Limitations Flashcards
1
Q
Maximum tailwind component for takeoff and landing?
A
10 kts.
2
Q
Load factor limits with flaps 10, 20, or 30 degrees?
A
0 to 2.0Gs
3
Q
Load factor limits with flaps at 0 degrees?
A
-1.0 to +3.2Gs
4
Q
What manuals are required to be on board?
A
The AFM
The POM
Pilot’s Checklist
AMS-5000 Pilot Guide
5
Q
Vmcg for flaps settings 0, 10, and 20 degrees?
A
88 kts
6
Q
Vmca flaps 0 degrees?
A
96 kts
7
Q
Vmca flaps 10 and 20 degrees?
A
89 kts
8
Q
Vmo S.L to 8,000’?
A
264 kts
9
Q
Vmo 8,000’ to 11,000’?
A
264 kts to 320 kts (linear between altitudes)
10
Q
Vmo 11,000’ to FL260?
A
320 kts
11
Q
Mmo above FL260?
A
Mach 0.78
12
Q
Vll (landing light)?
A
200 kts
13
Q
Vww (windshield wiper)?
A
200 kts
14
Q
Maximum demonstrated crosswind for takeoff and landing?
A
25 kts
15
Q
Maximum tailwind for engine start?
A
No limit.
16
Q
Maximum ZFW (Zero Fuel Weight)
A
13,000 lbs
17
Q
Maximum landing weight?
A
15,700 lbs
18
Q
Maximum takeoff weight (MTOW)?
A
16,100 lbs or 16,300 lbs with modification installed.
19
Q
Maximum ramp weight?
A
16,300 lbs or 16,500 lbs with modification installed.
20
Q
Ambient temperature limits for takeoff and landing?
A
-40C to ISA +35C
21
Q
Ambient temperature for en route ops?
A
-65C to ISA +35C
22
Q
Maximum airport pressure altitude for takeoff and landing?
A
10,000’ Pressure Altitude
23
Q
Maximum operating altitude?
A
FL450
24
Q
Per AFM, what items must be checked prior to every flight?
A
Trim
Stall warning
Speed brakes
Autopilot
25
Maximum capacity of Aft Baggage Compartment?
350 lbs
26
Maximum capacity of External Aft Baggage Compartment?
450 lbs
27
Minimum required flight crew?
1 pilot and 1 co-pilot
28
Authorized kinds of operations?
```
Day
Night
VFR
IFR
Known icing conditions
```
29
Required number of Air Data Computers for takeoff?
Both
30
Which AHRS is required for autopilot operation?
Both
31
For which ILS approach category is the autopilot approved?
Category 1 ILS only
32
When must the autopilot preflight be conducted?
Prior to EACH FLIGHT on which the autopilot is to be used
33
Minimum battery voltage required prior to battery assisted engine start?
22 volts
34
A GPU is recommended for engine starts below what ambient temperature?
Approximately -15C
35
3 main sources of DC power?
```
1 Lead-Acid Battery (24 VDC/40 Amps)
2 Generators (28 VDC/400 Amps)
1 GPU (28 VDC/1000 - 1500 Amps)
```
36
Sources of AC power?
2 inverters, each producing 26 VAC and 115 VAC
37
Maximum permitted generator load on the ground?
280 Amps each generator
38
Maximum generator load SL - FL410 with both generators operating?
280 Amps each generator
39
Maximum generator load above FL410 with both generators operating?
260 Amps each generator
40
Maximum generator load up to FL290 with one generator operating?
400 Amps
41
Maximum generator load up to FL290 with one generator operating in icing conditions?
440 Amps
42
Maximum generator load FL290 - FL410 with one generator operating?
280 Amps
43
Maximum generator load above FL410 with one generator operating?
260 Amps
44
Maximum transient generator load up to FL250?
525 Amps up to 30 seconds max
45
What 2 in-flight scenarios require the pilot to select the Master Generator switches to “EMER”?
Electrical smoke in the cockpit
| Loss of both generators
46
Maximum generator load when doing a generator-assisted start?
Operating generator must be below 150 Amps before starting the other engine.
47
What minimum N2 must be manually maintained with the EFC system selected off?
46% N2.
| Otherwise a potential exists for the generator to fall offline with the thrust lever at idle.
48
Starter time limits for GPU engine start?
30 seconds on, 5 minutes off
30 seconds on, 15 minutes off
30 seconds on, 60 minutes off
49
Max altitude for landing light extension?
FL200
50
What happens when the “ENG FIRE PUSH” switch is pressed?
Associated fuel SOV closes
Associated hydraulic SOV closes
Associated generator trips offline
Fire bottles are armed
51
Normal fire bottle pressure?
580 - 600 psi
52
When operating on emergency electrical power, is the fire DETECTION system available?
No
53
When operating on emergency electrical power, is the fire PROTECTION system available?
Yes
54
Vfe/Vfo for flaps 10 degrees / 20 degrees?
200 KIAS
55
Vfe/Vfo for flaps 30 degrees?
```
Vfe = 165 KIAS
Vfo = 170 KIAS
```
56
Max altitude for flap extension?
FL200
57
Van/Msb for speed brakes?
No limit
58
Maximum flap setting with the speed brakes extended in flight?
10 degrees
59
When must the rudder boost be operable and armed?
For all operations
60
When must the yaw damp be turned OFF?
Takeoff and landing
61
When must the yaw damp be turned ON?
Approach
Flight in icing conditions
Flight above FL280
62
What are the max usable fuel quantities?
Wings: 2,862 lbs
Fuselage: 2,050 lbs
Total: 4,912 lbs
63
What 3 components prevent the transfer pumps from overfilling the wing tanks?
Level Control Valve/Level Control Pilot Valve
Wing Overpressure Switch (3.5 psi)
Sniffle Valves (4 - 5 psi)
64
Which boost pump must be operating to accomplish a successful fuel crossfeed?
Donor-Side Boost Pump (starve the heavy side)
65
Maximum fuel imbalance for takeoff?
100 lbs
66
Maximum fuel imbalance for en route and landing?
300 lbs
67
Fuel temperature limits?
-40C to +50C
68
Is takeoff permitted with partial wing fuel and fuel in the fuselage tanks?
No
69
When will the boost pumps activate with the boost pump switches in AUTO?
Engine starting
Fuel crossfeed
Low fuel pressure
Low fuel feed quantity (77 lbs)
70
When will the fuel transfer pumps activate with the transfer pump switches in AUTO?
Fuel in the mid fuselage tanks
AND
One generator on line
71
What restrictions apply to the fuel crossfeed process?
Crossfeed w/ both engines operating is limited to level flight when less than 600 lbs remains in the supplying tank
Must be selected “NORM” for takeoff and landing
72
Normal pressure range of the hydraulic system?
Green arc (1,350 - 1,550 psi)
73
Maximum hydraulic system pressure?
Red Line (1,850 psi)
74
During preflight, how much hydraulic fluid should be seen in the reservoir sight gauge?
Any level of visible fluid
75
When will the HYD LEVEL LO annunciator illiminate?
0.6 gallons or less
76
Required type of hydraulic fluid?
MIL-H-5606
77
Which components are hydraulically actuated?
```
Landing gear
Flaps
Brakes
Speed brakes
Thrust reverser
```
78
Vww (windshield wipers)?
200 KIAS
79
In what position does the WING Anti-Ice solenoid valve fail when using emergency electrical power?
Fails closed
80
In what position does the ENGINE Anti-Ice solenoid valve fail when using emergency electrical power?
Fails Open
81
What ice protection systems must be selected OFF for takeoff?
Wing Anti-Ice
| Horizontal Stab Heat
82
Can engine anti-ice be on with ECS off?
No
83
What limitations apply to windshield anti-ice?
Must be on (LOW or HIGH) for all in-flight operations
| HIGH mode is prohibited for takeoff and landing
84
When is anti-ice system operation prohibited?
At ram air temperatures greater than 10C, unless in actual icing conditions
85
Engine power must be reduced below what N1 setting prior to turning on wing anti-ice?
90% N1
86
During flight in icing conditions, what is the required delay after selecting flaps 10 before selecting flaps 30?
15 seconds
87
During icing conditions, when is flaps 10 required for landing?
If icing conditions are encountered for more than 20 minutes after initial selection of flaps 10
88
What does the flight crew need to do to ensure proper wing anti-ice operation?
Maintain the wing anti/deice operation light on (approximately 70% N2)
89
When must engine anti-ice be turned on?
```
On Ground:
In visible moisture 5C or colder
In flight
Illumination of ICING annunciator
Airframe ice accumulation
In visible moisture and ram air temp 10C or less
```
90
What’s the only approved flap setting when taking off with type 2, 3, or 4 deice fluid?
Flaps 10
91
Vlo/Vle (landing gear)
200 KIAS
92
Vlo for alternate gear extension?
150 KIAS
93
Vtire (max tire speed)?
165 kts ground speed
94
Maximum altitude for gear extension?
FL200
95
What is used for emergency gear door retraction and emergency braking?
Nitrogen pressure
96
When the engines are not running, the parking brake must be set from which side?
Left side
97
At what cabin altitude will the passenger masks automatically deploy if armed?
12,500 +/- 500 ft
98
Normal pressure range of O2 system?
Green arc (1,600 - 1,800 psi)
99
Maximum cabin pressure differential?
9.1 PSI
100
What would cause the green Overboard Discharge indicator to be missing?
Thermal Expansion (overpressure)
101
When will the CABIN PRESS LO annunciator illuminate?
Cabin pressure reaches 9,500 +/- 500 ft
102
What is the max pressure altitude with full DECREASE on the Manual Pressurization Controller?
14,000’ (altitude limit regulator 12,500 +/- 1,500’)
103
Refrigeration air conditioning operation is prohibited...
Below 5C
During takeoff and landing
Above FL180
Horizontal stab deice ON
104
Normal operating range for the cabin differential pressure?
Green arc (0 - 9.1 PSI)
105
If the vent blower is used prior to engine start, then do not attempt to open the cabin door or emergency exit until...
Until the vent blows has been turned off for at least 45 seconds.
106
What engine is installed in the BeechJet 400A?
Pratt & Whitney JT15D-5 or -5R
107
Which oil is specified for use with the JT15D-5 engine?
Synthetic Oil Type 2
108
Max N1?
Red line (104%)
109
Max N2?
Red line (96%)
110
Minimum engine idle speed IN ICING CONDITIONS with EFC on?
Bottom of green arc (52% N2)
111
Minimum engine idle speed in NON-ICING conditions with EFC on?
Bottom of green arc (52% N2)
112
Minimum engine idle speed in non-icing conditions with EFC off?
46% N2
113
Max ITT when starting engines?
550 - 600C for 4 seconds max
| 600 - 700C for 2 seconds max
114
Max ITT for takeoff?
```
Red line (700C)
Limited to 5 minutes for both engines or 10 minutes for one engine
```
115
Minimum oil pressure at idle power?
Bottom red line (40 psi)
116
Max oil pressure?
Red line (83 psi)
117
Normal oil pressure range at N2 above 60%?
Wide portion of green arc (60 - 83 psi)
118
Minimum oil temperature for starting?
Bottom of yellow arc (-40C)
119
Minimum oil temp before setting takeoff power?
Bottom of green arc (10C)
120
Minimum oil temp when fuel does not have icing inhibitor?
10C
121
Max oil temp?
Red line (121C)
122
Max continuous ITT?
Top of green arc (680C)
123
Is takeoff permitted with an EFC off?
No
124
Minimum speed for using full reverse thrust?
55 KIAS
125
Max time for continuous reverse thrust above reverse idle?
30 seconds
126
Max time for reverse thrust at reverse idle during taxi operations?
5 seconds
127
Thrust reverser limits other than deploy times and speeds?
Ground use only
Cannot be used to back airplane
Do not attempt engine start with TR deployed
Re-stow envelope — FL300 or below and 135 KIAS or below
128
When is engine sync required to be off?
Takeoff
Approach
Landing
O.E.I. Operations
129
5 conditions that must be met for the “tab data” values to be valid?
```
Runway gradient is zero
No tailwind
ECS is on
Engine anti-ice is off
Anti-ice is on
```
