be20 ptm chapter 18 w&b perf charts
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DESCRIPTION
PROCEDIMIENTOS, TABLAS Y CARTAS DEL PERFORMANCE A SER APLICADOS AL BEECHCRAFT SUPERKING 200 BE20, CONOCIDO COMO CAPITULO 18 DEL PTMTRANSCRIPT
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-85
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-86 Reference Material: Revision IR: April 29, 2009
0 2 4 6 8 10 12 14 16 18 200
5
10
15
20
25
30
35
299
NOTES: RANGE INCLUDES START, TAXI, CLIMB, DESCENT AND 45 MINUTES RESERVE FUEL AT MAXIMUM RANGE POWER.
EXAMPLE:PRESSURE ALTITUDE... 26,000 FTFUEL................................ 3,645 LBSRANGE............................ 1,347 NM
ASSOCIATED CONDITIONS:WEIGHT.............. 12,500 LBS BEFORE ENGINE STARTFUEL.................... AVIATION KEROENEFUEL DENSITY... 6.7 LB/GALICE VANES.......... RETRACTED
CR
UIS
E C
LIM
B D
ISTA
NC
E
3645
LBS
(544
GAL)
FUL
L M
AIN
AND
AUX
TANK
S
1590
LB
S (2
37 G
AL)
AVA
ILA
BLE
FU
EL A
T M
AX
ZER
O F
UEL
WT
CRUISE TRUE AIRSPEED~ KNOTS
PRES
SUR
E A
LTIT
UD
E ~
1000
FT
RANGE ~ 100 NAUTICAL MILES
245249
254
260
265
270
276
281
287
292
298
305
310
308307
304
297
287
309
250
255
260
265
270
276
282
288
293
306
310
311310
309
306
300
290
245 245250
255
261
266
271
277
282
288
294
300
307
311
312312
311
308
302
294
2586
LBS
(386
GAL
) FUL
L M
AIN
TANK
S
RANGE PROFILE - NORMAL CRUISE POWER1800 RPM
STANDARD DAY (ISA)ZERO WIND
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-87
MAXIMUM CRUISE POWER 1800 RPM ISA -30C
NOTE: 1. IOAT, TORQUE AND FUEL FLOW BASED ON 11,000 POUNDS GROSS
WEIGHT. 2. DURING OPERATION WITH ICE VANES EXTENDED, TRUE AIRSPEED WILL
BE REDUCED IF ORIGINAL TORQUE IS NOT OR CANNOT BE RESET, BUT WILL BE UNCHANGED IF ORIGINAL TORQUE IS RESET.
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 -10 -15 2230 473 947 251 237 252 238 253 239
2,000 -14 -19 2230 460 920 249 242 250 243 250 243
4,000 -18 -23 2230 447 894 246 246 247 247 248 248
6,000 -22 -27 2230 435 869 244 251 245 252 246 253
8,000 -25 -31 2230 422 844 242 256 243 257 244 258
10,000 -29 -35 2230 411 822 240 261 241 262 242 263
12,000 -33 -39 2230 403 806 238 267 239 268 240 269
14,000 -36 -43 2230 396 791 235 272 236 273 237 274
16,000 -40 -47 2230 388 777 233 277 234 278 235 280
18,000 -44 -51 2230 381 763 231 283 232 284 233 285
20,000 - - - - - - - - - - -
22,000 - - - - - - - - - - -
24,000 - - - - - - - - - - -
26,000 - - - - - - - - - - -
28,000 - - - - - - - - - - -
29,000 - - - - - - - - - - -
31,000 - - - - - - - - - - -
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-88 Reference Material: Revision IR: April 29, 2009
MAXIMUM CRUISE POWER 1800 RPM ISA -20C
NOTE: 1. IOAT, TORQUE AND FUEL FLOW BASED ON 11,000 POUNDS GROSS
WEIGHT. 2. DURING OPERATION WITH ICE VANES EXTENDED, TRUE AIRSPEED WILL
BE REDUCED IF ORIGINAL TORQUE IS NOT OR CANNOT BE RESET, BUT WILL BE UNCHANGED IF ORIGINAL TORQUE IS RESET.
3. OBSERVE MMO LIMITATION WHERE APPLICABLE.
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 0 -5 2230 478 957 249 240 250 241 250 241
2,000 -4 -9 2230 464 928 246 244 247 245 248 246
4,000 -8 -13 2230 452 904 244 249 245 250 246 251
6,000 -11 -17 2230 440 879 242 254 243 255 243 255
8,000 -15 -21 2230 428 857 240 259 241 260 241 260
10,000 -19 -25 2230 418 836 238 265 239 266 240 267
12,000 -23 -29 2230 409 818 236 270 236 271 237 272
14,000 -26 -33 2230 402 803 233 275 234 276 235 277
16,000 -30 -37 2230 394 789 231 281 232 282 233 283
18,000 -34 -41 2230 387 773 228 286 230 288 231 289
20,000 -37 -45 2230 380 760 226 292 227 293 228 295
22,000 -41 -49 2230 375 749 223 297 224 299 225 300
24,000 -45 -53 2230 370 741 220 303 222 305 223 307
26,000 - - - - - - - - - - -
28,000 - - - - - - - - - - -
29,000 - - - - - - - - - - -
31,000 - - - - - - - - - - -
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-89
MAXIMUM CRUISE POWER 1800 RPM ISA -10C
NOTE: 1. IOAT, TORQUE AND FUEL FLOW BASED ON 11,000 POUNDS GROSS
WEIGHT. 2. DURING OPERATION WITH ICE VANES EXTENDED, TRUE AIRSPEED WILL
BE REDUCED IF ORIGINAL TORQUE IS NOT OR CANNOT BE RESET, BUT WILL BE UNCHANGED IF ORIGINAL TORQUE IS RESET.
3. OBSERVE MMO LIMITATION WHERE APPLICABLE.
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 10 5 2230 482 965 247 242 248 243 249 244
2,000 6 1 2230 469 938 245 247 246 248 246 248
4,000 2 -3 2230 457 914 242 251 243 252 244 253
6,000 -1 -7 2230 446 891 240 256 241 257 242 258
8,000 -5 -11 2230 434 869 237 261 238 262 239 263
10,000 -9 -15 2230 424 848 236 268 237 269 238 270
12,000 -12 -19 2230 415 830 233 273 234 274 235 275
14,000 -16 -23 2230 407 813 231 278 232 279 232 280
16,000 -20 -27 2230 399 797 229 284 230 285 230 286
18,000 -23 -31 2230 391 781 226 289 227 291 228 292
20,000 -27 -35 2230 384 769 223 295 224 296 226 298
22,000 -31 -39 2230 379 758 221 301 222 303 223 304
24,000 -34 -43 2230 376 751 218 308 220 310 220 311
26,000 -38 -47 2230 372 744 215 314 217 316 218 318
28,000 -42 -50 2179 363 727 209 317 212 320 214 323
29,000 -44 -52 2103 351 703 205 316 207 319 209 322
31,000 - - - - - - - - - - -
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-90 Reference Material: Revision IR: April 29, 2009
MAXIMUM CRUISE POWER 1800 RPM
ISA NOTE: 1. IOAT, TORQUE AND FUEL FLOW BASED ON 11,000 POUNDS GROSS
WEIGHT. 2. DURING OPERATION WITH ICE VANES EXTENDED, TRUE AIRSPEED WILL
BE REDUCED IF ORIGINAL TORQUE IS NOT OR CANNOT BE RESET, BUT WILL BE UNCHANGED IF ORIGINAL TORQUE IS RESET.
3. OBSERVE MMO LIMITATION WHERE APPLICABLE.
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 20 15 2230 489 977 245 245 245 245 246 246
2,000 16 11 2230 474 949 242 249 243 250 244 251
4,000 13 7 2230 461 922 240 254 241 255 242 256
6,000 9 3 2230 449 898 238 259 239 260 240 261
8,000 5 -1 2230 438 877 236 265 237 266 238 267
10,000 1 -5 2230 428 856 233 270 234 271 235 272
12,000 -2 -9 2230 419 838 231 276 232 277 233 278
14,000 -6 -13 2230 411 822 229 281 229 282 230 283
16,000 -10 -17 2230 404 807 227 287 227 288 228 289
18,000 -13 -21 2230 395 790 223 292 225 294 226 295
20,000 -17 -25 2230 388 777 221 298 222 299 223 301
22,000 -21 -29 2230 384 768 218 304 220 306 221 308
24,000 -24 -33 2230 381 761 216 311 217 313 218 315
26,000 -28 -37 2211 374 749 212 316 214 319 216 321
28,000 -32 -40 2071 353 706 203 314 206 318 207 320
29,000 -34 -42 2001 342 683 199 313 201 317 203 320
31,000 -38 -46 1842 316 632 189 309 192 313 194 317
33,000 -42 -50 1660 288 575 178 302 181 307 184 312
35,000 -47 -54 1480 259 517 165 292 169 299 173 305
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-91
MAXIMUM CRUISE POWER 1800 RPM ISA +10C
NOTE: 1. IOAT, TORQUE AND FUEL FLOW BASED ON 11,000 POUNDS GROSS
WEIGHT. 2. DURING OPERATION WITH ICE VANES EXTENDED, TRUE AIRSPEED WILL
BE REDUCED IF ORIGINAL TORQUE IS NOT OR CANNOT BE RESET, BUT WILL BE UNCHANGED IF ORIGINAL TORQUE IS RESET.
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 30 25 2230 494 987 243 247 244 248 244 248
2,000 27 21 2230 479 959 240 251 241 252 242 253
4,000 23 17 2230 466 932 238 256 239 257 240 258
6,000 19 13 2230 454 908 236 262 237 263 238 264
8,000 15 9 2230 443 885 233 267 235 269 236 270
10,000 12 5 2230 431 862 232 273 232 274 233 275
12,000 8 1 2230 423 846 229 278 230 279 231 280
14,000 4 -3 2230 415 830 226 283 228 285 228 286
16,000 0 -7 2230 407 813 225 290 226 292 227 293
18,000 -3 -11 2230 399 799 221 295 223 297 224 299
20,000 -7 -15 2230 393 785 219 301 220 303 221 304
22,000 -10 -19 2230 387 775 216 307 217 309 219 311
24,000 -15 -23 2070 364 727 206 304 209 307 210 309
26,000 -19 -27 1920 339 678 197 302 200 306 202 308
28,000 -23 -30 1795 317 635 189 300 192 304 194 307
29,000 -25 -32 1733 307 614 185 299 188 303 190 307
31,000 -29 -36 1593 284 569 175 295 179 300 181 304
33,000 -33 -40 1432 258 517 164 286 168 292 171 298
35,000 -38 -44 1271 233 465 150 273 156 283 161 291
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-92 Reference Material: Revision IR: April 29, 2009
MAXIMUM CRUISE POWER 1800 RPM ISA +20C
NOTE: 1. IOAT, TORQUE AND FUEL FLOW BASED ON 11,000 POUNDS GROSS
WEIGHT. 2. DURING OPERATION WITH ICE VANES EXTENDED, TRUE AIRSPEED WILL
BE REDUCED IF ORIGINAL TORQUE IS NOT OR CANNOT BE RESET, BUT WILL BE UNCHANGED IF ORIGINAL TORQUE IS RESET.
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 40 35 2230 501 1001 242 250 243 251 243 251
2,000 37 31 2230 485 971 238 253 239 254 240 255
4,000 33 27 2230 471 942 236 258 237 259 238 260
6,000 29 23 2230 458 916 234 265 236 267 237 268
8,000 25 19 2230 447 893 233 271 234 272 235 273
10,000 22 15 2230 435 871 230 276 231 277 232 278
12,000 18 11 2230 427 854 227 281 229 283 230 284
14,000 14 7 2230 418 836 225 287 226 288 227 290
16,000 11 3 2230 411 822 222 292 223 294 224 295
18,000 7 -1 2212 400 801 218 296 219 298 221 300
20,000 3 -5 2085 377 754 211 297 212 299 214 301
22,000 -1 -9 1913 349 699 201 293 203 296 205 298
24,000 -5 -13 1749 324 647 191 289 194 292 196 295
26,000 -9 -17 1603 299 598 182 284 184 288 187 292
28,000 -14 -20 1482 279 557 172 280 175 285 178 290
29,000 -16 -22 1424 268 536 168 278 171 283 174 288
31,000 -20 -26 1289 247 493 155 268 161 277 164 283
33,000 -25 -30 1135 222 444 138 250 147 265 153 275
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-93
MAXIMUM CRUISE POWER 1800 RPM ISA +30C
NOTE: 1. IOAT, TORQUE AND FUEL FLOW BASED ON 11,000 POUNDS GROSS
WEIGHT. 2. DURING OPERATION WITH ICE VANES EXTENDED, TRUE AIRSPEED WILL
BE REDUCED IF ORIGINAL TORQUE IS NOT OR CANNOT BE RESET, BUT WILL BE UNCHANGED IF ORIGINAL TORQUE IS RESET.
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 50 45 2230 507 1013 240 252 241 253 241 253
2,000 47 41 2230 490 981 237 256 239 258 239 258
4,000 43 37 2230 477 954 235 262 237 264 237 265
6,000 39 33 2230 464 928 233 268 234 269 235 270
8,000 36 29 2230 453 905 231 273 231 274 232 275
10,000 32 25 2230 441 882 228 278 229 279 230 281
12,000 28 21 2230 432 865 225 283 226 284 228 286
14,000 24 17 2180 416 831 220 286 222 288 223 290
16,000 20 13 2049 390 780 213 286 215 288 215 289
18,000 16 9 1916 366 731 205 284 206 286 208 288
20,000 12 5 1783 341 682 196 282 198 285 200 288
22,000 8 1 1597 312 624 185 275 187 279 189 282
24,000 4 -3 1450 288 577 174 268 178 274 180 277
26,000 0 -7 1316 265 530 162 261 167 268 171 274
28,000 -5 -10 1195 244 488 150 252 156 261 161 268
29,000 -7 -12 1133 234 468 143 244 151 256 156 264
31,000 -11 -16 1007 213 426 - - 137 244 144 256
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-94 Reference Material: Revision IR: April 29, 2009
MAXIMUM CRUISE POWER 1800 RPM ISA +37C
NOTE: 1. IOAT, TORQUE AND FUEL FLOW BASED ON 11,000 POUNDS GROSS
WEIGHT. 2. DURING OPERATION WITH ICE VANES EXTENDED, TRUE AIRSPEED WILL
BE REDUCED IF ORIGINAL TORQUE IS NOT OR CANNOT BE RESET, BUT WILL BE UNCHANGED IF ORIGINAL TORQUE IS RESET.
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 58 52 2230 510 1019 238 253 239 254 240 255
2,000 54 48 2230 494 989 236 258 237 259 238 260
4,000 50 44 2230 481 962 234 264 235 265 236 266
6,000 46 40 2230 468 936 231 269 232 270 233 271
8,000 43 36 2230 456 913 229 274 230 275 231 277
10,000 39 32 2230 443 885 227 280 228 281 228 282
12,000 35 28 2107 417 834 219 279 220 281 221 282
14,000 31 24 1977 392 783 211 278 213 280 214 282
16,000 27 20 1848 366 732 203 276 205 279 207 281
18,000 23 16 1719 342 683 195 275 197 278 199 280
20,000 19 12 1587 318 636 186 271 188 275 191 278
22,000 15 8 1428 291 583 174 263 177 268 180 272
24,000 10 4 1277 266 533 161 254 166 261 169 266
26,000 6 0 1130 243 485 147 241 154 251 158 258
28,000 1 -3 979 218 436 - - 139 236 145 247
29,000 - - - - - - - - - - -
31,000 - - - - - - - - - - -
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-95
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-96 Reference Material: Revision IR: April 29, 2009
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-97
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-98 Reference Material: Revision IR: April 29, 2009
0 2 4 6 8 10 12 14 16 18 200
5
10
15
20
25
30
35
299
NOTES: RANGE INCLUDES START, TAXI, CLIMB, DESCENT AND 45 MINUTES RESERVE FUEL AT MAXIMUM RANGE POWER.
EXAMPLE:PRESSURE ALTITUDE... 26,000 FTFUEL................................ 3,645 LBSRANGE............................ 1,331 NM
ASSOCIATED CONDITIONS:WEIGHT.............. 12,500 LBS BEFORE ENGINE STARTFUEL.................... AVIATION KEROENEFUEL DENSITY... 6.7 LB/GALICE VANES.......... RETRACTED
CR
UIS
E C
LIM
B D
ISTA
NC
E
3645
LBS
(544
GAL)
FUL
L M
AIN
AND
AUX
TANK
S
1590
LB
S (2
37 G
AL)
AVA
ILA
BLE
FU
EL A
T M
AX
ZER
O F
UEL
WT
CRUISE TRUE AIRSPEED~ KNOTS
PRES
SUR
E A
LTIT
UD
E ~
1000
FT
RANGE ~ 100 NAUTICAL MILES
245249
254
260
265
270
276
281
287
292
298
305
316
315314
310
304
294
311
250
255
260
265
270
276
282
288
293
306
312
318317
316
312
306
297
245 245250
255
261
266
271
277
282
288
294
300
307
313
319319
318
314
309
301
2586
LBS
(386
GAL
) FUL
L M
AIN
TANK
S
RANGE PROFILE - MAXIMUM CRUISE POWER1800 RPM
STANDARD DAY (ISA)ZERO WIND
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-99 FEET
CC
FT-LBLB
/HR
LB/H
RFT-LB
LB/H
RLB
/HR
FT-LBLB
/HR
LB/H
RSL
-12-15
1542365
7301456
355710
1373346
6922000
-16-19
1498347
6941409
337674
1323328
6564000
-19-23
1456331
6621365
321642
1274311
6226000
-23-27
1410315
6301318
304608
1224294
5888000
-27-31
1374300
6001280
290580
1185279
55810000
-31-35
1340286
5721245
276552
1148265
53012000
-35-39
1319275
5501223
265530
1125254
50814000
-39-43
1309266
5321206
255510
1105243
48616000
-43-47
1305258
5161195
246492
1094234
46818000
-47-51
1312251
5021197
238476
1091227
45420000
--
--
--
--
--
-22000
--
--
--
--
--
-24000
--
--
--
--
--
-26000
--
--
--
--
--
-28000
--
--
--
--
--
-29000
--
--
--
--
--
-31000
--
--
--
--
--
-33000
--
--
--
--
--
-35000
--
--
--
--
--
--
--
--
--
--
--
--
--
--
--
--
--
--
--
213208
203218
212207
207203
198210
205201
203200
195205
201196
201198
194202
198194
198195
192200
196193
AIR
SPEED
TAS
TAS
TAS
AIR
SPEED
TOR
Q/
ENG
WF/ EN
GW
F TO
TAL
WEIG
HT
12,000 POU
ND
S11,000 PO
UN
DS
10,000 POU
ND
SPR
ESS A
LT.IO
AT
OA
TTO
RQ
/ EN
GW
F/ ENG
WF
TOTA
LW
F/ ENG
WF
TOTA
L
MA
XIM
UM
RA
NG
E P
OW
ER
1600 RP
MIS
A -30C
NO
TE: DU
RIN
G O
PERATIO
N W
ITH IC
E VANES EXTEN
DED
, IN O
RD
ER TO
MAIN
TAIN M
AXIMU
M R
ANG
E CO
NFIG
UR
ATION
, RESET PO
WER
TOH
AND
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ILL REM
AIN U
NC
HAN
GED
.IO
AT BASED O
N 11,000 PO
UN
DS
AIR
SPEED
TOR
Q/
ENG
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-100 Reference Material: Revision IR: April 29, 2009
FEET
CC
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IOAT
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-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-101
FEETC
CFT-LB
LB/H
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G AN
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SPEED W
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NC
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-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-102 Reference Material: Revision IR: April 29, 2009
FE
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-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-103
FEETC
CFT-LB
LB/H
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HAN
GED
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AT BASED O
N 11,000 PO
UN
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Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-104 Reference Material: Revision IR: April 29, 2009 FE
ETC
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-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-105
FEETC
CFT-LB
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TAS
TAS
TAS
AIR
SPEED
TOR
Q/
ENG
WF/ EN
GW
F TO
TAL
WEIG
HT
12,000 POU
ND
S11,000 PO
UN
DS
10,000 POU
ND
SPR
ESS A
LT.IO
AT
OA
TTO
RQ
/ EN
GW
F/ ENG
WF
TOTA
LW
F/ ENG
WF
TOTA
L
MA
XIM
UM
RA
NG
E P
OW
ER
1600 RP
MIS
A +30C
NO
TE: DU
RIN
G O
PERATIO
N W
ITH IC
E VANES EXTEN
DED
, IN O
RD
ER TO
MAIN
TAIN M
AXIMU
M R
ANG
E CO
NFIG
UR
ATION
, RESET PO
WER
TOH
AND
BOO
K VALUE. FU
EL FLOW
WILL IN
CR
EASE APPRO
XIMATELY 20 LBS/H
R/EN
G AN
D TR
UE AIR
SPEED W
ILL REM
AIN U
NC
HAN
GED
.IO
AT BASED O
N 11,000 PO
UN
DS
AIR
SPEED
TOR
Q/
ENG
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-106 Reference Material: Revision IR: April 29, 2009 FE
ETC
CFT
-LB
LB/H
RLB
/HR
FT-L
BLB
/HR
LB/H
RFT
-LB
LB/H
RLB
/HR
SL56
5215
6239
679
214
7938
577
014
0637
675
220
0052
4815
3637
975
814
4636
873
613
7135
871
640
0048
4415
1836
472
814
2235
270
413
4234
268
460
0044
4015
0535
070
014
0333
867
613
1332
765
480
0040
3614
9333
867
613
7832
464
812
8831
362
610
000
3732
1469
324
648
1355
310
620
1258
298
596
1200
033
2814
4831
262
413
5730
160
212
3828
757
414
000
2924
1426
301
602
1342
291
582
1233
277
554
1600
025
2014
1129
158
213
1928
056
012
2926
953
818
000
2116
1430
285
570
1297
270
540
1209
259
518
2000
017
1214
3127
955
813
1826
553
011
9925
150
222
000
148
--
-13
0725
951
812
0624
749
424
000
--
--
--
--
1212
243
486
2600
0-
--
--
--
--
--
2800
0-
--
--
--
--
--
2900
0-
--
--
--
--
--
3100
0-
--
--
--
--
--
3300
0-
--
--
--
--
--
3500
0-
--
--
--
--
--
WF/
EN
GW
F TO
TAL
MA
XIM
UM
RA
NG
E P
OW
ER
1600
RP
MIS
A +
37C
NO
TE:
DU
RIN
G O
PER
ATIO
N W
ITH
ICE
VAN
ES E
XTEN
DED
, IN
OR
DER
TO
MAI
NTA
IN M
AXIM
UM
RAN
GE
CO
NFI
GU
RAT
ION
, RES
ET P
OW
ER T
OH
AND
BOO
K VA
LUE.
FU
EL F
LOW
WIL
L IN
CR
EASE
APP
RO
XIM
ATEL
Y 20
LBS
/HR
/EN
G A
ND
TR
UE
AIR
SPEE
D W
ILL
REM
AIN
UN
CH
ANG
ED.
IOAT
BAS
ED O
N 1
1,00
0 PO
UN
DS
AIR
SP
EED
TOR
Q/
ENG
WEI
GH
T12
,000
PO
UN
DS
11,0
00 P
OU
ND
S10
,000
PO
UN
DS
PRES
S A
LT.
IOA
TO
AT
TOR
Q/
ENG
WF/
EN
GW
F TO
TAL
AIR
SP
EED
TAS
TAS
TAS
AIR
SP
EED
TOR
Q/
ENG
WF/
EN
GW
F TO
TAL
214
211
208
216
213
210
219
215
212
222
218
215
225
221
217
228
223
219
231
227
222
233
230
225
236
233
229
242
235
232
246
241
235
-24
424
0-
-24
6-
--
--
--
--
--
-
--
--
--
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-107
0 2 4 6 8 10 12 14 16 18 200
5
10
15
20
25
30
35NOTES: RANGE INCLUDES START, TAXI, CLIMB, DESCENT AND 45 MINUTES RESERVE FUEL AT MAXIMUM RANGE POWER.
EXAMPLE:PRESSURE ALTITUDE... 26,000 FTFUEL................................ 3,645 LBSRANGE............................ 1,605 NM
ASSOCIATED CONDITIONS:WEIGHT.............. 12,500 LBS BEFORE ENGINE STARTFUEL.................... AVIATION KEROENEFUEL DENSITY... 6.7 LB/GALICE VANES.......... RETRACTED
CR
UIS
E C
L IM
B D
ISTA
NC
E
3645
LBS
(544
GAL)
FUL
L MA
IN A
ND A
UX T
ANKS
1590
LB
S (2
37 G
AL)
AVA
ILA
BLE
FU
EL A
T M
AX
ZER
O F
UEL
WT
CRUISE TRUE AIRSPEED~ KNOTS
PRES
SUR
E A
LTIT
UD
E ~
1000
FT
RANGE ~ 100 NAUTICAL MILES
206208
211
213
215
218
221
224
229
233
238
240
249
255256
255
259
261
242
207
209
211
213
216
218
222
226
231
235
239
241
245251254
256
257
260
205 204205
208
209
211
213
216
219
223
228
233
237
240
242247
251
256
256
259
2586
LBS
(386
GAL
) FUL
L M
AIN
TANK
S
RANGE PROFILE - MAXIMUM RANGE POWER1600 RPM
STANDARD DAY (ISA)ZERO WIND
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-108 Reference Material: Revision IR: April 29, 2009
0 2 4 6 8 10 12 14 16 18 200
5
10
15
20
25
30
35
MAX
CRU
ISE
POW
ER @
180
0RPM
NORM
AL C
RUIS
E PO
WER
@ 1
600R
PM
NOTES: RANGE INCLUDES START, TAXI, CLIMB, DESCENT AND 45 MINUTES RESERVE FUEL AT MAXIMUM RANGE POWER.
EXAMPLE:PRESSURE ALTITUDE............................... 31,000 FTRANGE @ MAX CRUISE POWER............... 1,535 NMRANGE @ MAX RANGE POWER................ 1,740 NM
ASSOCIATED CONDITIONS:WEIGHT.............. 12,500 LBS BEFORE ENGINE STARTFUEL.................... AVIATION KEROENEFUEL DENSITY... 6.7 LB/GALICE VANES.......... RETRACTED
CR
UIS
E C
LIM
B D
I STA
NC
E
MAX
RANG
E PO
WER
@ 16
00RP
M
CRUISE TRUE AIRSPEED~ KNOTS
PRES
SUR
E A
LTIT
UD
E ~
1000
FT
RANGE ~ 100 NAUTICAL MILES
204205
208
209
211
213
216
219
223
228
233
237
240
242247
251
256
256
259
RANGE PROFILE COMPARISION - FULL MAIN AND AUX TANKS
STANDARD DAY (ISA)ZERO WIND
301
309
314
318319
319
313
307
300
294
288
282
277
271
266
261
255
250245
289
298
304
308308
304
298
292
285
280
274
270
263
258
253
249
244
239235
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-109
0 1 2 3 4 5 6 7 80
5
10
15
20
25
30
35
MA
X C
RU
ISE
POW
ER @
180
0RPM
NO
RM
AL
CR
UIS
E PO
WER
@ 1
600R
PM
NOTES: RANGE INCLUDES START, TAXI, CLIMB, DESCENT AND 45 MINUTES RESERVE FUEL AT MAXIMUM RANGE POWER.
EXAMPLE:PRESSURE ALTITUDE............................... 31,000 FTENDURANCE @ MAX CRUISE POWER..... 5.20 HRSENDURANCE @ MAX RANGE POWER.......7.00 HRS
ASSOCIATED CONDITIONS:WEIGHT.............. 12,500 LBS BEFORE ENGINE STARTFUEL.................... AVIATION KEROENEFUEL DENSITY... 6.7 LB/GALICE VANES.......... RETRACTED
MAX
RANG
E PO
WER
@ 16
00RP
M
CRUISE TRUE AIRSPEED~ KNOTS
PRES
SUR
E A
LTIT
UD
E ~
1000
FT
RANGE ~ 100 NAUTICAL MILES
204205
208
209
211
213
216
219
223
228
233
237
240
242247251
256
256
259
ENDURANCE PROFILE COMPARISION - FULL MAIN AND AUX TANKS
STANDARD DAY (ISA)ZERO WIND
301
309
314
318319
319
313
307
300
294
288
282
277
271
266
261
255
250245
289
298
304
308308
304
298
292
285
280
274
270
263
258
253
249
244
239235
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-110 Reference Material: Revision IR: April 29, 2009
0 2 4 6 8 10 12 14 16 18 200
5
10
15
20
25
30
35
MAX
CRU
ISE
POW
ER @
180
0RPM
NOTES: RANGE INCLUDES START, TAXI, CLIMB, DESCENT AND 45 MINUTES RESERVE FUEL AT MAXIMUM RANGE POWER.
EXAMPLE:PRESSURE ALTITUDE............................... 31,000 FTRANGE @ MAX CRUISE POWER............... 1,000 NMRANGE @ MAX RANGE POWER................ 1,120 NM
ASSOCIATED CONDITIONS:WEIGHT.............. 12,500 LBS BEFORE ENGINE STARTFUEL.................... AVIATION KEROENEFUEL DENSITY... 6.7 LB/GALICE VANES.......... RETRACTED
CR
UI S
E C
LIM
B D
ISTA
NC
E
MAX
RAN
GE
POW
ER @
160
0RPM
CRUISE TRUE AIRSPEED~ KNOTS
PRES
SUR
E A
LTIT
UD
E ~
1000
FT
RANGE ~ 100 NAUTICAL MILES
RANGE PROFILE COMPARISION - FULL MAIN TANKS
STANDARD DAY (ISA)ZERO WIND
245
260
257
256
254251
241
239
235
231
226
222
218
216
213
211
209
207205
285
295
302
306306
303
297
291
284
279
274
269
263
257
253
248
243
238234
NORM
AL C
RUIS
E PO
WER
@ 1
600R
PM
297
306
312
316317
318
312
306
299
293
288
282
276
270
265
260
255
250245
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-111
0 1 2 3 4 5 6 7 80
5
10
15
20
25
30
35
MA
X C
RU
ISE
POW
ER @
180
0RPM
NOTES: RANGE INCLUDES START, TAXI, CLIMB, DESCENT AND 45 MINUTES RESERVE FUEL AT MAXIMUM RANGE POWER.
EXAMPLE:PRESSURE ALTITUDE............................... 31,000 FTENDURANCE @ MAX CRUISE POWER..... 3.56 HRSENDURANCE @ MAX RANGE POWER...... 4.60 HRS
ASSOCIATED CONDITIONS:WEIGHT.............. 12,500 LBS BEFORE ENGINE STARTFUEL.................... AVIATION KEROENEFUEL DENSITY... 6.7 LB/GALICE VANES.......... RETRACTED
MAX
RAN
GE
POW
ER @
160
0RPM
CRUISE TRUE AIRSPEED~ KNOTS
PRES
SUR
E A
LTIT
UD
E ~
1000
FT
RANGE ~ 100 NAUTICAL MILES
ENDURANCE PROFILE COMPARISION - FULL MAIN TANKS
STANDARD DAY (ISA)ZERO WIND
245
260
257
256
254251
241
239
235
231
226
222
218
216
213
211
209
207205
285
295
302
306306
303
297
291
284
279
274
269
263
257
253
248
243
238234
NO
RM
AL
CR
UIS
E PO
WER
@ 1
600R
PM
297
306
312
316317
318
312
306
299
293
288
282
276
270
265
260
255
250245
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-112 Reference Material: Revision IR: April 29, 2009
ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER
1900 RPM
DURING OPERATION WITH ICE VANES EXTENDED, TORQUE WILL DECREASE
APPROXIMATELY 500 FT-LB. IF HANDBOOK POWER IS NOT OR CANNOT BE RESET, 30 KNOTS AND FUEL FLOW WILL DECREASE APPROXIMATELY 50 LB/HR/ENG. IF HANDBOOK POWER IS RESET, TRUE AIRSPEED WILL BE UNCHANGED AND FUEL FLOW WILL INCREASE APPROXIMATELY 50 LB/HR/ENG.
IOAT, TORQUE AND FUEL FLOW BASED ON 11,000 LB.
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-113
ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER
1900 RPM ISA -30C
NOTE: SEE NOTES AT BEGINNING OF ONE ENGINE INOPERATIVE
MAXIMUM CRUISE SECTION
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 -12 -15 2230 422 422 194 185 196 186 198 188
2,000 -16 -19 2230 419 419 192 188 194 189 195 191
4,000 -20 -23 2230 416 416 190 191 192 192 193 194
6,000 -23 -27 2230 413 413 187 194 189 196 191 197
8,000 -27 -31 2230 411 411 185 197 187 199 189 201
10,000 -31 -35 2230 409 409 182 200 185 202 187 204
12,000 -35 -39 2230 408 408 180 203 182 205 184 208
14,000 -39 -43 2230 408 408 177 206 179 209 181 211
16,000 -43 -47 2230 407 407 173 208 176 212 178 214
18,000 -46 -51 2230 407 407 170 211 173 214 176 217
20,000 - - - - - - - - - - -
22,000 - - - - - - - - - - -
24,000 - - - - - - - - - - -
26,000 - - - - - - - - - - -
28,000 - - - - - - - - - - -
29,000 - - - - - - - - - - -
31,000 - - - - - - - - - - -
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-114 Reference Material: Revision IR: April 29, 2009
ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER
1900 RPM ISA -20 C
NOTE: SEE NOTES AT BEGINNING OF ONE ENGINE INOPERATIVE MAXIMUM
CRUISE SECTION.
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 -2 -5 2230 434 434 192 186 194 188 195 189
2,000 -6 -9 2230 429 429 190 189 192 191 193 192
4,000 -9 -13 2230 425 425 187 192 189 194 191 196
6,000 -13 -17 2230 422 422 185 195 187 197 189 199
8,000 -17 -21 2230 419 419 182 198 185 201 187 203
10,000 -21 -25 2230 417 417 180 201 182 204 184 206
12,000 -25 -29 2230 415 415 177 204 180 207 182 209
14,000 -29 -33 2230 414 414 174 207 177 210 179 213
16,000 -32 -37 2230 414 414 171 210 174 213 176 216
18,000 -36 -41 2230 413 413 168 212 171 216 173 219
20,000 -40 -45 2230 413 413 164 215 168 219 170 223
22,000 -44 -49 2230 415 415 161 217 164 222 167 226
24,000 -48 -53 2156 403 403 154 215 159 222 162 227
26,000 - - - - - - - - - - -
28,000 - - - - - - - - - - -
29,000 - - - - - - - - - - -
31,000 - - - - - - - - - - -
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-115
ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER
1900 RPM ISA -10C
NOTE: SEE NOTES AT BEGINNING OF ONE ENGINE INOPERATIVE
MAXIMUM CRUISE SECTION
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 8 5 2230 447 447 190 187 192 189 193 190
2,000 4 1 2230 439 439 187 190 189 192 191 194
4,000 1 -3 2230 436 436 185 193 187 195 189 197
6,000 -3 -7 2230 432 432 183 196 185 199 187 201
8,000 -7 -11 2230 429 429 180 200 182 202 184 204
10,000 -11 -15 2230 426 426 178 203 180 205 182 208
12,000 -15 -19 2230 424 424 175 206 177 208 179 211
14,000 -19 -23 2230 422 422 171 208 174 212 177 214
16,000 -22 -27 2230 421 421 168 211 171 215 174 218
18,000 -26 -31 2230 421 421 165 214 168 218 171 221
20,000 -30 -35 2230 420 420 162 216 165 221 168 225
22,000 -34 -39 2220 420 420 157 217 161 223 165 228
24,000 -38 -43 2055 391 391 147 210 153 218 157 224
26,000 -42 -47 1900 364 364 135 200 143 212 149 220
28,000 -47 -50 1756 339 339 - - 132 203 140 215
29,000 -49 -52 1683 326 326 - - 124 196 135 211
31,000 -50 -54 1638 317 317 - - - - 129 206
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-116 Reference Material: Revision IR: April 29, 2009
ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER
1900 RPM ISA
NOTE: SEE NOTES AT BEGINNING OF ONE ENGINE INOPERATIVE MAXIMUM CRUISE SECTION.
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 18 15 2230 464 464 188 188 189 190 191 192
2,000 14 11 2230 455 455 185 191 187 193 189 195
4,000 11 7 2230 449 449 183 194 185 197 187 199
6,000 7 3 2230 443 443 180 198 183 200 185 202
8,000 3 -1 2230 439 439 178 201 180 204 182 206
10,000 -1 -5 2230 435 435 175 204 178 207 180 209
12,000 -5 -9 2230 432 432 172 207 175 210 177 213
14,000 -9 -13 2230 431 431 169 210 172 213 175 216
16,000 -12 -17 2230 429 429 166 212 169 216 172 219
18,000 -16 -21 2230 428 428 163 215 166 219 169 223
20,000 -20 -25 2230 428 428 159 217 163 222 166 226
22,000 -24 -29 2115 408 408 151 213 156 220 160 225
24,000 -28 -33 1951 380 380 139 204 146 214 151 221
26,000 -33 -37 1802 353 353 - - 136 206 142 216
28,000 -37 -40 1668 329 329 - - 122 193 133 210
29,000 -39 -42 1627 320 320 - - - - 128 218
31,000 - - - - - - - - - - -
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-117
ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER
1900 RPM ISA +10C
NOTE: SEE NOTES AT BEGINNING OF ONE ENGINE INOPERATIVE
MAXIMUM CRUISE SECTION
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 28 25 2230 484 484 185 189 187 191 189 193
2,000 25 21 2230 474 474 183 192 185 195 187 196
4,000 21 17 2230 467 467 181 195 483 198 185 200
6,000 17 13 2230 461 461 178 199 180 201 182 203
8,000 13 9 2230 456 456 175 202 178 204 180 207
10,000 9 5 2230 450 450 172 205 175 208 177 210
12,000 5 1 2230 448 448 169 207 172 211 175 214
14,000 2 -3 2230 446 446 166 210 169 214 172 217
16,000 -2 -7 2230 444 444 163 213 166 217 169 221
18,000 -6 -11 2136 425 425 156 210 160 216 164 221
20,000 -10 -15 2006 400 400 147 205 153 213 157 218
22,000 -15 -19 1842 371 371 134 194 142 206 148 213
24,000 -19 -23 1690 344 344 - - 131 196 138 207
26,000 -23 -27 1589 321 321 - - - - 128 199
28,000 -27 -30 1450 299 299 - - - - 114 185
29,000 - - - - - - - - - - -
31,000 - - - - - - - - - - -
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-118 Reference Material: Revision IR: April 29, 2009
ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER
1900 RPM ISA +20 C
NOTE: SEE NOTES AT BEGINNING OF ONE ENGINE INOPERATIVE MAXIMUM
CRUISE SECTION
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 38 35 2230 512 512 183 190 185 192 187 194
2,000 35 31 2230 501 501 181 193 183 196 185 198
4,000 31 27 2230 492 492 178 196 181 199 183 201
6,000 27 23 2230 485 485 176 199 178 202 180 205
8,000 23 19 2230 478 478 173 202 175 205 178 208
10,000 19 15 2230 472 472 170 205 173 208 175 211
12,000 15 11 2177 459 459 165 205 168 209 171 213
14,000 11 7 2060 433 433 157 203 161 208 165 212
16,000 7 3 1943 408 408 I49 199 154 205 158 210
18,000 3 -1 1826 383 383 140 193 146 201 151 208
20,000 -1 -5 1704 359 359 127 181 137 195 143 204
22,000 -5 -9 1551 331 331 - - 123 182 133 196
24,000 -9 -13 1416 306 306 - - - - 119 183
26,000 - - - - - - - - - - -
28,000 - - - - - - - - - - -
29,000 - - - - - - - - - - -
31,000 - - - - - - - - - - -
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-119
ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER
1900 RPM ISA +30C
NOTE: SEE NOTES AT BEGINNING OF ONE ENGINE INOPERATIVE
MAXIMUM CRUISE SECTION
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 48 45 2230 541 541 181 191 183 193 185 195
2,000 45 41 2230 527 527 179 194 181 197 183 199
4,000 41 37 2230 518 518 176 197 179 200 181 202
6,000 37 33 2166 496 496 171 198 174 201 176 204
8,000 33 29 2082 472 472 165 197 169 201 171 204
10,000 29 25 1997 448 448 159 196 163 200 166 204
12,000 25 21 1884 422 422 151 192 156 198 160 202
14,000 21 17 1769 397 397 142 187 148 194 153 200
16,000 17 13 1650 371 371 131 178 139 189 145 196
18,000 12 9 1526 345 345 - - 128 180 136 191
20,000 9 5 1418 322 322 - - - - 126 183
22,000 - - - - - - - - - - -
24,000 - - - - - - - - - - -
26,000 - - - - - - - - - - -
28,000 - - - - - - - - - - -
29,000 - - - - - - - - - - -
31,000 - - - - - - - - - - -
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-120 Reference Material: Revision IR: April 29, 2009
ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER
1900 RPM ISA +37 C
NOTE: SEE NOTES AT BEGINNING OF ONE ENGINE INOPERATIVE MAXIMUM
CRUISE SECTION
FEET C C FT-LBS LBS/HR LBS/HR IAS TAS IAS TAS IAS TAS
0 55 52 2122 538 538 176 188 179 190 181 193
2,000 51 48 2083 516 516 172 189 175 192 177 195
4,000 48 44 2032 495 495 168 190 171 193 173 196
6,000 44 40 1967 472 472 163 190 166 194 169 197
8,000 40 36 1888 448 448 156 189 160 193 164 197
10,000 36 32 1809 424 424 150 187 155 192 158 197
12,000 32 28 1696 398 398 141 181 147 189 151 194
14,000 27 24 1580 373 373 129 171 138 183 143 191
16,000 23 20 1459 347 347 - - 126 174 135 185
18,000 19 16 1350 322 322 - - - - 123 176
20,000 - - - - - - - - - - -
22,000 - - - - - - - - - - -
24,000 - - - - - - - - - - -
26,000 - - - - - - - - - - -
28,000 - - - - - - - - - - -
29,000 - - - - - - - - - - -
31,000 - - - - - - - - - - -
33,000 - - - - - - - - - - -
35,000 - - - - - - - - - - -
AIRSPEED - KNOTS12,000 LBS 11,000 LBS 10,000 LBS
PRESSURE ALTITUDE IOAT OAT
TORQUE PER ENGINE
FUEL FLOW PER ENGINE
TOTAL FUEL FLOW
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
Reference Material: Revision IR: April 29, 2009 5-121
0 200 400 600 800 1000 1200 1400 16000
1
2
3
4
SL5,000
FT10,0
00 FT
15,000 F
T
POWER SETTING1060 FT-LBS AT 1600RPM
APPLICABLE FOR ALL TEMPERATURES
HOLDING TIME
NOTE: FOR OPERATION WITH ICE VANES EXTENDEDHOLDING TIME WILL BE REDUCED APPROXIMATELY 3%
HO
LDIN
G T
IME
~ H
RS
FUEL REQUIRED ~ LBS
20,000 F
T
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-122 Reference Material: Revision IR: April 29, 2009
0 5 10 15 20 25
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
PRES
SUR
E A
LTIT
UD
E ~
FEET
TIME TO DESCEND ~ MINUTES
0 10 20 30 40 50 60 70 80 90 100110120130
DISTANCE TO DESCEND ~ NAUTICAL MILES
0 50 100 150 200 250
EXAMPLE:INITIAL ALTITUDE.............................. 26,000 FTFINAL ALTITUDE................................ 4,732 FTTIME TO DESCEND (17-3)................. 14 MINFUEL TO DESCEND (208-42)............ 164 LBDISTANCE TO CLIMB (91-15)............ 76 NM
ASSOCIATED CONDITIONS:POWER........................ AS REQUIRED TO DESCEND AT 1500 FT/MINLANDING GEAR.......... UPFLAPS.......................... UPPROPELLER SPEED... 1700 RPM
TIME, FUEL, AND DISTANCE TO DESCEND
FUEL TO DESCEND ~ POUNDS
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
FAA-Approved: Revision IR: April 29, 2009 5-123
WEIGHT ~ POUNDS
9000100001100012000
RA
TE O
F C
LIM
B ~
FT/
MIN
-500
0
500
1000
1500
2000
2500
OUTSIDE AIR TEMPERATUE ~ C
-60 -50 -40 -30 -20 -10 0 10 20 30 40 50 60
CLIMB - BALKED LANDINGCLIMB SPEED 100 KNOTS (ALL WEIGHTS)
EXAMPLE:OAT......................................................PRESSURE ALTITUDE........................WEIGHT...............................................RATE OF CLIMB..................................CLIMB GRADIENT...............................
32C4,732 FT10,937 LBS1,630 FT/MIN14.3%
REF
EREN
CE
LIN
E
PRESS
URE A
LTITUD
E ~ FE
ET
14,000
12,00010,000
8,0006,000
4,0002,000
SL ISA
24
22
20
18
16
14
12
10
8
6
4
2
0
CLI
MB
GR
ADIE
NT
~ %
NOTE: FOR OPERATION WITH ICE VANES EXTENDED, ADD6C TO ACTUAL OAT BEFORE ENTERING GRAPH.
ASSOCIATED CONDITIONS:POWER................................FLAPS..................................LANDING GEAR...................
TAKE-OFFDOWNDOWN
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-124 FAA-Approved: Revision IR: April 29, 2009
LANDING APPROACH SPEEDS
GROSS WEIGHT ~ 1000 LB
9 10 11 12 13
AP
PR
OA
CH
SP
EE
D ~
KIA
S
70
80
90
100
110
120
130
FLAPS
0%
100%
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section V Performance
FAA-Approved: Revision IR: April 29, 2009 5-125
GUIDELINES NOT APPLICABLEFOR INTERMEDIATEOBSTACLE HEIGHTS
OUTSIDE AIR TEMPERATURE ~ C
-40 -30 -20 -10 0 10 20 30 40 50 60
PRESSURE ALTITU
DE~FEET 10,0008,000
6,0004,000
SL2,000
REF
EREN
CE
LIN
E
REF
EREN
CE
LIN
E
REF
EREN
CE
LIN
E
WEIGHT~LBS APPROACH SPEED~KNOTS 12,500 97 12,000 95 11,000 90 10,000 85 9,000 80
EXAMPLE: OAT.....................................................32CPRESSURE ALTITUDE.......................4,730 FTLANDING WEIGHT.............................10,937 LBSHEADWIND COMPONENT..................4.7 KTSAPPROACH SPEED............................90 KIASGROUND ROLL...................................1,580 FTTOTAL OVER 50 FT OBSTACLE.........2,325 FT
LANDING DISTANCE WITHOUT PROPELLER REVERSING - FLAPS DOWNSTANDARD GEAR
TAILW
IND
HEADWIND
OBSTACLE HEIGHT ~ FEET
0 50
DIS
TAN
CE
~ F
EET
0
1000
2000
3000
4000
WIND COMPONENT ~ KNOTS
0 10 20 30
ISA
WEIGHT ~ POUNDS
9000100001100012000
ASSOCIATED CONDITIONS: POWER................................
PROPELLER CONTROLS.....FLAPS..................................RUNWAY.............................APPROACH SPEED............BRAKING.............................
RETARDED TO MAINTAIN 1,000 FT.MINRATE OF DESCENT ON FINAL APPROACHFULL FORWARDDOWNPAVED, LEVEL, DRY SURFACEIAS AS TABULATEDMAXIMUM
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-126 FAA Approved: Revision IR: April 29, 2009
OBSTACLE HEIGHT ~ FEET
0 50
DIS
TAN
CE
~ FE
ET
0
1000
2000
3000
WIND COMPONENT ~ KNOTS
0 10 20 30
WEIGHT ~ POUNDS
9000100001100012000
OUTSIDE AIR TEMPERATURE ~ C
-40 -30 -20 -10 0 10 20 30 40 50 60
LANDING DISTANCE WITH PROPELLER REVERSING - FLAPS DOWNSTANDARD GEAR
WEIGHT ~ LBS
12,50012,00011,00010,0009,000
APPROACH SPEED ~ KNOTS
9795908580
REF
EREN
CE
LIN
E
REF
EREN
CE
LIN
E
REF
EREN
CE
LIN
E
HEADWIND
TAILW
IND
PRESSURE ALTITUDE ~ FEET
10,0008,000
6,000
2,000SL
ISA
4,000
EXAMPLE:OAT.............................................................PRESSURE ALTITUDE...............................LANDING WEIGHT.....................................HEADWIND COMPONENT.........................APPROACH SPEED...................................GROUND ROLL..........................................TOTAL OVER 50 FT OBSTACLE................
32C4,730 FT10,937 LBS4.7 KTS90 KIAS1,030 FT1,800 FT
ASSOCIATED CONDITIONS:POWER..................................
PROPELLER CONTROLS......FLAPS....................................RUNWAY................................APPROACH SPEED...............CONDITION LEVERS.............BRAKING................................POWER LEVERS...................
RETARDED TO MAINTAIN 1,000 FT/MINRATE OF DESCENT ON FINAL APPROACHFULL FORWARDDOWNPAVED, LEVEL, DRY SURFACEIAS AS TABULATEDHIGH IDLEMAXIMUMMAXIMUM REVERSE AFTER TOUCHDOWNUNTIL FULLY STOPPED
GUIDELINES NOT APPLICABLEFOR INTERMEDIATEOBSTACLE HEIGHTS
-
BEECHCRAFT Super King Air 200/B200 Series Equipped with Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
Document No. 09EA-52-116 Section VI Weight and Balance
Reference Material: Revision IR: April 29, 2009 5-127
FLAPS DOWN LANDING DISTANCE OVER 50 FT OBSTACLE ~ FEET
0 1000 2000 3000 4000
FLA
PS
UP
LA
ND
ING
DIS
TAN
CE
OV
ER
50
FT O
BS
TAC
LE ~
FE
ET
2000
3000
4000
5000
6000
7000
8000
LANDING DISTANCE WITHOUT PROPELLER REVERSING - FLAPS UPSTANDARD GEAR
WEIGHT ~ LBS12,50012,00011,00010,0009,000
APPROACH SPEED ~ KNOTS121119113108103
NOTE: 1.
2.
LANDING WITH FLAPS FULL DOWN IS NORMAL PROCEDURE. USE THIS GRAPH WHEN IT ISNECESSARY TO LAND WITH FLAPS UP.TO DETERMINE FLAPS UP LANDING DISTANCE, READ FROM THE LANDING DISTANCE WITHOUT PRO-PELLER REVERSING - FLAPS DOWN. GRAPH THE LANDING DISTANCE APPROPRIATE TO OAT,ALTITUDE, WEIGHT, WIND, AND 50-FT OBSTACLE. THEN ENTER THIS GRAPH WITH THE DERIVED VALUEAND READ THE FLAPS UP LANDING DISTANCE.
ASSOCIATED CONDITIONS:POWER.........................................
PROPELLER REVERSING............FLAPS............................................RUNWAY.......................................APPROACH SPEED......................BRAKING.......................................
RETARDED TO MAINTAIN 900 FT/MINON FINAL APPROACHFULL FORWARDUPPAVED, LEVEL, DRY SURFACEIAS AS TABULATEDMAXIMUM
EXAMPLE:FLAPS DOWN LANDING DISTANCEOVER 50 FT OBSTACLE...................................LANDING WEIGHT............................................FLAPS UP LANDING DISTANCEOVER 50 FT OBSTACLE...................................APPROACH SPEED..........................................
2,290 FT10,937 LBS
4,100 FT113 KTS
-
Document No. 09EA-52-116 Section V Performance
BEECHCRAFT Super King Air 200/B200 Series Equipped with: Enhanced Aero -52 Engines Quiet Turbofan Propellers Ram Air Recovery System Enhanced Performance Leading Edges Dual Aft Body Strakes Fully Enclosed MLG Doors (when HFG-equipped)
5-128 Reference Material: Revision IR: April 29, 2009
FLAPS DOWN LANDING DISTANCE OVER 50 FT OBSTACLE ~ FEET
0 1000 2000 3000
FLA
PS
UP
LA
ND
ING
DIS
TAN
CE
OV
ER
50
FT O
BS
TAC
LE ~
FE
ET
0
1000
2000
3000
4000
5000
LANDING DISTANCE WITH PROPELLER REVERSING - FLAPS UPSTANDARD GEAR
WEIGHT ~ LBS12,50012,00011,00010,0009,000
APPROACH SPEED ~ KNOTS121119113108103
ASSOCIATED CONDITIONS:POWER.........................................
FLAPS...........................................RUNWAY.......................................APPROACH SPEED......................BRAKING.......................................CONDITION LEVERS....................P