performance tables
DESCRIPTION
thtrjukuyksnsxTRANSCRIPT
Revision: 28.11.2007Page 1
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Limitations
Airspeed LimitationsCheyenne I Cheyenne IA Cheyenne II Cheyenne IIXL
KCAS KIAS KCAS KIAS KCAS KIAS KCAS KIASVMO 246 240 246 240 246 242 246 242VA 180 177 180 177 187 184 187 184VFE - 15° Flaps 174 171 174 171 174 181 174 181VFE - 40° Flaps 143 141 143 141 144 148 144 148VLE 156 154 156 154 156 153 156 153VLO 156 154 156 154 156 153 156 153VMCA 90 85 90 85 96 91 96 91Best single engine rate of climb speed
122 118 122 118
Stall speed(full flaps, power off)
77 72 77 72 76 75 80 77
Note:Minimum altitude loss in a stall is
800 ft. 600 ft. 750 ft. 800 ft.
Best multi engine rate of climb speed
126 123 126 123 126 122 120 116
Service CeilingCheyenne I Cheyenne IA Cheyenne II Cheyenne IIXL
29.000 ft. 29.000 ft. 29.000 ft. 31.000 ft
Revision: 28.11.2007Page 2
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Airspeed Indicator MarginsCheyenne I Cheyenne IA Cheyenne II Cheyenne IIXL
Green arc (normal operating range)
84 - 240 KIAS 84 - 240 KIAS 86 - 242 KIAS 86 - 242 KIAS
White arc (flaps extend range)
72 - 148 KIAS 72 - 148 KIAS 77 - 148 KIAS 77 - 148 KIAS
Radial red line (air minimum control speed)
85 KIAS 85 KIAS 91 KIAS 91 KIAS
Radial blue line (best rate of climb speed - single engine)
110 KIAS 110 KIAS 113 KIAS 118 KIAS
Power Plant LimitationsCheyenne I Cheyenne IA Cheyenne II Cheyenne IIXL
Tachometer (Propeller) Green arc (normal operation) Yellow arc (caution) Radial red line (maximum)
1800 - 2000 RPM 1800 - 2000 RPM 1800 - 2200 RPM 1800 - 1900 RPM2000 - 2200 RPM 2000 - 2200 RPM 2000 - 2200 RPM
2200 RPM 2200 RPM 2200 RPM 1900 RPMTachometer (Gas Generator) Green arc (normal operation) Radial red line (maximum)
51 - 101,5% 51 - 101,5% 51 - 101,5% 51 - 101,5%101,5% 101,5% 101,5% 101,5%
Fuel Pressure Green arc (normal operation) Yellow arc (caution) Radial red line (minimum)
15 - 50 PSI 15 - 50 PSI 15 - 50 PSI 15 - 50 PSI5 - 15 PSI 5 - 15 PSI 5 - 15 PSI 5 - 15 PSI
5 PSI 5 PSI 5 PSI 5 PSIFuel Flow (green arc) .5 - 5 PPH x 100 .5 - 5 PPH x 100 .5 - 5 PPH x 100 .5 - 5 PPH x 100Oil Pressure Green arc (normal operation) Yellow arc (caution)Radial red line (minimum) Radial red line (minimum)
80 - 100 PSI 80 - 100 PSI 80 - 100 PSI 85 - 105 PSI40 - 80 PSI 40 - 80 PSI 40 - 80 PSI 40 - 85 PSI
100 PSI 100 PSI 100 PSI 105 PSI40 PSI 40 PSI 40 PSI 40 PSI
Oil Temperature Green arc (normal operation) Yellow arc (caution) Radial red line (maximum)
55°C - 99°C 55°C - 99°C 55°C - 99°C 55°C - 99°C0°C - 55°C 0°C - 55°C 0°C - 55°C 0°C - 55°C
99°C 99°C 99°C 99°CITT green arc (normal ops)Radial red line (maximum)
500°C - 685°C 500°C - 685°C 500°C - 695°C 400°C - 805°C700°C 700°C 750°C 805°C
Engine Torque green arc Radial red line (maximum)
0 - 1194 lb-ft 0 - 1194 lb-ft 0 - 1484 lb-ft 0 - 1714 lb-ft1194 lb-ft 1194 lb-ft 1484 lb-ft 1714 lb-ft
Revision: 28.11.2007Page 3
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne I
Maximum Cruise Power - 1900 RPM - ISA
Pressure Altitude
ft.
IOAT Torque per Eng. Lb. Ft.
Fuel Flow per Eng. Lb./Hr.
Total Fuel Flow Lb./
Hr.
Airspeed - KTS
°F °C 8700 Lb. 8000 Lb. 7000 Lb.CAS TAS CAS TAS CAS TAS
Sea Level 65 18 1194 316 632 207 207 210 210 213 2132.000 58 14 1194 308 616 206 212 209 215 212 2184.000 51 10 1194 300 600 204 217 208 221 212 2256.000 44 6 1194 292 584 202 222 206 226 211 2318.000 37 3 1194 288 576 200 227 204 231 209 23610.000 30 -1 1194 283 566 198 232 202 236 207 24112.000 23 -5 1194 276 552 196 236 200 240 205 24514.000 16 -9 1185 272 544 193 240 196 243 199 24916.000 9 -13 1120 259 518 186 238 189 241 193 24618.000 2 -17 1065 246 492 179 236 182 240 186 24520.000 -5 -21 1005 232 464 171 234 174 238 178 24422.000 -12 -25 945 218 436 163 231 166 236 170 24124.000 -19 -29 880 206 412 154 226 158 232 162 23826.000 -27 -34 815 192 384 144 219 149 226 153 23329.000 -38 -39 705 170 340 128 204 135 215 142 227
Performance
Revision: 28.11.2007Page 4
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne I
Maximum Cruise Power - 2000 RPM - ISA
Sea Level 65 18 1194 324 648 213 213 216 216 219 2192.000 58 14 1194 316 632 212 218 215 221 218 2344.000 51 10 1194 308 616 210 223 214 227 218 2316.000 44 6 1194 302 604 208 228 212 232 217 2378.000 37 3 1194 296 592 206 233 210 237 216 24210.000 30 -1 1194 290 580 204 238 208 242 212 24712.000 23 -5 1194 283 566 202 243 202 246 209 25114.000 16 -9 1145 272 544 196 243 196 247 203 25216.000 9 -13 1057 259 518 189 242 192 246 197 25018.000 2 -17 1029 246 492 182 241 184 244 187 24820.000 -5 -21 972 232 464 174 238 177 242 180 24622.000 -12 -25 914 218 436 165 234 168 238 172 24424.000 -19 -29 833 206 412 156 229 160 234 164 24126.000 -27 -34 788 192 384 146 222 151 229 155 23629.000 -38 -39 683 170 340 129 207 136 218 143 230
Revision: 28.11.2007Page 5
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA
Maximum Cruise Power - 1800 RPM - ISA
Sea Level 65 18 1194 304 609 215 215 216 216 218 2182.000 58 14 1194 239 591 212 219 214 220 216 2224.000 51 10 1194 288 576 210 222 211 224 213 2266.000 44 6 1194 280 560 207 226 209 238 211 2318.000 37 2 1194 274 547 204 231 206 233 208 23510.000 30 -1 1194 269 539 202 235 204 237 206 24012.000 23 -5 1194 266 532 199 239 201 241 203 24414.000 16 -9 1194 264 527 196 244 198 246 201 24916.000 9 -13 1194 262 525 193 248 196 251 198 25418.000 2 -17 1168 257 514 188 250 191 253 194 25720.000 -5 -21 1100 242 484 180 247 183 251 187 25622.000 -12 -25 1031 227 454 172 244 175 249 179 25424.000 -19 -28 960 213 425 162 238 167 244 171 25226.000 -27 -32 890 197 395 151 230 157 239 163 24829.000 -38 -38 772 172 344 - - 138 220 147 237
Revision: 28.11.2007Page 6
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA
Maximum Cruise Power - 1900 RPM - ISA
Sea Level 65 18 1194 313 625 218 218 220 220 221 2212.000 58 14 1194 304 608 216 222 217 224 219 2264.000 51 10 1194 296 591 213 226 215 228 217 2306.000 44 6 1194 287 573 211 231 213 232 214 2348.000 37 2 1194 282 563 208 235 210 237 212 23910.000 30 -1 1194 277 554 205 239 207 241 209 24312.000 23 -5 1194 275 549 203 244 205 246 207 24814.000 16 -9 1194 276 546 200 248 202 251 204 25316.000 9 -13 1194 274 548 198 253 200 256 203 26018.000 2 -17 1135 258 516 190 252 193 255 195 25920.000 -5 -21 1063 242 485 182 249 184 253 188 25722.000 -12 -25 994 227 454 173 245 176 250 180 25524.000 -19 -28 928 213 425 164 240 168 247 172 25326.000 -27 -32 867 199 398 154 234 159 242 164 25029.000 -38 -38 747 173 345 - - 139 224 149 238
Revision: 28.11.2007Page 7
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA
Maximum Cruise Power - 2000 RPM - ISA
Sea Level 65 18 1194 321 642 222 222 223 223 226 2262.000 58 14 1194 312 623 219 226 221 228 224 2314.000 51 10 1194 304 608 217 230 218 232 221 2356.000 44 6 1194 295 591 214 234 216 236 219 2398.000 37 2 1194 290 580 212 239 213 241 216 24410.000 30 -1 1194 285 571 209 243 211 245 214 24912.000 23 -5 1194 283 566 206 248 208 250 211 25414.000 16 -9 1194 283 567 204 253 206 255 209 26016.000 9 -13 1168 275 550 199 255 207 257 205 26318.000 2 -17 1099 259 517 191 253 193 256 197 26120.000 -5 -21 1029 243 485 182 250 185 254 190 26022.000 -12 -25 962 228 455 174 246 177 251 182 25824.000 -19 -28 899 213 126 165 242 169 248 174 25626.000 -27 -32 840 200 399 155 236 161 244 167 25329.000 -38 -38 724 173 346 130 208 142 227 151 242
Revision: 28.11.2007Page 8
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II
Maximum Cruise Power - 1900 RPM - ISA
Pressure Altitude
ft.
IOAT Torque per Eng. Lb. Ft.
Fuel Flow per Eng. Lb./Hr.
Total Fuel Flow Lb./
Hr.
Airspeed - KTS
°F °C 9000 Lb. 8000 Lb. 7000 Lb.CAS TAS CAS TAS CAS TAS
Sea Level
For values below 10.000 ft. refer to economy cruise power tables2.0004.0006.0008.00010.000 28 -2 1628 365 730 233 271 236 274 239 27812.000 21 -6 1580 341 682 227 272 229 275 233 28014.000 14 -10 1485 318 636 218 270 221 273 225 27916.000 7 -14 1380 300 600 207 266 212 272 215 27618.000 0 -18 1280 280 560 199 263 202 268 206 27320.000 -9 -23 1195 260 520 188 258 193 264 197 27122.000 -17 -27 1115 243 486 178 253 183 260 188 26724.000 -24 -31 1045 227 454 168 248 175 256 180 26426.000 -31 -35 960 221 422 159 243 166 252 171 26029.000 -43 -42 870 190 380 145 233 152 244 158 254
Revision: 28.11.2007Page 9
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II
Maximum Cruise Power - 2000 RPM - ISA
Sea Level
For values below 10.000 ft. refer to economy cruise power tables2.0004.0006.0008.00010.000 28 -2 1628 365 730 238 277 241 281 244 28512.000 21 -6 1535 344 688 231 277 235 281 238 28614.000 14 -10 1445 322 344 222 274 226 279 229 28416.000 7 -14 1350 304 608 212 271 216 277 220 28118.000 0 -18 1260 284 568 202 267 207 273 211 27920.000 -9 -23 1180 265 530 192 262 196 269 202 27622.000 -17 -27 1100 248 496 182 258 188 266 193 27324.000 -24 -31 1040 232 464 172 253 174 262 184 27026.000 -31 -35 960 217 434 163 248 169 257 175 26729.000 -42 -41 870 196 392 149 240 156 250 162 261
Revision: 28.11.2007Page 10
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II
Economy Cruise Power - 1900 RPM - ISA
Pressure Altitude
ft.
IOAT Torque per Eng. Lb. Ft.
Fuel Flow per Eng. Lb./Hr.
Total Fuel Flow Lb./
Hr.
Airspeed - KTS
°F °C 9000 Lb. 8000 Lb. 7000 Lb.CAS TAS CAS TAS CAS TAS
Sea Level 63 17 1628 368 736 246 246 246 246 246 2462.000 55 13 1628 362 724 242 249 246 253 246 2534.000 48 9 1628 356 172 241 256 243 258 246 2616.000 41 5 1580 346 692 235 257 238 261 241 2638.000 34 1 1500 328 656 227 256 230 260 234 26310.000 27 -3 1420 310 620 218 254 221 258 226 26312.000 19 -7 1330 291 582 209 252 214 257 217 26114.000 12 -11 1255 273 546 201 249 205 255 209 26016.000 5 -15 1175 257 214 192 247 196 252 201 25818.000 -2 -19 1085 240 480 182 242 188 249 192 25620.000 -11 -24 1040 227 454 174 239 180 247 184 25322.000 -18 -28 975 212 424 165 235 171 243 176 25024.000 -26 -32 905 198 396 155 228 162 239 168 24826.000 -33 -36 840 185 370 147 223 154 234 160 24329.000 -44 -42 760 165 330 128 205 139 223 147 235
Revision: 28.11.2007Page 11
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II
Economy Cruise Power - 2000 RPM - ISA
Sea Level 63 17 1628 377 754 246 246 246 246 246 2462.000 55 13 1628 372 744 246 253 246 253 246 2534.000 48 9 1590 363 726 245 261 246 261 246 2616.000 41 5 1515 346 692 237 261 241 263 243 2668.000 34 1 1444 328 656 230 260 234 263 236 26610.000 27 -3 1365 311 622 221 258 225 262 228 26512.000 19 -7 1285 292 584 213 255 216 260 220 26414.000 12 -11 1215 275 550 204 254 208 258 212 26316.000 5 -15 1140 259 518 195 250 200 255 204 26118.000 -2 -19 1055 243 486 187 248 191 253 195 25920.000 -11 -24 1015 230 460 178 244 183 250 188 25722.000 -18 -28 950 215 430 169 240 175 248 180 25524.000 -26 -32 890 202 404 160 235 167 245 172 25226.000 -33 -36 830 189 378 151 229 157 239 163 24629.000 -44 -42 755 171 342 137 220 144 231 151 242
Revision: 28.11.2007Page 12
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IIXL
Maximum Cruise Power - 1900 RPM - ISA
Pressure Altitude
ft.
Torque per Eng. Lb. Ft.
Fuel Flow per Eng. Lb./Hr.
Total Fuel Flow Lb./
Hr.
Airspeed - KTS
IOAT OAT 9474 Lb. 8500 Lb. 7500 Lb.°C °C CAS TAS CAS TAS CAS TAS
Sea Level 19 15 1714 402 804 242 242 243 243 244 2442.000 15 11 1714 391 782 240 247 241 248 242 2494.000 12 7 1714 381 762 238 252 241 253 240 2546.000 8 3 1714 374 748 235 257 236 258 237 2598.000 4 -1 1714 367 734 232 261 233 262 234 26310.000 0 -5 1714 362 724 229 266 230 267 231 26812.000 -4 -9 1714 357 714 226 271 227 273 228 27414.000 -7 -13 1660 350 700 221 274 223 277 225 27916.000 -11 -17 1550 327 654 212 272 214 274 216 27718.000 -16 -21 1445 307 614 203 269 205 272 207 27520.000 -20 -25 1355 287 574 195 267 197 270 199 27322.000 -24 -29 1270 270 540 186 264 189 268 192 27124.000 -28 -33 1185 255 510 178 261 181 266 184 26926.000 -32 -37 1110 238 476 169 256 173 262 177 26629.000 -37 -42 990 212 424 154 246 159 255 163 26131.000 -41 -46 910 197 394 143 238 150 250 155 258
Revision: 28.11.2007Page 13
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne I - Takeoff Power Settings
Revision: 28.11.2007Page 14
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA - Takeoff Power Settings
Revision: 28.11.2007Page 15
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II - Takeoff Power Settings
Revision: 28.11.2007Page 16
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IIXL - Takeoff Power Settings
Revision: 28.11.2007Page 17
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne I - Takeoff distance over 50 feet
Revision: 28.11.2007Page 18
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA - Takeoff distance over 50 feet
Revision: 28.11.2007Page 19
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II - Takeoff distance over 50 feet
Revision: 28.11.2007Page 20
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IIXL - Takeoff distance over 50 feet
Revision: 28.11.2007Page 21
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne I - Max climb power (torque)
Revision: 28.11.2007Page 22
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA - Max climb power (torque)
Revision: 28.11.2007Page 23
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II - Max climb power (torque)
Revision: 28.11.2007Page 24
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IIXL - max climb power (torque)
Revision: 28.11.2007Page 25
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne I - Time, fuel and distance to climb
Revision: 28.11.2007Page 26
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA - Time, fuel and distance to climb
Revision: 28.11.2007Page 27
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II - Time, fuel and distance to climb
Revision: 28.11.2007Page 28
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IIXL - Time, fuel and distance to climb
Revision: 28.11.2007Page 29
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne I - Speed vs. Altitude
Revision: 28.11.2007Page 30
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA - Speed vs. Altitude
Revision: 28.11.2007Page 31
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II - Speed vs. Altitude
Revision: 28.11.2007Page 32
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IIXL - Speed vs. Altitude
Revision: 28.11.2007Page 33
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne I - Endurance profile
Revision: 28.11.2007Page 34
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA - Endurance profile
Revision: 28.11.2007Page 35
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II - Endurance profile
Revision: 28.11.2007Page 36
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IIXL - Endurance profile
Revision: 28.11.2007Page 37
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne I - Range profile
Revision: 28.11.2007Page 38
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA - Range profile
Revision: 28.11.2007Page 39
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II - Range profile
Revision: 28.11.2007Page 40
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IIXL - Range profile
Revision: 28.11.2007Page 41
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne I - Time, fuel and distance to descend
Revision: 28.11.2007Page 42
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA - Time, fuel and distance to descend
Revision: 28.11.2007Page 43
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II - Time, fuel and distance to descend
Revision: 28.11.2007Page 44
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IIXL - Time, fuel and distance to descend
Revision: 28.11.2007Page 45
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne I - Landing distance over 50 feet
Revision: 28.11.2007Page 46
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IA - Landing distance over 50 feet
Revision: 28.11.2007Page 47
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne II - Landing distance over 50 feet
Revision: 28.11.2007Page 48
Performance TablesPiper Cheyenne I, IA, II, IIXL
For flight simulation use only
Cheyenne IIXL - Landing distance over 50 feet