Brainscape's Knowledge GenomeTM


Top Flashcards (Certified)
All Flashcards

Challenger 300 > CL30 Limitations > Flashcards

CL30 Limitations Flashcards

1
Q

Max Taxi and Ramp Weight

A

39,000 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Max Takeoff Weight

A

38,850 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Max Landing Weight

A

33,750 lb

(5,100 lb less than Max Takeoff)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

How much fuel must you burn before landing if you took off at Max Takeoff Weight?

A

5,100 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Max Zero Fuel Weight

A

27,200 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Maxumum Usable Fuel (lb) - Pressure Refuel

A

14,150 lb Total

(7,075 lb / Side)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Maxumum Usable Fuel (lb) - Gravity Refuel

A

13,000 lb Total

(6,500 lb / Side)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Maximum Fuel imbalance

A

Varies from 250 - 600 lb

250 lbs with Total fuel more than 13,700 lbs

600 lbs with Total fuel less than 4,700 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Minumum Fuel for Go-Around

A

500 lb per side

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Maximum Bulk Fuel Temp for TakeOff

A

50 C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Minimum Bulk Fuel Temps for Takeoff

A

-30 (Jet A)

  • 35 (Jet 1)
  • 40 (Jet B)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Fuel X-Flow Position For TakeOff

A

Power and Gravity X-Flow Must be OFF

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Maximum Operating Altitude

A

45,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Maximum Takeoff and Landing Altitude

A

10,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Minimum Altitude for Autopilot Useage

(Climb, Enroute or Descent)

A

700 ft AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Minimum Altitude for Autopilot Useage

(Visual or Non Precision)

A

200 ft AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Minimum Altitude for Autopilot Useage

(Precision Approach with Glidepath of 3.5 or less)

A

80 ft AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Minimum Altitude for Autopilot Useage

(Precision Approach with Glidepath 4.5 or less)

A

160 ft AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Maximum Altitude with Yaw Damper OFF

A

31,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Maximum Gear Extension Altitude

A

18,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Maximum Flaps Extension Altitude

A

18,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Minimum Altitude for Spoilers

A

500 ft AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Maximum Altitude With the APU Running

A

37,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

Maximum Altitude with APU GEN

A

30,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Maximum Altitude with ECS Bleed
20,000 ft
26
Maximum Altitude for Engine (APU) Start
20,000 ft
27
Maximum Altitude for Crew/PAX O2 Masks
40,000 ft
28
Maximum Tailwind Component
10 knots
29
Maximum Demonstrated Crosswind (Takeoff)
28 knots for Takeoff
30
Maximum Demonstrated Crosswind (Landing)
24 knots for landing
31
Maximum Demonstrated Crosswind (NWS Inop)
15 knots
32
Maximum Demonstrated Crosswind (On AHRS Channel Inop)
15 kntos
33
Vmo (Up to 8,000 ft)
300 KIAS
34
Vmo (8,001 - 29,475 ft)
320 KIAS
35
Mmo (Above 29,475 ft)
0.83 Mach
36
Vra (Rough Air Penetration Speed)
265 KIAS / 0.75 Mach
37
VLO ret
200 KIAS
38
VLO ext
250 KIAS
39
VLE (Operations with the Gear Extended)
250 KIAS
40
VFE (10/20)
210 KIAS
41
VFE (30)
175 KIAS
42
Tire Speed Limit
182 KIAS
43
Minimum Spoiler Speed
VAPP + 8 KIAS
44
Thrust Reverse IDLE Only
Below 40 KIAS
45
Use of Engine Anti-Ice In Flight
SAT (Static Air Temperature) is 10 to -40 C with visible moisture, or when ICE DETECTED CAS message is displayed.
46
Minimum Temp for Takeoff
-40 C
47
Minimum Oil Temperature for Starting
-40 C
48
After three start attempts, how long must the starter be allowed to cool?
15 min cooling period
49
How long should an starter be allowed to cool after a 5 minutes (cranking) attempt?
15 min
50
How long must an engine be motored after an aborted start?
30 sec
51
Minimum Oil Pressure At IDLE
28 psi
52
Minimum Idle N2
46.0%
53
Max Ground Start ITT
650 C
54
Maximum ITT to Begin a Start
350 C
55
Maximum Generator Electrical Load (2 or 3 Gens Operating)
400 amps
56
Maximum Generator Electrical Load (1 Gen on the ground)
400 amps
57
Maximum Generator Electrical Load (1 Gen in Flight)
500 amps
58
Maximum Generator Electrical Load (Transient 5 min)
600 amps
59
Maximum APU RPM
108%
60
Maximum APU EGT (Start)
973 C
61
Maximum APU EGT (Normal)
718 C
62
How many start attempts do you get to start the APU?
3, followed by a 1 minute cooling period.
63
How much of a cooling period do you need after each of your 3 APU start attempts?
1 min
64
How long of a cooling period do you need after the 3rd APU start attempt?
20 min
65
How long should you wait to make another APU start, after a successful start.
10 min
66
How many successful start attemps can you make with 10 minute cooling intervals before you need to wait an hour?
6 attempts
67
How long do you need to wait after 6 successful starting attempts?
1 hour
68
Can you use the APU during de/anti-ice operations?
No - Use is Prohibited.
69
Is TakeOff with a APU SHUTDOWN CAS Message allowed?
No - Takeoff without inspection is prohibited.
70
Five Limitations for use of Thrust Reverse
1. Use on paved surfaces only. 2. Do not deploy in flight. 3. Do not back up the airplane. 4. No use for touch and go landings. 5. Below 40 KIAS - IDLE Only.
71
TRIM AIR ONLY
Prohibited on ground.
72
Max Pressurization Differential On Ground
0.1 psi
73
Max Pressurization Differential - Landing
1.0 psi
74
Max Pressurization Differential (Positive)
9.4 psi
75
Max Pressurization Differential (Negative)
-0.5 psi
76
Minimum flight weight?
23,100 lbs
77
To be used for navigation, the FMS must be recieving:
1. One VOR/DME or 2. Two DMEs or 3. GPS (RAIM must be available)
78
Minimum battery temp for takeoff?
-20 C
79
Use of Takeoff Power (time)?
5 min
80
Use of APR power (auto)?
10 min
81
Use of APR power (manual)?
5 min
82
When should you remove the battery?
When the temp is expected to be less than -30 C for more than 10 hours.
83
What is the limitation for use of battery or GPU on the ground?
If temp is above 40 C, no more than 30 min.
84
Minimum Oil temp for above Idle?
5 C
85
Minimum Oil temp for Takeoff?
15 C
86
Maximum pressure for pressure refueling?
55 psi
87
Maximum pressure for pressure defueling?
-8.0 psi
88
Types of operation
Day, Night, VMC, IMC Icing
89
What equippment is required for RVSM?
Autopilot Altitude Alerting System One Altitude Reporting Transponder Two Air Data Computers
90
Restriction on Holding in Ice
No Flaps
91
Side window building ice
Assume flight in super cooled large droplets. Wing and Engine anti-ice ON Leave icing conditions as soon as possible.
92
Engine Anti-Ice System On For Takeoff (Ground)
OAT 10 C or colder with visible moister (such as fog with vis. of 1 mile or less).
93
Engine Anti-Ice System On For Taxi (Ground)
OAT 10 C or colder with surface contaminants

Challenger 300 (2 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2025 Bold Learning Solutions. Terms and Conditions