Limitations Flashcards
1
Q
Maximum Ramp Weight CL300
A
39,000 lbs.
2
Q
Maximum Takeoff Weight CL300
A
38,850 lbs.
3
Q
Maximum Zero Fuel Weight CL300
A
27,200 lbs.
4
Q
Maximum Landing Weight CL300
A
33,750 lbs.
5
Q
Minimum Flight Weight CL300
A
23,100 lbs.
6
Q
VRA-Rough Air
A
265 KIAS/0.75 M
7
Q
VLO-Retraction
A
200 KIAS
8
Q
VLO-Extension
A
250 KIAS
9
Q
VLE-Extended
A
250 KIAS
10
Q
VFE Flaps 10
A
210 KIAS
11
Q
VFE Flaps 20
A
210 KIAS
12
Q
VFE Flaps 30
A
175 KIAS
13
Q
Maximum Tire Speed
A
182 kts
14
Q
Maximum T/O and Landing Pressure Altitude
A
10,000’
15
Q
Maximum Tailwind Component
A
10 knots
16
Q
Maximum Runway Slopes
A
+2% to -2%
17
Q
Maximum Pressure Altitude
A
45,000’
18
Q
Maneuvering Load Factors Flaps Up
A
+2.6 to -1.0
19
Q
Maneuvering Load Factors Flaps Extended
A
+2.0 to 0.0
20
Q
RVSM Required Equipment
A
Autopilot-1
Altitude Alerting System-1
Altitude Reporting Transponder-1
Air Data Computers-2
21
Q
Minimum Oil Temp for starting?
A
-40C
22
Q
When side window icing is observed you may be in ______ and should?
A
SLD and turn on anti ice equipment and exit conditions.
23
Q
Engine Anti-ice must be on when on the ground and for takeoff if?
A
OAT is below 10C and visible moisture is present.
24
Q
Flight Icing conditions as described by Bombardier are?
A
OAT is from 10C to -40C and visible moisture is present.
25
What are two conditions that require engine anti-ice to be on?
1. In icing conditions.
| 2. ICE DETECTED CAS
26
The wing anti-ice must be on when on the ground when?
The OAT is 5C or below and visible moisture or standing moisture is present.
27
The wing anti ice must be on in flight when?
1. In icing conditions (10C to -40C with visible moisture).
(and speed less than 210 KIAS)
2. ICE DETECTED CAS displayed.
28
Maximum operating speed up to 8,000' is?
300 KIAS
29
Maximum operating speed from 8,001' to 29,475' is?
320 KIAS
30
Maximum operating speed above 29,475' is?
0.83 M
31
Vra is
265 KIAS/0.75 M
32
When on the ground do not select the AIR SOURCE to?
TRIM AIR ONLY
33
The pack must be operating when aircraft electrical power is on for more than _______ minutes and the OAT is?
more than 30 minutes and OAT is above 40C.
34
Crew and passenger oxygen masks are not APPROVED for use above?
40,000' cabin altitude.
35
Prolonged operation of passenger masks above _______ is not RECOMMENDED.
25,000 cabin altitude.
36
The maximum cabin differential pressure on the ground must not exceed?
0.1 PSI
37
The maximum cabin differential during landing must not exceed?
1.0 PSI
38
The maximum positive differential pressure is?
9.4 PSI
39
The maximum negative differential pressure is?
-0.5 PSI
40
Autopilot operation with an ILS glidepath angle that exceeds ______ is prohibited.
4.49 degrees
41
Autopilot minimum use height for Climbs, Enroute, or Descents is?
700' AGL
42
Autopilot minimum use height for Precision Approach is?
| <3.5 >3.5
80' AGL less than 3.5 glidepath/ 3.5 to 4.5 glidepath angle is 160' AGL
43
Autopilot minimum use height for Visual or Non-Precision approach is?
200' AGL
44
Maximum altitude with Yaw Damper off is?
31,000'
45
DATALINK is approved for tx/rx of messages that?
will not create an unsafe condition if the message is improperly received.
46
FMS V-speed data is prohibited for temperatures?
Above ISA + 33C
47
To be used for navigation the FMS must be receiving suitable nav data from? (CL300 only)
1. One VOR/DME or
2. Two DMEs or
3. GPS
48
Maximum continuous amps with 2-3 generators operating?
400 amps
49
Maximum continuous amps with one generator operating on the ground?
400 amps.
50
Maximum continuous amps with one generator operating in flight?
500 amps
51
Transient amp limit?
600 amps
52
Do not takeoff if battery temperatures are below?
-20C
53
Do not extend flaps above?
18,000'
54
Flight spoilers must not be extended in flight at airspeeds?
below approach speed plus 8 KIAS
55
Flight spoilers must not be extended in flight below _____' AGL
500 AGL
56
Do not extend landing gear above?
18,000'
57
Maximum usable fuel with a pressure refuel?
14,150 lbs. total/7,075 lbs per side
58
Maximum usable fuel with a gravity refuel?
13,000 lbs. total/6,500 lbs per side
59
Minimum fuel for go-around?
500 lbs. per side
60
Ground Start ITT limit?
650C/650C
61
Air Start ITT limit?
700C/800C
62
Idle N2 minimum?
46.0%
45% for PMA to power FADEC
63
Idle oil pressure minimum?
28 PSI
64
Max reverse N1?
70.7% N1
65
Max reverse ITT?
928C/955C
66
Maximum Continuous Climb ITT?
928C/950C
67
Maximum Continuous Climb oil temp?
138C
68
Normal Takeoff ITT?
928C/955C
69
Normal Takeoff oil temperature range?
27C minimum to 138C maximum
70
APR (Max Power) ITT?
946C/955C
71
APR (Max Power) Oil Temp?
138C
72
APU Max Altitude Operation
37,000'
73
APU Max Altitude for use as generator?
30,000'
74
APU max altitude for bleed air for engine start?
20,000'
75
The APU may be started up to an altitude of?
| ground/flight
30,000' in flight and 14,000' on the ground
76
What is N1 for?
1. max climb/continuous
2. normal takeoff
3. APR (max power)
1. max climb/continuous 95.2
2. normal takeoff 96.1
3. APR (max power) 96.1
77
What is N2 for?
1. max climb/continuous
2. normal takeoff
3. APR (max power)
1. max climb/continuous 97.2
2. normal takeoff 97.2
3. APR (max power) 98.1
78
What is ITT for?
1. max climb/continuous
2. normal takeoff
3. APR (max power)
1. max climb/continuous 928
2. normal takeoff 928
3. APR (max power) 946
79
Hydraulic Fluid type?
Type 4
80
Approve Fuels?
Jet A, Jet A-1, Jet B, JP-4, JP-5, JP-8
81
What type of engines?
HTF7000
82
Takeoff Power time limit?
5 minutes
83
Time limit on APR power?
10 minutes if automatically selected, 5 minutes for manually selected
84
Max reverse thrust is automatically reduced at what speed?
85 knots
85
What is the minimum oil temperature required to operate engines above ground idle?
(minimum oil temperature to advance the TLs at all after starting)
5C
86
With oil temperatures between 5C and 14C engines may be?
operated from idle up to but NOT including climb power.
87
How many consecutive engine start cycles may be conducted?
3, followed by a cooling period of 15 minutes.
88
After an aborted start the engine...?
must be motored for 30 seconds.
89
APU type?
Honeywell 36-150BD
90
Do not use the APU to start the left engine above?
9,000'
91
APU starting limitations?
1-60 seconds
2-60 seconds
3-20 minutes
92
Max APU RPM?
108%
93
Max APU EGT for start?
973 C
94
Max APU ITT for normal operations?
718 C
95
Reverse thrust above idle reverse is prohibited below _____ KIAS.
40
96
Thrust reversers on touch and go landings are_______.
prohibited.
97
When deicing the aircraft with fluid operation of the APU is ______.
prohibited.
98
Wingspan CL300 CL350
63'10" / 69'00"
99
Length CL 300/350
68'08"
100
Height. CL300/350
20'00"
101
Minimum Pavement for a 180
| CL300 and CL350
58'00"
102
Wingtip Clearance for 180 turn CL300 CL350?
95'5" / 101'00"
103
Do not hold in icing conditions with flaps _________?
extended
104
CL350 Max Ramp Wt?
40,750
105
CL350 Max T/O Weight?
40,600
106
CL350 Max Zero Fuel Wt?
28,200
107
CL350 Max Landing Weight?
34,150
108
CL350 Min Flight Weight?
24,800
109
Max demo x-wind takeoff?
28 KTS
110
Max demo x-wind landing?
24 KTS
111
CL350 FMS as a navigation source must be receiving?
2 GNSS or
1 VOR/DME or
2 DMEs or
1 IRS
112
If a life raft is required, the maximum PASSENGERS on board is?
10
113
Maximum lap children?
2
*more are possible with mgmt approval considering oxygen and life rafts.
114
Minimum bleed air for normal start?
32
