source: src/mlx/acft.py@ 130:f3b2a892af5a

Last change on this file since 130:f3b2a892af5a was 117:af3d52b9adc4, checked in by István Váradi <ivaradi@…>, 13 years ago

Implemented the weight help tab
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.humanWeight = 82.0
32
33 self._checkers = []
34
35 # Loggers
36
37 self._checkers.append(checks.StageChecker())
38 self._checkers.append(checks.TakeOffLogger())
39
40 self._checkers.append(checks.AltimeterLogger())
41
42 self._checkers.append(checks.NAV1Logger())
43 self._checkers.append(checks.NAV2Logger())
44 self._checkers.append(checks.SquawkLogger())
45
46 self._checkers.append(checks.AnticollisionLightsLogger())
47 self._checkers.append(checks.LandingLightsLogger())
48 self._checkers.append(checks.StrobeLightsLogger())
49 self._checkers.append(checks.NavLightsLogger())
50
51 self._checkers.append(checks.FlapsLogger())
52
53 self._checkers.append(checks.GearsLogger())
54 self._checkers.append(checks.CruiseSpeedLogger())
55 self._checkers.append(checks.SpoilerLogger())
56
57 # Fault checkers
58
59 self._checkers.append(checks.AntiCollisionLightsChecker())
60 self._checkers.append(checks.LandingLightsChecker())
61 self._checkers.append(checks.NavLightsChecker())
62 self._checkers.append(checks.StrobeLightsChecker())
63
64 self._checkers.append(checks.BankChecker())
65
66 self._checkers.append(checks.FlapsRetractChecker())
67 self._checkers.append(checks.FlapsSpeedLimitChecker())
68
69 self._checkers.append(checks.GearsDownChecker())
70 self._checkers.append(checks.GearSpeedLimitChecker())
71
72 self._checkers.append(checks.GLoadChecker())
73
74 self._checkers.append(checks.MLWChecker())
75 self._checkers.append(checks.MTOWChecker())
76 self._checkers.append(checks.MZFWChecker())
77 self._checkers.append(checks.PayloadChecker())
78
79 self._checkers.append(checks.SpeedChecker())
80 self._checkers.append(checks.VSChecker())
81 self._checkers.append(checks.OverspeedChecker())
82 self._checkers.append(checks.StallChecker())
83
84 self._checkers.append(checks.PitotChecker())
85
86 self._checkers.append(checks.ReverserChecker())
87
88 @property
89 def type(self):
90 """Get the type of the aircraft."""
91 return self._flight.aircraftType
92
93 @property
94 def flight(self):
95 """Get the flight the aircraft belongs to."""
96 return self._flight
97
98 @property
99 def logger(self):
100 """Get the logger to use for the aircraft."""
101 return self._flight.logger
102
103 def getFlapsSpeedLimit(self, flaps):
104 """Get the speed limit for the given flaps setting."""
105 return self.flapSpeedLimits[flaps] if flaps in self.flapSpeedLimits \
106 else None
107
108 def modelChanged(self, timestamp, aircraftName, modelName):
109 """Called when the simulator's aircraft changes."""
110 self._flight.logger.message(timestamp,
111 "Aircraft: name='%s', model='%s'" % \
112 (aircraftName, modelName))
113
114 def handleState(self, aircraftState):
115 """Called when the state of the aircraft changes."""
116 for checker in self._checkers:
117 checker.check(self._flight, self, self._flight.logger,
118 self._aircraftState, aircraftState)
119
120 self._flight.handleState(self._aircraftState, aircraftState)
121
122 self._maxVS = max(self._maxVS, aircraftState.vs)
123 self._minVS = min(self._minVS, aircraftState.vs)
124
125 self._aircraftState = aircraftState
126
127 def setStage(self, aircraftState, newStage):
128 """Set the given stage as the new one and do whatever should be
129 done."""
130 if self._flight.setStage(aircraftState.timestamp, newStage):
131 if newStage==const.STAGE_PUSHANDTAXI:
132 self.logger.message(aircraftState.timestamp, "Block time start")
133 self.logFuel(aircraftState)
134 self.logger.message(aircraftState.timestamp,
135 "Zero-fuel weight: %.0f kg" % (aircraftState.zfw))
136 elif newStage==const.STAGE_TAKEOFF:
137 self.logger.message(aircraftState.timestamp, "Flight time start")
138 self.logger.message(aircraftState.timestamp,
139 "Takeoff weight: %.0f kg, MTOW: %.0f kg" % \
140 (aircraftState.grossWeight, self.mtow))
141 self.logger.message(aircraftState.timestamp,
142 "Wind %03.0f degrees at %.0f knots" % \
143 (aircraftState.windDirection,
144 aircraftState.windSpeed))
145 self._logV1R2()
146 elif newStage==const.STAGE_TAXIAFTERLAND:
147 self.logger.message(aircraftState.timestamp, "Flight time end")
148 self.logFuel(aircraftState)
149 self.logger.message(aircraftState.timestamp,
150 "Landing weight: %.0f kg, MLW: %.0f" % \
151 (aircraftState.grossWeight, self.mlw))
152 self.logger.message(aircraftState.timestamp,
153 "Vertical speed range: %.0f..%.0f feet/min" % \
154 (self._minVS, self._maxVS))
155 elif newStage==const.STAGE_PARKING:
156 self.logger.message(aircraftState.timestamp, "Block time end")
157 elif newStage==const.STAGE_END:
158 flightLength = self._flight.flightTimeEnd - self._flight.flightTimeStart
159 self.logger.message(aircraftState.timestamp,
160 "Flight time: " +
161 util.getTimeIntervalString(flightLength))
162 self.logger.message(aircraftState.timestamp,
163 "Flown distance: %.2f NM" % \
164 (self._flight.flownDistance,))
165 blockLength = self._flight.blockTimeEnd - self._flight.blockTimeStart
166 self.logger.message(aircraftState.timestamp,
167 "Block time: " +
168 util.getTimeIntervalString(blockLength))
169
170 def prepareFlare(self):
171 """Called when it is detected that we will soon flare.
172
173 On the first call, it should start monitoring some parameters more
174 closely to determine flare time."""
175 self.flight.simulator.startFlare()
176
177 def flareStarted(self, windSpeed, windDirection, visibility,
178 flareStart, flareStartFS):
179 """Called when the flare has started."""
180 self.logger.message(self._aircraftState.timestamp, "The flare has begun")
181 self.logger.message(self._aircraftState.timestamp,
182 "Wind %03.0f degrees at %.0f knots" % \
183 (windDirection, windSpeed))
184 self.logger.message(self._aircraftState.timestamp,
185 "Visibility: %.0f metres" % (visibility,))
186 self.logger.message(self._aircraftState.timestamp,
187 "Altimeter setting: %.0f hPa" % \
188 (self._aircraftState.altimeter,))
189 self._logVRef()
190 self.flight.flareStarted(flareStart, flareStartFS)
191
192 def flareFinished(self, flareEnd, flareEndFS, tdRate, tdRateCalculatedByFS,
193 ias, pitch, bank, heading):
194 """Called when the flare has finished."""
195 (flareTimeFromFS, flareTime) = self.flight.flareFinished(flareEnd,
196 flareEndFS)
197 self.logger.message(self._aircraftState.timestamp,
198 "Flare time: %.1f s (from %s)" % \
199 (flareTime,
200 "the simulator" if flareTimeFromFS else "real time",))
201 self.logger.message(self._aircraftState.timestamp,
202 "Touchdown rate: %.0f feet/min" % (tdRate,))
203 self.logger.message(self._aircraftState.timestamp,
204 "Touchdown rate was calculated by the %s" % \
205 ("simulator" if tdRateCalculatedByFS else "logger",))
206 self.logger.message(self._aircraftState.timestamp,
207 "Touchdown speed: %.0f knots" % (ias,))
208 self.logger.message(self._aircraftState.timestamp,
209 "Touchdown pitch: %.1f degrees" % (pitch,))
210 self.logger.message(self._aircraftState.timestamp,
211 "Touchdown bank: %.1f degrees" % (bank,))
212 self.logger.message(self._aircraftState.timestamp,
213 "Touchdown heading: %03.0f degrees" % (heading,))
214
215 def cancelFlare(self):
216 """Cancel flare, if it has started."""
217 self.flight.simulator.cancelFlare()
218
219 def checkFlightEnd(self, aircraftState):
220 """Check if the end of the flight has arrived.
221
222 This default implementation checks the N1 values, but for
223 piston-powered aircraft you need to check the RPMs."""
224 for n1 in aircraftState.n1:
225 if n1>=0.5: return False
226 return True
227
228 def updateV1R2(self):
229 """Update the V1, Vr and V2 values from the flight, if the these values
230 have already been logged."""
231 if self._v1r2LineIndex is not None:
232 self._logV1R2()
233
234 def _logV1R2(self):
235 """Log the V1, Vr and V2 value either newly, or by updating the
236 corresponding line."""
237 message = "Speeds calculated by the pilot: V1: %s, VR: %s, V2: %s" % \
238 ("-" if self._flight.v1 is None
239 else str(self._flight.v1),
240 "-" if self._flight.vr is None
241 else str(self._flight.vr),
242 "-" if self._flight.v2 is None
243 else str(self._flight.v2))
244
245 if self._v1r2LineIndex is None:
246 self._v1r2LineIndex = \
247 self.logger.message(self._aircraftState.timestamp, message)
248 else:
249 self.logger.updateLine(self._v1r2LineIndex, message)
250
251 def updateVRef(self):
252 """Update the Vref value from the flight, if the Vref value has already
253 been logged."""
254 if self._vrefLineIndex is not None:
255 self._logVRef()
256
257 def _logVRef(self):
258 """Log the Vref value either newly, or by updating the corresponding
259 line."""
260 message = "VRef speed calculated by the pilot: %s" % \
261 ("-" if self._flight.vref is None else str(self._flight.vref))
262 if self._vrefLineIndex is None:
263 self._vrefLineIndex = \
264 self.logger.message(self._aircraftState.timestamp, message)
265 else:
266 self.logger.updateLine(self._vrefLineIndex, message)
267
268#---------------------------------------------------------------------------------------
269
270class Boeing737(Aircraft):
271 """Base class for the various aircraft in the Boeing 737 family.
272
273 The aircraft type-specific values in the aircraft state have the following
274 structure:
275 - fuel: centre, left, right
276 - n1: left, right
277 - reverser: left, right"""
278 def __init__(self, flight):
279 super(Boeing737, self).__init__(flight)
280 self._checkers.append(checks.ThrustChecker())
281
282 self.gearSpeedLimit = 270
283 self.flapSpeedLimits = { 1 : 260,
284 2 : 260,
285 5 : 250,
286 10 : 210,
287 15 : 200,
288 25 : 190,
289 30 : 175,
290 40 : 162 }
291
292 def logFuel(self, aircraftState):
293 """Log the amount of fuel"""
294 self.logger.message(aircraftState.timestamp,
295 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
296 (aircraftState.fuel[1], aircraftState.fuel[0],
297 aircraftState.fuel[2]))
298 self.logger.message(aircraftState.timestamp,
299 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
300
301#---------------------------------------------------------------------------------------
302
303class B736(Boeing737):
304 """Boeing 737-600 aircraft."""
305 def __init__(self, flight):
306 super(B736, self).__init__(flight)
307 self.dow = 38307
308 self.mtow = 58328
309 self.mlw = 54657
310 self.mzfw = 51482
311
312#---------------------------------------------------------------------------------------
313
314class B737(Boeing737):
315 """Boeing 737-700 aircraft."""
316 def __init__(self, flight):
317 super(B737, self).__init__(flight)
318 self.dow = 39250
319 self.mtow = 61410
320 self.mlw = 58059
321 self.mzfw = 54657
322
323#---------------------------------------------------------------------------------------
324
325class B738(Boeing737):
326 """Boeing 737-800 aircraft."""
327 def __init__(self, flight):
328 super(B738, self).__init__(flight)
329 self.dow = 42690
330 self.mtow = 71709
331 self.mlw = 65317
332 self.mzfw = 61688
333
334#---------------------------------------------------------------------------------------
335
336class B738Charter(B738):
337 """Boeing 737-800 aircraft used for charters."""
338 def __init__(self, flight):
339 super(B738Charter, self).__init__(flight)
340 self.mtow = 77791
341
342#---------------------------------------------------------------------------------------
343
344class B733(Boeing737):
345 """Boeing 737-300 aircraft."""
346 def __init__(self, flight):
347 super(B733, self).__init__(flight)
348 self.dow = 32700
349 self.mtow = 62820
350 self.mlw = 51700
351 self.mzfw = 48410
352
353#---------------------------------------------------------------------------------------
354
355class B734(Boeing737):
356 """Boeing 737-400 aircraft."""
357 def __init__(self, flight):
358 super(B734, self).__init__(flight)
359 self.dow = 33200
360 self.mtow = 68050
361 self.mlw = 56200
362 self.mzfw = 53100
363
364#---------------------------------------------------------------------------------------
365
366class B735(Boeing737):
367 """Boeing 737-500 aircraft."""
368 def __init__(self, flight):
369 super(B735, self).__init__(flight)
370 self.dow = 31300
371 self.mtow = 60550
372 self.mlw = 50000
373 self.mzfw = 46700
374
375#---------------------------------------------------------------------------------------
376
377class DH8D(Aircraft):
378 """Bombardier Dash-8 Q400 aircraft.
379
380 The aircraft type-specific values in the aircraft state have the following
381 structure:
382 - fuel: centre, left, right
383 - n1: left, right
384 - reverser: left, right."""
385 def __init__(self, flight):
386 super(DH8D, self).__init__(flight)
387 self.dow = 17185
388 self.mtow = 29257
389 self.mlw = 28009
390 self.mzfw = 25855
391 self.gearSpeedLimit = 215
392 self.flapSpeedLimits = { 5 : 200,
393 10 : 181,
394 15 : 172,
395 35 : 158 }
396
397 def logFuel(self, aircraftState):
398 """Log the amount of fuel"""
399 self.logger.message(aircraftState.timestamp,
400 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
401 (aircraftState.fuel[1], aircraftState.fuel[0],
402 aircraftState.fuel[2]))
403 self.logger.message(aircraftState.timestamp,
404 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
405
406#---------------------------------------------------------------------------------------
407
408class Boeing767(Aircraft):
409 """Base class for the various aircraft in the Boeing 767 family.
410
411 The aircraft type-specific values in the aircraft state have the following
412 structure:
413 - fuel: centre, left, right
414 - n1: left, right
415 - reverser: left, right"""
416 def __init__(self, flight):
417 super(Boeing767, self).__init__(flight)
418 self._checkers.append(checks.ThrustChecker())
419 self.gearSpeedLimit = 270
420 self.flapSpeedLimits = { 1 : 255,
421 5 : 235,
422 10 : 215,
423 20 : 215,
424 25 : 185,
425 30 : 175 }
426
427 def logFuel(self, aircraftState):
428 """Log the amount of fuel"""
429 self.logger.message(aircraftState.timestamp,
430 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
431 (aircraftState.fuel[1], aircraftState.fuel[0],
432 aircraftState.fuel[2]))
433 self.logger.message(aircraftState.timestamp,
434 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
435
436#---------------------------------------------------------------------------------------
437
438class B762(Boeing767):
439 """Boeing 767-200 aircraft."""
440 def __init__(self, flight):
441 super(B762, self).__init__(flight)
442 self.dow = 84507
443 self.mtow = 175540
444 self.mlw = 126098
445 self.mzfw = 114758
446
447#---------------------------------------------------------------------------------------
448
449class B763(Boeing767):
450 """Boeing 767-300 aircraft."""
451 def __init__(self, flight):
452 super(B763, self).__init__(cflight)
453 self.dow = 91311
454 self.mtow = 181436
455 self.mlw = 137892
456 self.mzfw = 130635
457
458#---------------------------------------------------------------------------------------
459
460class CRJ2(Aircraft):
461 """Bombardier CRJ-200 aircraft.
462
463 The aircraft type-specific values in the aircraft state have the following
464 structure:
465 - fuel: centre, left, right
466 - n1: left, right
467 - reverser: left, right."""
468 def __init__(self, flight):
469 super(CRJ2, self).__init__(flight)
470 self._checkers.append(checks.ThrustChecker())
471 self.dow = 14549
472 self.mtow = 22995
473 self.mlw = 21319
474 self.mzfw = 19958
475 self.gearSpeedLimit = 240
476 self.flapSpeedLimits = { 8 : 260,
477 20 : 220,
478 30 : 190,
479 45 : 175 }
480
481 def logFuel(self, aircraftState):
482 """Log the amount of fuel"""
483 self.logger.message(aircraftState.timestamp,
484 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
485 (aircraftState.fuel[1], aircraftState.fuel[0],
486 aircraftState.fuel[2]))
487 self.logger.message(aircraftState.timestamp,
488 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
489
490#---------------------------------------------------------------------------------------
491
492class F70(Aircraft):
493 """Fokker 70 aircraft.
494
495 The aircraft type-specific values in the aircraft state have the following
496 structure:
497 - fuel: centre, left, right
498 - n1: left, right
499 - reverser: left, right."""
500 def __init__(self, flight):
501 super(F70, self).__init__(flight)
502 self._checkers.append(checks.ThrustChecker())
503 self.dow = 24283
504 self.mtow = 38100 # FIXME: differentiate by registration number,
505 # MTOW of HA-LMF: 41955
506 self.mlw = 36740
507 self.mzfw = 32655
508 self.gearSpeedLimit = 200
509 self.flapSpeedLimits = { 8 : 250,
510 15 : 220,
511 25 : 220,
512 42 : 180 }
513
514 def logFuel(self, aircraftState):
515 """Log the amount of fuel"""
516 self.logger.message(aircraftState.timestamp,
517 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
518 (aircraftState.fuel[1], aircraftState.fuel[0],
519 aircraftState.fuel[2]))
520 self.logger.message(aircraftState.timestamp,
521 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
522
523#---------------------------------------------------------------------------------------
524
525class DC3(Aircraft):
526 """Lisunov Li-2 (DC-3) aircraft.
527
528 The aircraft type-specific values in the aircraft state have the following
529 structure:
530 - fuel: left, right, left aux, right aux
531 - rpm: left, right
532 - reverser: left, right."""
533 def __init__(self, flight):
534 super(DC3, self).__init__(flight)
535 self.dow = 8627
536 self.mtow = 11884
537 self.mlw = 11793
538 self.mzfw = 11780
539 self.gearSpeedLimit = 148
540 self.flapSpeedLimits = { 15 : 135,
541 30 : 99,
542 45 : 97 }
543
544 def _checkFlightEnd(self, aircraftState):
545 """Check if the end of the flight has arrived.
546
547 This implementation checks the RPM values to be 0."""
548 for rpm in aircraftState.rpm:
549 if rpm>0: return False
550 return True
551
552 def logFuel(self, aircraftState):
553 """Log the amount of fuel"""
554 self.logger.message(aircraftState.timestamp,
555 "Fuel: left aux=%.0f kg - left=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
556 (aircraftState.fuel[2], aircraftState.fuel[0],
557 aircraftState.fuel[1], aircraftState.fuel[3]))
558 self.logger.message(aircraftState.timestamp,
559 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
560
561#---------------------------------------------------------------------------------------
562
563class T134(Aircraft):
564 """Tupolev Tu-134 aircraft.
565
566 The aircraft type-specific values in the aircraft state have the following
567 structure:
568 - fuel: centre, left tip, left aux, right tip, right aux, external 1,
569 external 2
570 - n1: left, right
571 - reverser: left, right."""
572 def __init__(self, flight):
573 super(T134, self).__init__(flight)
574 self._checkers.append(checks.ThrustChecker())
575 self.dow = 29927
576 self.mtow = 47600
577 self.mlw = 43000
578 self.mzfw = 38500
579 self.gearSpeedLimit = 216
580 self.flapSpeedLimits = { 10 : 240,
581 20 : 216,
582 30 : 161 }
583
584 def logFuel(self, aircraftState):
585 """Log the amount of fuel"""
586 self.logger.message(aircraftState.timestamp,
587 "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" % \
588 (aircraftState.fuel[2], aircraftState.fuel[1],
589 aircraftState.fuel[0],
590 aircraftState.fuel[3], aircraftState.fuel[4],
591 aircraftState.fuel[5], aircraftState.fuel[6]))
592 self.logger.message(aircraftState.timestamp,
593 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
594
595#---------------------------------------------------------------------------------------
596
597class T154(Aircraft):
598 """Tupolev Tu-154 aircraft.
599
600 The aircraft type-specific values in the aircraft state have the following
601 structure:
602 - fuel: centre, left, right, centre 2, left aux, right aux
603 - n1: left, centre, right
604 - reverser: left, right"""
605 def __init__(self, flight):
606 super(T154, self).__init__(flight)
607 self._checkers.append(checks.ThrustChecker())
608 self.dow = 53259
609 self.mtow = 98000
610 self.mlw = 78000
611 self.mzfw = 72000
612 self.gearSpeedLimit = 216
613 self.flapSpeedLimits = { 15 : 227,
614 28 : 194,
615 45 : 162 }
616
617 def logFuel(self, aircraftState):
618 """Log the amount of fuel"""
619 self.logger.message(aircraftState.timestamp,
620 "Fuel: left aux=%.0f kg - left=%.0f kg - centre=%.0f kg - centre 2=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
621 (aircraftState.fuel[4], aircraftState.fuel[1],
622 aircraftState.fuel[0], aircraftState.fuel[3],
623 aircraftState.fuel[2], aircraftState.fuel[5]))
624 self.logger.message(aircraftState.timestamp,
625 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
626
627#---------------------------------------------------------------------------------------
628
629
630class YK40(Aircraft):
631 """Yakovlev Yak-40 aircraft.
632
633 The aircraft type-specific values in the aircraft state have the following
634 structure:
635 - fuel: left, right
636 - n1: left, right
637 - reverser: left, right"""
638 def __init__(self, flight):
639 super(YK40, self).__init__(flight)
640 self._checkers.append(checks.ThrustChecker())
641 self.dow = 9400
642 self.mtow = 17200
643 self.mlw = 16800
644 self.mzfw = 12100
645 self.gearSpeedLimit = 165
646 self.flapSpeedLimits = { 20 : 165,
647 35 : 135 }
648
649 def logFuel(self, aircraftState):
650 """Log the amount of fuel"""
651 self.logger.message(aircraftState.timestamp,
652 "Fuel: left=%.0f kg - right=%.0f kg" % \
653 (aircraftState.fuel[0], aircraftState.fuel[1]))
654 self.logger.message(aircraftState.timestamp,
655 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
656
657#---------------------------------------------------------------------------------------
658
659_classes = { const.AIRCRAFT_B736 : B736,
660 const.AIRCRAFT_B737 : B737,
661 const.AIRCRAFT_B738 : B738,
662 const.AIRCRAFT_B733 : B733,
663 const.AIRCRAFT_B734 : B734,
664 const.AIRCRAFT_B735 : B735,
665 const.AIRCRAFT_DH8D : DH8D,
666 const.AIRCRAFT_B762 : B762,
667 const.AIRCRAFT_B763 : B763,
668 const.AIRCRAFT_CRJ2 : CRJ2,
669 const.AIRCRAFT_F70 : F70,
670 const.AIRCRAFT_DC3 : DC3,
671 const.AIRCRAFT_T134 : T134,
672 const.AIRCRAFT_T154 : T154,
673 const.AIRCRAFT_YK40 : YK40 }
674
675#---------------------------------------------------------------------------------------
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