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Aircraft > BE-350 > Flashcards

BE-350 Flashcards

0
Q

Max takeoff weight

A

15,000 lbs

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1
Q

Maximum ramp weight

A

15,100 lbs

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2
Q

Max landing weight

A

15,000 lbs

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3
Q

Max zero fuel weight

A

12,500 lbs

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4
Q

Prohibited maneuvers

A

Acrobatic maneuvers, including spins

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5
Q

Flaps up G limits

A

3.1 Positive, 1.24 negative

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6
Q

Flaps down G limits

A

2.0 positive, 0 negative

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7
Q

Maximum part 91 occupancy

A

15 passengers

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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.

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9
Q

Max operating altitude

A

35,000 ft

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10
Q

Max operating alt with yaw damper inoperative

A

5000 ft

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11
Q

The yaw damp works. When does it need to be engaged by?

A

5000 ft

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12
Q

Max altitude with either standby fuel pump inoperative

A

Flight is prohibited (sorry)

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13
Q

Max altitude with no cross feed capability

A

20,000 ft

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14
Q

Max operating air temp limits from sea level to 25,000 ft PA

A

ISA + 37 C

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15
Q

Max operating air temp limits from above 25,000 ft PA

A

ISA + 31 C

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16
Q

Minimum operating air temp limit

A

-53.9 C

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17
Q

Maximum cabin pressure differential

A

6.6 psi

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18
Q

Maneuvering speed

A

184 KIAS

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19
Q

Approach flaps extension speed

A

202 KIAS

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20
Q

Full flaps extension speed

A

158 KIAS

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21
Q

Max Landing gear extension speed

A

184 KIAS

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22
Q

Max Landing gear retraction speed

A

166 KIAS

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23
Q

Max landing gear speed with gear fully extended

A

184 KIAS

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24
Q

Min control speed (Vmca) flaps up

A

94 KIAS

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25
Q

Min control speed (Vmca) flaps approach

A

93 KIAS

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26
Q

Max operating speed (SL to 21,000 ft)

A

263 KIAS

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27
Q

Max operating speed (21,000 to 35,000 ft)

A

263-194 / .58M

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28
Q

Max ITT for start

A

1000 C for 5 seconds maximum

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29
Q

Normal oil pressure for start

A

0-200 psi

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30
Q

Normal oil temp for start

A

-40 C minimum

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31
Q

Max ITT for idle

A

750 C for 5 seconds max

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32
Q

Idle N1

A

62% (min)

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33
Q

Idle prop RPM

A

1050 (min)

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34
Q

Idle oil pressure

A

60 psi (min)

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35
Q

Idle oil pressure

A

-40 to 110 C

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36
Q

Torque (takeoff and max continuous)*

A

100

*inadvertent excursions up to 102% is time limited to 7 minutes.

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37
Q

Max ITT (takeoff, max continuous, and max cruise)

A

820 C

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38
Q

Max N1 (takeoff max continuous, cruise climb, max cruise, and transient)

A

104%

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39
Q

Max prop RPM (takeoff, max continuous, cruise climb, max cruise)*

A

1700 RPM

*Excursions up to 1735 are limited up to 7 minutes

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40
Q

Oil pressure range (all phases except for start, idle, and max reverse)*

A

0 to 110 psi

*fluctuations +/- 10psi are acceptable

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41
Q

Max transient torque*

A

156%

*time limited to 20 seconds

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42
Q

Max cruise climb ITT

A

785 C

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43
Q

Max reverse ITT

A

760 C

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44
Q

Max transient ITT*

A

850

*time limited to 20 seconds

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45
Q

Max reverse prop RPM

A

1650

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46
Q

Max transient prop RPM*

A

1870

*time limited to 20 seconds

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47
Q

Max transient oil pressure

A

200 psi

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48
Q

Max reverse oil temp

A

0-99 C

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49
Q

When the prop RPM is below 1000psi, what is torque limited to?

A

62% N1

50
Q

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.

A

Undesirable; 60psi, 62% N1

51
Q

Min oil temp of __C recommended for few heater option at takeoff power.

A

55 C

52
Q

Oil tank capacity per engine

A

Approx 14 quarts

53
Q

Oil that can be drained per engine

A

Approx 11 quarts

54
Q

What is the propeller type? 5 things

A 
Constant-speed, 
Full feathering,
Reversing
Counter-weighted
Hydraulically-actuated
55
Q

Propeller RPM transient

A

1870 RPM for 20 seconds max

56
Q

What does sustained prop order speed faster than 1700 RPM indicate?

A

Failure of the primary governor.

57
Q

Flight with a failed primary governor can continue as long as…

A

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
Q

When must prop autofeather be armed?

A

For takeoff, climb, and approach.

59
Q

Emergency exits must be unlocked prior to _______.

A

Takeoff

60
Q

Do not _____ power levers in flight.

A

Lift

61
Q

Can the aircraft be towed with the control locks installed?

A

No

62
Q

Do not tow the aircraft if one or more ____ ___ _____ are deflated.

A

Landing gear struts.

63
Q

Fuel quantity yellow arc

A

0-265 lbs

64
Q

Pneumatic pressure green arc range

A

12 to 20 psi

65
Q

Vacuum gauge (normal from 35K to 15K ft)

A

2.8 to 4.3 inches HG

66
Q

Vacuum gauge wide green arc (normal from 15K to Sea Level)

A

4,3 to 5.9 inches HG

67
Q

Prop device ammeter normal range

A

26 to 32 amps

68
Q

Max weight in baggage compartment

A

550 lbs

69
Q

Max demonstrated crosswind

A

20 knots

70
Q

Max tailwind component for takeoff and landing

A

10 knots

71
Q

The MFD must be operational prior to _______.

A

Engine start

72
Q

Minimum autopilot engage height after takeoff is ___

A

400 AGL

73
Q

Minimum autopilot use height during cruise

A

1000 ft AGL

74
Q

Minimum autopilot use height during approach

A

79 ft AGL

75
Q

Minimum autopilot use height during steep approach

A

160 ft AGL

76
Q

Yaw damper must not be used for ___________

A

Take off and landing

77
Q

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.

A

TERR INHIBIT; 15 NM

78
Q

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.

A

2 ft

79
Q

External power unit voltage output.

A

28 to 28.4 VDC

80
Q

External power unit amperage output

A

300 amps continuous

81
Q

External power unit amp surge capability

A

1000 amp surge

82
Q

Max generator load (sea level to 34000 ft)

A

100%

83
Q

Max generator load (above 34,000 ft)

A

95%

84
Q

62-70% N1 (Ground operations) max generator load

A

75%

85
Q

70 to 100% N1 (Ground operations) max generator load

A

100%

86
Q

Starter Limitation- standard start cycle

A

30 secs ON, 5 mins OFF
30 secs ON, 5 mins OFF
30 secs ON, 30 mins OFF

87
Q

What phases of flights must the rudder boost be on for?

A

All phases of flight

88
Q

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.

A

1 standby pump; will not

89
Q

When is cross feed permitted?

A

Only when one engine is inoperative.

90
Q

When is crossfeed capability for flight above 20,000 ft required?

A

When operating on emergency fuels.

91
Q

In what order must you fuel up the gas tanks?

A

Mains full and then the auxiliary tanks

92
Q

Lathing with low fuel pressure is limited to __ hours before overhaul of the __________ is required.

A

10; engine driven fuel pump

93
Q

Maximum allowable fuel imbalance

A

300 lbs

94
Q

Total usable fuel quantity

A

3611 lbs

95
Q

Each main fuel tank capacity

A

1273 lbs

96
Q

Each aux tank capacity

A

533 lbs

97
Q

When should left and right anti-ice be on?

A

When in ambient temperatures of +5 C or below when flight free of visible moisture cannot be assured

98
Q

Min temp for de-ice boots

A

-40 C

99
Q

Do not operate the brake de-ice above what temp?

A

15 C

100
Q

The cabin shall not be pressurized during what phases of flight?

A

Takeoff and landing

101
Q

When should you not operate the electric heat (hint: it’s not a temp limit)

A

When the pedestal floor outlet is blocked or the cockpit door is closed.

102
Q

Landing gear cycle limits

A

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
Q

L/R OIL PRES LO annunciator

A

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
Q

L/R CHIP DETECT light

A

Indicates possible metal contamination in the forward gear reduction case oil supply

105
Q

L/R IGNITION ON light

A

Indicates the start switch is on and that the auto ignition system is armed and engine torque is below 17%

106
Q

L/R PROP PITCH light

A

Designated prop is below the flight idle stop

107
Q

PROP GND SOL

A

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
Q

L/R AUTOFEATHER light

A

Indicates that the designated autofeather is armed and power levers are above approx 90% N1

109
Q

L/R GEN light

A

Designated generator is offline

110
Q

L/R GEN TIE OPEN

A

Indicates that the designated bus is isolated from the center bus

111
Q

MAN TIES CLOSE light

A

Indicates generator bus ties have been manually closed

112
Q

BAT TIE OPEN light

A

Indicates that the battery is isolated from the gen buses

113
Q

L/R FUEL PRESS LOW light

A

Indicates that fuel pressure is below approx 10 psi

114
Q

L/R NO FUEL XFR light

A

Indicates motive flow pressure is lost while fuel remains in the aux tank on the same side.

115
Q

FUEL CROSSFEED light

A

Indicates that the CROSSFEED valve is in the selected position

116
Q

L/R FUEL QTY

A

Illumination indicates that the designated side has less than 30 minutes of fuel remaining at max continuous power

117
Q

Illumination of a light in the gear handle means 1 of 5 things:

A
  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
Q

LDG/TAXI LIGHT annunciator on

A

Means that the gear is up but the taxi lights are still on

119
Q

CABIN ALTITUDE light

A

Indicates that cabin altitude exceeds 10,000 ft

120
Q

CABIN ALT HI (warning)

A

Indicates that cabin pressure altitude exceeds 12,000 ft

121
Q

CABIN DIFF HI (warning)

A

Indicates cabin differentiate exceeds 6.9 psi

122
Q

L/R BLEED FAIL warning light

A

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
Q

DUCT OVERTEMP caution

A

Floor distribution air duct has reached 300 F

Aircraft (1 decks)

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