source: src/mlx/acft.py@ 98:f017d907fa39

Last change on this file since 98:f017d907fa39 was 96:aa6a0b79c073, checked in by István Váradi <ivaradi@…>, 13 years ago

The contents of log lines can be modified after they are written, and we are using it for Vref
File size: 26.4 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._vrefLineIndex = None
29
30 self._checkers = []
31
32 # Loggers
33
34 self._checkers.append(checks.StageChecker())
35 self._checkers.append(checks.TakeOffLogger())
36
37 self._checkers.append(checks.AltimeterLogger())
38
39 self._checkers.append(checks.NAV1Logger())
40 self._checkers.append(checks.NAV2Logger())
41 self._checkers.append(checks.SquawkLogger())
42
43 self._checkers.append(checks.AnticollisionLightsLogger())
44 self._checkers.append(checks.LandingLightsLogger())
45 self._checkers.append(checks.StrobeLightsLogger())
46 self._checkers.append(checks.NavLightsLogger())
47
48 self._checkers.append(checks.FlapsLogger())
49
50 self._checkers.append(checks.GearsLogger())
51 self._checkers.append(checks.CruiseSpeedLogger())
52 self._checkers.append(checks.SpoilerLogger())
53
54 # Fault checkers
55
56 self._checkers.append(checks.AntiCollisionLightsChecker())
57 self._checkers.append(checks.LandingLightsChecker())
58 self._checkers.append(checks.NavLightsChecker())
59 self._checkers.append(checks.StrobeLightsChecker())
60
61 self._checkers.append(checks.BankChecker())
62
63 self._checkers.append(checks.FlapsRetractChecker())
64 self._checkers.append(checks.FlapsSpeedLimitChecker())
65
66 self._checkers.append(checks.GearsDownChecker())
67 self._checkers.append(checks.GearSpeedLimitChecker())
68
69 self._checkers.append(checks.GLoadChecker())
70
71 self._checkers.append(checks.MLWChecker())
72 self._checkers.append(checks.MTOWChecker())
73 self._checkers.append(checks.MZFWChecker())
74 self._checkers.append(checks.PayloadChecker())
75
76 self._checkers.append(checks.SpeedChecker())
77 self._checkers.append(checks.VSChecker())
78 self._checkers.append(checks.OverspeedChecker())
79 self._checkers.append(checks.StallChecker())
80
81 self._checkers.append(checks.PitotChecker())
82
83 self._checkers.append(checks.ReverserChecker())
84
85 @property
86 def type(self):
87 """Get the type of the aircraft."""
88 return self._flight.aircraftType
89
90 @property
91 def flight(self):
92 """Get the flight the aircraft belongs to."""
93 return self._flight
94
95 @property
96 def logger(self):
97 """Get the logger to use for the aircraft."""
98 return self._flight.logger
99
100 def getFlapsSpeedLimit(self, flaps):
101 """Get the speed limit for the given flaps setting."""
102 return self.flapSpeedLimits[flaps] if flaps in self.flapSpeedLimits \
103 else None
104
105 def modelChanged(self, timestamp, aircraftName, modelName):
106 """Called when the simulator's aircraft changes."""
107 self._flight.logger.message(timestamp,
108 "Aircraft: name='%s', model='%s'" % \
109 (aircraftName, modelName))
110
111 def handleState(self, aircraftState):
112 """Called when the state of the aircraft changes."""
113 for checker in self._checkers:
114 checker.check(self._flight, self, self._flight.logger,
115 self._aircraftState, aircraftState)
116
117 self._flight.handleState(self._aircraftState, aircraftState)
118
119 self._maxVS = max(self._maxVS, aircraftState.vs)
120 self._minVS = min(self._minVS, aircraftState.vs)
121
122 self._aircraftState = aircraftState
123
124 def setStage(self, aircraftState, newStage):
125 """Set the given stage as the new one and do whatever should be
126 done."""
127 if self._flight.setStage(aircraftState.timestamp, newStage):
128 if newStage==const.STAGE_PUSHANDTAXI:
129 self.logger.message(aircraftState.timestamp, "Block time start")
130 self.logFuel(aircraftState)
131 self.logger.message(aircraftState.timestamp,
132 "Zero-fuel weight: %.0f kg" % (aircraftState.zfw))
133 elif newStage==const.STAGE_TAKEOFF:
134 self.logger.message(aircraftState.timestamp, "Flight time start")
135 self.logger.message(aircraftState.timestamp,
136 "Takeoff weight: %.0f kg, MTOW: %.0f kg" % \
137 (aircraftState.grossWeight, self.mtow))
138 self.logger.message(aircraftState.timestamp,
139 "Wind %03.0f degrees at %.0f knots" % \
140 (aircraftState.windDirection,
141 aircraftState.windSpeed))
142 self.logger.message(aircraftState.timestamp,
143 "Speeds calculated by the pilot: V1: %s, VR: %s, V2: %s" % \
144 ("-" if self._flight.v1 is None
145 else str(self._flight.v1),
146 "-" if self._flight.vr is None
147 else str(self._flight.vr),
148 "-" if self._flight.v2 is None
149 else str(self._flight.v2)))
150 elif newStage==const.STAGE_TAXIAFTERLAND:
151 self.logger.message(aircraftState.timestamp, "Flight time end")
152 self.logFuel(aircraftState)
153 self.logger.message(aircraftState.timestamp,
154 "Landing weight: %.0f kg, MLW: %.0f" % \
155 (aircraftState.grossWeight, self.mlw))
156 self.logger.message(aircraftState.timestamp,
157 "Vertical speed range: %.0f..%.0f feet/min" % \
158 (self._minVS, self._maxVS))
159 elif newStage==const.STAGE_PARKING:
160 self.logger.message(aircraftState.timestamp, "Block time end")
161 elif newStage==const.STAGE_END:
162 flightLength = self._flight.flightTimeEnd - self._flight.flightTimeStart
163 self.logger.message(aircraftState.timestamp,
164 "Flight time: " +
165 util.getTimeIntervalString(flightLength))
166 self.logger.message(aircraftState.timestamp,
167 "Flown distance: %.2f NM" % \
168 (self._flight.flownDistance,))
169 blockLength = self._flight.blockTimeEnd - self._flight.blockTimeStart
170 self.logger.message(aircraftState.timestamp,
171 "Block time: " +
172 util.getTimeIntervalString(blockLength))
173
174 def prepareFlare(self):
175 """Called when it is detected that we will soon flare.
176
177 On the first call, it should start monitoring some parameters more
178 closely to determine flare time."""
179 self.flight.simulator.startFlare()
180
181 def flareStarted(self, windSpeed, windDirection, visibility,
182 flareStart, flareStartFS):
183 """Called when the flare has started."""
184 self.logger.message(self._aircraftState.timestamp, "The flare has begun")
185 self.logger.message(self._aircraftState.timestamp,
186 "Wind %03.0f degrees at %.0f knots" % \
187 (windDirection, windSpeed))
188 self.logger.message(self._aircraftState.timestamp,
189 "Visibility: %.0f metres" % (visibility,))
190 self.logger.message(self._aircraftState.timestamp,
191 "Altimeter setting: %.0f hPa" % \
192 (self._aircraftState.altimeter,))
193 self._vrefLineIndex = \
194 self.logger.message(self._aircraftState.timestamp,
195 "VRef speed calculated by the pilot: %s" % \
196 ("-" if self._flight.vref is None
197 else str(self._flight.vref)))
198 self.flight.flareStarted(flareStart, flareStartFS)
199
200 def flareFinished(self, flareEnd, flareEndFS, tdRate, tdRateCalculatedByFS,
201 ias, pitch, bank, heading):
202 """Called when the flare has finished."""
203 (flareTimeFromFS, flareTime) = self.flight.flareFinished(flareEnd,
204 flareEndFS)
205 self.logger.message(self._aircraftState.timestamp,
206 "Flare time: %.1f s (from %s)" % \
207 (flareTime,
208 "the simulator" if flareTimeFromFS else "real time",))
209 self.logger.message(self._aircraftState.timestamp,
210 "Touchdown rate: %.0f feet/min" % (tdRate,))
211 self.logger.message(self._aircraftState.timestamp,
212 "Touchdown rate was calculated by the %s" % \
213 ("simulator" if tdRateCalculatedByFS else "logger",))
214 self.logger.message(self._aircraftState.timestamp,
215 "Touchdown speed: %.0f knots" % (ias,))
216 self.logger.message(self._aircraftState.timestamp,
217 "Touchdown pitch: %.1f degrees" % (pitch,))
218 self.logger.message(self._aircraftState.timestamp,
219 "Touchdown bank: %.1f degrees" % (bank,))
220 self.logger.message(self._aircraftState.timestamp,
221 "Touchdown heading: %03.0f degrees" % (heading,))
222
223 def cancelFlare(self):
224 """Cancel flare, if it has started."""
225 self.flight.simulator.cancelFlare()
226
227 def checkFlightEnd(self, aircraftState):
228 """Check if the end of the flight has arrived.
229
230 This default implementation checks the N1 values, but for
231 piston-powered aircraft you need to check the RPMs."""
232 for n1 in aircraftState.n1:
233 if n1>=0.5: return False
234 return True
235
236 def updateVRef(self):
237 """Update the Vref value from the flight, if the Vref value has already
238 been logged."""
239 if self._vrefLineIndex is not None:
240 self._logVRef()
241
242 def _logVRef(self):
243 """Log the Vref value either newly, or by updating the corresponding
244 line."""
245 message = "VRef speed calculated by the pilot: %s" % \
246 ("-" if self._flight.vref is None else str(self._flight.vref))
247 if self._vrefLineIndex is None:
248 self._vrefLineIndex = \
249 self.logger.message(self._aircraftState.timestamp, message)
250 else:
251 self.logger.updateLine(self._vrefLineIndex, message)
252
253#---------------------------------------------------------------------------------------
254
255class Boeing737(Aircraft):
256 """Base class for the various aircraft in the Boeing 737 family.
257
258 The aircraft type-specific values in the aircraft state have the following
259 structure:
260 - fuel: centre, left, right
261 - n1: left, right
262 - reverser: left, right"""
263 def __init__(self, flight):
264 super(Boeing737, self).__init__(flight)
265 self._checkers.append(checks.ThrustChecker())
266
267 self.gearSpeedLimit = 270
268 self.flapSpeedLimits = { 1 : 260,
269 2 : 260,
270 5 : 250,
271 10 : 210,
272 15 : 200,
273 25 : 190,
274 30 : 175,
275 40 : 162 }
276
277 def logFuel(self, aircraftState):
278 """Log the amount of fuel"""
279 self.logger.message(aircraftState.timestamp,
280 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
281 (aircraftState.fuel[1], aircraftState.fuel[0],
282 aircraftState.fuel[2]))
283 self.logger.message(aircraftState.timestamp,
284 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
285
286#---------------------------------------------------------------------------------------
287
288class B736(Boeing737):
289 """Boeing 737-600 aircraft."""
290 def __init__(self, flight):
291 super(B736, self).__init__(flight)
292 self.dow = 38307
293 self.mtow = 58328
294 self.mlw = 54657
295 self.mzfw = 51482
296
297#---------------------------------------------------------------------------------------
298
299class B737(Boeing737):
300 """Boeing 737-700 aircraft."""
301 def __init__(self, flight):
302 super(B737, self).__init__(flight)
303 self.dow = 39250
304 self.mtow = 61410
305 self.mlw = 58059
306 self.mzfw = 54657
307
308#---------------------------------------------------------------------------------------
309
310class B738(Boeing737):
311 """Boeing 737-800 aircraft."""
312 def __init__(self, flight):
313 super(B738, self).__init__(flight)
314 self.dow = 42690
315 self.mtow = 71709
316 self.mlw = 65317
317 self.mzfw = 61688
318
319#---------------------------------------------------------------------------------------
320
321class B738Charter(B738):
322 """Boeing 737-800 aircraft used for charters."""
323 def __init__(self, flight):
324 super(B738Charter, self).__init__(flight)
325 self.mtow = 77791
326
327#---------------------------------------------------------------------------------------
328
329class B733(Boeing737):
330 """Boeing 737-300 aircraft."""
331 def __init__(self, flight):
332 super(B733, self).__init__(flight)
333 self.dow = 32700
334 self.mtow = 62820
335 self.mlw = 51700
336 self.mzfw = 48410
337
338#---------------------------------------------------------------------------------------
339
340class B734(Boeing737):
341 """Boeing 737-400 aircraft."""
342 def __init__(self, flight):
343 super(B734, self).__init__(flight)
344 self.dow = 33200
345 self.mtow = 68050
346 self.mlw = 56200
347 self.mzfw = 53100
348
349#---------------------------------------------------------------------------------------
350
351class B735(Boeing737):
352 """Boeing 737-500 aircraft."""
353 def __init__(self, flight):
354 super(B735, self).__init__(flight)
355 self.dow = 31300
356 self.mtow = 60550
357 self.mlw = 50000
358 self.mzfw = 46700
359
360#---------------------------------------------------------------------------------------
361
362class DH8D(Aircraft):
363 """Bombardier Dash-8 Q400 aircraft.
364
365 The aircraft type-specific values in the aircraft state have the following
366 structure:
367 - fuel: centre, left, right
368 - n1: left, right
369 - reverser: left, right."""
370 def __init__(self, flight):
371 super(DH8D, self).__init__(flight)
372 self.dow = 17185
373 self.mtow = 29257
374 self.mlw = 28009
375 self.mzfw = 25855
376 self.gearSpeedLimit = 215
377 self.flapSpeedLimits = { 5 : 200,
378 10 : 181,
379 15 : 172,
380 35 : 158 }
381
382 def logFuel(self, aircraftState):
383 """Log the amount of fuel"""
384 self.logger.message(aircraftState.timestamp,
385 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
386 (aircraftState.fuel[1], aircraftState.fuel[0],
387 aircraftState.fuel[2]))
388 self.logger.message(aircraftState.timestamp,
389 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
390
391#---------------------------------------------------------------------------------------
392
393class Boeing767(Aircraft):
394 """Base class for the various aircraft in the Boeing 767 family.
395
396 The aircraft type-specific values in the aircraft state have the following
397 structure:
398 - fuel: centre, left, right
399 - n1: left, right
400 - reverser: left, right"""
401 def __init__(self, flight):
402 super(Boeing767, self).__init__(flight)
403 self._checkers.append(checks.ThrustChecker())
404 self.gearSpeedLimit = 270
405 self.flapSpeedLimits = { 1 : 255,
406 5 : 235,
407 10 : 215,
408 20 : 215,
409 25 : 185,
410 30 : 175 }
411
412 def logFuel(self, aircraftState):
413 """Log the amount of fuel"""
414 self.logger.message(aircraftState.timestamp,
415 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
416 (aircraftState.fuel[1], aircraftState.fuel[0],
417 aircraftState.fuel[2]))
418 self.logger.message(aircraftState.timestamp,
419 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
420
421#---------------------------------------------------------------------------------------
422
423class B762(Boeing767):
424 """Boeing 767-200 aircraft."""
425 def __init__(self, flight):
426 super(B762, self).__init__(flight)
427 self.dow = 84507
428 self.mtow = 175540
429 self.mlw = 126098
430 self.mzfw = 114758
431
432#---------------------------------------------------------------------------------------
433
434class B763(Boeing767):
435 """Boeing 767-300 aircraft."""
436 def __init__(self, flight):
437 super(B763, self).__init__(cflight)
438 self.dow = 91311
439 self.mtow = 181436
440 self.mlw = 137892
441 self.mzfw = 130635
442
443#---------------------------------------------------------------------------------------
444
445class CRJ2(Aircraft):
446 """Bombardier CRJ-200 aircraft.
447
448 The aircraft type-specific values in the aircraft state have the following
449 structure:
450 - fuel: centre, left, right
451 - n1: left, right
452 - reverser: left, right."""
453 def __init__(self, flight):
454 super(CRJ2, self).__init__(flight)
455 self._checkers.append(checks.ThrustChecker())
456 self.dow = 14549
457 self.mtow = 22995
458 self.mlw = 21319
459 self.mzfw = 19958
460 self.gearSpeedLimit = 240
461 self.flapSpeedLimits = { 8 : 260,
462 20 : 220,
463 30 : 190,
464 45 : 175 }
465
466 def logFuel(self, aircraftState):
467 """Log the amount of fuel"""
468 self.logger.message(aircraftState.timestamp,
469 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
470 (aircraftState.fuel[1], aircraftState.fuel[0],
471 aircraftState.fuel[2]))
472 self.logger.message(aircraftState.timestamp,
473 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
474
475#---------------------------------------------------------------------------------------
476
477class F70(Aircraft):
478 """Fokker 70 aircraft.
479
480 The aircraft type-specific values in the aircraft state have the following
481 structure:
482 - fuel: centre, left, right
483 - n1: left, right
484 - reverser: left, right."""
485 def __init__(self, flight):
486 super(F70, self).__init__(flight)
487 self._checkers.append(checks.ThrustChecker())
488 self.dow = 24283
489 self.mtow = 38100 # FIXME: differentiate by registration number,
490 # MTOW of HA-LMF: 41955
491 self.mlw = 36740
492 self.mzfw = 32655
493 self.gearSpeedLimit = 200
494 self.flapSpeedLimits = { 8 : 250,
495 15 : 220,
496 25 : 220,
497 42 : 180 }
498
499 def logFuel(self, aircraftState):
500 """Log the amount of fuel"""
501 self.logger.message(aircraftState.timestamp,
502 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
503 (aircraftState.fuel[1], aircraftState.fuel[0],
504 aircraftState.fuel[2]))
505 self.logger.message(aircraftState.timestamp,
506 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
507
508#---------------------------------------------------------------------------------------
509
510class DC3(Aircraft):
511 """Lisunov Li-2 (DC-3) aircraft.
512
513 The aircraft type-specific values in the aircraft state have the following
514 structure:
515 - fuel: left, right, left aux, right aux
516 - rpm: left, right
517 - reverser: left, right."""
518 def __init__(self, flight):
519 super(DC3, self).__init__(flight)
520 self.dow = 8627
521 self.mtow = 11884
522 self.mlw = 11793
523 self.mzfw = 11780
524 self.gearSpeedLimit = 148
525 self.flapSpeedLimits = { 15 : 135,
526 30 : 99,
527 45 : 97 }
528
529 def _checkFlightEnd(self, aircraftState):
530 """Check if the end of the flight has arrived.
531
532 This implementation checks the RPM values to be 0."""
533 for rpm in aircraftState.rpm:
534 if rpm>0: return False
535 return True
536
537 def logFuel(self, aircraftState):
538 """Log the amount of fuel"""
539 self.logger.message(aircraftState.timestamp,
540 "Fuel: left aux=%.0f kg - left=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
541 (aircraftState.fuel[2], aircraftState.fuel[0],
542 aircraftState.fuel[1], aircraftState.fuel[3]))
543 self.logger.message(aircraftState.timestamp,
544 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
545
546#---------------------------------------------------------------------------------------
547
548class T134(Aircraft):
549 """Tupolev Tu-134 aircraft.
550
551 The aircraft type-specific values in the aircraft state have the following
552 structure:
553 - fuel: centre, left tip, left aux, right tip, right aux, external 1,
554 external 2
555 - n1: left, right
556 - reverser: left, right."""
557 def __init__(self, flight):
558 super(T134, self).__init__(flight)
559 self._checkers.append(checks.ThrustChecker())
560 self.dow = 29927
561 self.mtow = 47600
562 self.mlw = 43000
563 self.mzfw = 38500
564 self.gearSpeedLimit = 216
565 self.flapSpeedLimits = { 10 : 240,
566 20 : 216,
567 30 : 161 }
568
569 def logFuel(self, aircraftState):
570 """Log the amount of fuel"""
571 self.logger.message(aircraftState.timestamp,
572 "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" % \
573 (aircraftState.fuel[2], aircraftState.fuel[1],
574 aircraftState.fuel[0],
575 aircraftState.fuel[3], aircraftState.fuel[4],
576 aircraftState.fuel[5], aircraftState.fuel[6]))
577 self.logger.message(aircraftState.timestamp,
578 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
579
580#---------------------------------------------------------------------------------------
581
582class T154(Aircraft):
583 """Tupolev Tu-154 aircraft.
584
585 The aircraft type-specific values in the aircraft state have the following
586 structure:
587 - fuel: centre, left, right, centre 2, left aux, right aux
588 - n1: left, centre, right
589 - reverser: left, right"""
590 def __init__(self, flight):
591 super(T154, self).__init__(flight)
592 self._checkers.append(checks.ThrustChecker())
593 self.dow = 53259
594 self.mtow = 98000
595 self.mlw = 78000
596 self.mzfw = 72000
597 self.gearSpeedLimit = 216
598 self.flapSpeedLimits = { 15 : 227,
599 28 : 194,
600 45 : 162 }
601
602 def logFuel(self, aircraftState):
603 """Log the amount of fuel"""
604 self.logger.message(aircraftState.timestamp,
605 "Fuel: left aux=%.0f kg - left=%.0f kg - centre=%.0f kg - centre 2=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
606 (aircraftState.fuel[4], aircraftState.fuel[1],
607 aircraftState.fuel[0], aircraftState.fuel[3],
608 aircraftState.fuel[2], aircraftState.fuel[5]))
609 self.logger.message(aircraftState.timestamp,
610 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
611
612#---------------------------------------------------------------------------------------
613
614
615class YK40(Aircraft):
616 """Yakovlev Yak-40 aircraft.
617
618 The aircraft type-specific values in the aircraft state have the following
619 structure:
620 - fuel: left, right
621 - n1: left, right
622 - reverser: left, right"""
623 def __init__(self, flight):
624 super(YK40, self).__init__(flight)
625 self._checkers.append(checks.ThrustChecker())
626 self.dow = 9400
627 self.mtow = 17200
628 self.mlw = 16800
629 self.mzfw = 12100
630 self.gearSpeedLimit = 165
631 self.flapSpeedLimits = { 20 : 165,
632 35 : 135 }
633
634 def logFuel(self, aircraftState):
635 """Log the amount of fuel"""
636 self.logger.message(aircraftState.timestamp,
637 "Fuel: left=%.0f kg - right=%.0f kg" % \
638 (aircraftState.fuel[0], aircraftState.fuel[1]))
639 self.logger.message(aircraftState.timestamp,
640 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
641
642#---------------------------------------------------------------------------------------
643
644_classes = { const.AIRCRAFT_B736 : B736,
645 const.AIRCRAFT_B737 : B737,
646 const.AIRCRAFT_B738 : B738,
647 const.AIRCRAFT_B733 : B733,
648 const.AIRCRAFT_B734 : B734,
649 const.AIRCRAFT_B735 : B735,
650 const.AIRCRAFT_DH8D : DH8D,
651 const.AIRCRAFT_B762 : B762,
652 const.AIRCRAFT_B763 : B763,
653 const.AIRCRAFT_CRJ2 : CRJ2,
654 const.AIRCRAFT_F70 : F70,
655 const.AIRCRAFT_DC3 : DC3,
656 const.AIRCRAFT_T134 : T134,
657 const.AIRCRAFT_T154 : T154,
658 const.AIRCRAFT_YK40 : YK40 }
659
660#---------------------------------------------------------------------------------------
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