######################################
#FJCC UNIVERSAL FMC CONFIGURATION    #
#Bombardier Challenger 300           #
#Configuration file by Javier Cortes #
#  UFMC Version: 2.4                 #
#  Config file Version V2.4          #  
# INSERT HERE ANY OTHER COMMENT 1    #
# INSERT HERE ANY OTHER COMMENT 2    #
#             ....                   #
#             ....                   #
# INSERT HERE ANY OTHER COMMENT n    #
######################################
#PLANE NAME
Bombardier CL-300
#ENGINES MODEL
HTF7000
#FMC COLOUR (00=BROWN-GREEN, 01=BROWN-GRAY 02=BROWN-WHITE 10=GRAY-GREEN 11=GRAY-GRAY 12=GRAY-WHITE 14=AIRBUS 26=Q400)
26
#TYPICAL CLIMB SPEED (KIAS, IN A NORMAL CONFIGURATION. IF MACH IS NEEDED, IT IS CALCULATED BY THE FMC OR YOU CAN ENTER MANUALLY IN THE VNAV CLB PAGE)
280
#TYPICAL DESCENT SPEED (KIAS, IN A NORMAL CONFIGURATION)
280
#OPTIMAL CRUISE SPEED (NORMALLY MACH. IF THE CRUISE LEVEL IS LOW THEN KIAS)
0.78
#TYPICAL CLIMB RATE (FPM)
2500
#TYPICAL DESCENT RATE (FPM)
2700
#TYPICAL CRUISE ALTITUDE (FEETS. THE OPTIMAL AND MAX ALTITUDE IS GROSS WEIGHT DEPENDING. WILL ENTER IN A TABLE BELOW)
41000
#THROTTLE CONTROL (1 = UFMC TAKES CONTROL OVER THE THROTTLE AS EVERY JET AIRLINER. 0 = UFMC DOESN'T TAKE CONTROL OVER THE THROTTLE AS SOME TURBOPROPELLERS)
0
#FUEL CONSUMPTION AS PLANEMAKER SPACE SEPARATOR: MAX TRUST, LOW ALT HALF POWER SPEC, LOW ALT MAX POWER SPEC, ALTITUDE, HI ALT HALF POWER SPEC, HI ALT MAX POWER SPEC
7726 0.450 0.500 45000 0.780 0.930
######################################
TAKEOFF FLAPS POSITIONS FROM FIRST POSITION TO THE LAST POSIBLE. FOR EXAMPLE 3 AND 4, OR 3 AND 3 IF JUST ONE POSITION
#####################################
#TAKE_OFF FLAPS POSITION 1 (FIRST POSIBLE FLAP POSITION FOR TAKEOFF 1,2,3,4,5,6)
1
#TAKE_OFF FLAPS POSITION 2 (LAST POSIBLE FLAP POSITION FOR TAKEOFF 1,2,3,4,....)
2
#LANDING FLAPS POSITION 1 (FIRST POSIBLE FLAP POSITION FOR LANDING 1,2,3,4,....)
3
#LANDING FLAPS POSITION 2 (LAST POSIBLE FLAP POSITION FOR LANDING 1,2,3,4,....)
3
######################################
V1, VR AND V2. KIAS FROM THE FIRST FLAPS TAKEOFF POSITIONS TO THE LAST ONE. MINIMAL FOR LIGHT CONFIGURATION AND MAX FOR HEAVY CONFIGURATION
#####################################
#V1MIN_1
108
#V1MAX_1
134
#VRMIN_1
111
#VRMAX_1
135
#V2MIN_1
126
#V2MAX_1
140
#V1MIN_2
104
#V1MAX_2
126
#VRMIN_2
107
#VRMAX_2
126
#V2MIN_2
125
#V2MAX_2
130
#V1MIN_3

#V1MAX_3

#VRMIN_3

#VRMAX_3

#V2MIN_3

#V2MAX_3

#######################################
MAXIMUM AND MINIMUM FLAPS SPEEDS. KIAS. FOR EVERY FLAP POSITION: 
MINIMUM (LIGHTEST CONFIGURATION) AND MAXIMUM (HEAVIEST CONFIGURATION) FOR LANDING AND MAXIMUM FLAP SPEED FOR TAKEOFF 
#######################################
#VF1MIN_LANDING
133
#VF1MAX_LANDING
144
#VF1MAX_TAKE_OFF
140
#VF2MIN_LANDING
123
#VF2MAX_LANDING
134
#VF2MAX_TAKE_OFF
130
#VF3MIN_LANDING
113
#VF3MAX_LANDING
124
#VF3MAX_TAKE_OFF

#VF4MIN_LANDING

#VF4MAX_LANDING

#VF4MAX_TAKE_OFF

#VF5MIN_LANDING

#VF5MAX_LANDING

#VF5MAX_TAKE_OFF

#VF6MIN_LANDING

#VF6MAX_LANDING

#VF6MAX_TAKE_OFF

########################################
LEAVE BLANK THE MAXIMUM IF UNKNOWN
OPTIMAL AND MAXIMUM LEVEL CRUISE. THREE VALUES: WEIGHT-OPTIMAL LEVEL- MAXIMUM LEVEL.
1 IS MIN WEIGHT, 6 IS MAX WEIGHT. LEAVE BLANK THE MAXIMUM IF UNKNOWN.WEIGHT POUNDS. LEVEL FEET
AT LEAST TWO POINTS
########################################
#WEIGHT_1

#OPTIMAL_LEVEL_1

#MAXIMUM_LEVEL_1

#WEIGHT_2

#OPTIMAL_LEVEL_2

#MAXIMUM_LEVEL_2

#WEIGHT_3

#OPTIMAL_LEVEL_3

#MAXIMUM_LEVEL_3

#WEIGHT_4

#OPTIMAL_LEVEL_4

#MAXIMUM_LEVEL_4

#WEIGHT_5

#OPTIMAL_LEVEL_5

#MAXIMUM_LEVEL_5

#WEIGHT_6

#OPTIMAL_LEVEL_6

#MAXIMUM_LEVEL_6

#WEIGHT_7

#OPTIMAL_LEVEL_7

#MAXIMUM_LEVEL_7

#WEIGHT_8

#OPTIMAL_LEVEL_8

#MAXIMUM_LEVEL_8

#WEIGHT_9

#OPTIMAL_LEVEL_9

#MAXIMUM_LEVEL_9

#WEIGHT_10

#OPTIMAL_LEVEL_10

#MAXIMUM_LEVEL_10

########################################
N1 TAKEOFF THRUST LIMITS. IF YOU LEAVE IT BLANK, UFMC WILL USE A STANDAR LIMITS
ENTER DATA PAIR OF AIRPORT TEMPERATURE (CELCIUS) AND N1 AT SEA LEVEL. AT THE OTHER PRESS ALTITUDES, N1 WILL BE COMPUTED BY THE UFMC
AT LEAST TWO DATA PAIR FROM LESS TEMPERATURE TO GREATER TEMPERATURE
########################################
#TEMP_N1_1_SL
-40 77.3
#TEMP_N1_2_SL
00 83.9
#TEMP_N1_3_SL
20 87.0
#TEMP_N1_4_SL
40 86.5
#TEMP_N1_5_SL
50 83.7
#TEMP_N1_6_SL
00 00
########################################
N1 MAXIMUM CLIMB THRUST LIMITS. IF YOU LEAVE IT BLANK, UFMC WILL USE A STANDAR LIMITS
ENTER DATA PAIR OF PRESSURE ALTITUDE (FEET) AND N1 AT ZERO CELCIUS DEGREES. AT THE OTHER TEMPERATURES, N1 WILL BE COMPUTED BY THE UFMC
AT LEAST TWO DATA PAIR FROM LESS ALTITUDE TO GREATER ALTITUDE
########################################
#ALT_N1_1_0C
0 85.9
#ALT_N1_2_0C
4000 89.2
#ALT_N1_3_0C
10000 91.5
#ALT_N1_4_0C
20000 91.5
#ALT_N1_5_0C
29000 92.1
#ALT_N1_6_0C
45000 90.1
########################################
N1 MAXIMUM OPTIMUM CRUISE THRUST LIMITS. IF YOU LEAVE IT BLANK, UFMC WILL USE A STANDAR LIMITS
ENTER FOUR DATA PAIR OF PRESSURE ALTITUDE (FEET) AND N1 AT MIN AND MAX AIRCRAFT WEIGHT. AT THE OTHER PRESSURE ALTITUDE AND WEIGHTS, N1 WILL BE COMPUTED BY THE UFMC
FOUR POINTS MANDATORY
########################################
#MIN_ALT_N1 AT MIN_WEIGHT

#MAX_ALT_N1 AT MIN_WEIGHT

#MIN_ALT_N1 AT MAX_WEIGHT

#MAX_ALT_N1 AT MAX_WEIGHT

########################################
NOMINAL CLIMB RATE FOR SEVERAL PRESSURE ALTITUDES. IF YOU LEAVE IT ALL BLANK (ENTER 00), UFMC WILL USE THE TYPICAL CLIMB RATE (FPM) ENTERED BEFORE
ENTER UP TO 10 DATA PAIR OF PRESSURE ALTITUDE (FEET) AND CLIMB RATE (FPM)FOR NOMINAL WEIGHT CONFIGURATION (NOT HEAVIEST CONFIGURATION)
AT LEAST TWO POINTS. FROM LOW ALTITUDE TO HIGH ALTITUDE
########################################
#PRESSURE_ALTITUDE_1 CLIMB_RATE_1
0 100
#PRESSURE_ALTITUDE_2 CLIMB_RATE_2
5000 6000
#PRESSURE_ALTITUDE_4 CLIMB_RATE_3
10000 5500
#PRESSURE_ALTITUDE_5 CLIMB_RATE_4
15000 5000
#PRESSURE_ALTITUDE_6 CLIMB_RATE_5
20000 4200
#PRESSURE_ALTITUDE_7 CLIMB_RATE_6
25000 3200
#PRESSURE_ALTITUDE_8 CLIMB_RATE_7
30000 2300
#PRESSURE_ALTITUDE_9 CLIMB_RATE_8
35000 1900
#PRESSURE_ALTITUDE_10 CLIMB_RATE_9
40000 1200
#PRESSURE_ALTITUDE_11 CLIMB_RATE_10
44000 600
########################################
NOMINAL DESCENT RATE FOR SEVERAL PRESSURE ALTITUDES. IF YOU LEAVE IT ALL BLANK (ENTER 00), UFMC WILL USE THE TYPICAL DESCENT RATE (FPM) ENTERED BEFORE
ENTER UP TO 10 DATA PAIR OF PRESSURE ALTITUDE (FEET) AND DESCENT RATE (FPM) FOR NOMINAL WEIGHT CONFIGURATION (NOT HEAVIEST CONFIGURATION)
AT LEAST TWO POINTS. FROM LOW ALTITUDE TO LOW ALTITUDE
########################################
#PRESSURE_ALTITUDE_1 DESCENT_RATE_1
0 700
#PRESSURE_ALTITUDE_2 DESCENT_RATE_2
5000 1200
#PRESSURE_ALTITUDE_3 DESCENT_RATE_3
10000 2500
#PRESSURE_ALTITUDE_4 DESCENT_RATE_4
15000 2650
#PRESSURE_ALTITUDE_5 DESCENT_RATE_5
20000 2700
#PRESSURE_ALTITUDE_6 DESCENT_RATE_6
25000 2700
#PRESSURE_ALTITUDE_7 DESCENT_RATE_7
30000 2700
#PRESSURE_ALTITUDE_8 DESCENT_RATE_8
35000 2700
#PRESSURE_ALTITUDE_9 DESCENT_RATE_9
40000 2900
#PRESSURE_ALTITUDE_10 DESCENT_RATE_10
44000 3000
########################################
NOMINAL FUEL CONSUMPTION IN CLIMB RATE FOR SEVERAL PRESSURE ALTITUDES. IF YOU LEAVE IT ALL BLANK (ENTER 00), UFMC WILL USE THE FUEL CONSUMPTION AS PLANEMAKER ENTERED BEFORERATE (FPM) ENTERED
ENTER UP TO 10 DATA PAIR OF PRESSURE ALTITUDE (FEET) AND FUEL CONSUPTION (POUNDS/MIN) FOR NOMINAL WEIGHT CONFIGURATION (NOT HEAVIEST CONFIGURATION)
AT LEAST TWO POINTS. FROM LOW ALTITUDE TO LOW ALTITUDE
########################################
#PRESSURE_ALTITUDE_1 FUEL_CLIMB_1
0 00
#PRESSURE_ALTITUDE_2 FUEL_CLIMB_2
5000 93.00
#PRESSURE_ALTITUDE_3 FUEL_CLIMB_3
10000 77.00
#PRESSURE_ALTITUDE_4 FUEL_CLIMB_4
15000 65.00
#PRESSURE_ALTITUDE_5 FUEL_CLIMB_5
20000 60.00
#PRESSURE_ALTITUDE_6 FUEL_CLIMB_6
25000 55.00
#PRESSURE_ALTITUDE_7 FUEL_CLIMB_7
30000 48.00
#PRESSURE_ALTITUDE_8 FUEL_CLIMB_8
35000 41.00
#PRESSURE_ALTITUDE_9 FUEL_CLIMB_9
40000 35.00
#PRESSURE_ALTITUDE_10 FUEL_CLIMB_10
44000 32.00
########################################
NOMINAL FUEL CONSUMPTION IN CRUISE FASE FOR SEVERAL PRESSURE ALTITUDES. IF YOU LEAVE IT ALL BLANK (ENTER 00), UFMC WILL USE THE FUEL CONSUMPTION AS PLANEMAKER ENTERED BEFORERATE (FPM) ENTERED
ENTER UP TO 10 DATA PAIR OF PRESSURE ALTITUDE (FEET) AND FUEL CONSUPTION (POUNDS/MIN) FOR NOMINAL WEIGHT CONFIGURATION (NOT HEAVIEST CONFIGURATION)
AT LEAST TWO POINTS. FROM LOW ALTITUDE TO LOW ALTITUDE
########################################
#PRESSURE_ALTITUDE_1 FUEL_CRUISE_1
00 00
#PRESSURE_ALTITUDE_2 FUEL_CRUISE_2
5000 20.00
#PRESSURE_ALTITUDE_3 FUEL_CRUISE_3
10000 24.00
#PRESSURE_ALTITUDE_4 FUEL_CRUISE_4
15000 24.00
#PRESSURE_ALTITUDE_5 FUEL_CRUISE_5
20000 27.00
#PRESSURE_ALTITUDE_6 FUEL_CRUISE_6
25000 27.00
#PRESSURE_ALTITUDE_7 FUEL_CRUISE_7
30000 33.00
#PRESSURE_ALTITUDE_8 FUEL_CRUISE_8
35000 31.00
#PRESSURE_ALTITUDE_9 FUEL_CRUISE_9
40000 29.33
#PRESSURE_ALTITUDE_10 FUEL_CRUISE_10
44000 28.00
########################################
NOMINAL FUEL CONSUMPTION IN DESCENT FASE FOR SEVERAL PRESSURE ALTITUDES. IF YOU LEAVE IT ALL BLANK (ENTER 00), UFMC WILL USE THE FUEL CONSUMPTION AS PLANEMAKER ENTERED BEFORERATE (FPM) ENTERED
ENTER UP TO 10 DATA PAIR OF PRESSURE ALTITUDE (FEET) AND FUEL CONSUPTION (POUNDS/MIN) FOR NOMINAL WEIGHT CONFIGURATION (NOT HEAVIEST CONFIGURATION)
AT LEAST TWO POINTS. FROM LOW ALTITUDE TO LOW ALTITUDE
########################################
#PRESSURE_ALTITUDE_1 FUEL_DESCENT_1
00 00
#PRESSURE_ALTITUDE_2 FUEL_DESCENT_2
5000 15.0
#PRESSURE_ALTITUDE_3 FUEL_DESCENT_3
10000 10.0
#PRESSURE_ALTITUDE_4 FUEL_DESCENT_4
15000 9.0
#PRESSURE_ALTITUDE_5 FUEL_DESCENT_5
20000 9.0
#PRESSURE_ALTITUDE_6 FUEL_DESCENT_6
25000 9.0
#PRESSURE_ALTITUDE_7 FUEL_DESCENT_7
30000 9.0
#PRESSURE_ALTITUDE_8 FUEL_DESCENT_8
35000 9.0
#PRESSURE_ALTITUDE_9 FUEL_DESCENT_9
40000 9.0
#PRESSURE_ALTITUDE_10 FUEL_DESCENT_10
44000 9.0