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BeechJet Memory Items > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum tailwind component for takeoff and landing?

A

10 kts.

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2
Q

Load factor limits with flaps 10, 20, or 30 degrees?

A

0 to 2.0Gs

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3
Q

Load factor limits with flaps at 0 degrees?

A

-1.0 to +3.2Gs

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4
Q

What manuals are required to be on board?

A

The AFM
The POM
Pilot’s Checklist
AMS-5000 Pilot Guide

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5
Q

Vmcg for flaps settings 0, 10, and 20 degrees?

A

88 kts

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6
Q

Vmca flaps 0 degrees?

A

96 kts

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7
Q

Vmca flaps 10 and 20 degrees?

A

89 kts

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8
Q

Vmo S.L to 8,000’?

A

264 kts

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9
Q

Vmo 8,000’ to 11,000’?

A

264 kts to 320 kts (linear between altitudes)

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10
Q

Vmo 11,000’ to FL260?

A

320 kts

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11
Q

Mmo above FL260?

A

Mach 0.78

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12
Q

Vll (landing light)?

A

200 kts

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13
Q

Vww (windshield wiper)?

A

200 kts

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14
Q

Maximum demonstrated crosswind for takeoff and landing?

A

25 kts

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15
Q

Maximum tailwind for engine start?

A

No limit.

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16
Q

Maximum ZFW (Zero Fuel Weight)

A

13,000 lbs

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17
Q

Maximum landing weight?

A

15,700 lbs

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18
Q

Maximum takeoff weight (MTOW)?

A

16,100 lbs or 16,300 lbs with modification installed.

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19
Q

Maximum ramp weight?

A

16,300 lbs or 16,500 lbs with modification installed.

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20
Q

Ambient temperature limits for takeoff and landing?

A

-40C to ISA +35C

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21
Q

Ambient temperature for en route ops?

A

-65C to ISA +35C

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22
Q

Maximum airport pressure altitude for takeoff and landing?

A

10,000’ Pressure Altitude

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23
Q

Maximum operating altitude?

A

FL450

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24
Q

Per AFM, what items must be checked prior to every flight?

A

Trim
Stall warning
Speed brakes
Autopilot

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25
Q

Maximum capacity of Aft Baggage Compartment?

A

350 lbs

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26
Q

Maximum capacity of External Aft Baggage Compartment?

A

450 lbs

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27
Q

Minimum required flight crew?

A

1 pilot and 1 co-pilot

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28
Q

Authorized kinds of operations?

A 
Day
Night
VFR
IFR
Known icing conditions
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29
Q

Required number of Air Data Computers for takeoff?

A

Both

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30
Q

Which AHRS is required for autopilot operation?

A

Both

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31
Q

For which ILS approach category is the autopilot approved?

A

Category 1 ILS only

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32
Q

When must the autopilot preflight be conducted?

A

Prior to EACH FLIGHT on which the autopilot is to be used

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33
Q

Minimum battery voltage required prior to battery assisted engine start?

A

22 volts

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34
Q

A GPU is recommended for engine starts below what ambient temperature?

A

Approximately -15C

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35
Q

3 main sources of DC power?

A 
1 Lead-Acid Battery (24 VDC/40 Amps)
2 Generators (28 VDC/400 Amps)
1 GPU (28 VDC/1000 - 1500 Amps)
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36
Q

Sources of AC power?

A

2 inverters, each producing 26 VAC and 115 VAC

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37
Q

Maximum permitted generator load on the ground?

A

280 Amps each generator

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38
Q

Maximum generator load SL - FL410 with both generators operating?

A

280 Amps each generator

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39
Q

Maximum generator load above FL410 with both generators operating?

A

260 Amps each generator

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40
Q

Maximum generator load up to FL290 with one generator operating?

A

400 Amps

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41
Q

Maximum generator load up to FL290 with one generator operating in icing conditions?

A

440 Amps

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42
Q

Maximum generator load FL290 - FL410 with one generator operating?

A

280 Amps

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43
Q

Maximum generator load above FL410 with one generator operating?

A

260 Amps

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44
Q

Maximum transient generator load up to FL250?

A

525 Amps up to 30 seconds max

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45
Q

What 2 in-flight scenarios require the pilot to select the Master Generator switches to “EMER”?

A

Electrical smoke in the cockpit

Loss of both generators

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46
Q

Maximum generator load when doing a generator-assisted start?

A

Operating generator must be below 150 Amps before starting the other engine.

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47
Q

What minimum N2 must be manually maintained with the EFC system selected off?

A

46% N2.

Otherwise a potential exists for the generator to fall offline with the thrust lever at idle.

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48
Q

Starter time limits for GPU engine start?

A

30 seconds on, 5 minutes off
30 seconds on, 15 minutes off
30 seconds on, 60 minutes off

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49
Q

Max altitude for landing light extension?

A

FL200

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50
Q

What happens when the “ENG FIRE PUSH” switch is pressed?

A

Associated fuel SOV closes
Associated hydraulic SOV closes
Associated generator trips offline
Fire bottles are armed

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51
Q

Normal fire bottle pressure?

A

580 - 600 psi

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52
Q

When operating on emergency electrical power, is the fire DETECTION system available?

A

No

53
Q

When operating on emergency electrical power, is the fire PROTECTION system available?

A

Yes

54
Q

Vfe/Vfo for flaps 10 degrees / 20 degrees?

A

200 KIAS

55
Q

Vfe/Vfo for flaps 30 degrees?

A 
Vfe = 165 KIAS
Vfo = 170 KIAS
56
Q

Max altitude for flap extension?

A

FL200

57
Q

Van/Msb for speed brakes?

A

No limit

58
Q

Maximum flap setting with the speed brakes extended in flight?

A

10 degrees

59
Q

When must the rudder boost be operable and armed?

A

For all operations

60
Q

When must the yaw damp be turned OFF?

A

Takeoff and landing

61
Q

When must the yaw damp be turned ON?

A

Approach
Flight in icing conditions
Flight above FL280

62
Q

What are the max usable fuel quantities?

A

Wings: 2,862 lbs
Fuselage: 2,050 lbs
Total: 4,912 lbs

63
Q

What 3 components prevent the transfer pumps from overfilling the wing tanks?

A

Level Control Valve/Level Control Pilot Valve
Wing Overpressure Switch (3.5 psi)
Sniffle Valves (4 - 5 psi)

64
Q

Which boost pump must be operating to accomplish a successful fuel crossfeed?

A

Donor-Side Boost Pump (starve the heavy side)

65
Q

Maximum fuel imbalance for takeoff?

A

100 lbs

66
Q

Maximum fuel imbalance for en route and landing?

A

300 lbs

67
Q

Fuel temperature limits?

A

-40C to +50C

68
Q

Is takeoff permitted with partial wing fuel and fuel in the fuselage tanks?

A

No

69
Q

When will the boost pumps activate with the boost pump switches in AUTO?

A

Engine starting
Fuel crossfeed
Low fuel pressure
Low fuel feed quantity (77 lbs)

70
Q

When will the fuel transfer pumps activate with the transfer pump switches in AUTO?

A

Fuel in the mid fuselage tanks
AND
One generator on line

71
Q

What restrictions apply to the fuel crossfeed process?

A

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
Q

Normal pressure range of the hydraulic system?

A

Green arc (1,350 - 1,550 psi)

73
Q

Maximum hydraulic system pressure?

A

Red Line (1,850 psi)

74
Q

During preflight, how much hydraulic fluid should be seen in the reservoir sight gauge?

A

Any level of visible fluid

75
Q

When will the HYD LEVEL LO annunciator illiminate?

A

0.6 gallons or less

76
Q

Required type of hydraulic fluid?

A

MIL-H-5606

77
Q

Which components are hydraulically actuated?

A 
Landing gear
Flaps
Brakes
Speed brakes
Thrust reverser
78
Q

Vww (windshield wipers)?

A

200 KIAS

79
Q

In what position does the WING Anti-Ice solenoid valve fail when using emergency electrical power?

A

Fails closed

80
Q

In what position does the ENGINE Anti-Ice solenoid valve fail when using emergency electrical power?

A

Fails Open

81
Q

What ice protection systems must be selected OFF for takeoff?

A

Wing Anti-Ice

Horizontal Stab Heat

82
Q

Can engine anti-ice be on with ECS off?

A

No

83
Q

What limitations apply to windshield anti-ice?

A

Must be on (LOW or HIGH) for all in-flight operations

HIGH mode is prohibited for takeoff and landing

84
Q

When is anti-ice system operation prohibited?

A

At ram air temperatures greater than 10C, unless in actual icing conditions

85
Q

Engine power must be reduced below what N1 setting prior to turning on wing anti-ice?

A

90% N1

86
Q

During flight in icing conditions, what is the required delay after selecting flaps 10 before selecting flaps 30?

A

15 seconds

87
Q

During icing conditions, when is flaps 10 required for landing?

A

If icing conditions are encountered for more than 20 minutes after initial selection of flaps 10

88
Q

What does the flight crew need to do to ensure proper wing anti-ice operation?

A

Maintain the wing anti/deice operation light on (approximately 70% N2)

89
Q

When must engine anti-ice be turned on?

A 
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
Q

What’s the only approved flap setting when taking off with type 2, 3, or 4 deice fluid?

A

Flaps 10

91
Q

Vlo/Vle (landing gear)

A

200 KIAS

92
Q

Vlo for alternate gear extension?

A

150 KIAS

93
Q

Vtire (max tire speed)?

A

165 kts ground speed

94
Q

Maximum altitude for gear extension?

A

FL200

95
Q

What is used for emergency gear door retraction and emergency braking?

A

Nitrogen pressure

96
Q

When the engines are not running, the parking brake must be set from which side?

A

Left side

97
Q

At what cabin altitude will the passenger masks automatically deploy if armed?

A

12,500 +/- 500 ft

98
Q

Normal pressure range of O2 system?

A

Green arc (1,600 - 1,800 psi)

99
Q

Maximum cabin pressure differential?

A

9.1 PSI

100
Q

What would cause the green Overboard Discharge indicator to be missing?

A

Thermal Expansion (overpressure)

101
Q

When will the CABIN PRESS LO annunciator illuminate?

A

Cabin pressure reaches 9,500 +/- 500 ft

102
Q

What is the max pressure altitude with full DECREASE on the Manual Pressurization Controller?

A

14,000’ (altitude limit regulator 12,500 +/- 1,500’)

103
Q

Refrigeration air conditioning operation is prohibited…

A

Below 5C
During takeoff and landing
Above FL180
Horizontal stab deice ON

104
Q

Normal operating range for the cabin differential pressure?

A

Green arc (0 - 9.1 PSI)

105
Q

If the vent blower is used prior to engine start, then do not attempt to open the cabin door or emergency exit until…

A

Until the vent blows has been turned off for at least 45 seconds.

106
Q

What engine is installed in the BeechJet 400A?

A

Pratt & Whitney JT15D-5 or -5R

107
Q

Which oil is specified for use with the JT15D-5 engine?

A

Synthetic Oil Type 2

108
Q

Max N1?

A

Red line (104%)

109
Q

Max N2?

A

Red line (96%)

110
Q

Minimum engine idle speed IN ICING CONDITIONS with EFC on?

A

Bottom of green arc (52% N2)

111
Q

Minimum engine idle speed in NON-ICING conditions with EFC on?

A

Bottom of green arc (52% N2)

112
Q

Minimum engine idle speed in non-icing conditions with EFC off?

A

46% N2

113
Q

Max ITT when starting engines?

A

550 - 600C for 4 seconds max

600 - 700C for 2 seconds max

114
Q

Max ITT for takeoff?

A 
Red line (700C)
Limited to 5 minutes for both engines or 10 minutes for one engine
115
Q

Minimum oil pressure at idle power?

A

Bottom red line (40 psi)

116
Q

Max oil pressure?

A

Red line (83 psi)

117
Q

Normal oil pressure range at N2 above 60%?

A

Wide portion of green arc (60 - 83 psi)

118
Q

Minimum oil temperature for starting?

A

Bottom of yellow arc (-40C)

119
Q

Minimum oil temp before setting takeoff power?

A

Bottom of green arc (10C)

120
Q

Minimum oil temp when fuel does not have icing inhibitor?

A

10C

121
Q

Max oil temp?

A

Red line (121C)

122
Q

Max continuous ITT?

A

Top of green arc (680C)

123
Q

Is takeoff permitted with an EFC off?

A

No

124
Q

Minimum speed for using full reverse thrust?

A

55 KIAS

125
Q

Max time for continuous reverse thrust above reverse idle?

A

30 seconds

126
Q

Max time for reverse thrust at reverse idle during taxi operations?

A

5 seconds

127
Q

Thrust reverser limits other than deploy times and speeds?

A

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
Q

When is engine sync required to be off?

A

Takeoff
Approach
Landing
O.E.I. Operations

129
Q

5 conditions that must be met for the “tab data” values to be valid?

A 
Runway gradient is zero
No tailwind
ECS is on
Engine anti-ice is off
Anti-ice is on

BeechJet Memory Items (1 decks)

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