CRJ 200 Limitations Flashcards
1
Q
Max Ramp Wt ________lbs.
A
53,250
2
Q
Max T/O Wt ________lbs.
A
53,000
3
Q
Max Lnd Wt______lbs.
A
47,000
4
Q
Max Zero Fuel Wt _______lbs.
A
44,000
5
Q
Min Flight Wt _______lbs.
A
30,000
6
Q
Wing Span
A
69ft 8in
7
Q
Aircraft Length
A
87ft 10in
8
Q
Tail Height
A
20ft 8in
9
Q
Max Ops Alt_______ft.
A
37,000(SW)
10
Q
Max T/O & Lnd Altitude_______ft.
A
10,000
11
Q
Max Temp T/O & Lnd_______°C
A
ISA+35
12
Q
Min Temp T/O_______°C
A
-40
13
Q
Max Tailwind T/O & Lnd____kts.
A
10
14
Q
Crosswind Limitation: Takeoff or Landing
A
27kt (SW)
15
Q
Crosswind Limitation: Takeoff or Landing with RCC 1 or 2 or Poor BA, >1/8” Standing Water, > 1/8” Slush, Ice
A
10kt (SW)
16
Q
Crosswind Limitation: Takeoff or Landing with Wet ice, Slush over Ice, Water over Compact Snow, Dry Snow over Ice, Wet Snow over Ice
A
Prohibited
17
Q
VMO_____KIAS
A
335
18
Q
MMO_______M
A
0.85
19
Q
VLO EXT______KIAS(SW)
A
220
20
Q
VLO RET______KIAS
A
200
21
Q
VLE_____KIAS
A
220
22
Q
VTire______kts.(GS)
A
182
23
Q
VTire______kts.(GS)
A
182
24
Q
V ADG DEPLOY MAX (Wet)______KIAS
A
250
25
V ADG DEPLOY MAX (Dry)
VMO/MMO
26
VB______KIAS
280
27
MB______M
0.75
28
V WIPER OPS Max______KIAS
220
29
VFO 8____KIAS
200
30
VFO 20____KIAS
200
31
VFE 8 ____KIAS
215
32
VFE 20 ____KIAS
215
33
VFE 30____KIAS
185
34
VFE 45____KIAS
170
35
Max Flaps Alt______ft.
15,000
36
Use of flaps is_______ for enroute ops.
prohibited
37
Min spoiler speed
Appr. speed + 20
(Appr. speed is current flaps maneuvering or straight-in speed)
38
Min Alt. Spoilers
1,000 ft. HAT(SW)
39
Spoilers use with flaps at____ prohibited
45°
40
Minimum Runway Width____ft.
100
41
Minimum Taxiway Width____ft.
35 (SW)
42
STANDING WATER Takeoff/Landing
0.50 in./0.75 in.
43
SLUSH Takeoff/Landing
0.50 in./ 0.88 in.
44
WET SNOW Takeoff/Landing
1.00 in./1.50 in
45
DRY SNOW Takeoff/Landing
3.00 in./3.75 in.
46
When operating on runways contaminated with ice, dispatch with one thrust reverser is_____.
prohibited
47
The taxi lights must be switched OFF whenever______.
the airplane is stationary in excess of 10 minutes
48
FMS - The temperature compensation function should not be used at any time. It should be selected______.
OFF
49
FMS - The temperature compensation function should not be used at any time. It should be selected______.
OFF
50
Operations are prohibited on routes where ozone concentrations exceed limits in __________________________________.
Quick Reference Handbook (QRH) Volume 1
51
APU Min Temp Start______°C
-40
52
APU Max Ops Alt_______ft.
37,000
53
APU Max Start Alt_______ft.
30,000
54
APU Max Alt Bleed use_______ft.
15,000
55
APU Max Alt Eng Start_______ft.
13,000
56
Max Door Open with APU not operating_____KIAS
300
57
APU Starter Duty Cycle
58
Autopilot must be engaged above_______ unless otherwise permitted by the MEL.
FL200
59
IAS MODE is ______ during approach
prohibited
60
DES MODE (F/D or A/P coupled) is ______ during approach
prohibited
61
APPR MODE is _____ for ___ approaches
prohibited
VOR
62
ADC SOURCE coupled to active autopilot must be _______ to ATC transponder during flight in RVSM airspace.
the same as that coupled
63
AUTOMATIC FC SYSTEM(AFCS)
64
Ground Ops DC ONLY
5 min
65
Max continuous DC TRU
100 A
66
APU generator (maximum load)
to FL370-30kVA
67
CARGO FIREX-Flight time to suitable airport
45 min
68
Total - Pressure Refueling______lbs.
14,518
69
Total - Gravity Refueling_______lbs.
13,906
70
Max Imbalance for T/O____lbs.
800
71
Min for GA per wing______lbs.
500
(Assumes a maximum airplane climb attitude of 10° nose up)
72
Min Bulk Fuel Temp for T/O______°C
-30
73
Min Bulk Fuel Temp in flight______°C
-40
74
Takeoff with fuel in excess of ____ lbs. in the center tank is not permitted unless: Each main wing tank is above ______lb., or :Each main wing tank is above ______lb., and the allowable zero fuel weight is reduced by the weight of the fuel in the center tank in excess of 500 lb., and the allowable center of gravity (CG) in this configuration is verified to be within allowable CG envelope.
500
4,400
2,000
75
Powered crossflow and gravity crossflow must be ___ for takeoff.
off
76
Powered crossflow and gravity crossflow must be ___ for takeoff.
off
77
When fuel other than Jet-A is to be used, consult _______________ for limitations.
QRH Volume 1
78
Min Reduced Thrust 3A1:____%
85
79
Min Reduced Thrust 3B1:____%
83.5
80
Automatic Performance Reserve (APR) must be used when takeoff performance is predicated upon use of ______.
APR
81
The APR system must be selected ___ when an APR INOP caution message is displayed on EICAS.
off
82
APR OFF Performance must be used when an ________ caution message is displayed.
APR INOP
83
The APR system must be selected OFF for takeoff and APR OFF performance must be used when the ambient temperature is _____ and below, and pressure altitude is less than ______ft. (3A1 engines only)
-18°C
1000
84
Engine Start(Ground)
85
Dry Motoring(Ground)
86
Max wind milling/starter-assisted cross-bleed relight altitude:______
FL210
87
Until oil pressure reaches green band:______
Do not exceed idle
88
Do not exceed 75% N1 until:______or_________,whichever is longer.
2 minutes, all operating indications in green band
89
Ground idle N2 split:_______
≤2%
90
During 2nd engine APU bleed start:_____
Operating engine ≤70%N2
91
With OAT ≥-20°C, thrust levers at idle,N2:_______
>57%. If N2 is ≤57% with OAT of -20°C or greater, do not advance thrust levers above idle. Contact Maintenance.
92
Engines must not be shutdown until:______
2 minutes at idle/near idle thrust. Note- Taxi time counts towards this limitation.
93
SkyWest prohibits the use of thrust reversers__________
during taxi operations
94
Max OIL PRESSURE after cold start:_______
Engine must remain at idle until oil psi returns to normal range. Must be in normal range within 10 min.
95
Single Pack Ops to FL______
250
96
Max Ramp Wt ________lbs.
53,250
97
Max T/O Wt ________lbs.
53,000
98
Max Tailwind T/O & Lnd____kts.
10
