Limitations Flashcards
1
Q
Max ramp weight crj200
A
53250lbs
2
Q
Max takeoff weight crj200
A
53000lbs
3
Q
Max landing weight crj200
A
47000lbs
4
Q
Max zero fuel weight crj200
A
44000lbs
5
Q
Max aft cargo crj200
A
3500lbs
6
Q
Vmo/Mmo crj200
A
335KIAS/.85M
7
Q
Vma/Mma crj200
A
280KIAS/.75M
8
Q
Vfe/Vfo
8, 20, 30, 45
Crj200
A
200/230, 200/230, 185, 170
9
Q
Vle/Vlo/Vlr
Crj200
A
250, 250, 200
10
Q
Xwind t/o and ldg limits
dry, wet, contaminated
crj200
A
27, 22, 15kts
11
Q
Cat 2/3 xwind limits
A
13kts
12
Q
Max tailwind takeoff and ldg
A
10kts
13
Q
Max headwind, cat 2/3
A
19kts
14
Q
Max fuel imbalance
A
800lbs
15
Q
Max fuel imbalance for takeoff crj900
A
300lbs
16
Q
Min go around fuel per side
Crj200
A
450lbs
17
Q
Hydraulic pressure range
A
2800-3200psi
18
Q
Hydraulic quantities crj200
A
45-85%
19
Q
Max ramp weight crj900
A
85000lbs
20
Q
Max takeoff weight crj900
A
84500lbs
21
Q
Max ldg weight crj900
A
75100lbs
22
Q
Max zero fuel weight crj900
A
70750lbs
23
Q
Max aft cargo crj900
A
2892lbs
24
Q
Max foreword cargo crj900
A
1700lbs
25
Vmo/Mmo/rvsm crj900
335KIAS/.842M/.82M
26
Vma/Mma crj900
280KIAS/.75M
27
Vfe
1,8,20,30,45
Crj900
230, 230, 220, 185, 170KIAS
28
Vle/Vlo/Vlr
Crj900
220KIAS
29
Max xwind takeoff
Dry, wet, contaminated
Crj900
35, 27, 15kts
30
Max xwind ldg
Dry, wet, contaminated
Crj900
32, 27, 15kts
31
Max tire speed crj200
182KIAS
32
Max tire speed crj900
195KAIS
33
Min go around fuel per side
Crj900
600lbs
34
Min hydraulic quantities
Crj900
34, 29, 31%
35
APU max operating altitude crj200
37000'
36
APU max starting altitude crj200
30000'
37
APU min start temp crj200
-40C
38
Max APU bleed altitude crj200
15000'
39
Max APU door speed crj200
300KIAS
40
Max single pack ops crj200
25000'
41
Min altitude for spoilers
300'agl
42
Min autopilot altitude (agl) on takeoff, visual, precision, A mode, and single engine (900)
600', 400', 80', 650', 110'
43
Max temp for takeoff crj200
50C
44
Max temp for takeoff crj900
ISA+35C
45
Min temp for takeoff
-40C
46
Max APU altitude crj900
41000'
47
Max APU start altitude crj900
37000'
48
Max APU bleed altitude crj900
25000'
49
Max APU door speed APU off, crj900
220KIAS
50
Max single pack
More than 82 occupants
Crj900
25000'
51
Max single pack ops
Less than 83 occupants
Crj900
31000'
52
Flap retraction speed on flaps 8 takeoff
Crj200
V2+12
53
Flap retraction speeds on flaps 20 takeoff
Crj200
V2+12 flaps 8
V2+20 flaps 0
54
Flap retraction speeds on flaps 8 takeoff
Crj900
V2+12 flaps 1
Vt-15 flaps 0
55
Flap retraction speeds on flaps 20 takeoff
Crj900
V2+12 flaps 8
V2+20 flaps 1
Vt-15 flaps 0
56
Max glideslope angle for autopilot
3.5
57
HGS glideslope limits
Primary and vmc
2.5-4.5
58
HGS glideslope limits A1 mode
2.5-3.5
59
HGS glideslope limits
AIII mode
2.5-3.0
60
HGS modes available for use with abnormal landing flap configurations
Primary only
61
Fuel tanks quantities pressure refueling
| Crj200
Wings-4760lbs each
Center-4998lbs
Total-14518lbs
62
Fuel tanks quantities when pressure refueling
Crj900
Wings 7492lbs
Center 4610lbs
Total 19594lbs
63
Glideslope angle limits for scda
2.9-3.5
64
Min fuel temp for takeoff
+5
65
No more than 500lbs fuel in center tank unless
Wings are each above 4400
OR
Wings are above 2000 and max zero fuel weight is reduced by the amount above 500lbs in the center tank
66
Bleeds will be set on ________ for takeoff with anti-ice on.
Crj200
APU
67
Max windshield wiper speed crj200
220KIAS
68
Max windshield wiper speed
Crj900
250KIAS
69
On the ground with an OAT of 10C or below in visible moisture
cowl anti ice must be on.
70
On ground with temps below 5C in any condition
wing anti ice must be on for taxi, except after deicing.
71
On ground with an OAT of 5 or below and visible moisture
wing and cowl anti-ice must be on.
72
Icing conditions exist in flight when
TAT is 10C or below and SAT is above -40C or the ice message appears on the EICAS.
73
Wing anti ice can be turned off in icing conditions if
IAS is above 230 and there is no ice message on EICAS.
74
On the crj200 wing anti-ice must be on
when descending with a TAT of 10C or below regardless of conditions until deployment of flaps for final approach.
75
Crank limits crj200
Attempt 1 - 60s on, 10s off
Attempt 2 - 60s on, 10s off
Attempt 3+ - 60s on, 5 minutes off
76
Crank limits crj900
Attempt 1 - 90s on 10s off
Attempt 2 - 90s on 10s off
Attempts 3-5 - 90s on 5 minutes off
77
Max ITT for engine start in air/on ground
120/90C
78
Dry motor limits for crj200
Attempt 1 - 90s on, 5 minutes off
| Attempts 2+ - 30s on 5 minutes off
79
Dry motor limits crj900
Attempt 1 - 2 minutes on 10s off
| Attempts 2-5 - 1 minute on 5 minutes off
80
Max crosswind landing from right seat
20kts
81
If cold soaked below -30C for 8 hours before starting you must
dry motor for 1 minute to verify N1 rotation.
82
After starting a cold soaked airplane (8 hours below -30C) you must
Actuate the reversers until deploy and stow times are 5 seconds (crj200) or 2 seconds (crj900).
83
Continuous ignition is required if (7)
In heavy precipitation
In the vicinity of thunderstorms
In moderate or heavy turbulence
In windshear conditions
When departing from a contaminated runway
When departing after being deiced
For takeoff in crosswinds above 15kts (crj200)
84
In the crj900 for winds between 5 and 30kts that are more than 30 degrees off the nose
rolling takeoffs or standing takeoffs are permitted.
| For standing takeoff N1 can not exceed 75% before brake release.
85
In the crj900 for winds above 30kts that are more than 30 degrees off the nose
standing takeoffs are prohibited.
86
Standing takeoffs are required when
necessary for performance or below 1200rvr.
87
The minimum RVR for the first officer to conduct a takeoff is
1200.
88
Max time with only DC power on ground
5 minutes
89
What happens at 500’ on an AIII approach
Approach warn becomes active
90
After ________ AIII mode will not arm
800’
91
```
Standard approach maneuvering speeds for flaps,
0
1(900)
8
20-45
```
200
190
180
Ref+10
92
For Lnav or Lnav/Vnav approaches in a 900ng you must select _______
Baro in the arrival data page
93
Minima for a circling approach is
1000’ and 1sm above the min vis for the approach being flown
If the plated minima is above 1000’ and 3sm then increase the required vis by 1sm
Calculated vis should not exceed 3sm
94
Stabilized approach factors are
```
Configured for landing
Ref +10, -5kias
<1000fpm (should)
<1200fpm (shall)
No turns to final below 500agl (except for sidestep)
```
95
After starting the APU you must wait _______ before bleed air extraction.
2 minutes
96
When initiating an emergency landing the captain shall notify the flight attendants by,
Calling “incharge to the interphone, incharge to the interphone”
97
The interrupted start procedure is
Affected thrust lever - shutoff
Ignition off (200)
Dry motor until crank limit or below ITT 120C
Press eng stop switch
98
In the event of a double flameout you of shall target and airspeed of
240kias to avoid core lock
Try to maintain at least 4% N1
99
In the 900ng before each flight, what must be done with the IRS?
It must undergo a rapid realignment by selecting off (no more than 5 seconds) then nav.
