CRJ 200 Limitations Flashcards
(146 cards)
0
Q
Max T/O weight
A
53,000 lbs
1
Q
Max ramp weight
A
53,250 lbs
2
Q
Max landing weight
A
47,000 lbs
3
Q
Max zero fuel weight
A
44,000 lbs
4
Q
Max aft cargo
A
3,500 lbs
5
Q
Max operating alt (SkyWest)
A
37,000’
6
Q
Max T/O and landing alt
A
10,000’
7
Q
Max temp T/O and land
A
ISA + 35C
8
Q
Minimum temp T/O
A
-40C
9
Q
Max runway slope
A
+/-2%
10
Q
Max tailwind
A
10 kts
11
Q
Vmo
A
335 KIAS
12
Q
Mmo
A
0.85 M
13
Q
Vfo8
A
200 KIAS
14
Q
Vfo20
A
200 KIAS
15
Q
Vfe8
A
215 KIAS
16
Q
Vfe20
A
215 KIAS
17
Q
Vfe30
A
185 KIAS
18
Q
Vfe45
A
170 KIAS
19
Q
Vlo ext
A
220 KIAS
20
Q
Vlo RET
A
200 KIAS
21
Q
Vle
A
220 KIAS
22
Q
Vtire
A
182 kts GS
23
Q
Vadg deploy max
A
250 KIAS
24
Vb
280 KIAS
25
Mb
.75 M
26
Vwiper ops max
220 KIAS
27
Anti-skid
>35 kts or WOW +5 sec
28
Anti-skid inop below
10 kts
29
Max alt slats/flaps
15,000'
30
Minimum spoiler speed
Approach speed +17
31
Minimum alt spoilers
300' AGL
32
Min reduced thrust
3B1: 83.5%
3A1: 85%
33
N2 Start
20% (green)
34
N2 idle
56.5-68% (green)
35
Engine start (ground)
60 sec on/10 sec off
60 sec on/10 sec off
60 sec on/5 min off
60 sec on/5 min off
36
At initiation of thrust lever movement from...
...shut off to idle, ITT must be 120C or less for all ground starts.
37
Dry motoring
90 sec on - 5 min off
| 30 sec on - 5 min off
38
```
Usable fuel
L Main (pressure refueling)
```
4,760 lbs
39
```
Usable fuel
R Main (pressure refueling)
```
4,760 lbs
40
Usable fuel
| Center (pressure refueling)
4,998 lbs
41
Usable fuel
| Total
14,518 lbs
42
Usable fuel
| Max imbalance
800 lbs
43
Max fuel imbalance for T/O
800 lbs
44
Minimum fuel for GA per wing
450 pounds (amber)
45
Minimum fuel temp for T/O
+5C
46
Main Gen
To 35,000': 30 KVA
| > 35,000': 25 KVA
47
APU Gen
To 37,000': 30 KVA
48
Electric
| Ground ops DC only
5 minutes
49
AFCS mode prohibited during approach
IAS mode
50
AFCS mode prohibited for VOR approaches
APPR mode
51
AFCS T/O minimum alt
600' AGL
52
AFCS non-precision/visual approach minimum alt
400' AGL
53
AFCS precision approach glide path angle/minimum alt
54
Max press diff
8.7 psi
55
Max negative pressure diff
-0.5
56
Single pack ops to
FL250
57
Pack overheat
88C
58
Pack over pressure
>53 psi
59
APU max op alt
37,000'
60
APU max start alt
30,000'
61
APU max alt bleed use
15,000'
62
APU max alt eng start
13,000'
63
APU Start Aircraft Battery
2x30 seconds on - 20 minutes off
| 2x30 seconds on - 40 minutes off
64
APU Start DC External
2x15 seconds on - 20 minutes off
| 2x15 seconds on - 40 minutes off
65
Engine (blank) at ground idle power should not be greater than (blank) split
N2, 2%
66
If (blank) is (blank) or less with an OAT of (blank), do not accelerate above (blank). This indicates a mechanical problem with the engine.
N2, 57%, -20C or warmer, idle
67
After all (blank), do not exceed (blank) for (blank) after start, or until all operating indications are in normal range, whichever is longer.
Starts, 75% N1, two minutes
68
Before the first flight of the day, when the airplane is (blank) at a temperature of (blank) for more than (blank) hours, the engines must be motored for (blank) seconds and fan rotation verified before engine start is initiated.
Cold soaked, -30C or below, 8 hours, 60 seconds
69
During preflight checks of the thrust reversers after being cold soaked for more than (blank) hours, the (blank) must be actuated until the deploy and stow cycles are less than (blank) seconds.
8 hours, thrust reversers, 5 seconds
70
Continuous ignition must be used... (5 conditions)
```
Contaminated runways
Crosswind >10 kts (200 only)
Moderate or heavier rain
Moderate or heavier turbulence
Vicinity of thunderstorms
```
71
During landing, allocation of (blank) is (blank) at airspeeds (blank) KIAS. Below (blank) KIAS, reverse thrust must be reduced to (blank). Not above (blank)
Reverse thrust, not permitted, below 75 KIAS, 60 KIAS, idle, 30% N1
72
The engine oil level must be checked within (blank) to (blank) of every engine shutdown.
3 minutes to 2 hours
73
If use of the oil replenishment system is required, then the engine(s) should be replenished within (blank) to (blank) after engine shutdown.
15 minutes to 2 hours
74
Maximum refill allowable is (blank) quarts without dry motoring the engine
Two
75
If both engines are to be started using the (blank), then the operating engine's thrust must not exceed (blank)
APU bleed air, 70% N2
76
(Blank) must be switched off any time the aircraft is stationary for more than (blank) minutes (SkyWest procedure)
All landing and taxi lights, 10 minutes
77
(Blank) with a fuel load in excess of (blank) in the (blank) tank is not permitted unless each (blank) tank is above (blank)
Takeoff, 500 lbs, center, main, 4,400 lbs
78
Takeoff with engine fuel temperature indications (blank) is (blank)
Below +5C, prohibited
79
Bulk fuel takeoff limit
-30C
80
Bulk fuel freezing point
-40C
81
Tuning (blank) and (blank) from the FMS is (blank)
Transponder 1, transponder 2, prohibited
82
Minimum climb speed: reference long range cruise/minimum speed/holding speed chart in the (blank)
Performance cards
83
Maximum climb speed profile above (blank) - (blank)
10,000', 290 KIAS to .70 M
84
(Blank) will be the minimum (blank) speed once transition is made from IAS to MACH speed
.70 Mach, climb
85
Maximum authorized altitude
FL370
86
Reduced thrust takeoffs are prohibited when... (6 items)
```
Cowl and/or wing anti-ice ON
Runway is contaminated
Tailwind in excess of 5 kts
Warnings of windshear/downdrafts
Anti-skid is inoperative
T/O behind heavy aircraft
```
87
Reduced thrust takeoff on (blank) are (blank)
Wet runways, permitted
88
The appropriate additions to (blank) using the laminated flight deck (blank) must be made if (blank) performance is not available.
V1 and Vr, flip cards, ACARS
89
Conditions conducive to icing exist on the (blank) when the (blank) is (blank), when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.
Ground and for takeoff, OAT, 10C or below
90
Icing conditions exist in (blank) when the (blank) is (blank) and (blank) in any form is encountered (such as clouds, rain, snow, sleet, or ice crystals), except when the (blank) is (blank) or below.
Flight, TAT, 10C or below, visible moisture, SAT, -40C(-40F)
91
The cowl anti-ice system must be on when the (blank) is (blank) and (blank) in any form (blank) (such as fog with visibility of one mile or less, rain, snow, sleet and ice crystals)
OAT, 10C or below, visible moisture, is present
92
The cowl anti-ice system must also be on when the (blank) is (blank) when operating on ramps, taxiways, or runways where surface snow, ice, standing water or slush is present.
OAT, 10C or below
93
Turn (blank) anti-ice on for final taxi unless (blank) or (blank) anti-ice fluids have been applied.
Wing, Type II, Type IV
94
The L or R WING A/ICE caution messages may be displayed during taxi but the WING/COWL A/I ON advisory message must be displayed (blank)
Prior to takeoff
95
If APU is not operating, a (blank) caution message will be displayed. This is a normal indication for this configuration; however, the message must be extinguished prior to takeoff. During this condition, takeoff N1 values will not be displayed on EICAS.
Bleed misconfig
96
The term "final taxi" has caused some confusion. Bombardier defines final taxi as that period following (blank) or about (blank) prior to takeoff.
2nd engine start, 2 minutes
97
```
T/O OAT 5C or colder
Turn the (blank) anti-ice (blank) just prior to (blank)
```
Wing, off
98
The wing anti-ice system must be on for T/O when
Visible moisture below 400' AGL is reported
99
Operate the anti-ice system during takeoff and take the associated weight penalty, only if the above actually exist (blank)
At the time of takeoff
100
(Blank) - the (blank) anti-ice system must be ON:
A) when in (blank), or
B) when (blank) by the ice detection system
Cowl, engine cowl, icing conditions, ICE is annunciated
101
(Blank) - the (blank) anti-ice system must be ON:
A) when (blank) by the ice detection system, or
B) when in (blank) and the airspeed is less than (blank)
Wing, wing, ICE is annunciated, icing conditions, 230 KIAS
102
(Blank) takeoff on a contaminated runway is (blank) for the CRJ200/700/900
Flaps 8, authorized
103
Usable Fuel L Main (Gravity Refueling)
4488 lbs
104
Usable Fuel R Main (Gravity Refueling)
4488 lbs
105
Usable Fuel Center (Gravity Refueling)
4930 lbs
106
Usable Fuel Total (Gravity Refueling)
13,906 lbs
107
APU Max RPM
107%
108
APU Max Continuous EGT
743 C
109
APU Max EGT Start
974 C
110
APU Min Temp Start
-40 C
111
APU Max Gen Load
30 KVA
112
Max Speed Door Open with APU not operating
300 KIAS
113
Engine ITT
| Max APR not operating operating/normal T/O
First 2 min: 900 C
| Next 3 min: 884 C
114
Engine ITT
| Max APR Operating
First 2 min: 928 C
| Next 3 min: 900 C
115
Engine ITT
| Max Cont Thrust
3B1: 874 C (860 C 3A1)
116
Engine ITT
| Max Start
900 C
117
Oil Temp
| Min Start
-40 C
118
Oil Temp
| Max Cont
155 C
119
Oil Temp
| Max (15 Min)
163 C
120
Oil Pressure
| Min Start/Idle
25 psi
121
Oil Pressure
| Max T/O Thrust
45 psi
122
Oil Pressure
| Max Cont
115 psi
123
Oil Pressure
| Max after cold start
130 psi at idle for max of 10 min
Engine must remain at idle until oil psi returns to normal range
124
Max oil consumption
.05 GPH (1 qt/5 hours)
125
Engine thrust normal T/O
8729 lbs
126
Engine thrust APR
9220 lbs
127
Min Flight Weight
30,000 lbs
128
CRJ 200: flight time to suitable airport
45 minutes
129
Max Cont DC TRU
100 amps
130
Max press diff taxi, T/O, landing
.1 psi
131
No man ops (pressurization)
To -1500 ft
132
Cabin alt caution
8,500' to 10,000'
133
Cabin alt warning
>10,000'
134
CPAM drops O2 masks
14,000 +/- 500'
135
CPAM
| No smoking/seatbelt signs on
10,000'
136
Emergency depress maintains
14,250 +/- 750'
137
Normal brake pressure
1000-3200 psi
138
Nose steering
Rudder: 5 degrees L/R
Tiller: 70 degrees L/R
139
Minimum runway width
100'
140
Hydraulics
| Norm psi
2950-3050 psi
141
Hydraulics
| Low psi
<1800 psi
142
Hydraulics
| Pressure relief
>3750 psi
143
Hydraulics
| Accumulator pressure
1500 psi
144
Hydraulics
| Norm level
45-85%
145
Hydraulics
| High temp caution
93-96 degrees C
