All Flashcards
Max ramp weight
53,250 lbs
Max TO weigh
53,000 lbs
Max landing weight
Max fuel weight
47,000 lbs
44,000 lbs
Min flight weight
Max cargo weight
30,000lbs
3500 lbs
Max operating Alt
41,000ft
Max Turbulent speed
Max Operating speed
280 kias .75 M
335 kias. 85 M
Flap Speed 8 20 30 45
VFO VFE
8 200 230
20 200 230
30 185 185
45 170 170
vLE max gear extension speed
Max gear retraction speed
Max windshield wipers speed
250
200
220
Max dif pressure
Max negative pressure
Max dif for taxi TO and landings
Min cabin ALT in manual mode
8.7
-.5
.1
-1500ft
Max ATL for single pack
AP for Visual and NPA (disconnect before__agl)
AP for precision approach
25,000ft
400ft
80ft
Fuel quant
Left main
Right main
Center tank
Total
Pressure Gravity
Left main 4760 4488
Right main 4760 4488
Center tank 4998 4930
Total. 14,518 13906
Min Eng fuel temp for TO
Max fuel imbalance
Min wing tank fuel for G/A
Break cooling time
Started cranking time
Min Eng fuel temp for TO 5degrees🌡
Max fuel imbalance
800lbs
Min wing tank fuel for G/A
450lbs
Break cooling time
15 mins
Started cranking time
1min on, 10 sec off (x2)
1min on, 5 mins off
APU
max operating ALT
max starting ALT
max bleed ALT
Max engine start ALT
APU
max operating ALT 37,000
max starting ALT. 30,000
max bleed ALT. 15,000
Max engine start ALT. 13,000
Continuous ignition must be used during…
TO and landing on contamined runways
With high cross wind components (15kts 90 degrees
Through moderate and severe icing
Vicinity of TS
Through moderate or heavy Turb
TO after deice/antiICE
Flex power CRJ 200
If reduced thrust used, must not be lower the 85.0%
Reduce thrust must not be used if…..
If N1 fan is less then 85.0%
When anti ice system is INOP
When WING AND COWL ANTI ICE system is on for TO
When the RW is contaminated with standing water, slush, snow or ice
Areas of windsher and downdrafts
On wet RWs, Unless “wet performance data” is used
When AeroDate requires you to use max thrust
- wet RW flex data is only availability when it’s warmer then +10 degrees outside
- FMS “flex N1” must be greater or equal to AeroDate calculated flex N1 data