exist at the time the flammability requirements were
written. The existing requirements are based on both material types, as
well as use, and have been specified in light of the state-of-the-art
of materials available to perform a given function. In the absence of a
specific reference, the default requirement would be for the type of
material used to construct the inflatable restraint, which is a fabric
in this case. However, in writing special conditions, the FAA must also
consider the use of the material, and whether the default requirement
is appropriate. In this case, the specialized function of the
inflatable shoulder strap means that highly specialized materials are
needed. The standard normally applied to fabrics is a 12-second
vertical ignition test. However, materials that meet this standard do
not perform adequately as inflatable shoulder straps. Since the safety
benefit of the inflatable shoulder strap is significant, the
flammability standard appropriate for these devices should not screen
out suitable materials, thereby effectively eliminating use of
inflatable shoulder straps. The FAA will need to establish a balance
between the safety benefit of the inflatable shoulder strap and its
flammability performance. At this time, the 2.5-inch per minute
horizontal test is considered to provide that balance. As the
technology in materials progresses (which is expected), the FAA may
change this standard in subsequent special conditions to account for
improved materials.
    The following special conditions can be characterized as addressing
either the safety performance of the system or the system's integrity
against inadvertent activation. Because a crash requiring use of the
inflatable shoulder strap is a relatively rare event, and because the
consequences of an inadvertent activation are potentially quite severe,
these latter requirements are probably the more rigorous from a design
standpoint.
    Finally, it should be noted that these special conditions are
applicable to the inflatable shoulder straps as installed. These
special conditions are not an installation approval. Therefore, while
these special conditions relate to each such system installed, the
overall installation approval is a separate finding and must consider
the combined effects of all such systems installed.

Applicability

    As discussed above, these special conditions are applicable to the
Dassault Aviation Model Falcon 7X. Should Dassault Aviation apply at a
later date for a change to the type certificate to include another
model incorporating the same novel or unusual design feature, the
special conditions would apply to that model as well.

Conclusion

    This action affects only certain novel or unusual design features
on one model of airplanes. It is not a rule of general applicability.
    The substance of these special conditions has been subjected to the
notice and comment period in several prior instances and has been
derived without substantive change from those previously issued. It is
unlikely that prior public comment would result in a significant change
from the substance contained herein. Therefore, because a delay would
significantly affect the certification of the airplane, which is
imminent, the FAA has determined that prior public notice and comment
are unnecessary and impracticable, and good cause exists for adopting
these special conditions upon issuance. The FAA is requesting comments
to allow interested persons to submit views that may not have been
submitted in response to the prior opportunities for comment described
above.

List of Subjects in 14 CFR Part 25

    Aircraft, Aviation safety, Reporting and recordkeeping
requirements.

    The authority citation for these special conditions is as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704.

The Special Conditions

    Accordingly, pursuant to the authority delegated to me by the
Administrator, the following special conditions are issued as part of
the type certification basis for Dassault Aviation Model Falcon 7X
airplanes.
    1. Seats with Inflatable Shoulder Straps. It must be shown that the
airbag system in the shoulder strap will deploy and provide protection
under crash conditions where it is necessary to prevent serious injury.
The means of protection must take into consideration a range of stature
from a two-year-old child to a ninety-fifth percentile male. The airbag
system in the shoulder strap must provide a consistent approach to
energy absorption throughout that range of occupants. In addition, the
following situations must be considered:
    a. The seat occupant is holding an infant.
    b. The seat occupant is a child in a child restraint device.
    c. The seat occupant is a child not using a child restraint device.
    d. The seat occupant is a pregnant woman.
    2. The airbag system in the shoulder strap must provide adequate
protection for each occupant regardless of the number of occupants of
the seat assembly, considering that unoccupied seats may have an active
airbag system in the shoulder strap.
    3. The design must prevent the airbag system in the shoulder strap
from being either incorrectly buckled or incorrectly installed, such
that the airbag system in the shoulder strap would not properly deploy.
Alternatively, it must be shown that such deployment is not hazardous
to the occupant and will provide the required injury protection.
    4. It must be shown that the airbag system in the shoulder strap is
not susceptible to inadvertent deployment as a result of wear and tear
or inertial loads resulting from in-flight or ground maneuvers
(including gusts and hard landings) and other operating and
environmental conditions (vibrations, moisture, etc.) likely to be
experienced in service.
    5. Deployment of the airbag system in the shoulder strap must not
introduce injury mechanisms to the seated occupant or result in
injuries that could impede rapid egress. This assessment should include
an occupant whose belt is loosely fastened.
    6. It must be shown that inadvertent deployment of the airbag
system in the shoulder strap, during the most critical part of the
flight, will either meet the requirement of Sec.  25.1309(b) or not
cause a hazard to the airplane or its occupants.
    7. It must be shown that the airbag system in the shoulder strap
will not impede rapid egress of occupants 10 seconds after airbag
deployment.
    8. The airbag system must be protected from lightning and HIRF. The
threats to the airplane specified in existing regulations regarding
lightning, Sec.  25.1316, and special conditions regarding HIRF,
Special Condition No. 25-346-SC, are incorporated by reference for the
purpose of measuring lightning and HIRF protection. For the purposes of
complying with HIRF requirements, the airbag system in the shoulder
strap is considered a ``critical system'' if its deployment could have
a hazardous effect on the airplane; otherwise, it is considered an
``essential'' system.
    9. The airbag system in the shoulder strap must function properly
after loss of normal aircraft electrical power and after a transverse
separation of the fuselage at the most critical location. A separation
at the location of the airbag system in the shoulder strap does not
have to be considered.
    10. It must be shown that the airbag system in the shoulder strap
will not release hazardous quantities of gas or particulate matter into
the cabin.
    11. The airbag system in the shoulder strap installation must be
protected from the effects of fire such that no hazard to occupants
will result.
    12. There must be a means for a crewmember to verify the integrity
of the airbag system in the shoulder strap activation system prior to
each flight, or it must be demonstrated to reliably operate between
inspection intervals. The FAA considers the loss of the airbag-system
deployment function alone (i.e., independent of the conditional event
that requires the airbag system deployment) to be a major failure
condition.
    13. With regard to Sec.  25.853, the inflatable material may not
have an average burn rate of greater than 2.5 inches/minute when tested
using the horizontal flammability test defined in part 25, appendix F,
part I, paragraph (b)(5).
    14. The airbag system in the shoulder strap, once deployed, must
not adversely affect the emergency-lighting system (i.e., block floor
proximity lights to the extent that the lights no longer meet their
intended function).

    Issued in Renton, Washington, on March 19, 2012.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-7280 Filed 3-26-12; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 88, Number 85 (Wednesday, May 3, 2023)]
[Notices]
[Page 27937]
[FR Doc No: 2023-09333]

-----------------------------------------------------------------------

SECURITIES AND EXCHANGE COMMISSION

[Release No. 34-97394; File No. SR-NYSEAMER-2023-17]

Self-Regulatory Organizations; NYSE American LLC; Notice of
Designation of a Longer Period for Commission Action on Proposed New
Rule 980NYP and Conforming Amendments to Rule 935NY

April 27, 2023.
    On February 28, 2023, NYSE American LLC (``Exchange'') filed with
the Securities and Exchange Commission (``Commission''), pursuant to
Section 19(b)(1) of the Securities Exchange Act of 1934 (``Act'') \1\
and Rule 19b-4 thereunder,\2\ a proposed rule change to adopt Rule
980NYP (Electronic Complex Order Trading) to reflect the implementation
of the Exchange's PILLAR trading technology on its options market and
to make conforming amendments to Rule 935NY (Order Exposure
Requirements). The proposed rule change was published for comment in
the Federal Register on March 17, 2023.\3\
---------------------------------------------------------------------------

    \1\ 15 U.S.C. 78s(b)(1).
    \2\ 17 CFR 240.19b-4.
    \3\ See Securities Exchange Act Release No. 97125 (March 13,
2023), 88 FR 16467.
---------------------------------------------------------------------------

    Section 19(b)(2) of the Act \4\ provides that, within 45 days of
the publication of notice of the filing of a proposed rule change, or
within such longer period up to 90 days as the Commission may designate
if it finds such longer period to be appropriate and publishes its
reasons for so finding, or as to which the self-regulatory organization
consents, the Commission shall either approve the proposed rule change,
disapprove the proposed rule change, or institute proceedings to
determine whether the proposed rule change should be disapproved. The
45th day after publication of the notice for this proposed rule change
is May 1, 2023.
---------------------------------------------------------------------------

    \4\ 15 U.S.C. 78s(b)(2).
---------------------------------------------------------------------------

    The Commission is extending this 45-day time period. The Commission
finds that it is appropriate to designate a longer period within which
to take action on the proposed rule change so that it has sufficient
time to consider the proposed rule change. Accordingly, the Commission,
pursuant to Section 19(b)(2) of the Act,\5\ designates June 15, 2023,
as the date by which the Commission shall either approve or disapprove,
or institute proceedings to determine whether to disapprove, the
proposed rule change (File No. SR-NYSEAMER-2023-17).
---------------------------------------------------------------------------

    \5\ Id.

    For the Commission, by the Division of Trading and Markets,
pursuant to delegated authority.\6\
---------------------------------------------------------------------------

    \6\ 17 CFR 200.30-3(a)(31).
---------------------------------------------------------------------------

Sherry R. Haywood,
Assistant Secretary.
[FR Doc. 2023-09333 Filed 5-2-23; 8:45 am]
BILLING CODE 8011-01-P


Assessing the Effect of Five Gasoline Properties on Exhaust Emissions from Light-Duty Vehicles certified to Tier-2 Standards

                       Analysis of Data from EPA Phase 3

                                (EPAct/V2/E-89)

                                 Appendix G.5
                              Final Model Fitting
                       Oxides of Nitrogen (NOx) (Bag 3)

No. Observations:			   931
No. Vehicles:		  		     15
No. censored measurements:		     25
No. missing measurements:		       2
No. measurements removed:		       1
Model Type:				Tobit regression

G.5.1  Model Fitting based on the 11-term design model.

    Models fit for NOx (Bag 3): (Grand Intercept not fit by Tobit models).
Model Term
                                   Notation
                                     Model

                                     Full
                                    FM2[1]
                                      FM3
                                      FM4
                                      FM5
                                      FM6
                                      FM7
                                     etOH
Ze
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                     Arom
Za
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      RVP
Zr
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      T50
Z5
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      x
                                      T90
Z9
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                 etOH x etOH
ZZee
                                      ●
                                      x

                                  T50 x T50
ZZ55
                                      ●
                                      ●
                                      ●
                                      ●
                                      x

                                 etOH x Arom
ZZea
                                      ●
                                      ●
                                      ●
                                      x

                                  etOH x RVP
ZZer
                                      ●
                                      x

                                  etOH x T50
ZZe5
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      x

                                  etOH x T90
ZZe9
                                      ●
                                      ●
                                      x

1 Indicates "Full minus 2," etc.

  NOx (Bag 3): Model fitting history, starting with the 11-term design model.
                                Fit Parameters

                             Test with respect to
                                Previous Model
Model
                                                                         p-1[1]
                                     -2lnL

                                                                           Dev.
                                                                              d
                                                                    Pr>χ[2]
Full Model
                                                                             11
                                   2809.349

FM2
                                                                              9
                                   2809.676

                                     0.327
                                       2
                                     0.849
FM3
                                                                              8
                                   2810.499

                                     0.823
                                       1
                                     0.364
FM4
                                                                              7
                                   2811.808

                                     1.309
                                       1
                                     0.253
FM5
                                                                              6
                                   2813.571

                                     1.763
                                       1
                                     0.184
FM6
                                                                              5
                                   2815.925

                                     2.354
                                       1
                                     0.125
FM7
                                                                              4
                                   2817.195

                                     1.270
                                       1
                                     0.260

[1] Total number of terms excludes the intercept, as the Tobit
models do not fit intercepts.
[2] Best fit with respect to the 16-term extended model.

NOx (Bag 3): Coefficients and Tests of Effect for the Full and Reduced Models, with respect to the 11-term design model.

G.5.2 Model Fitting based on the 16-term extended model.

    Models fit for NOx (Bag 3): (Grand Intercept not fit by Tobit models).
Model Term
                                   Notation
                                     Model

                                     Full
                                    FM4[1]
                                      FM5
                                      FM6
                                      FM7
                                      FM8
                                      FM9
                                     etOH
Ze
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                     Arom
Za
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      RVP
Zr
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      T50
Z5
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      T90
Z9
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                 etOH x etOH
ZZee
                                      ●
                                      x

                                  T50 x T50
ZZ55
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      x
                                 etOH x Arom
ZZea
                                      ●
                                      ●
                                      x

                                  etOH x RVP
ZZer
                                      ●
                                      ●
                                      ●
                                      ●
                                      x

                                  etOH x T50
ZZe5
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                  etOH x T90
ZZe9
                                      ●
                                      ●
                                      ●
                                      x

                                  T90 x T90
ZZ99
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                  Arom x RVP
ZZar
                                      ●
                                      x

                                  Arom x T50
ZZa5
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                  Arom x T90
ZZa9
                                      ●
                                      ●
                                      ●
                                      ●
                                      ●
                                      x

                                  T50 x T90
ZZ59
                                      ●
                                      x

                                  RVP x T90
ZZr9
                                      ●
                                      x

 NOx (Bag 3): Model fitting history, starting with the 17-term extended model.
                                Fit Parameters

                             Test with respect to
                                Previous Model
Model
                                                                         p-1[1]
                                     -2lnL

                                                                           Dev.
                                                                              d
                                                                    Pr>χ[2]
Full Model
                                                                             16
                                                                       2801.073

FM4
                                                                             12
                                                                       2801.869

                                     0.796
                                       4
                                     0.939
FM5
                                                                             11
                                                                       2802.472

                                     0.603
                                       1
                                     0.437
FM6
                                                                             10
                                                                       2803.337

                                     0.865
                                       1
                                     0.352
FM7
                                                                              9
                                                                       2804.295

                                     0.958
                                       1
                                     0.328
FM8
                                                                              8
                                                                       2806.313

                                     2.018
                                       1
                                     0.155
FM9
                                                                              7
                                                                       2808.530

                                     2.217
                                       1
                                     0.136

[1] Total number of terms excludes the intercept, as the Tobit
Models do not fit intercepts.
[2] Best fit with respect to the 17-term extended model.

NOx (Bag 3): Coefficients and Tests of Effect for the Full and Reduced Models, with respect to the 16-term extended model.


[Federal Register Volume 79, Number 216 (Friday, November 7, 2014)]
[Proposed Rules]
[Page 66346]
[FR Doc No: 2014-26524]

=======================================================================
-----------------------------------------------------------------------

ENVIRONMENTAL PROTECTION AGENCY

40 CFR Part 60

[EPA-HQ-OAR-2010-0706; FRL-9919-03-OAR]
RIN 2060-AP06

Standards of Performance for Grain Elevators

AGENCY: Environmental Protection Agency.

ACTION: Proposed rule; reopening of public comment period.

-----------------------------------------------------------------------

SUMMARY: The Environmental Protection Agency (EPA) is announcing that
the period for providing public comments on the July 9, 2014, proposed
rule titled ``Standards of Performance for Grain Elevators'' is being
extended an additional 45 days.

DATES: The public comment period for the proposed rule published July
9, 2014 (79 FR 39241), and initially extended by 30 days on September
16, 2014 (79 FR 55413), is being extended an additional 45 days to
December 22, 2014, in order to provide the public additional time to
submit comments and supporting information.

ADDRESSES: Written comments on the proposed rule may be submitted to
the EPA electronically, by mail, by facsimile or through hand delivery/
courier. Please refer to the proposal (79 FR 39241) for the addresses
and detailed instructions.
    Docket. Publicly available documents relevant to this action are
available for public inspection either electronically at http://www.regulations.gov or in hard copy at the EPA Docket Center, EPA WJC
West Building, Room 3334, 1301 Constitution Ave. NW., Washington, DC.
The Public Reading Room is open from 8:30 a.m. to 4:30 p.m., Monday
through Friday, excluding legal holidays. A reasonable fee may be
charged for copying. The EPA has established the official public docket
for this rulemaking under Docket No. EPA-HQ-OAR-2010-0706.
    World Wide Web. The EPA Web site containing information for this
rulemaking is: http://www.epa.gov/ttn/atw/nsps/grain/genspspg.html.

FOR FURTHER INFORMATION CONTACT: Mr. William Schrock, Natural Resources
Group (E143-03), Sector Policies and Programs Division, Research
Triangle Park, North Carolina 27711; telephone number<PHONE_NUMBER>;
fax number<PHONE_NUMBER>; and email address<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Comment Period

    The EPA is extending the public comment period for an additional 45
days. The public comment period will end on December 22, 2014, rather
than November 6, 2014. This will ensure that the public has sufficient
time to review and comment on all of the information available,
including the proposed rule and other materials in the docket.

    Dated: November 3, 2014.
Mary E. Henigin,
Acting Director for Office of Air Quality Planning and Standards.
[FR Doc. 2014-26524 Filed 11-6-14; 8:45 am]
BILLING CODE 6560-50-P