200 Limitations Flashcards
1
Q
RNAV Required Equipment (7)
A
VOR (2) DME (2) FMS Current FMS Database GPS (1) Flight Directors (2) Autopilot
2
Q
RNAV operations must not be conducted with any of the following messages displayed (9):
A
GPS NOT AVAILABLE GPS DISABLED GPS-FMS DISAGREE DME-FMS DISAGREE FMS-FMS DISAGREE LOW POS ACCURACY CHK POS NO APPR GPS RAIM NO GPS RAIM
3
Q
When may RNAV operations be continued following the display of an FMS “CHK POS” message?
A
If the message is displayed for less than one minute while en-route, and clears itself with no action from the pilot.
4
Q
When must the ADC source coupled to the autopilot must be the same as that coupled to the transponder?
A
During flight in RVSM airspace
5
Q
Operational Limitations for Category II Operations (9)
A
Flap configuration - 45-degrees Both Engines Operating Autopilot Coupled Aircraft Placarded as Certified for Category II Both Pilots Trained and Qualified Both Pilots Have 100 hrs. In-Seat in CL-65 at Endeavor Flight Director Transferred to FO's Side Maximum Headwind - 17 kts. Maximum Tailwind/Crosswind - 10 kts.
6
Q
The minimum required oxygen pressure guarantees there is adequate oxygen to:
A
Perform an emergency descent from 41,000 ft. to 10,000 ft. in 10 minutes, followed by 110 minutes of cruise at 10,000 ft. with a “Normal” mask setting.
7
Q
What oxygen pressure will trigger the OXY LO PRESS caution message?
A
1410 psi
8
Q
Under what conditions may a flight be conducted with an OXY LO PRESS caution message (3)?
A
No leak suspected
Flight conducted where MEAs are 10,000 ft. and below
Sufficient pressure is verified
9
Q
What is the maximum crew oxygen bottle pressure?
A
1850 psi
10
Q
Maximum number of passengers on the main cabin door:
A
Four
11
Q
Maximum weight on the main cabin door
A
1000 lb
12
Q
If cargo is carried in the cargo compartment, how close must a flight always be to a suitable airport?
A
45 minutes
13
Q
Maximum cargo capacity
A
3500 lb
14
Q
Maximum pressure altitude for takeoff and landing
A
10,000 ft
15
Q
Maximum operating altitude
A
41,000 ft
37,000 ft (company)
16
Q
Maximum operating altitude during single-pack operations
A
25,000 ft
17
Q
Maximum ambient temperature for takeoff and landing
A
ISA +35-deg C
18
Q
Minimum ambient temperature for takeoff
A
-40-deg C
19
Q
Target rotation rate on takeoff
A
3-degrees per second
20
Q
When calculating landing performance, when must “Wet” data be used?
A
The runway is wet
The visibility is less than RVR40 or 3/4SM
21
Q
Maximum Taxi and Ramp Weight
A
53,250 lb
22
Q
Maximum Takeoff Weight
A
53,000 lb
23
Q
Maximum Landing Weight
A
47,000 lb
24
Q
Maximum Zero Fuel Weight
A
44,000 lb
25
Minimum Flight Weight
30,000 lb
26
Maneuvering Load Limits
- 1.0g - 2.5g (F Up)
| 0. 0g - 2.0g (F Dn)
27
Avoid unnecessary and large side-slip maneuvers during which flight regime?
Low-speed, high-altitude cruise
28
Maximum Runway Slope
+2 uphill / -2 downhill
29
Maximum tailwind component for takeoff and landing
10 kt
30
Maximum crosswind component for takeoff and landing on a wet runway
27 kt
31
Maximum crosswind component for takeoff and landing on a dry runway
27 kt
32
Maximum crosswind component for takeoff and landing on a contaminated runway
15 kt
33
Definition of Visible Moisture
Clouds, fog with visibility of one mile or less, rain, snow, sleet, or ice crystals.
34
Engine Anti-Ice
| ground operations
OAT is 10C or below and visible moisture is present
OAT is 10C or below when operating on contaminated surfaces
35
When must the Wing Anti-Ice be selected ON for takeoff?
OAT is 5C or below and:
Visible moisture below 400 ft AGL, or
Runway is wet or contaminated, or
Presence of any precipitation
36
When must the Wing Anti-Ice be selected ON during final taxi?
OAT is 5C or below, unless anti-ice fluid has been applied
37
For the purpose of Wing Anti-Ice, what is considered "Final Taxi"?
Initiation of the Before Takeoff Checklist
38
If required for taxi, when may the Wing Anti-Ice be selected ON?
After both engines are running, but no later than the commencement of the Before Takeoff Checklist
39
If anti-ice fluid has been applied, when may the Wing Anti-Ice be selected ON?
Just prior to thrust increase for takeoff
40
If anti-ice is not required for takeoff, when may the Wing Anti-Ice be selected OFF?
Just prior to takeoff
41
Engine Anti-Ice
| flight operations
In icing conditions
| When ICE is detected
42
Wing Anti-Ice
| flight operations
In icing conditions less than 230 kt
| When ICE is detected
43
Definition of Icing Conditions in-flight
TAT of 10C or below with visible moisture present, except when SAT is -40C or below
44
Takeoff is permitted with frost adhering to which aircraft surfaces?
Upper surface of the fuselage
| Underside of wing (caused by cold-soaked fuel)
45
A tactile check of the wing leading edge, and forward and rear upper surfaces, is required when:
OAT is 10C or less, or wing fuel temperature is 0C or less, and:
There is visible moisture
Water is present on the wing
Temp/Dew Point spread is 3C or less
Conditions conducive to frost formation
46
What are the maximum depths of standing water acceptable for takeoff and landing?
1/2 in. for Takeoff
| 3/4 in. for Landing
47
What are the maximum depths of slush acceptable for takeoff and landing?
1/2 in. for Takeoff
| 7/8 in. for Landing
48
What are the maximum depths of wet snow acceptable for takeoff and landing?
1 in. for Takeoff
| 1 1/2 in. for Landing
49
What are the maximum depths of dry snow acceptable for takeoff and landing?
3 in. for Takeoff
| 3 3/4 in. for Landing
50
Is a takeoff authorized on a contaminated runway with one thrust reverser inoperative?
No
51
Is a landing authorized on a contaminated runway with one thrust reverser inoperative?
Yes, unless a Special Winter Operations Airport
52
Under what condition is landing prohibited on a contaminated runway with one thrust reverser inoperative?
Special Winter Operations Airports
53
Maximum Flap Operating Speeds
200 kt - Flaps 8
200 kt - Flaps 20
185 kt - Flaps 30
170 kt - Flaps 45
54
Maximum Flap Extended Speeds
230 kt - Flaps 8
230 kt - Flaps 20
185 kt - Flaps 30
170 kt - Flaps 45
55
Maximum Landing Gear Extended Speed
250 kt
56
Maximum Landing Gear Operating Speeds
200 kt - Retraction
| 250 kt - Extension
57
Maximum Tire Limit Speed
182 kt groundspeed
58
Maximum Turbulent Air Penetration Speed
280 kt or 0.75M, whichever is lower
59
Maximum Speed with STAB or MACH TRIM Inoperative
250 kt or 0.70M, unless the autopilot is engaged
60
Bank angle is limited to 15-degrees when operating below which speed?
Maneuvering Speed
| Vref + 10 kt
61
Maximum Windshield Wiper Speed
220 kt
62
If the windshield wiper has failed in a non-parked position, the speed must not exceed:
220 kt
63
What occurrence signifies the onset of a stall warning?
Stick Shaker Operation
64
When is it acceptable to climb below 250 kt/0.70M above 10,000 ft (3)?
In mountainous terrain, until clear of terrain or reaching MEA - Vx or Vref + 10
When specifically asked by ATC - Vy, except in icing conditions above 15,000 ft.
Highest speed allowed by an MEL, but not below Vx
65
A climb will be stopped when the vertical speed at 250 kt/0.70M decreases to:
300 ft/min
66
Minimum Enroute Cruise Speeds
Long Range Cruise - Above FL310
Two-Engine Vmd - At and Below FL310
67
Full application of rudder and ailerons are restricted to airspeeds below:
Maneuvering Speed
68
Minimum N2% for Engine Starting
20%
69
Maximum ITT During Engine Start
900C
70
Maximum ITT During Engine Acceleration
900C
71
Maximum Continuous ITT
874C
72
Maximum ITT During Normal Takeoff
884C for 5 minutes
| 900C for 2 of 5 minutes
73
Maximum ITT During Go-Around or APR Thrust
900C for 5 minutes
| 928C for 2 of 5 minutes
74
Maximum N2 Split at Idle Power
2%
75
With an OAT of -20 or warmer, the engine must not be accelerated above Idle with an N2 of what (or less)?
57%
76
What defines a cold-soaked airplane?
Exposed to temperatures of -30C or below for more than 8 hours
77
Prior to the first flight of the day, what must take place for a cold-soaked airplane?
Engine dry-motored for 60 s, and fan rotation verified prior to engine start
Reverse thrust actuated until deploy/stow cycles are less than 5 s
78
Minimum Oil Temperature for Engine Starting
-40C
79
Maximum Continuous Oil Temperature
155C
80
Maximum Permissible Oil Temperature
163C
| 15 min maximum
81
Minimum Oil Pressure at Steady State Idle
25 psi
82
Minimum Oil Pressure at Takeoff Power
45 psi
83
Maximum Continuous Oil Pressure
115 psi
84
Maximum Transient Oil Pressure After Cold Start
156 psi
| 130 psi at idle, 10 min maximum
85
Continuous Ignition must be used during the following conditions:
Takeoff and landing on contaminated runways
Takeoffs when crosswind exceeds 10 kt
Flight through moderate or heavier rain
Flight through moderate or heavier turbulence
Flight in the vicinity of thunderstorms
86
How long must the engines run prior to takeoff?
2 min
87
How long must the engines stabilize at idle prior to shutdown?
2 min
88
For the purpose of engine stabilization, what maximum engine speed may be considered as part of the cool-down period?
80% N2
89
If after an engine shutdown ITT is observed to rise rapidly above 350C, what action must be taken?
Carry out a dry-motoring cycle
90
Maximum N2 RPM for engagement of the engine starter
55% N2
91
Engine Starter Limits
1 - 60 s on, 10 s off
2 - 60 s on, 10 s off
3+ - 60 s on, 5 min off
92
Dry Motoring Cycle Limits
1 - 90 s on, 5 min off
| 2+ - 30 s on, 5 min off
93
Maximum ITT for thrust level movement from SHUT OFF to IDLE
120C for ground starts
| 90C for air starts
94
Maximum Altitude for Airborne Engine Relight
21,000 ft
95
Target Airspeed for Windmilling Engine Relight
300 kt
96
Reduced thrust may not be used in the following situations (7):
Normal N1 is less than 85%
Engine unable to achieve full rated thrust
Anti-ice in use
Contaminated runway
Warnings of windshear or downdrafts forecast
Special DP specifies full thrust
Anti-skid inoperative
97
Maximum permissible fuel imbalance between left and right main tanks:
800 lb
98
When may takeoffs be initiated with more than 500 lb of fuel in the center tank?
If each wing tank contains more than 4400 lb
99
Minimum fuel for a go-around
900 lb
| 450 lb per wing
100
Minimum engine fuel temperature for takeoff
5C
101
Minimum bulk fuel temperature for takeoff
-30C
102
Powered fuel crossflow and gravity crossflow must be in what configuration for takeoff?
Both must be off for takeoff.
103
When may the engine oil level be checked?
Within 3 minutes to 2 hours after engine shutdown
104
Minimum ambient temperature for APU starting
-40C
105
APU Start Limits on Battery Power
1 - 30 s on, 2 min off
2 - 30 s on, 20 min off
3 - 30 s on, 2 min off
4 - 30 s on, 40 min off
106
APU Start Limits on DC Ground Power
1 - 15 s on, 2 min off
2 - 15 s on, 20 min off
3 - 15 s on, 2 min off
4 - 15 s on, 40 min off
107
Maximum APU Operating Altitude
37,000 ft
108
Maximum APU Start Altitude
30,000 ft
109
Maximum Altitude for APU Bleed Air Extraction
15,000 ft
110
Maximum Altitude for APU-Assisted Engine Starts In-Flight
13,000 ft
111
If both engines are started using APU bleed air, the operating engine thrust must not exceed:
70% N2
112
When operating with the APU door open, the following limitation applies:
Airspeed limited to 300 kt, OR
| APU must remain in operation
113
Maximum Positive Differential Cabin Pressure
8.7 psid
114
Maximum Negative Differential Cabin Pressure
-0.5 psid
115
Maximum Differential Cabin Pressure During Taxi, Takeoff, and Landing
0.1 psid
116
What is the minimum cabin altitude that the pressurization system may be operated in manual mode?
-1500 ft
117
The EMER DEPRESS button must not be pushed above what altitude?
15,000 ft
118
Which door must remain open when the low-pressure air ground connection is used?
Passenger Door
119
Rated AC Load for Main Generators
30 kVA to 35,000 ft
| 25 kVA above 35,000 ft
120
Rated AC Load for APU Generator
30 kVA to 37,000 ft
121
Maximum Load on Each TRU
100 a
122
Maximum Permissible Time on Ground DC Power
5 min
123
Except for touch-and-go training, flaps must be selected from which detent?
0-degrees
124
Maximum Altitude for Flap Extension
15,000 ft
125
Upon arrival at the destination airport, an approach shall not be commenced, nor shall the flaps be extended unless one of the following criteria exists (4):
1. Precision approach - Visibility at/above minimums
2. Non-precision approach - Ceiling/visibility at/above minimums.
3. Emergency requires landing at nearest suitable airport
4. Fuel sufficient to divert and land with 1000 lb remaining
126
For the purpose of flap limitation, a diversion route must allow a minimum flight altitude not to exceed:
15,000 ft
127
Flight spoilers must not be extended below what altitude?
1000 ft AGL
128
Minimum airspeed for flight spoiler use:
Recommended maneuvering speed + 17 kt
129
Maximum flap setting for flight spoiler use:
30-degrees
130
Unless operating under MEL guidance, takeoff with the following thrust reverser indications is prohibited (3):
THRUST REVERSER UNLK light
REV icon on N1 gauge
L(R) REV UNLOCKED caution messge
131
Maximum reverse thrust is not authorized below what airspeed?
60 kt
132
For the purpose of reverse thrust, what is considered "idle thrust"?
Not above 30% N1
133
Taxi lights must be switched OFF whenever the aircraft is stationary in excess of:
10 mins
134
When is the use of the FCP submode "DES" prohibited?
During approaches
135
Minimum altitude for autopilot use (general)
600 ft AGL
136
Minimum altitude for autopilot use on a non-precision approach
400 ft AGL
137
Minimum altitude for autopilot use on a precision appraoch
80 ft AGL
138
If the GPS is inoperative, what must be inhibited for operations below FL180?
Terrain awareness alerting and display functions
139
FMS-calculated thrust settings must not be used for advisory information above which altitude?
36,000 ft
