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Aircraft limitations > G 280 > Flashcards

G 280 Flashcards

0
Q

How many Vortex Generators are on the wings

A

42 per wing

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1
Q

Tail Height

A

22 feet

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2
Q

What is the wing sweep?

A

27 degrees

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3
Q

Tiller and Pedal steering angles

A

60 degrees/3 degrees

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4
Q

How many vortex generators are on the horizontal stabilizer

A

20

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5
Q

Max Ramp Weight

A

39,750

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6
Q

Max Takeoff Weight

A

39,600

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7
Q

Max Landing Weight

A

32,700

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8
Q

Max Zero Fuel Weight

A

28,200

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9
Q

Max Cargo Weight

A

1,980

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10
Q

Max Cargo Floor Loading

A

120 lbs. / sq. foot

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11
Q

Gear Up Landing Fuel

A

1,000 lbs. max

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12
Q

Elevator Disconnect Force

A

95 lbs.

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13
Q

Manual Elevator Forces

A

150 lbs.

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14
Q

Max Fuel Capacity

A

14,600 lbs.

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15
Q

Fuel Capacity Forward Center Tank

A

1,600 lbs. / 13,000 lbs remaining

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16
Q

Fuel Capacity Aft Center Tank

A

1,100 lbs. / 12,000 lbs remaining

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17
Q

Fuel Quantity Center Tank

A

2,130 lbs. / 9,900 lbs remaining

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18
Q

Fuel Capacity Wing Tanks

A

4,350 lbs per wing / 530 lbs remaining per wing

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19
Q

Fuel Capacity Feeder Tank

A

530 lbs per wing / 0 remaining

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20
Q

Max Fuel Imbalance Take off

A

450 lbs.

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21
Q

Max Fuel Imbalance Flight

A

900 lbs.

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22
Q

Fuel Jettison Flow Rate

A

5,500 lbs./hr

100 lbs./min

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23
Q

Fuel Jettison Auto-Stop

A

800 lbs./ wing

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24
Q

L-R Fuel Level Low

A

580 lbs. or less

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25
Q

L, R Feed Fuel Low

A

280 lbs/ side

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26
Q

Fuel XFlow Rate

A

3500 pph

300 lbs./ 5 min.

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27
Q

L-R Feed Fuel LVL Low

A

280 lbs or less on both sides

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28
Q

Max Operating Altitude

A

45,000 ft.

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29
Q

APU Operating Altitude

A

40,000 ft.

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30
Q

Max Approved O2 mask usage

A

40,000

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31
Q

Interior Baggage Access Limit Altitude

A

40,000 ft. And above

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32
Q

EMP Operating Altitude < 10 min. limitation

A

39,000 ft.

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33
Q

APU Max Starting Altitude

A

35,000 ft.

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34
Q

Altitude above which cruise performance is effected by Anti-Ice

A

35,000 ft.

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35
Q

Yaw Damp Inop Limit Altitude

A

25,000 ft.

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36
Q

Max Prolonged O2 Use Altitude

A

25,000 ft.

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37
Q

Waste Water Vacuum Generator Altitudes

A

16,000 ft. and below

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38
Q

O2 Mask Drop Altitude in AUTO Mode

A

13,500/14,750 (+- 250 ft.)

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39
Q

Cabin Altitude High CAS Message

A

10,000/14,750 ft.

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40
Q

Min. OMS Usage Altitude

A

10,000 ft.

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41
Q

CPCS High Elevation Mode LFE

A

8,000 ft.

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42
Q

Minimum Altitude

A

-1,400 ft.

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43
Q

Va

0-20,000ft

A

215-225 KIAS

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44
Q

Va

20,000-35,000

A

225-264 KIAS

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45
Q

Va

35,000-39,000

A

264 KIAS

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46
Q

Va

39,000-45,000

A

.80 M

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47
Q

Thrust Reverse to Idle Speed

A

40 KIAS

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48
Q

Vmcg

A

95 KIAS

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49
Q

Vmca

A

98 KIAS

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50
Q

Vmcl

A

98 KIAS

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51
Q

Emergency Vle

A

175 KIAS

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52
Q

Flaps LND Speed

A

180 KIAS

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53
Q

Nose Tire Speed

A

182 KIAS

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54
Q

Main Tire Speed

A

195 KIAS

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55
Q

Vle

A

195 KIAS

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56
Q

Vlo

A

195 KIAS

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57
Q

Maximum Thrust Reverse Deploy Speed

A

200 KIAS

58
Q

Flaps 20 Speed

A

220 KIAS

59
Q

Flaps 10 Speed

A

250 KIAS

60
Q

YD Inop Max Speed

A

250 KIAS

61
Q

Mach Trim Inop Max Speed

A

340 KIAS/.77M

62
Q

When does the Seatbelt/No Smoking illuminate in AUTO?

A

Nose Uplock Open

63
Q

When does the beacon come on automatically?

A

When batteries are discharging

64
Q

What is the maximum capacity of occupants allowed per the AFM?

A

19 or the limitation from you seating configuration.

65
Q

What is the maximum slope approved for takeoff?

A

2% uphill or downhill

66
Q

What is the maximum tail wind component approved to take off and landing?

A

10 kts.

67
Q

What is the maximum demonstrated crosswind for take off and landing?

A

25 kts

68
Q

When is auto speed prohibited?

A

When gear and flaps extended.

69
Q

What is the highest elevation for an airport for takeoff or landing?

A

10,000 ft.

70
Q

What is the coldest temperature for the aircraft on the ground?

A

More than 10 hours at -20 degree C temps require use of cold weather operations chart.

71
Q

What is the maximum temperature on the ground?

A

ISA+35

72
Q

What is the maximum altitude with gear or flaps extended?

A

20,000 ft.

73
Q

What is the minimum holding speed in icing conditions?

A

185 KIAS

74
Q

What are the acceptable maneuvering flight loads?

A

Flaps up: -1.0 - 2.6

Flaps down: 0 - 2.0

75
Q

What is the maximum cabin differential?

A

9.2 psi

Max for taxi, takeoff, and landing is 0.2 psi

76
Q

At what altitude must the internal baggage door be closed?

A

40,000 except for emergencies.

77
Q

When is the ECS HI flow mode allowed to be on?

A

On the ground with the APU as the bleed source.

78
Q

What is the minimum height to engage the autopilot?

A

200 ft.

79
Q

What is the minimum disengage height for the autopilot from an ILS approach?

A

80 ft.

80
Q

What is the minimum height to disengage the autopilot from an LNAV/VNAV and LPV approach?

A

80 ft.

81
Q

What is the maximum demonstrated altitude loss for a coupled go-around?

A

61 ft.

82
Q

Are CAT II operations approved for single engine operations?

A

No

83
Q

What is the maximum load for generator output?

A

100%

84
Q

What is the minimum battery voltage SAT above and below 0?

A

Above 0: 23.5 Vdc

Below 0: 22.5 Vdc

85
Q

Who must confirm the flap setting before takeoff?

A

Both pilots

86
Q

What are the minimum and maximum temperatures for Jet A fuel?

A

-36 - 57 degrees C

87
Q

What is the pre-charge pressure on the brake accumulators?

A

700 +-30 psi

88
Q

What is the pre-charge pressure for the emergency gear bottle?

A

2600-3000 psi

89
Q

What is the normal operations pressure for the hydraulic system?

A

2700-3250 psi

90
Q

What is the maximum hydraulic pressure limit?

A

3500 psi

91
Q

What is the maximum hydraulic temperature limit?

A

95 degrees C

92
Q

What is the recommended temperature range to use wing anti-ice?

A

10- -40 degrees C TAT

93
Q

What is the limitation for Wing Anti-Ice?

A

Auto mode is prohibited and both selectors must be turned on within 1 second of each other.

94
Q

Must wing anti-ice be on for take off into anticipated icing conditions?

A

Yes

95
Q

When is the use of flaps restricted?

A

In icing conditions except for takeoff, approach, and landing.

96
Q

Holding in icing conditions?

A

Limited to flaps 0

97
Q

When can you use the CAS aural inhibit?

A

Only when directed by the checklist.

98
Q

When must you use the terrain inhibit switch?

A

When the airport has no published instrument approach
The longest runway is less than 3500 ft.
The airport is not in the database
QFE altimeter setting are used for approach and landing on a subsequent takeoff without the available geometric altitude.

99
Q

When can you selected APPR mode during an ILS?

A

With 60 degrees of the approach course.

100
Q

What checklists are approved for electronic use?

A

Normal checklist only

101
Q

What altitude are crew and passenger O2 masks approved for?

A

Altitudes up to 40,000 ft.

102
Q

What altitude is use of the OMS limited to?

A

Above 10,000 ft.

103
Q

Can you dispatch with an AMBER CAS?

A

Not normally, consult the MEL.

104
Q

How long must you allow the APU to cool down before another start cycle?

A

2 minutes.

After 3 starts, allow 30 minutes to cool down.

105
Q

What else must be operative to run the APU.

A

Right standby fuel pump or right engine.

106
Q

Can you run the APU during ground de-icing?

A

No, APU must be off with the door closed.

107
Q

What is the maximum altitude to use APU bleed air?

A

20,000 ft.

108
Q

What is the maximum APU EGT while running?

A

718 degrees C

109
Q

What is the maximum APU EGT while using bleed air?

A

666 degrees C

110
Q

What is the maximum transient APU EGT for starting?

A

Below 50%, 974 degrees C

111
Q

What is the maximum APU rotor speed?

A

108%

112
Q

What is the engine model and type?

A

Honeywell HTF7250G

113
Q

What is the maximum continous thrust?

A

7240 lbs

114
Q

What is the maximum takeoff rated thrust per engine?

A

7624 lbs

115
Q

What is the maximum crosswind component for engine start?

A

20 kts.

116
Q

What is the maximum tailwind component for engine start?

A

15 kts.

117
Q

What is the Max ITT during start?

N2 above and below 40%

A

Below 40% - 650 degrees C

Above 40% - 928 degrees C

118
Q

N1 tailwind limitation on the ground?

A

N1 is limited to 50% if tailwind component is more than 15 kts.

119
Q

What is the limitation on when you can motor an engine after shutdown, for cooling?

A

Must begin motoring within 3 minutes of engine shutdown.

120
Q

Max Continuous Limits?

N1, N2, ITT

A

N1: 96.5%
N2: 98%
ITT: 928 C

121
Q

Max Takeoff Limits?

N1, N2, ITT

A

N1: 96.8%
N2: 98%
ITT: 928

122
Q

Max APR limits?

N1, N2, ITT

A

N1: 96.8%
N2: 98.5%
ITT: 946 C

123
Q

Max Transient limit?

N1, N2

A

N1: 98%
N2: 99.9%

124
Q

How long is takeoff thrust limited to?

A

5 minutes

125
Q

How long is APR thrust limited to?

A

10 minutes

126
Q

Minimum temperature of fuel at the fuel filter?

A

3 C

127
Q

What are the acceptable fuel types?

A

Jet A, Jet A1

128
Q

At what speed must thrust reversers be at idle?

A

40 kts.

129
Q

Are thrust reversers approved to power back?

A

No

130
Q

What is the minimum engine oil temperature for engine start?

A

-40 C

131
Q

What is the minimum oil temperature for continuous ground operations above idle?

A

5 C

132
Q

What is the maximum oil temperature and transient limit?

A

138 C max

154 C not to exceed 2 minutes

133
Q

What is the starter duty cycle?

A

3 consecutive starts followed by a 15 minute cooling period

134
Q

What is the engine motoring limit?

A

Maximum of 5 minutes followed by 15 minute cooling period

135
Q

Turbulence Penetration Speed

SL-13,000

A

230 KIAS

136
Q

Turbulence Penetration Speed

13,000-20,000

A

250 KIAS

137
Q

Turbulence Penetration Speed

20,000-35,000

A

270 KIAS

138
Q

Turbulence Penetration Speed

35,000-45,000

A

.80 M

139
Q

Vmo

SL-10,000

A

300 KCAS

140
Q

Vmo

10,000-20,000

A

300-330 KCAS

141
Q

Vmo

20,000-28,000

A

340 KCAS

142
Q

Mmo

Above 28,000

A

.85 M

Aircraft limitations (1 decks)

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