Weight: 1180 kg
Throttle Levers: IDLE
Landing Gear: Down
CG: Most Forward (16.5%)
No ground effect
| | | | | | | | | ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ---------------------------------------------------------------- | ------------ | ------------- | -------------- | -------- | -- | -- | |WEIGHT
\[kg]
|BANK ANGLE
\[deg]
| **FLAPS 0°** | **FLAPS T/O** | **FLAPS FULL** | | | | | **KIAS** | **KCAS** | **KIAS** | **KCAS** | **KIAS** | **KCAS** | | | |1180
(FWD C.G.)
| 0 | 66 | 64 | 56 | 56 | 53 | 54 | | 15 | 67 | 65 | 57 | 57 | 54 | 55 | | | 30 | 70 | 69 | 60 | 60 | 58 | 58 | | | 45 | 77 | 76 | 67 | 67 | 64 | 64 | | | 60 | 93 | 90 | 81 | 79 | 78 | 76 | | *** ### Take-Off Performances |Weight = 1180 kg
Flaps: T/O
Speed at Lift-Off: 65 KIAS
Speed Over 50ft Obstacle: 70 KIAS
Throttle Levers: Full Forward
Runway: Grass
|Corrections
Headwind: - 2.5m for each kt (8 ft/kt)
Tailwind: + 10m for each kt (33ft/kt)
Paved Runway: - 6% to Ground Roll
Runway slope: + 5% to Ground Roll for each +1%
| | | | | | | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ----------------- | ------ | ---- | ------- | ------- | |Pressure
Altitude
\[ft]
| | **Distance \[m]** | | | | | | **Temperature \[°C]** | **ISA** | | | | | | | **-25** | **0** | **25** | **50** | | | | | **S.L.** | **Ground Roll** | 208 | 258 | 313 | 374 | **290** | | **At 50 ft AGL** | 266 | 331 | 404 | 485 | **373** | | | **1000** | **Ground Roll** | 230 | 284 | 346 | 413 | **315** | | **At 50 ft AGL** | 294 | 366 | 447 | 537 | **407** | | | **2000** | **Ground Roll** | 254 | 315 | 382 | 457 | **343** | | **At 50 ft AGL** | 326 | 406 | 495 | 595 | **444** | | | **3000** | **Ground Roll** | 281 | 348 | 423 | 505 | **374** | | **At 50 ft AGL** | 401 | 499 | 610 | 733 | **529** | | | **4000** | **Ground Roll** | 311 | 385 | 468 | 560 | **408** | | **At 50 ft AGL** | 401 | 499 | 610 | 733 | **529** | | | **5000** | **Ground Roll** | 345 | 427 | 519 | 620 | **445** | | **At 50 ft AGL** | 445 | 555 | 677 | 814 | **579** | | | **6000** | **Ground Roll** | 383 | 474 | 575 | 688 | **486** | | **At 50 ft AGL** | 495 | 617 | 753 | 906 | **633** | | | **7000** | **Ground Roll** | 425 | 526 | 639 | 764 | **531** | | **At 50 ft AGL** | 551 | 686 | 839 | 1008 | **693** | | | **8000** | **Ground Roll** | 472 | 585 | 710 | 849 | **581** | | **At 50 ft AGL** | 614 | 765 | 934 | 1123 | **759** | | | **9000** | **Ground Roll** | 525 | 650 | 790 | 945 | **635** | | **At 50 ft AGL** | 685 | 853 | 1042 | 1253 | **833** | | | **10000** | **Ground Roll** | 585 | 724 | 879 | 1052 | **696** | | **At 50 ft AGL** | 764 | 952 | 1163 | 1399 | **914** | | |Weight = 930 kg
Flaps: T/O
Speed at Lift-Off: 65 KIAS
Speed Over 50ft Obstacle: 70 KIAS
Throttle Levers: Full Forward
Runway: Grass
|Corrections
Headwind: - 2.5m for each kt (8 ft/kt))
Tailwind: + 10m for each kt (33ft/kt
Paved Runway: - 6% to Ground Roll
Runway slope: + 5% to Ground Roll for each +1%
| | | | | | | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ----------------- | ------ | --- | ------- | ------- | |Pressure
Altitude
\[ft]
| | **Distance \[m]** | | | | | | **Temperature \[°C]** | **ISA** | | | | | | | **-25** | **0** | **25** | **50** | | | | | **S.L.** | **Ground Roll** | 100 | 127 | 158 | 194 | **146** | | **At 50 ft AGL** | 131 | 167 | 207 | 254 | **190** | | | **1000** | **Ground Roll** | 112 | 142 | 177 | 216 | **160** | | **At 50 ft AGL** | 146 | 186 | 231 | 283 | **209** | | | **2000** | **Ground Roll** | 125 | 159 | 197 | 242 | **175** | | **At 50 ft AGL** | 163 | 208 | 258 | 316 | **229** | | | **3000** | **Ground Roll** | 140 | 177 | 221 | 270 | **192** | | **At 50 ft AGL** | 204 | 260 | 323 | 395 | **277** | | | **4000** | **Ground Roll** | 156 | 198 | 247 | 302 | **212** | | **At 50 ft AGL** | 204 | 260 | 323 | 395 | **277** | | | **5000** | **Ground Roll** | 175 | 222 | 277 | 338 | **233** | | **At 50 ft AGL** | 229 | 291 | 362 | 443 | **305** | | | **6000** | **Ground Roll** | 196 | 249 | 310 | 379 | **256** | | **At 50 ft AGL** | 257 | 326 | 406 | 496 | **335** | | | **7000** | **Ground Roll** | 220 | 280 | 348 | 426 | **282** | | **At 50 ft AGL** | 288 | 366 | 455 | 557 | **370** | | | **8000** | **Ground Roll** | 247 | 314 | 391 | 478 | **312** | | **At 50 ft AGL** | 323 | 411 | 512 | 626 | **408** | | | **9000** | **Ground Roll** | 278 | 353 | 440 | 538 | **344** | | **At 50 ft AGL** | 364 | 462 | 575 | 704 | **450** | | | **10000** | **Ground Roll** | 313 | 397 | 495 | 605 | **380** | | **At 50 ft AGL** | 409 | 520 | 648 | 792 | **498** | | *** ### Take-Off Rate Of Climb |Power Setting: Maximum Continuous Power
Flaps: Take-Off
Landing Gear: Up
| | | | | | | | | ---------------------------------------------------------------------------------------------------------------------------------------------- | ---------------------------------------------------------------------- | --------------------------------------------------------------------- | --------------------------- | ---- | ---- | -------- | -------- | |Weight
\[kg]
|Pressure Altitude
\[ft]
|Climb Speed VY
\[KIAS]
| **Rate of Climb \[ft/min]** | | | | | | **Temperature \[°C]** | **ISA** | | | | | | | | **-25** | **0** | **25** | **50** | | | | | | 1180 | **S.L.** | **85** | 1347 | 1154 | 982 | 826 | **1048** | | **2000** | **82** | 1200 | 1010 | 841 | 688 | **933** | | | **4000** | **79** | 1054 | 867 | 701 | 551 | **818** | | | **6000** | **76** | 908 | 725 | 561 | 413 | **704** | | | **8000** | **73** | 763 | 583 | 422 | 277 | **589** | | | **10000** | **70** | 618 | 441 | 283 | 141 | **474** | | | **12000** | **67** | 473 | 300 | 145 | 5 | **359** | | | **14000** | **64** | 330 | 159 | 7 | -130 | **244** | | | 930 | **S.L.** | **85** | 1803 | 1575 | 1372 | 1189 | **1451** | | **2000** | **82** | 1630 | 1406 | 1206 | 1026 | **1315** | | | **4000** | **79** | 1457 | 1238 | 1041 | 864 | **1180** | | | **6000** | **75** | 1286 | 1070 | 877 | 703 | **1045** | | | **8000** | **72** | 1114 | 902 | 713 | 542 | **909** | | | **10000** | **69** | 944 | 735 | 549 | 382 | **774** | | | **12000** | **65** | 774 | 569 | 387 | 222 | **639** | | | **14000** | **62** | 604 | 404 | 224 | 63 | **503** | | *** ### Enroute Rate Of Climb |Power Setting: Maximum Continuous Power
Flaps: Up
Landing Gear: Up
| | | | | | | | | ---------------------------------------------------------------------------------------------------------------------------------------- | ---------------------------------------------------------------------- | --------------------------------------------------------------------- | --------------------------- | ---- | ---- | -------- | -------- | |Weight
\[kg]
|Pressure Altitude
\[ft]
|Climb Speed VY
\[KIAS]
| **Rate of Climb \[ft/min]** | | | | | | **Temperature \[°C]** | **ISA** | | | | | | | | **-25** | **0** | **25** | **50** | | | | | | 1180 | **S.L.** | **84** | 1392 | 1205 | 1038 | 887 | **1102** | | **2000** | **83** | 1249 | 1066 | 901 | 753 | **991** | | | **4000** | **81** | 1108 | 927 | 766 | 620 | **880** | | | **6000** | **79** | 966 | 789 | 630 | 487 | **768** | | | **8000** | **77** | 826 | 651 | 495 | 355 | **657** | | | **10000** | **75** | 685 | 514 | 361 | 223 | **546** | | | **12000** | **73** | 545 | 377 | 227 | 92 | **434** | | | **14000** | **71** | 406 | 241 | 93 | -39 | **323** | | | 930 | **S.L.** | **82** | 1873 | 1649 | 1449 | 1269 | **1527** | | **2000** | **81** | 1703 | 1483 | 1286 | 1109 | **1393** | | | **4000** | **79** | 1533 | 1317 | 1124 | 950 | **1260** | | | **6000** | **77** | 1364 | 1151 | 962 | 791 | **1127** | | | **8000** | **75** | 1196 | 987 | 800 | 632 | **994** | | | **10000** | **73** | 1028 | 823 | 639 | 474 | **861** | | | **12000** | **71** | 860 | 659 | 479 | 317 | **727** | | | **14000** | **69** | 693 | 496 | 319 | 160 | **594** | | *** ### One-Engine Rate Of Climb |Power Setting: Maximum Continuous Power (operative engine), propeller feathered (inoperative engine)
Flaps: Up
Landing Gear: Up
| | | | | | | | | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ---------------------------------------------------------------------- | --------------------------------------------------------------------- | --------------------------- | --- | ---- | ------- | ------- | |Weight
\[kg]
|Pressure Altitude
\[ft]
|Climb Speed VY
\[KIAS]
| **Rate of Climb \[ft/min]** | | | | | | **Temperature \[°C]** | **ISA** | | | | | | | | **-25** | **0** | **25** | **50** | | | | | | 1180 | **S.L.** | **80** | 362 | 261 | 171 | 89 | **206** | | **1000** | **80** | 324 | 224 | 134 | 53 | **176** | | | **2000** | **80** | 285 | 186 | 97 | 17 | **146** | | | **3000** | **79** | 247 | 148 | 60 | -19 | **116** | | | **4000** | **79** | 209 | 111 | 24 | -55 | **85** | | | **5000** | **79** | 171 | 74 | -13 | -91 | **55** | | | **6000** | **79** | 132 | 36 | -49 | -127 | **25** | | | **7000** | **78** | 94 | -1 | -86 | -163 | **-5** | | | 930 | **S.L.** | **79** | 574 | 455 | 349 | 253 | **390** | | **1000** | **79** | 529 | 411 | 305 | 211 | **355** | | | **2000** | **79** | 483 | 367 | 262 | 168 | **319** | | | **3000** | **78** | 438 | 322 | 219 | 126 | **284** | | | **4000** | **78** | 393 | 278 | 176 | 83 | **248** | | | **5000** | **78** | 348 | 235 | 133 | 41 | **213** | | | **6000** | **78** | 304 | 191 | 90 | -1 | **178** | | | **7000** | **77** | 259 | 147 | 47 | -43 | **142** | | *** ### Cruise Performances |Weight: 1150 kg
Pressure Altitude: 0 ft
| | | | | | | | | | | | -------------------------------------------------------------------------------------- | ---------------------------------------------------------- | ---------------------------------------------------------------- | -------------- | --------------------- | ---------------------------------------------------------------- | ------- | -------- | ---------------------------------------------------------------- | --- | ---- | | **RPM\*** |MAP
\[inHg]
| **ISA - 30°C (-15°C)** | **ISA (15°C)** | **ISA + 30°C (45°C)** | | | | | | | | **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| | | | **2250** | **29.5** | 103% | 143 | 28.6 | 97% | 145 | 27.1 | 92% | 146 | 25.8 | | **2250** | **28** | 88% | 134 | 24.5 | 83% | 136 | 23.2 | 79% | 138 | 22 | | **2250** | **26** | 69% | 122 | 19.2 | 65% | 124 | 18.2 | 62% | 125 | 17.3 | | **2250** | **24** | 59% | 115 | 16.6 | 56% | 116 | 15.7 | 53% | 117 | 14.9 | | **2250** | **22** | 46% | 103 | 12.8 | 43% | 103 | 12.1 | 41% | 103 | 11.5 | | **2250** | **20** | 39% | 96 | 11 | 37% | 95 | 10.4 | 35% | 94 | 9.9 | | **2100** | **28** | 84% | 132 | 23.5 | 80% | 134 | 22.2 | 76% | 135 | 21.1 | | **2100** | **26** | 66% | 121 | 18.5 | 63% | 122 | 17.5 | 60% | 123 | 16.7 | | **2100** | **24** | 57% | 114 | 16 | 54% | 114 | 15.1 | 52% | 115 | 14.4 | | **2100** | **22** | 43% | 100 | 12.1 | 41% | 100 | 11.5 | 39% | 100 | 10.9 | | **2100** | **20** | 37% | 92 | 10.2 | 35% | 91 | 9.7 | 33% | 89 | 9.2 | | **1900** | **26** | 61% | 117 | 17.1 | 58% | 118 | 16.2 | 55% | 119 | 15.4 | | **1900** | **24** | 53% | 110 | 14.9 | 50% | 111 | 14.1 | 48% | 111 | 13.4 | | **1900** | **22** | 41% | 97 | 11.4 | 39% | 97 | 10.8 | 37% | 96 | 10.2 | | **1900** | **20** | 35% | 89 | 9.6 | 33% | 88 | 9.1 | 31% | 85 | 8.7 | |\*Propeller RPM
\*\*Fuel Consumption for each Engine
| | | | | | | | | | | |Weight: 1150 kg
Pressure Altitude: 3000 ft
| | | | | | | | | | | | ----------------------------------------------------------------------------------------- | ---------------------------------------------------------- | ---------------------------------------------------------------- | -------------- | --------------------- | ---------------------------------------------------------------- | ------- | -------- | ---------------------------------------------------------------- | --- | ---- | | **RPM\*** |MAP
\[inHg]
| **ISA - 30°C (-15°C)** | **ISA (15°C)** | **ISA + 30°C (45°C)** | | | | | | | | **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| | | | **2388** | **26.4** | 92% | 141 | 25.7 | 87% | 143 | 24.3 | 83% | 144 | 21.1 | | **2250** | **26.4** | 89% | 139 | 25 | 85% | 141 | 23.6 | 80% | 143 | 22.4 | | **2250** | **26** | 85% | 137 | 23.9 | 81% | 138 | 22.6 | 77% | 140 | 21.5 | | **2250** | **24** | 72% | 128 | 20 | 68% | 129 | 18.9 | 64% | 130 | 18 | | **2250** | **22** | 57% | 116 | 16 | 54% | 117 | 15.1 | 51% | 118 | 14.3 | | **2250** | **20** | 48% | 108 | 13.4 | 45% | 108 | 12.7 | 43% | 108 | 12.1 | | **2250** | **26.4** | 85% | 137 | 23.9 | 81% | 138 | 22.6 | 77% | 140 | 21.4 | | **2100** | **26** | 82% | 134 | 22.8 | 77% | 136 | 21.6 | 73% | 137 | 20.5 | | **2100** | **24** | 69% | 125 | 19.2 | 65% | 127 | 18.1 | 62% | 128 | 17.2 | | **2100** | **22** | 54% | 114 | 15.2 | 51% | 114 | 14.3 | 49% | 115 | 13.6 | | **2100** | **20** | 45% | 104 | 12.6 | 43% | 104 | 11.9 | 41% | 104 | 11.3 | | **2100** | **26.4** | 78% | 132 | 21.9 | 74% | 134 | 20.7 | 70% | 135 | 19.6 | | **1900** | **26** | 75% | 130 | 20.9 | 71% | 131 | 19.8 | 67% | 132 | 18.8 | | **1900** | **24** | 63% | 121 | 17.7 | 60% | 122 | 16.7 | 57% | 123 | 15.9 | | **1900** | **22** | 50% | 110 | 14.1 | 48% | 110 | 13.3 | 45% | 110 | 12.6 | | **1900** | **20** | 42% | 101 | 11.7 | 40% | 101 | 11.1 | 38% | 100 | 10.6 | |\*Propeller RPM
\*\*Fuel Consumption for each Engine
| | | | | | | | | | | |Weight: 1150 kg
Pressure Altitude: 6000 ft
| | | | | | | | | | | | ----------------------------------------------------------------------------------------- | ---------------------------------------------------------- | ---------------------------------------------------------------- | -------------- | --------------------- | ---------------------------------------------------------------- | ------- | -------- | ---------------------------------------------------------------- | --- | ---- | | **RPM\*** |MAP
\[inHg]
| **ISA - 30°C (-15°C)** | **ISA (15°C)** | **ISA + 30°C (45°C)** | | | | | | | | **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| | | | **2388** | **26.4** | 92% | 141 | 25.7 | 87% | 143 | 24.3 | 83% | 144 | 21.1 | | **2250** | **26.4** | 89% | 139 | 25 | 85% | 141 | 23.6 | 80% | 143 | 22.4 | | **2250** | **26** | 85% | 137 | 23.9 | 81% | 138 | 22.6 | 77% | 140 | 21.5 | | **2250** | **24** | 72% | 128 | 20 | 68% | 129 | 18.9 | 64% | 130 | 18 | | **2250** | **22** | 57% | 116 | 16 | 54% | 117 | 15.1 | 51% | 118 | 14.3 | | **2250** | **20** | 48% | 108 | 13.4 | 45% | 108 | 12.7 | 43% | 108 | 12.1 | | **2250** | **26.4** | 85% | 137 | 23.9 | 81% | 138 | 22.6 | 77% | 140 | 21.4 | | **2100** | **26** | 82% | 134 | 22.8 | 77% | 136 | 21.6 | 73% | 137 | 20.5 | | **2100** | **24** | 69% | 125 | 19.2 | 65% | 127 | 18.1 | 62% | 128 | 17.2 | | **2100** | **22** | 54% | 114 | 15.2 | 51% | 114 | 14.3 | 49% | 115 | 13.6 | | **2100** | **20** | 45% | 104 | 12.6 | 43% | 104 | 11.9 | 41% | 104 | 11.3 | | **2100** | **26.4** | 78% | 132 | 21.9 | 74% | 134 | 20.7 | 70% | 135 | 19.6 | | **1900** | **26** | 75% | 130 | 20.9 | 71% | 131 | 19.8 | 67% | 132 | 18.8 | | **1900** | **24** | 63% | 121 | 17.7 | 60% | 122 | 16.7 | 57% | 123 | 15.9 | | **1900** | **22** | 50% | 110 | 14.1 | 48% | 110 | 13.3 | 45% | 110 | 12.6 | | **1900** | **20** | 42% | 101 | 11.7 | 40% | 101 | 11.1 | 38% | 100 | 10.6 | |\*Propeller RPM
\*\*Fuel Consumption for each Engine
| | | | | | | | | | | |Weight: 1150 kg
Pressure Altitude: 9000 ft
| | | | | | | | | | | | ----------------------------------------------------------------------------------------- | ---------------------------------------------------------- | ---------------------------------------------------------------- | -------------- | --------------------- | ---------------------------------------------------------------- | ------- | -------- | ---------------------------------------------------------------- | --- | ---- | | **RPM\*** |MAP
\[inHg]
| **ISA - 30°C (-15°C)** | **ISA (15°C)** | **ISA + 30°C (45°C)** | | | | | | | | **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| **PWR** | **KTAS** |F.C.\*\*
\[lt/hr]
| | | | **2388** | **21.1** | 75% | 137 | 20.9 | 71% | 139 | 19.7 | 67% | 140 | 18.7 | | **2250** | **21.1** | 73% | 136 | 20.3 | 69% | 137 | 19.2 | 65% | 138 | 18.2 | | **2250** | **20** | 65% | 130 | 18.3 | 62% | 131 | 17.2 | 58% | 131 | 16.3 | | **2250** | **18** | 53% | 118 | 14.9 | 50% | 119 | 14 | 48% | 118 | 13.3 | | **2100** | **21.1** | 69% | 133 | 19.4 | 65% | 134 | 18.3 | 62% | 135 | 17.4 | | **2100** | **20** | 62% | 127 | 17.4 | 59% | 128 | 16.4 | 56% | 128 | 15.6 | | **2100** | **18** | 51% | 116 | 14.2 | 48% | 116 | 13.4 | 46% | 116 | 12.7 | | **1900** | **21.1** | 64% | 128 | 17.8 | 60% | 129 | 16.8 | 57% | 130 | 15.9 | | **1900** | **20** | 57% | 122 | 16 | 54% | 123 | 15.1 | 51% | 123 | 14.3 | | **1900** | **18** | 47% | 112 | 13.2 | 44% | 112 | 12.4 | 42% | 111 | 11.8 | |\*Propeller RPM
\*\*Fuel Consumption for each Engine
| | | | | | | | | | | *** ### Landing Performances |Weight = 1150kg
Flaps: LAND
Short Final Approach Speed: 70 KIAS
Throttle Levers: Idle
Runway: Grass
|Corrections
Headwind: -5m for each kt (16 ft/kt)
Tailwind: +11m for each kt (36 ft/kt)
Paved Runway: -2% to Ground Roll
Runway slope: -2.5% to Ground Roll for each +1%
| | | | | | | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------------------ | ------ | --- | ------- | ------- | | **Pressure Altitude \[ft]** | | **Dinstance \[m]** | | | | | | **Temperature \[°C]** | **ISA** | | | | | | | **-25** | **0** | **25** | **50** | | | | | **S.L.** | **Ground Roll** | 183 | 202 | 220 | 238 | **213** | | ***At 50 ft AGL*** | 288 | 312 | 335 | 358 | **326** | | | **1000** | **Ground Roll** | 190 | 209 | 228 | 247 | **219** | | ***At 50 ft AGL*** | 297 | 324 | 345 | 369 | **334** | | | **2000** | **Ground Roll** | 197 | 217 | 237 | 256 | **226** | | ***At 50 ft AGL*** | 306 | 331 | 356 | 381 | **342** | | | **3000** | **Ground Roll** | 204 | 225 | 245 | 266 | **232** | | ***At 50 ft AGL*** | 325 | 352 | 379 | 405 | **360** | | | **4000** | **Ground Roll** | 212 | 233 | 255 | 276 | **239** | | ***At 50 ft AGL*** | 325 | 352 | 379 | 405 | **360** | | | **5000** | **Ground Roll** | 220 | 242 | 264 | 287 | **247** | | ***At 50 ft AGL*** | 335 | 363 | 391 | 418 | **369** | | | **6000** | **Ground Roll** | 228 | 251 | 275 | 298 | **254** | | ***At 50 ft AGL*** | 346 | 375 | 403 | 431 | **378** | | | **7000** | **Ground Roll** | 237 | 261 | 285 | 309 | **262** | | ***At 50 ft AGL*** | 357 | 387 | 416 | 445 | **388** | | |Weight = 930kg
Flaps: LAND
Short Final Approach Speed: 70 KIAS
Throttle Levers: Idle
Runway: Grass
|Corrections
Headwind: -5m for each kt (16 ft/kt)
Tailwind: +11m for each kt (36 ft/kt)
Paved Runway: -2% to Ground Roll
Runway slope: -2.5% to Ground Roll for each +1%
| | | | | | | ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------------------ | ------ | --- | ------- | ------- | | **Pressure Altitude \[ft]** | | **Dinstance \[m]** | | | | | | **Temperature \[°C]** | **ISA** | | | | | | | **-25** | **0** | **25** | **50** | | | | | **S.L.** | **Ground Roll** | 150 | 166 | 181 | 196 | **175** | | ***At 50 ft AGL*** | 233 | 252 | 271 | 290 | **264** | | | **1000** | **Ground Roll** | 156 | 172 | 187 | 203 | **180** | | ***At 50 ft AGL*** | 240 | 260 | 280 | 299 | **270** | | | **2000** | **Ground Roll** | 162 | 178 | 194 | 211 | **185** | | ***At 50 ft AGL*** | 248 | 268 | 288 | 309 | **277** | | | **3000** | **Ground Roll** | 168 | 185 | 202 | 219 | **191** | | ***At 50 ft AGL*** | 263 | 285 | 307 | 328 | **291** | | | **4000** | **Ground Roll** | 174 | 192 | 209 | 227 | **197** | | ***At 50 ft AGL*** | 263 | 285 | 307 | 328 | **291** | | | **5000** | **Ground Roll** | 181 | 199 | 217 | 235 | **203** | | ***At 50 ft AGL*** | 272 | 294 | 317 | 339 | **299** | | | **6000** | **Ground Roll** | 188 | 207 | 226 | 244 | **209** | | ***At 50 ft AGL*** | 280 | 304 | 327 | 350 | **307** | | | **7000** | **Ground Roll** | 195 | 215 | 234 | 254 | **215** | | ***At 50 ft AGL*** | 289 | 313 | 338 | 361 | **315** | | *** ### Balked Landing Climb Gradient Flight conditions (ISA and SL): * **Weight:** 1180kg * **Throttle levers:** Both FULL FORWARD * **Flaps:** T/O * **Landing Gear:** DOWN * **Weight:** MTOW (1180 kg) * **Speed:** 66KIAS * **Climb Gradient:** 10.8% (6.2°)