Limitations Flashcards
(107 cards)
1
Q
Max Ramp Weight
A
42,400 lbs
2
Q
Max Takeoff Weight
A
42,200 lbs
3
Q
Max Landing Weight
A
39,300 lbs
4
Q
Max Zero Fuel Weight
A
29,700 lbs
5
Q
Max Baggage Compt Weight
A
1,600 lbs
6
Q
Max Payload
A
5,990 lbs
7
Q
Maneuvering Speed (VA)
A
198 KIAS
8
Q
SF1 Max Speed
A
200 KIAS
9
Q
SF2 Max Speed
A
190 KIAS
10
Q
SF3 Max Speed
A
180 KIAS
11
Q
Max Landing Gear Operating Speed (VLO/MLO)
A
190 KIAS/MI 0.7
12
Q
Max Landing Gear Extended Speed (VLE/MLE)
A
245 KIAS/MI 0.75
13
Q
Minimum Control Speed in the Air (VMCA)
A
90 KIAS
14
Q
Minimum Control Speed during Approach and Landing (VMCL)
A
90 KIAS
15
Q
Minimum Control Speed on the Ground (VMCG)
A
98 KIAS
16
Q
Windshield Operating Speed (VWWO)
A
215 KIAS
17
Q
Pilot Sliding Window Speed (V Window)
A
215 KIAS
18
Q
Tire Max Operating Speed (V Tire)
A
195 KT (Ground Speed)
19
Q
Max Airport Pressure Altitudes for Takeoff and Landing
A
-1,000 ft/8,000 ft
-1,000 ft/14,000 ft (M2706)
20
Q
Max Runway Slope for Takeoff and Landing
A
+/- 2%
21
Q
Runway Type Required for Takeoff and Landing
A
Paved and Hard Surfaced
22
Q
Max Tailwind for Takeoff and Landing
A
10 KIAS
23
Q
Max Enroute Operating Altitude
A
47,000 ft
24
Q
Max Differential Cabin Pressure
A
9.3 PSI
25
Max Negative Differential Cabin Pressure
-0.3 PSI
26
Can Autopilot be Engaged on the Ground?
No
27
Autopilot Minimum Engagement Speed during climb out
V2 + 10 kt
28
Autopilot Minimum Engagement Speed during Go Around
VREF + 10 kt
29
Autopilot minimum height during climb out
400 ft
30
Autopilot Minimum Height during Level Flight
1,000 ft
31
Autopilot Minimum Height during standard non-precision approach
160 ft
32
Autopilot use height during ILS approach with operational radar altimeter
50 ft
33
Autopilot min height during an ILS approach and inoperative radar altimeter
160 ft
34
Autopilot minimum height during ILS steep approach (between 4.5 and 6.65 degrees in SF3 and AB1 configuration)
285 ft
35
Autopilot minimum use height during circling approach below 200 KIAS in clean configuration
500 ft
36
Autopilot minimum use height during circling approach
500 ft
37
Flight director minimum use height at takeoff
400 ft
38
Can Autothrottle be engaged during takeoff and landing?
No
39
Should Autothrottle be disengaged during go-around?
Yes
40
Autothrottle minimum engagement height during initial climb out
400 ft
41
Autothrottle minimum disengagement height for standard approach path angle
50 ft
42
Autothrottle minimum disengagement height during ILS steep approach (between 4.5 and 6.65 degrees in SF3 and AB1 configuration
285 ft
43
Can the Autothrottle be engaged before aircraft is in clean configuration after takeoff and go around when FMS is selected on guidance panel?
No
44
Can the thrust director be displayed before aircraft is in clean configuration after takeoff when FMS speed is selected on guidance panel?
No
45
Max DC System Voltage
29.5 V
46
Max Engine Generator Output in Flight
Stabilized: 400 A
Transient (5 sec): 800 A
Transient (40 sec): 600 A
Transient (160 sec): 500 A
47
Max engine generator output on ground for basic generators
300 A
48
WARM BAT CAS Message Temperature
48.9 degrees C or above
49
HOT BAT CAS Message temperature
71.1 degrees C or above
50
Max Speed with Inoperative Arthur Unit
260 KIAS/MI 0.76
51
Can the aircraft maintain a configuration with flaps or slats extended above 20,000 ft?
No
52
How is flap extension or retraction executed?
One notch at a time
53
Can the airbrake configuration be changed in flight below 300 ft?
No
54
Max Usable Fuel Quantity
16,674 lbs
55
Minimum inflight fuel tank temperature
3 degrees C above freezing point of fuel being used
56
Max fuel dissymmetry
2,200 lbs
57
Max fuel feed pressure
50 PSI
58
Can the Fuel Quantity Management Computer (FQMC) be inoperative for takeoff?
No
59
Approved Hydraulic Fluid Types
Fluid Conforming to:
AIR 3520
MIL-H-5606
60
Hydraulic Reservoir 1 max capacity
1.95 gallons
61
Hydraulic Reservoir 2 max capacity
1.58 gallons
62
Normal hydraulic operating pressure (green range)
3,000 +/- 200 PSI
63
Normal Standby Pump Auto mode pressure
1,650 - 2,300 +/- 100 PSI
64
When do Icing Conditions Exist?
TAT + 10 degrees C and visible moisture
OAT + 10 degrees C on ground when moisture may be ingested or freeze
65
Is the Ice Detection System a Primary Detection System?
No - it is a secondary or backup detection system
66
Is prolonged flight in icing conditions with slats/flaps extended authorized?
No
67
When should engine anti-ice be deactivated?
TAT exceeds 10 degrees C
68
When should wing anti-ice be deactivated?
TAT exceeds 10 degrees C
69
When can wing anti-ice be used during ground operations?
Only for limited checks conducted in accordance with AFM
70
What type of tires must be installed on Nose Wheel?
Chinned Tires
71
Max Brake Energy
16,875 kJ per brake
72
Reference to minimum turn around table is not required prior to taxi if each brake temperature is below what?
160 degrees C and decreasing
73
Is brake cooling time affected by park brake application?
No
74
Ground operating limitations of landing lights
15 min On
45 min cooling time
75
Passenger Oxygen System automatically drops masks at what cabin altitude?
14,500 ft +/- 500 ft
76
What APU is installed on the aircraft?
Honeywell GTCP 36-150 (F2M)
77
Max Operating Altitude (APU)
35,000 ft
78
APU max starting altitude
35,000 ft
79
Can APU be operated with PAX in the cabin without crew monitoring?
No
80
APU max N1 speed
110%
81
APU average fuel flow
100 lb/hr
82
APU EGT limit during start
988 degrees C for less than 10 sec
83
APU stabilized EGT limit
746 degrees C
84
APU Max Generator Output - Stabilized
0-10,000 ft: 300 A
10,000-25,000 ft: 250 A
25,000-35,000 ft: 200 A
85
APU Max Generator Output - Transient
40 sec: 450 A
180 sec: 375 A
86
Max weight authorized of PAX door
1,500 lbs
87
Max Weight authorized on one step of PAX door
440 lbs
88
When is the in cabin baggage compartment door required to be closed and latched?
When access to baggage compartment is not required
89
What type of engine is installed on the aircraft?
Pratt & Whitney 308C
90
Engine Takeoff Thrust Rating
6,998 lbs
91
Max Continuous Thrust Rating
6,998 lbs
92
Engine Takeoff Thrust time limit
5 minutes
93
What is used as thrust setting parameter?
N1
94
Engine Rotor Speed Limits
(N1/N2)
Normal Takeoff (5 min max): 102.5%/102%
Max Takeoff (5 min max): 102.5%/102%
Max Continuous: 102.5%/102%
Transient (20 sec): 103.5%/103%
95
Max Rotor Speed Limit at 100% N1
10,400 rpm
96
Max Rotor Speed Limit at 100% N2
26,780 rpm
97
Overall Engine Vibration Limit
0.96 in/sec average
98
Engine ITT Limits (Starts)
Ground Start: 950 degrees C
Airstart: 950 degrees C
Airstart - Max restart: 500 degrees C
Ground Start - Max Restart: 340 degrees C
99
Engine ITT Limits
Max TO (APR) transient: 905 C (2 min max)
Max TO (APR): 895 C (5 min max)
Normal TO: 875 C (5 min max)
Max Continuous: 860 C
Flight Transient: 890 C (20 sec max)
875 C (5 min max)
100
Engine Start Times (Ground)
From Start to 5.2% N2: 15 sec max
From start to light off: 20 sec max
From light off to idle: 60 sec max
101
Airstart Time Limits (From Lightoff to Idle)
Assisted: 90 sec
Windmilling: 180 sec
102
Max N2 starter re-engagement limit
Starter Cutout N2 (50%)
103
Engine GPU start Limitations
Max Temp: 250 C
Max Pressure: 50 PSI
Max Flow: 82 lb/min
104
Are the Thrust Reversers Authorized in flight?
No
105
Engine Oil Pressure Limits
Start: 0-240 PSI
Ground & Idle: 20-100 PSI
Above Idle: 36-100 PSI
106
Engine Max Transient Oil Pressure Limits
0-10 PSI: 20 sec
10&20 psi Engine Idle: 90 sec
10&36 psi Engine above Idle: 90 sec
100 & 220 psi: 90 sec
107
Engine Oil Temperature Limits
Maximum: 135 C
Minimum for Takeoff: 27 C
Minimum: 16 C
Transient for 90 sec: 143 C
Cold Start: -40 C
