BE-350 Flashcards
(124 cards)
0
Q
Max takeoff weight
A
15,000 lbs
1
Q
Maximum ramp weight
A
15,100 lbs
2
Q
Max landing weight
A
15,000 lbs
3
Q
Max zero fuel weight
A
12,500 lbs
4
Q
Prohibited maneuvers
A
Acrobatic maneuvers, including spins
5
Q
Flaps up G limits
A
3.1 Positive, 1.24 negative
6
Q
Flaps down G limits
A
2.0 positive, 0 negative
7
Q
Maximum part 91 occupancy
A
15 passengers
8
Q
What is the restriction on aft-facing seats on takeoff and landing
A
The seatback and headrest of each occupied aft-facing seats must be in the full upright position.
9
Q
Max operating altitude
A
35,000 ft
10
Q
Max operating alt with yaw damper inoperative
A
5000 ft
11
Q
The yaw damp works. When does it need to be engaged by?
A
5000 ft
12
Q
Max altitude with either standby fuel pump inoperative
A
Flight is prohibited (sorry)
13
Q
Max altitude with no cross feed capability
A
20,000 ft
14
Q
Max operating air temp limits from sea level to 25,000 ft PA
A
ISA + 37 C
15
Q
Max operating air temp limits from above 25,000 ft PA
A
ISA + 31 C
16
Q
Minimum operating air temp limit
A
-53.9 C
17
Q
Maximum cabin pressure differential
A
6.6 psi
18
Q
Maneuvering speed
A
184 KIAS
19
Q
Approach flaps extension speed
A
202 KIAS
20
Q
Full flaps extension speed
A
158 KIAS
21
Q
Max Landing gear extension speed
A
184 KIAS
22
Q
Max Landing gear retraction speed
A
166 KIAS
23
Q
Max landing gear speed with gear fully extended
A
184 KIAS
24
Min control speed (Vmca) flaps up
94 KIAS
25
Min control speed (Vmca) flaps approach
93 KIAS
26
Max operating speed (SL to 21,000 ft)
263 KIAS
27
Max operating speed (21,000 to 35,000 ft)
263-194 / .58M
28
Max ITT for start
1000 C for 5 seconds maximum
29
Normal oil pressure for start
0-200 psi
30
Normal oil temp for start
-40 C minimum
31
Max ITT for idle
750 C for 5 seconds max
32
Idle N1
62% (min)
33
Idle prop RPM
1050 (min)
34
Idle oil pressure
60 psi (min)
35
Idle oil pressure
-40 to 110 C
36
Torque (takeoff and max continuous)*
100
*inadvertent excursions up to 102% is time limited to 7 minutes.
37
Max ITT (takeoff, max continuous, and max cruise)
820 C
38
Max N1 (takeoff max continuous, cruise climb, max cruise, and transient)
104%
39
Max prop RPM (takeoff, max continuous, cruise climb, max cruise)*
1700 RPM
| *Excursions up to 1735 are limited up to 7 minutes
40
Oil pressure range (all phases except for start, idle, and max reverse)*
0 to 110 psi
| *fluctuations +/- 10psi are acceptable
41
Max transient torque*
156%
| *time limited to 20 seconds
42
Max cruise climb ITT
785 C
43
Max reverse ITT
760 C
44
Max transient ITT*
850
| *time limited to 20 seconds
45
Max reverse prop RPM
1650
46
Max transient prop RPM*
1870
*time limited to 20 seconds
47
Max transient oil pressure
200 psi
48
Max reverse oil temp
0-99 C
49
When the prop RPM is below 1000psi, what is torque limited to?
62% N1
50
Oil pressure under 90 PSI is ________. Under emergency conditions, to complete a flight, a lower oil px of __ psi is permissible at power not exceeding __% torque.
Undesirable; 60psi, 62% N1
51
Min oil temp of __C recommended for few heater option at takeoff power.
55 C
52
Oil tank capacity per engine
Approx 14 quarts
53
Oil that can be drained per engine
Approx 11 quarts
54
What is the propeller type? 5 things
```
Constant-speed,
Full feathering,
Reversing
Counter-weighted
Hydraulically-actuated
```
55
Propeller RPM transient
1870 RPM for 20 seconds max
56
What does sustained prop order speed faster than 1700 RPM indicate?
Failure of the primary governor.
57
Flight with a failed primary governor can continue as long as...
Prop over speeds do no exceed 1768 RPM and torque doesn't exceed 96% N1. Sustained prop over speeds fastere than 1768 RPM are not approved.
58
When must prop autofeather be armed?
For takeoff, climb, and approach.
59
Emergency exits must be unlocked prior to _______.
Takeoff
60
Do not _____ power levers in flight.
Lift
61
Can the aircraft be towed with the control locks installed?
No
62
Do not tow the aircraft if one or more ____ ___ _____ are deflated.
Landing gear struts.
63
Fuel quantity yellow arc
0-265 lbs
64
Pneumatic pressure green arc range
12 to 20 psi
65
Vacuum gauge (normal from 35K to 15K ft)
2.8 to 4.3 inches HG
66
Vacuum gauge wide green arc (normal from 15K to Sea Level)
4,3 to 5.9 inches HG
67
Prop device ammeter normal range
26 to 32 amps
68
Max weight in baggage compartment
550 lbs
69
Max demonstrated crosswind
20 knots
70
Max tailwind component for takeoff and landing
10 knots
71
The MFD must be operational prior to _______.
Engine start
72
Minimum autopilot engage height after takeoff is ___
400 AGL
73
Minimum autopilot use height during cruise
1000 ft AGL
74
Minimum autopilot use height during approach
79 ft AGL
75
Minimum autopilot use height during steep approach
160 ft AGL
76
Yaw damper must not be used for ___________
Take off and landing
77
The terrain awareness and display must be inhibited by selecting _____ ______ when within __ NM of takeoff, approach, or landing at an airport not contained in the EGPWS airport database.
TERR INHIBIT; 15 NM
78
The area within the scan arc and within __ ft of the BE-350 operating weather radar can be dangerous. Do not operate in any moded other than STBY or TEST when a person in that range.
2 ft
79
External power unit voltage output.
28 to 28.4 VDC
80
External power unit amperage output
300 amps continuous
81
External power unit amp surge capability
1000 amp surge
82
Max generator load (sea level to 34000 ft)
100%
83
Max generator load (above 34,000 ft)
95%
84
62-70% N1 (Ground operations) max generator load
75%
85
70 to 100% N1 (Ground operations) max generator load
100%
86
Starter Limitation- standard start cycle
30 secs ON, 5 mins OFF
30 secs ON, 5 mins OFF
30 secs ON, 30 mins OFF
87
What phases of flights must the rudder boost be on for?
All phases of flight
88
When using recommended engine fuels, __ standby pump(s) is required for takeoff, but in such a case, cross feed of fuel _____ (will/will not) be available from the side of the inoperative standby fuel pump.
1 standby pump; will not
89
When is cross feed permitted?
Only when one engine is inoperative.
90
When is crossfeed capability for flight above 20,000 ft required?
When operating on emergency fuels.
91
In what order must you fuel up the gas tanks?
Mains full and then the auxiliary tanks
92
Lathing with low fuel pressure is limited to __ hours before overhaul of the __________ is required.
10; engine driven fuel pump
93
Maximum allowable fuel imbalance
300 lbs
94
Total usable fuel quantity
3611 lbs
95
Each main fuel tank capacity
1273 lbs
96
Each aux tank capacity
533 lbs
97
When should left and right anti-ice be on?
When in ambient temperatures of +5 C or below when flight free of visible moisture cannot be assured
98
Min temp for de-ice boots
-40 C
99
Do not operate the brake de-ice above what temp?
15 C
100
The cabin shall not be pressurized during what phases of flight?
Takeoff and landing
101
When should you not operate the electric heat (hint: it's not a temp limit)
When the pedestal floor outlet is blocked or the cockpit door is closed.
102
Landing gear cycle limits
1 up and 1 down cycle is limited to 1 every 5 minutes for a total of 6 cycles, followed by a 15 minute cool-down period
103
L/R OIL PRES LO annunciator
Indicates engine oil pressure is below 60 psi. Oil pressure between 60-90 is undesirable; tolerate only to the completion of the flight. Do not exceed 62% torque.
104
L/R CHIP DETECT light
Indicates possible metal contamination in the forward gear reduction case oil supply
105
L/R IGNITION ON light
Indicates the start switch is on and that the auto ignition system is armed and engine torque is below 17%
106
L/R PROP PITCH light
Designated prop is below the flight idle stop
107
PROP GND SOL
Indicates that the prop ground idle stop solenoid has failed. One or both props won't decrease to ground idle upon touchdown resulting in an increase in drag and possible yawing
108
L/R AUTOFEATHER light
Indicates that the designated autofeather is armed and power levers are above approx 90% N1
109
L/R GEN light
Designated generator is offline
110
L/R GEN TIE OPEN
Indicates that the designated bus is isolated from the center bus
111
MAN TIES CLOSE light
Indicates generator bus ties have been manually closed
112
BAT TIE OPEN light
Indicates that the battery is isolated from the gen buses
113
L/R FUEL PRESS LOW light
Indicates that fuel pressure is below approx 10 psi
114
L/R NO FUEL XFR light
Indicates motive flow pressure is lost while fuel remains in the aux tank on the same side.
115
FUEL CROSSFEED light
Indicates that the CROSSFEED valve is in the selected position
116
L/R FUEL QTY
Illumination indicates that the designated side has less than 30 minutes of fuel remaining at max continuous power
117
Illumination of a light in the gear handle means 1 of 5 things:
1. Landing gear in transit
2. One or more gear not down and locked
3. One or more gear not fully retracted
4. Gear up but power back below 84-86% N1
5. Gear up but flaps extended beyond approach
118
LDG/TAXI LIGHT annunciator on
Means that the gear is up but the taxi lights are still on
119
CABIN ALTITUDE light
Indicates that cabin altitude exceeds 10,000 ft
120
CABIN ALT HI (warning)
Indicates that cabin pressure altitude exceeds 12,000 ft
121
CABIN DIFF HI (warning)
Indicates cabin differentiate exceeds 6.9 psi
122
L/R BLEED FAIL warning light
Indicates melted or failed plastic bleed air failure warning line. They may also momentarily illuminate during simultaneous wing boot and brake de-ice operation at low N1 speed
123
DUCT OVERTEMP caution
Floor distribution air duct has reached 300 F
