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Exhaust Emissions from In-Use General Aviation Aircraft (2016) / Chapter Skim
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Pages 90-93

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From page 90...
... 90 Several considerations apply to the data that follow: 1. Emission indices were calculated based on a fuel composition of 3067 grams of CO2 per kilogram of fuel for AVGAS 100 LL and 3160 grams of CO2 per kilogram of fuel for Jet A
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From page 91...
... -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- Engine Stateb -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- Engine State -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -Unique ID Engine Make Engine Model HPa # Engines Class T/O C/O Cruise AppFinal App Taxi Idle T/O C/O Cruise AppFinal App Taxi Idle -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- % of max propellor speed -- -- -- -- -- -- -- -- -- -- -- - - -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- % of max fuel flow -- -- -- -- -- -- -- -- -- -- -- -Recommended for Subs„tu„on in EDMS/AEDT Lycoming O-320 150-160 1 100% 100% 91% 70% 69% 46% 34% 98% 98% 80% 41% 39% 18% 12% Individual Engine Tests 1 Rotax 912 100 1 100% 100% 90% 66% 66% 58% 57% 72% 72% 50% 30% 30% 22% 13% 2 Connental O-200-A 100 1 -- -- -- -- -- 46% -- -- -- -- -- -- 19% -3 Connental O-200-A 100 1 100% 100% 90% 71% 71% 41% 24% 90% 90% 70% 44% 44% 21% 14% 4 Connental O-200-A 100 1 100% 100% 96% 64% 48% 40% 40% 90% 90% 82% 37% 25% 20% 20% 5 Connental O-200-A 100 1 100% 85% 100% 65% 65% 46% 29% 90% 62% 90% 38% 38% 23% 15% 6 Connental O-200-A 100 1 100% 100% 100% 83% 63% 46% 30% 90% 90% 90% 60% 35% 23% 16% 7 Lycoming O-235-L2C 115 1 100% 100% 94% 77% 47% 43% 33% 98% 98% 81% 49% 20% 18% 14% 8 Lycoming O-235-L2C 115 1 100% 100% 93% 77% 48% 43% 37% 98% 98% 81% 50% 21% 19% 15% 9 Lycoming O-235-L2C 115 1 100% 100% 100% 67% 67% 67% 33% 98% 98% 98% 37% 37% 40% 14% 10 Lycoming O-320-E2D 150 1 100% 100% 94% 68% 68% 51% 31% 100% 100% 86% 37% 37% 21% 11% 11 Lycoming O-320-E2D 150 1 99% 99% 93% 57% 57% 43% 30% 100% 100% 86% 25% 25% 16% 11% 12.1 Lycoming O-320-E2D 150 1 100% 100% 100% 91% 68% 45% 36% 100% 100% 100% 79% 37% 18% 13% 12.2 Lycoming O-320-E2D 150 1 100% 100% 95% 68% 68% 55% 39% 100% 100% 92% 37% 37% 24% 14% 13 Lycoming O-320-E2D 150 1 -- -- -- 52% 65% 43% 30% -- -- -- 22% 34% 16% 11% 14 Lycoming O-320-E2D 150 1 98% 98% 96% 74% 56% 35% 31% 99% 99% 92% 45% 25% 12% 11% 15 Lycoming O-320-E2D 150 1 100% 100% 72% 70% 70% 43% 28% 100% 100% 58% 39% 39% 16% 10% 16 Lycoming O-320-E2D 150 1 100% 100% 92% 67% 63% 50% 41% 100% 100% 81% 35% 31% 20% 15% 17 Lycoming O-320-E2G 150 1 100% 100% 90% 69% 73% 48% 27% 100% 100% 77% 39% 43% 19% 10% 18 Lycoming O-320-E2G 150 1 100% 100% 96% 87% 70% 46% 33% 100% 100% 92% 69% 39% 18% 12% 19 Lycoming O-320-E3D 150 1 100% 100% 96% 67% 67% 42% 26% 100% 100% 93% 35% 35% 16% 9% 20 Lycoming O-320-B2C 160 1 Helicopter 102% 102% 75% -- -- -- 58% 100% 100% 43% -- -- -- 24% 21 Lycoming O-320-B2C 160 1 Helicopter -- -- 75% -- -- -- -- -- -- 43% -- -- -- -22 Lycoming O-320-D2J 160 1 -- -- -- -- -- 48% 32% -- -- -- -- -- 18% 10% 23 Lycoming O-320-D3G 160 1 100% 100% 100% 57% 100% 43% 33% 100% 100% 100% 23% 100% 15% 11% 24 Lycoming O-320-D3G 160 1 102% 102% 91% 65% 65% 43% 31% 100% 100% 75% 31% 31% 15% 10% 25 Lycoming O-320-D3G 160 1 100% 100% 91% 81% 72% 64% 34% 100% 100% 75% 53% 40% 30% 11% 26 Lycoming O-320-D3G 160 1 100% 100% 96% 58% 54% 42% 35% 100% 100% 87% 25% 22% 14% 11% 27 Lycoming O-320-H2AD 160 1 92% 92% 88% 68% 68% 40% 32% 75% 75% 66% 35% 35% 14% 11% 28 Lycoming O-320-H2AD 160 1 99% 99% 95% 91% 82% 45% 37% 94% 94% 84% 73% 54% 17% 13% 29 Franklin 6A4-165 165 1 100% 100% 91% 77% 45% 45% 32% 100% 100% 79% 50% 18% 18% 11% 30 Lycoming O-360-A4M 180 1 100% 100% 95% 64% 64% 45% 40% 96% 96% 62% 35% 35% 15% 14% 31 Lycoming O-360-C2E 180 1 100% 100% 91% 66% 68% 45% 40% 62% 62% 45% 28% 31% 18% 16% 32.1 Lycoming O-360-F1A6 180 1 100% 97% 88% 85% 77% 42% 31% 100% 92% 70% 62% 48% 15% 10% 32.2 Lycoming O-360-F1A6 180 1 100% 94% 90% 61% 61% 45% 24% 100% 84% 73% 28% 28% 17% 8% 33 Lycoming O-360-A1A 180 2 97% 94% 88% 57% 57% 34% 37% 95% 88% 71% 26% 26% 12% 20% 34 Lycoming O-360-A1G6D 180 2 100% 93% 85% 81% 74% 37% 41% 106% 83% 66% 58% 46% 14% 22% 35 Lycoming IO-360-L2A 160 1 Fuel Injected 100% 100% 99% 69% 69% 48% 36% 100% 100% 64% 14% 14% 18% 12% 36 Lycoming IO-360-A3B6D 200 1 Fuel Injected 99% 99% 70% 74% 78% 48% 30% 98% 98% 37% 25% 31% 11% 10% 37 Lycoming IO-360-C1C6 200 1 Fuel Injected 100% 100% 91% 58% 50% 38% 26% 76% 76% 61% 25% 19% 19% 13% 38 Lycoming IO-360-C1C6 200 1 Fuel Injected 102% 102% 81% 64% 64% 51% 37% 100% 100% 56% 32% 32% 20% 13%
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From page 92...
... -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- Engine Stateb -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- Engine State -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -Unique ID Engine Make Engine Model HPa # Engines Class T/O C/O Cruise AppFinal App Taxi Idle T/O C/O Cruise AppFinal App Taxi Idle -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- % of max propellor speed -- -- -- -- -- -- -- -- -- -- -- - - -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- % of max fuel flow -- -- -- -- -- -- -- -- -- -- -- -39 Lycoming IO-520-1AB5 230 1 Fuel Injected 100% 100% 100% 77% 77% 45% 35% 100% 100% 56% 44% 44% 16% 15% 40 Connental O-470-11 230 1 -- -- 87% 65% 65% 39% 26% -- -- 71% 36% 36% 16% 10% 41 TCM O-470-U 230 1 100% 100% 100% 68% 45% 45% 36% 100% 100% 61% 30% 16% 14% 3% 42 Lycoming O-540-B4B5 235 1 100% 96% 84% 80% 56% 52% 40% 95% 84% 59% 52% 25% 22% 15% 43 Lycoming O-540-A1D5 250 1 100% 96% 92% 65% 65% 42% 26% 96% 85% 75% 32% 32% 15% 9% 44 Lycoming O-540-J3C5D 250 1 100% 100% 78% 63% 63% 37% 31% 100% 100% 52% 33% 33% 15% 13% 45 Lycoming IO-540-C4B5 250 2 Fuel Injected -- -- -- -- -- -- 25% -- -- -- -- -- -- 11% 46 Lycoming IO-540-C4B5 250 2 Fuel Injected 100% 94% 86% 51% 51% 47% 28% 100% 92% 73% 25% 25% 22% 13% 47.1 Lycoming IO-540-C4B5 250 2 Fuel Injected 100% 100% 92% 80% 88% 42% 33% 98% 62% 54% 61% 50% 18% 15% 47.2 Lycoming IO-540-C4B5 250 2 Fuel Injected 100% 100% 92% 68% 68% 56% 31% 100% 100% 87% 42% 42% 29% 14% 48 TCM IO-540-BB 285 1 Fuel Injected -- 98% 94% 82% 82% 45% 25% -- 90% 80% 56% 56% 18% 10% 49 Lycoming IO-540-K1G5D 300 1 Fuel Injected 93% 93% 90% 82% 82% 49% 37% 72% 72% 64% 51% 51% 19% 13% 50 Connental IO-550-N 300 1 Fuel Injected -- -- -- -- -- -- 30% -- -- -- -- -- -- 15% 51 TCM TSIO-520-C 300 1 Fuel Injected 96% 85% 96% 67% 67% 43% 27% 76% 61% 76% 34% 34% 16% 10% 52 TCM IO-550-C 300 2 Fuel Injected -- -- 96% 75% 75% 43% 33% -- -- 89% 50% 50% 22% 17% 53 Unknown (Skybolt Experimental)
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From page 93...
... -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- Engine Stateb -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- Engine State -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -Unique ID Engine Make Engine Model HPa # Engines Class T/O C/O Cruise AppFinal App Taxi Idle T/O C/O Cruise AppFinal App Taxi Idle -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- % of max propellor speed -- -- -- -- -- -- -- -- -- -- -- - - -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- % of max fuel flow -- -- -- -- -- -- -- -- -- -- -- -Preexis‚ng Data FOCAc.,e.
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