source: src/mlx/acft.py@ 101:35e361b4c306

Last change on this file since 101:35e361b4c306 was 101:35e361b4c306, checked in by István Váradi <ivaradi@…>, 12 years ago

Takeoff V-speeds can be entered after takeoff as well.
File size: 26.6 KB
Line 
1# Module for the simulator-independent aircraft classes
2
3#---------------------------------------------------------------------------------------
4
5import const
6import checks
7import util
8
9import time
10
11#---------------------------------------------------------------------------------------
12
13class Aircraft(object):
14 """Base class for aircraft."""
15 @staticmethod
16 def create(flight):
17 """Create an aircraft instance for the type in the given flight."""
18 return _classes[flight.aircraftType](flight)
19
20 def __init__(self, flight):
21 """Construct the aircraft for the given type."""
22 self._flight = flight
23 self._aircraftState = None
24
25 self._maxVS = -10000.0
26 self._minVS = 10000.0
27
28 self._v1r2LineIndex = None
29 self._vrefLineIndex = None
30
31 self._checkers = []
32
33 # Loggers
34
35 self._checkers.append(checks.StageChecker())
36 self._checkers.append(checks.TakeOffLogger())
37
38 self._checkers.append(checks.AltimeterLogger())
39
40 self._checkers.append(checks.NAV1Logger())
41 self._checkers.append(checks.NAV2Logger())
42 self._checkers.append(checks.SquawkLogger())
43
44 self._checkers.append(checks.AnticollisionLightsLogger())
45 self._checkers.append(checks.LandingLightsLogger())
46 self._checkers.append(checks.StrobeLightsLogger())
47 self._checkers.append(checks.NavLightsLogger())
48
49 self._checkers.append(checks.FlapsLogger())
50
51 self._checkers.append(checks.GearsLogger())
52 self._checkers.append(checks.CruiseSpeedLogger())
53 self._checkers.append(checks.SpoilerLogger())
54
55 # Fault checkers
56
57 self._checkers.append(checks.AntiCollisionLightsChecker())
58 self._checkers.append(checks.LandingLightsChecker())
59 self._checkers.append(checks.NavLightsChecker())
60 self._checkers.append(checks.StrobeLightsChecker())
61
62 self._checkers.append(checks.BankChecker())
63
64 self._checkers.append(checks.FlapsRetractChecker())
65 self._checkers.append(checks.FlapsSpeedLimitChecker())
66
67 self._checkers.append(checks.GearsDownChecker())
68 self._checkers.append(checks.GearSpeedLimitChecker())
69
70 self._checkers.append(checks.GLoadChecker())
71
72 self._checkers.append(checks.MLWChecker())
73 self._checkers.append(checks.MTOWChecker())
74 self._checkers.append(checks.MZFWChecker())
75 self._checkers.append(checks.PayloadChecker())
76
77 self._checkers.append(checks.SpeedChecker())
78 self._checkers.append(checks.VSChecker())
79 self._checkers.append(checks.OverspeedChecker())
80 self._checkers.append(checks.StallChecker())
81
82 self._checkers.append(checks.PitotChecker())
83
84 self._checkers.append(checks.ReverserChecker())
85
86 @property
87 def type(self):
88 """Get the type of the aircraft."""
89 return self._flight.aircraftType
90
91 @property
92 def flight(self):
93 """Get the flight the aircraft belongs to."""
94 return self._flight
95
96 @property
97 def logger(self):
98 """Get the logger to use for the aircraft."""
99 return self._flight.logger
100
101 def getFlapsSpeedLimit(self, flaps):
102 """Get the speed limit for the given flaps setting."""
103 return self.flapSpeedLimits[flaps] if flaps in self.flapSpeedLimits \
104 else None
105
106 def modelChanged(self, timestamp, aircraftName, modelName):
107 """Called when the simulator's aircraft changes."""
108 self._flight.logger.message(timestamp,
109 "Aircraft: name='%s', model='%s'" % \
110 (aircraftName, modelName))
111
112 def handleState(self, aircraftState):
113 """Called when the state of the aircraft changes."""
114 for checker in self._checkers:
115 checker.check(self._flight, self, self._flight.logger,
116 self._aircraftState, aircraftState)
117
118 self._flight.handleState(self._aircraftState, aircraftState)
119
120 self._maxVS = max(self._maxVS, aircraftState.vs)
121 self._minVS = min(self._minVS, aircraftState.vs)
122
123 self._aircraftState = aircraftState
124
125 def setStage(self, aircraftState, newStage):
126 """Set the given stage as the new one and do whatever should be
127 done."""
128 if self._flight.setStage(aircraftState.timestamp, newStage):
129 if newStage==const.STAGE_PUSHANDTAXI:
130 self.logger.message(aircraftState.timestamp, "Block time start")
131 self.logFuel(aircraftState)
132 self.logger.message(aircraftState.timestamp,
133 "Zero-fuel weight: %.0f kg" % (aircraftState.zfw))
134 elif newStage==const.STAGE_TAKEOFF:
135 self.logger.message(aircraftState.timestamp, "Flight time start")
136 self.logger.message(aircraftState.timestamp,
137 "Takeoff weight: %.0f kg, MTOW: %.0f kg" % \
138 (aircraftState.grossWeight, self.mtow))
139 self.logger.message(aircraftState.timestamp,
140 "Wind %03.0f degrees at %.0f knots" % \
141 (aircraftState.windDirection,
142 aircraftState.windSpeed))
143 self._logV1R2()
144 elif newStage==const.STAGE_TAXIAFTERLAND:
145 self.logger.message(aircraftState.timestamp, "Flight time end")
146 self.logFuel(aircraftState)
147 self.logger.message(aircraftState.timestamp,
148 "Landing weight: %.0f kg, MLW: %.0f" % \
149 (aircraftState.grossWeight, self.mlw))
150 self.logger.message(aircraftState.timestamp,
151 "Vertical speed range: %.0f..%.0f feet/min" % \
152 (self._minVS, self._maxVS))
153 elif newStage==const.STAGE_PARKING:
154 self.logger.message(aircraftState.timestamp, "Block time end")
155 elif newStage==const.STAGE_END:
156 flightLength = self._flight.flightTimeEnd - self._flight.flightTimeStart
157 self.logger.message(aircraftState.timestamp,
158 "Flight time: " +
159 util.getTimeIntervalString(flightLength))
160 self.logger.message(aircraftState.timestamp,
161 "Flown distance: %.2f NM" % \
162 (self._flight.flownDistance,))
163 blockLength = self._flight.blockTimeEnd - self._flight.blockTimeStart
164 self.logger.message(aircraftState.timestamp,
165 "Block time: " +
166 util.getTimeIntervalString(blockLength))
167
168 def prepareFlare(self):
169 """Called when it is detected that we will soon flare.
170
171 On the first call, it should start monitoring some parameters more
172 closely to determine flare time."""
173 self.flight.simulator.startFlare()
174
175 def flareStarted(self, windSpeed, windDirection, visibility,
176 flareStart, flareStartFS):
177 """Called when the flare has started."""
178 self.logger.message(self._aircraftState.timestamp, "The flare has begun")
179 self.logger.message(self._aircraftState.timestamp,
180 "Wind %03.0f degrees at %.0f knots" % \
181 (windDirection, windSpeed))
182 self.logger.message(self._aircraftState.timestamp,
183 "Visibility: %.0f metres" % (visibility,))
184 self.logger.message(self._aircraftState.timestamp,
185 "Altimeter setting: %.0f hPa" % \
186 (self._aircraftState.altimeter,))
187 self._logVRef()
188 self.flight.flareStarted(flareStart, flareStartFS)
189
190 def flareFinished(self, flareEnd, flareEndFS, tdRate, tdRateCalculatedByFS,
191 ias, pitch, bank, heading):
192 """Called when the flare has finished."""
193 (flareTimeFromFS, flareTime) = self.flight.flareFinished(flareEnd,
194 flareEndFS)
195 self.logger.message(self._aircraftState.timestamp,
196 "Flare time: %.1f s (from %s)" % \
197 (flareTime,
198 "the simulator" if flareTimeFromFS else "real time",))
199 self.logger.message(self._aircraftState.timestamp,
200 "Touchdown rate: %.0f feet/min" % (tdRate,))
201 self.logger.message(self._aircraftState.timestamp,
202 "Touchdown rate was calculated by the %s" % \
203 ("simulator" if tdRateCalculatedByFS else "logger",))
204 self.logger.message(self._aircraftState.timestamp,
205 "Touchdown speed: %.0f knots" % (ias,))
206 self.logger.message(self._aircraftState.timestamp,
207 "Touchdown pitch: %.1f degrees" % (pitch,))
208 self.logger.message(self._aircraftState.timestamp,
209 "Touchdown bank: %.1f degrees" % (bank,))
210 self.logger.message(self._aircraftState.timestamp,
211 "Touchdown heading: %03.0f degrees" % (heading,))
212
213 def cancelFlare(self):
214 """Cancel flare, if it has started."""
215 self.flight.simulator.cancelFlare()
216
217 def checkFlightEnd(self, aircraftState):
218 """Check if the end of the flight has arrived.
219
220 This default implementation checks the N1 values, but for
221 piston-powered aircraft you need to check the RPMs."""
222 for n1 in aircraftState.n1:
223 if n1>=0.5: return False
224 return True
225
226 def updateV1R2(self):
227 """Update the V1, Vr and V2 values from the flight, if the these values
228 have already been logged."""
229 if self._v1r2LineIndex is not None:
230 self._logV1R2()
231
232 def _logV1R2(self):
233 """Log the V1, Vr and V2 value either newly, or by updating the
234 corresponding line."""
235 message = "Speeds calculated by the pilot: V1: %s, VR: %s, V2: %s" % \
236 ("-" if self._flight.v1 is None
237 else str(self._flight.v1),
238 "-" if self._flight.vr is None
239 else str(self._flight.vr),
240 "-" if self._flight.v2 is None
241 else str(self._flight.v2))
242
243 if self._v1r2LineIndex is None:
244 self._v1r2LineIndex = \
245 self.logger.message(self._aircraftState.timestamp, message)
246 else:
247 self.logger.updateLine(self._v1r2LineIndex, message)
248
249 def updateVRef(self):
250 """Update the Vref value from the flight, if the Vref value has already
251 been logged."""
252 if self._vrefLineIndex is not None:
253 self._logVRef()
254
255 def _logVRef(self):
256 """Log the Vref value either newly, or by updating the corresponding
257 line."""
258 message = "VRef speed calculated by the pilot: %s" % \
259 ("-" if self._flight.vref is None else str(self._flight.vref))
260 if self._vrefLineIndex is None:
261 self._vrefLineIndex = \
262 self.logger.message(self._aircraftState.timestamp, message)
263 else:
264 self.logger.updateLine(self._vrefLineIndex, message)
265
266#---------------------------------------------------------------------------------------
267
268class Boeing737(Aircraft):
269 """Base class for the various aircraft in the Boeing 737 family.
270
271 The aircraft type-specific values in the aircraft state have the following
272 structure:
273 - fuel: centre, left, right
274 - n1: left, right
275 - reverser: left, right"""
276 def __init__(self, flight):
277 super(Boeing737, self).__init__(flight)
278 self._checkers.append(checks.ThrustChecker())
279
280 self.gearSpeedLimit = 270
281 self.flapSpeedLimits = { 1 : 260,
282 2 : 260,
283 5 : 250,
284 10 : 210,
285 15 : 200,
286 25 : 190,
287 30 : 175,
288 40 : 162 }
289
290 def logFuel(self, aircraftState):
291 """Log the amount of fuel"""
292 self.logger.message(aircraftState.timestamp,
293 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
294 (aircraftState.fuel[1], aircraftState.fuel[0],
295 aircraftState.fuel[2]))
296 self.logger.message(aircraftState.timestamp,
297 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
298
299#---------------------------------------------------------------------------------------
300
301class B736(Boeing737):
302 """Boeing 737-600 aircraft."""
303 def __init__(self, flight):
304 super(B736, self).__init__(flight)
305 self.dow = 38307
306 self.mtow = 58328
307 self.mlw = 54657
308 self.mzfw = 51482
309
310#---------------------------------------------------------------------------------------
311
312class B737(Boeing737):
313 """Boeing 737-700 aircraft."""
314 def __init__(self, flight):
315 super(B737, self).__init__(flight)
316 self.dow = 39250
317 self.mtow = 61410
318 self.mlw = 58059
319 self.mzfw = 54657
320
321#---------------------------------------------------------------------------------------
322
323class B738(Boeing737):
324 """Boeing 737-800 aircraft."""
325 def __init__(self, flight):
326 super(B738, self).__init__(flight)
327 self.dow = 42690
328 self.mtow = 71709
329 self.mlw = 65317
330 self.mzfw = 61688
331
332#---------------------------------------------------------------------------------------
333
334class B738Charter(B738):
335 """Boeing 737-800 aircraft used for charters."""
336 def __init__(self, flight):
337 super(B738Charter, self).__init__(flight)
338 self.mtow = 77791
339
340#---------------------------------------------------------------------------------------
341
342class B733(Boeing737):
343 """Boeing 737-300 aircraft."""
344 def __init__(self, flight):
345 super(B733, self).__init__(flight)
346 self.dow = 32700
347 self.mtow = 62820
348 self.mlw = 51700
349 self.mzfw = 48410
350
351#---------------------------------------------------------------------------------------
352
353class B734(Boeing737):
354 """Boeing 737-400 aircraft."""
355 def __init__(self, flight):
356 super(B734, self).__init__(flight)
357 self.dow = 33200
358 self.mtow = 68050
359 self.mlw = 56200
360 self.mzfw = 53100
361
362#---------------------------------------------------------------------------------------
363
364class B735(Boeing737):
365 """Boeing 737-500 aircraft."""
366 def __init__(self, flight):
367 super(B735, self).__init__(flight)
368 self.dow = 31300
369 self.mtow = 60550
370 self.mlw = 50000
371 self.mzfw = 46700
372
373#---------------------------------------------------------------------------------------
374
375class DH8D(Aircraft):
376 """Bombardier Dash-8 Q400 aircraft.
377
378 The aircraft type-specific values in the aircraft state have the following
379 structure:
380 - fuel: centre, left, right
381 - n1: left, right
382 - reverser: left, right."""
383 def __init__(self, flight):
384 super(DH8D, self).__init__(flight)
385 self.dow = 17185
386 self.mtow = 29257
387 self.mlw = 28009
388 self.mzfw = 25855
389 self.gearSpeedLimit = 215
390 self.flapSpeedLimits = { 5 : 200,
391 10 : 181,
392 15 : 172,
393 35 : 158 }
394
395 def logFuel(self, aircraftState):
396 """Log the amount of fuel"""
397 self.logger.message(aircraftState.timestamp,
398 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
399 (aircraftState.fuel[1], aircraftState.fuel[0],
400 aircraftState.fuel[2]))
401 self.logger.message(aircraftState.timestamp,
402 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
403
404#---------------------------------------------------------------------------------------
405
406class Boeing767(Aircraft):
407 """Base class for the various aircraft in the Boeing 767 family.
408
409 The aircraft type-specific values in the aircraft state have the following
410 structure:
411 - fuel: centre, left, right
412 - n1: left, right
413 - reverser: left, right"""
414 def __init__(self, flight):
415 super(Boeing767, self).__init__(flight)
416 self._checkers.append(checks.ThrustChecker())
417 self.gearSpeedLimit = 270
418 self.flapSpeedLimits = { 1 : 255,
419 5 : 235,
420 10 : 215,
421 20 : 215,
422 25 : 185,
423 30 : 175 }
424
425 def logFuel(self, aircraftState):
426 """Log the amount of fuel"""
427 self.logger.message(aircraftState.timestamp,
428 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
429 (aircraftState.fuel[1], aircraftState.fuel[0],
430 aircraftState.fuel[2]))
431 self.logger.message(aircraftState.timestamp,
432 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
433
434#---------------------------------------------------------------------------------------
435
436class B762(Boeing767):
437 """Boeing 767-200 aircraft."""
438 def __init__(self, flight):
439 super(B762, self).__init__(flight)
440 self.dow = 84507
441 self.mtow = 175540
442 self.mlw = 126098
443 self.mzfw = 114758
444
445#---------------------------------------------------------------------------------------
446
447class B763(Boeing767):
448 """Boeing 767-300 aircraft."""
449 def __init__(self, flight):
450 super(B763, self).__init__(cflight)
451 self.dow = 91311
452 self.mtow = 181436
453 self.mlw = 137892
454 self.mzfw = 130635
455
456#---------------------------------------------------------------------------------------
457
458class CRJ2(Aircraft):
459 """Bombardier CRJ-200 aircraft.
460
461 The aircraft type-specific values in the aircraft state have the following
462 structure:
463 - fuel: centre, left, right
464 - n1: left, right
465 - reverser: left, right."""
466 def __init__(self, flight):
467 super(CRJ2, self).__init__(flight)
468 self._checkers.append(checks.ThrustChecker())
469 self.dow = 14549
470 self.mtow = 22995
471 self.mlw = 21319
472 self.mzfw = 19958
473 self.gearSpeedLimit = 240
474 self.flapSpeedLimits = { 8 : 260,
475 20 : 220,
476 30 : 190,
477 45 : 175 }
478
479 def logFuel(self, aircraftState):
480 """Log the amount of fuel"""
481 self.logger.message(aircraftState.timestamp,
482 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
483 (aircraftState.fuel[1], aircraftState.fuel[0],
484 aircraftState.fuel[2]))
485 self.logger.message(aircraftState.timestamp,
486 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
487
488#---------------------------------------------------------------------------------------
489
490class F70(Aircraft):
491 """Fokker 70 aircraft.
492
493 The aircraft type-specific values in the aircraft state have the following
494 structure:
495 - fuel: centre, left, right
496 - n1: left, right
497 - reverser: left, right."""
498 def __init__(self, flight):
499 super(F70, self).__init__(flight)
500 self._checkers.append(checks.ThrustChecker())
501 self.dow = 24283
502 self.mtow = 38100 # FIXME: differentiate by registration number,
503 # MTOW of HA-LMF: 41955
504 self.mlw = 36740
505 self.mzfw = 32655
506 self.gearSpeedLimit = 200
507 self.flapSpeedLimits = { 8 : 250,
508 15 : 220,
509 25 : 220,
510 42 : 180 }
511
512 def logFuel(self, aircraftState):
513 """Log the amount of fuel"""
514 self.logger.message(aircraftState.timestamp,
515 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
516 (aircraftState.fuel[1], aircraftState.fuel[0],
517 aircraftState.fuel[2]))
518 self.logger.message(aircraftState.timestamp,
519 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
520
521#---------------------------------------------------------------------------------------
522
523class DC3(Aircraft):
524 """Lisunov Li-2 (DC-3) aircraft.
525
526 The aircraft type-specific values in the aircraft state have the following
527 structure:
528 - fuel: left, right, left aux, right aux
529 - rpm: left, right
530 - reverser: left, right."""
531 def __init__(self, flight):
532 super(DC3, self).__init__(flight)
533 self.dow = 8627
534 self.mtow = 11884
535 self.mlw = 11793
536 self.mzfw = 11780
537 self.gearSpeedLimit = 148
538 self.flapSpeedLimits = { 15 : 135,
539 30 : 99,
540 45 : 97 }
541
542 def _checkFlightEnd(self, aircraftState):
543 """Check if the end of the flight has arrived.
544
545 This implementation checks the RPM values to be 0."""
546 for rpm in aircraftState.rpm:
547 if rpm>0: return False
548 return True
549
550 def logFuel(self, aircraftState):
551 """Log the amount of fuel"""
552 self.logger.message(aircraftState.timestamp,
553 "Fuel: left aux=%.0f kg - left=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
554 (aircraftState.fuel[2], aircraftState.fuel[0],
555 aircraftState.fuel[1], aircraftState.fuel[3]))
556 self.logger.message(aircraftState.timestamp,
557 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
558
559#---------------------------------------------------------------------------------------
560
561class T134(Aircraft):
562 """Tupolev Tu-134 aircraft.
563
564 The aircraft type-specific values in the aircraft state have the following
565 structure:
566 - fuel: centre, left tip, left aux, right tip, right aux, external 1,
567 external 2
568 - n1: left, right
569 - reverser: left, right."""
570 def __init__(self, flight):
571 super(T134, self).__init__(flight)
572 self._checkers.append(checks.ThrustChecker())
573 self.dow = 29927
574 self.mtow = 47600
575 self.mlw = 43000
576 self.mzfw = 38500
577 self.gearSpeedLimit = 216
578 self.flapSpeedLimits = { 10 : 240,
579 20 : 216,
580 30 : 161 }
581
582 def logFuel(self, aircraftState):
583 """Log the amount of fuel"""
584 self.logger.message(aircraftState.timestamp,
585 "Fuel: left aux=%.0f kg - left tip=%.0f kg - centre= %.0f kg - right tip=%.0f kg - right aux=%.0f kg - external 1=%.0f kg - external 2=%.0f kg" % \
586 (aircraftState.fuel[2], aircraftState.fuel[1],
587 aircraftState.fuel[0],
588 aircraftState.fuel[3], aircraftState.fuel[4],
589 aircraftState.fuel[5], aircraftState.fuel[6]))
590 self.logger.message(aircraftState.timestamp,
591 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
592
593#---------------------------------------------------------------------------------------
594
595class T154(Aircraft):
596 """Tupolev Tu-154 aircraft.
597
598 The aircraft type-specific values in the aircraft state have the following
599 structure:
600 - fuel: centre, left, right, centre 2, left aux, right aux
601 - n1: left, centre, right
602 - reverser: left, right"""
603 def __init__(self, flight):
604 super(T154, self).__init__(flight)
605 self._checkers.append(checks.ThrustChecker())
606 self.dow = 53259
607 self.mtow = 98000
608 self.mlw = 78000
609 self.mzfw = 72000
610 self.gearSpeedLimit = 216
611 self.flapSpeedLimits = { 15 : 227,
612 28 : 194,
613 45 : 162 }
614
615 def logFuel(self, aircraftState):
616 """Log the amount of fuel"""
617 self.logger.message(aircraftState.timestamp,
618 "Fuel: left aux=%.0f kg - left=%.0f kg - centre=%.0f kg - centre 2=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
619 (aircraftState.fuel[4], aircraftState.fuel[1],
620 aircraftState.fuel[0], aircraftState.fuel[3],
621 aircraftState.fuel[2], aircraftState.fuel[5]))
622 self.logger.message(aircraftState.timestamp,
623 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
624
625#---------------------------------------------------------------------------------------
626
627
628class YK40(Aircraft):
629 """Yakovlev Yak-40 aircraft.
630
631 The aircraft type-specific values in the aircraft state have the following
632 structure:
633 - fuel: left, right
634 - n1: left, right
635 - reverser: left, right"""
636 def __init__(self, flight):
637 super(YK40, self).__init__(flight)
638 self._checkers.append(checks.ThrustChecker())
639 self.dow = 9400
640 self.mtow = 17200
641 self.mlw = 16800
642 self.mzfw = 12100
643 self.gearSpeedLimit = 165
644 self.flapSpeedLimits = { 20 : 165,
645 35 : 135 }
646
647 def logFuel(self, aircraftState):
648 """Log the amount of fuel"""
649 self.logger.message(aircraftState.timestamp,
650 "Fuel: left=%.0f kg - right=%.0f kg" % \
651 (aircraftState.fuel[0], aircraftState.fuel[1]))
652 self.logger.message(aircraftState.timestamp,
653 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
654
655#---------------------------------------------------------------------------------------
656
657_classes = { const.AIRCRAFT_B736 : B736,
658 const.AIRCRAFT_B737 : B737,
659 const.AIRCRAFT_B738 : B738,
660 const.AIRCRAFT_B733 : B733,
661 const.AIRCRAFT_B734 : B734,
662 const.AIRCRAFT_B735 : B735,
663 const.AIRCRAFT_DH8D : DH8D,
664 const.AIRCRAFT_B762 : B762,
665 const.AIRCRAFT_B763 : B763,
666 const.AIRCRAFT_CRJ2 : CRJ2,
667 const.AIRCRAFT_F70 : F70,
668 const.AIRCRAFT_DC3 : DC3,
669 const.AIRCRAFT_T134 : T134,
670 const.AIRCRAFT_T154 : T154,
671 const.AIRCRAFT_YK40 : YK40 }
672
673#---------------------------------------------------------------------------------------
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