CRJ 200 Limitations Flashcards
(160 cards)
1
Q
MAX RAMP
A
53,250LB
2
Q
MAX T/O
A
53,000LB
3
Q
MAX LND
A
47,000LB
4
Q
MAX ZFW
A
44,000LB
5
Q
MIN FLT WT.
A
30,000LB
6
Q
WING SPAN
A
69’8”
7
Q
AIRCRAFT LENGTH
A
87’10”
8
Q
TAIL HEIGHT
A
20’8”
9
Q
MAX OPS ALT
A
41,000’
10
Q
MAX T/O & LND ALT
A
10,000’
11
Q
MAX TEMP T/O & LND
A
ISA +35C
12
Q
MIN TEMP T/0
A
-40C
13
Q
MAX TAILWIND T/O & LND
A
10KTS
14
Q
VMO
A
335KTS
15
Q
MMO
A
MACH .85
16
Q
VLO EXT
A
250KTS
17
Q
VLO RET
A
200KTS
18
Q
VLE
A
250KTS
19
Q
VTIRE
A
182KTS (GS)
20
Q
VADG DEPLOY MAX
A
250KTS(WET) VMO/MMO(DRY)
21
Q
VB
A
280KTS
22
Q
MB
A
MACH .75
23
Q
VWIPER OPS MAX
A
22OKTS
24
Q
VFO 8
A
200KTS
25
VFO 20
200KTS
26
VFE 8
215KTS
27
VFE 20
215KTS
28
VFE 30
185KTS
29
VFE 45
170KTS
30
MAX ALT SLATS/FLAPS
15,000'
31
FLAPS/SLATS ENROUTE
PROHIBITED
32
MIN SPOILER SPEED (stuck)
Approach speed Vref (flaps 45) +17kts
33
MIN ALT SPOILER
800' AGL
34
SPOILERS WITH FLAPS 45
PROHIBITED
35
MIN RUNWAY WIDTH
75'
36
STANDING WATER T/0
.5 INCH
37
STANDING WATER LND
.75 INCH
38
SLUSH T/O
.5 INCH
39
SLUSH LND
.88 INCH
40
WET SNOW T/O
1 INCH
41
WET SNOW LND
1.5 INCH
42
DRY SNOW T/O
3 INCH
43
DRY SNOW LND
3.75 INCH
44
APU MIN TEMP START
-40C
45
MAX APU OPS ALT
37,000'
46
MAX APU START ALT
30,000'
47
MAX APU ALT BLEED USE
15,000'
48
MAX ALT APU ENG START
13,000'
49
MAX DOOR OPEN SPEED APU NOT IN USE
300KIAS
50
APU BAT START 1
30 SECONDS ON 2 MINUTES OFF
51
APU BAT START 2
30 SECONDS ON 20 MINUTES OFF
52
APU BAT START 3
30 SECONDS ON 2 MINUTES OFF
53
APU BAT START 4
30 SECONDS ON 40 MINUTES OFF
54
AUTO PILOT MUST BE ENGAGED IN
RVSM Airspace
55
AUTO PILOT IAS MODE
PROHIBITED DURING APP
56
AUTO PILOT DES MODE
PROHIBITED DURING APP
57
AUTO PILOT APPR MODE
PROHIBITED DURING VOR APPROACH
58
MAX TIME DC ONLY
5 MINUTES
59
MAX CONTINUOUS DC TRU
100A
60
TOTAL FUEL (PRESSURE REFUELING)
14,518LB
61
TOTAL FUEL(GRAVITY REFUELING)
13,906LB
62
MAX FUEL IMBALANCE FOR T/O
800 LB
63
MIN FUEL FOR GO-AROUND PER WING
459 LB
64
MIN BULK FUEL TEMP FOR T/O
-30C
65
MIN BULK FUEL TEMP IN FLIGHT
-40C
66
MIN REDUCED THRUST 3A1
85%
67
MIN REDUCED THRUST 3B1
83.5%
68
ENG START ON GND 1
60 SECONDS ON 10 SECONDS OFF
69
ENG START ON GND 2
60 SECONDS ON 10 SECONDS OFF
70
ENG START ON GND 3
60 SECONDS ON 5 MINUTES OFF
71
ENG START ON GND 4
60 SECONDS ON 5 MINUTES OFF
72
WHEN BOTH ENGINES ARE TO BE STARTED USING THE APU THE OPERATING ENGINE MUST NOT EXCEED
70% N2
73
DRY MOTORING 1
90 SECONDS ON 5 MINUTES OFF
74
DRY MOTORING 2
30 SECONDS ON 5 MINUTES OFF
75
MAX WINDMILLING/STARTER ASSISTED CROSS BLEED RELIGHT ALT
FL210
76
DO NOT EXCEED 75% N1 UNTIL:
2 MINUTES OR ALL OPERATING INDICATIONS ARE IN THE GREEN BAND, WHICHEVER IS LONGER.
77
MAX GROUND IDLE SPLIT N2
LESS THAN OR EQUAL TO 2%
78
WITH OAT -20C THRST LEVERS AT IDLE N2
GREATER THAN 57%
79
IF N2 IS NOT GREATER THAN 57% AT IDLE WITH -20C
DO NOT ADVANCE THRUST LEVER, CONTACT MX
80
ENGINE COOL DOWN
2 MINUTES AT IDLE/NEAR IDLE THRUST
81
THRUST REVERSER USE DURING TAXI
PROHIBITED
82
OIL PRESSURE: STEADY STATE IDLE
25 psi minimum
83
SINGLE PACK OPS
FL250
84
CPAM PAX O2
14,000' +/- 500'
85
BEFORE THE FIRST FLIGHT OF THE DAY WHEN THE AIRPLANE IS COLD SOAKED THE ENGINES MUST BE
MOTORED FOR 60 SECONDS AND FAN ROTATION VERIFIED BEFORE ENGINE START IS INITIATED
86
AFTER BEING COLD SOAKED THE THRUST REVERSERS MUST BE ACTUATED UNTIL:
THE DEPLOY AND STOW CYCLES ARE LESS THAN 5 SECONDS
87
HOT START, INTERRUPTED START N2 STAGNATION "QRC MEMORY ITEM"
AFFECTED THRUST LEVER......SHUTOFF
IGNITION....OFF
DRY MOTOR.....UNTIL ITT REDUCED BELOW 12O DEGREES, RESPECTING THE STARTER TIME LIMIT
AFFECTED ENGINE...STOP
88
NO LIGHT OFF "QRC MEMORY ITEM"
AFFECTED THRUST LEVER...SHUTOFF
IGNITION...OFF
DRY MOTOR...UNTIL STARTER LIMIT
AFFECTED ENGINE...STOP
89
At what crosswind component is continuous ignition required for takeoff
Greater than 10 kts
90
When is reduced thrust prohibited?
- Wings/Cowls anti-icing bleeds are in use
- Contaminated RWY
- Warnings of windshear or downdrafts are forecast
91
For an unpressurized landing, the pressurization is set to what altitude before takeoff?
3000' above field elevation
92
What conditions/indications would direct a decision to abort the takeoff?
- Engine Failures
- Fire
- Loss of Directional Control
- Windshear
- Unable to Fly
93
The autopilot must be engaged above
RVSM Airspace - FL290
94
The autopilot can be engaged at
600'
95
What is the climb speed schedule below 10,000
250
96
What is the climb speed schedule above 10,000
290/.74
97
What bank deviation requires a PM call out
In excess of 30 Degrees
98
What Speed deviation requires a PM call out
+10/-5 KIAS or .02M
99
What heading from bugged or course deflection require PM call out
+/- 10 degrees
Course from established 1/4 deflection
100
What are the PM callouts
```
SPEED
BANK
HEADING
COURSE
PITCH
VERTICAL SPEED
```
101
On the Speed Cards VMD speed line, what do the dashed lines indicate?
Does not provide adequate bank protection for turns in excess of 15 degrees. Bank angles in excess of 15 degrees and holding are prohibited at these altitudes and weights
102
Double Engine Failure Memory Item
IGNITION CONTINOUS
NO LESS THAN 240KIAS
103
When should you arrive at traffic pattern altitude and flap 0 maneuving speed?
12 miles out straight-in approach, or
8 miles out abeam approach
104
For VMC circle-to-land the aircraft must be aligned with the runway by?
500ft HAT
105
Arming the APPR too early may result in a?
False localizer capture
106
What are the STABILIZER TRIM RUNAWAY memory items?
- Control Wheel…….Assume Manual Control and Override runaway
- Both Stab Trim Disc…..Press,Hold,and Release
- Airplane Control…….Transfer to Pilot (LH) side
- Circuit Breakers (2F5 and 4A1).....OPEN
107
Maximum rate of descent for an overweight landing
360fpm
108
What are the EXCESSIVE ASYMMETRY OR LOSS OF BRAKING memory items?
- Wheel Brakes……..Release Momentarily
- Anti-Skid……….OFF
- Wheel Brakes…...Re-Apply, as required
109
What is the allowance for delamination along the edge of the windshield or window
2 inches from the edge of the window around the entire periphery
110
What is the allowance for delamination along the corner of the windshield or window
4 inches of penetration is allowable in the corners
111
When is a cold weather preflight required
- OAT Less than 5
- Wing Fuel Temp is 0 or less
- Atmospheric conditions have been conducive to frost formation
112
What is a Holdover Time (HOT)
Is an estimate of the time the deicing/anti-icing fluid is effective in preventing the formation of frost, ice, or the accumulation of snow on a treated surface.
113
What is the clean wing concept
Aircraft must not take off when frost, ice, or snow is adhering to the wings, control surfaces, engine inlets, and other critical surfaces of the aircraft.
114
What Altitude does RVSM start?
FL290
115
MIN FUEL
1,550 lb
116
EMER FUEL
1,050 lb
117
Max X-Wind TO/LND CRJ 200
27 Kts
118
Max X-Wind TO/LND RCC 1 or 2
> 1/8" Standing Water
> 1/8" Slush
Ice
10 Kts
119
```
TO/LND Wet Ice
Slush Over Ice
Water over Compact snow
Dry Snow over ice
Wet snow over ice
```
Prohibited
120
Max Number of PAX on Door
4 PAX or 1,000 pounds
121
Flaps AD for Landing
Flaps should not be extended out of 0° unless:
* Prec. app vis. is above the vis. associated with the landing min and expected to remain so.
* Non. prec. same as prec. app but ceilings must also remain above requirments
* An emergency requires landing at nearest airport
* Fuel remaining is sufficient to conduct app, go missed, divert with flaps extended in landing config., conduct app, and land with 1,000lbs of fuel remianing.
122
Min. Oil Pressure Idle
Min. 25psi
123
Min. Oil Pressure for Takeoff
Min. 45psi
124
Max Oil Continious Temp.
+155° C
125
Max. Oil Permissable Temp.
+163° C
126
APU Max EGT
743° C
127
Never Go Below What Mach Speed in a Climb
.70M
128
Holding Speeds
200 KIAS = Below 6001’
230 KIAS = 6001 - 14,000’
265 KIAS = Above 14,000’
129
RVSM Required Equipment
* Two independent altitude measuring systems
* An altitude alerting system
* An automatic altitude control system
* A seconday survellance radar transponder with altitude reporting system that can be connected to the altitude measuring system in use for altitude keeping
130
Max Rotation Rate
3° per second
131
Kinds of Operations
IFR, VFR, Known Icing
132
MIN OIL PRESSURE: TAKEOFF THRUST
45 psi minimum
133
OIL PRESSURE: MAXIMUM CONTINUOUS
115 psi maximum
134
OIL PRESSURE: MAXIMUM TRANSIENT AFTER COLD START
156 psi maximum
(130 psi at idle. 10 min max)
135
COWL A/I MUST BE ON? (GROUND)
OAT 10° C or below AND =
* Visible moisture is present
* When operating on any contaminated runway
* Anytime the wing A/I system is on
136
WITH COWL A/I ON, CAUTION MESSAGE SHOULD DISAPPEAR BY
78% N2 or must call maintenance
137
COWL A/I MUST BE ON? (FLIGHT)
* In icing conditions
* When "ICE" is annunciated by the ice detection system
138
WING A/I ON WHEN (GROUND)
* During final taxi prior to takeoff if the OAT is 5° C or less (Unless type II, III, or IV have been applied)
* On for Takeoff when OAT is 5° C or less and
- Visible moisture in any form below 400' AGL
- contaminated runway
- Presence of any precipitation
139
WING A/I ON WHEN (FLIGHT)
* "ICE" is annuciated by the ice detection system
* In icing conditions and airspeed less than 230 KIAS
140
WHEN DO YOU TURN ON WING A/I IF TYPE II, III, OR IV HAVE BEEN APPLIED
JUST BEFORE TAKEOFF THRUST IS APPLIED
141
CRITICAL AIRCRAFT SURFACES
* Wings
* Upper fuselage
* Horizontal stabilizers
* Vertical stabilizers
* Control surfaces
* Engine inlets
142
MAX RUNWAY SLOPE FOR T/O
* 2% uphill
* -2% downhill
143
MINIMUM FLIGHT CREW
One pilot and one copilot
144
MAXIMUM CABIN DIFFERENTIAL PRESSURE
8.7 psi
145
MAX NEGATIVE PRESSURE DIFFERNTIAL
-0.5 psi
146
MAX DIFFERENTIAL PRESSURE DURING GROUND MANEUVERING
0.1 psi
147
MAX DIFFERENTIAL PRESSURE AT TOUCHDOWN
1.0 psi
148
MIN ALT FOR AUTOPILOT ENGAGEMENT ON NON-PREC APP
400' AGL but no lower than 50' below the DDA, whichever is higher
149
MIN ALT FOR AUTOPILOT ENGAGEMENT ON PREC APP
50' below the DA or 80', whichever is higher
150
CIRCUT BREAKER RESET LIMITATION
Unless in the AFM, no reset unless safety of flight
151
TAXI LIGHT USE LIMIT
Must be off if aircraft is stationary for more than 10 min
152
COLD SOAKED AIRCRAFT DEFINITION
Ambient temperature of -30° C or less for more than 8 hours
153
MIN FUEL TEMP FOR TAKEOFF
5° C
154
MAX OIL CONSUPTION PER HOUR
6.4 ounces per hour (0.05 gallons / 0.2 qts)
155
MAX HOURS WITHOUT OIL SERVICING
16 Hours
156
MAX OIL REFILL ALLOWED
2 qts without dry motoring
157
MAX TURBULENT PENETRATION SPEED
280 kias / 0.75M
158
MAX LOAD FACTOR
* Flaps up: -1.0G to 2.5G
* Flaps down: 0.0G to 2.0G
159
VFO 30
185kts
160
VFO 45
170kts
