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g550 > Limits > Flashcards

Limits Flashcards

1
Q

Vmo FL290-FL320

A

0.85M

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2
Q

Vmo FL320-FL440

A

0.885M

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3
Q

Vmo FL440-FL510

A

0.86M

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4
Q

Vmo Above 8,000 ft

A

340 KCAS

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5
Q

Vmo Below 8,000 ft

A

300 KCAS

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6
Q

Vmca

A

112 KCAS

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7
Q

Vmca (Landing)

A

110 KCAS

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8
Q

Vmcg (SL)

A

107 KCAS

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9
Q

Vmcg (15,000 ft)

A

86 KCAS

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10
Q

Vmcg decreases by ____ per 1,000 ft from SL to 15,000 ft

A

~1 KCAS

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11
Q

Va (Maneuvering)

A

206 KCAS

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12
Q

Vb (Turb Pen) Below 10,000 ft

A

240 KCAS

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13
Q

Vb (Turb Pen) Above 10,000 ft

A

270 KCAS / 0.8M

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14
Q

Max Tire Speed

A

195.5 KCAS

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15
Q

Max Mach Trim Inop speed

A

0.8 M

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16
Q

Min Holding speed in Icing

A

160 KCAS

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17
Q

Max airport Alt

A

14,500 ft

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18
Q

Max airport Alt w/ HFLE

A

15,000 ft

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19
Q

Max operating Alt

A

51,000 ft

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21
Q

Max single pack operating Alt

A

48,000 ft

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21
Q

Baggage door open over 40,000 ft

A

Max 5 min

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22
Q

Do not open the baggage door with single pack ops over

A

45,000 ft

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23
Q

max alt with no yaw damper

A

45,000 ft

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24
Q

Max APU op alt

A

45,000 ft

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25
Q

APU guaranteed start up to

A

39,000 ft

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26
Q

APU may start up to

A

43,000 ft

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27
Q

Max APU EGT (start)

A

1050 deg C

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28
Q

Max APU EGT (running)

A

732 deg C

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29
Q

Max APU rotor speed

A

106% RPM

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30
Q

APU Alternator below 45,000 ft

A

40 kVa

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31
Q

Max fuel temp

A

140 deg C

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32
Q

Fuel temp may be up to ___ for ____ min

A

165 deg C, 15

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33
Q

Min fuel temp

A

-40 deg C

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34
Q

Cowl Anti-Ice

A

SAT 10 deg C or below and visible moisture

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35
Q

Wing Anti-Ice

A

Icing conditions are imminent or immediately upon detection

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36
Q

Max Engine Oil temp

A

160 deg C

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37
Q

Min Engine Oil temp (start)

A

-30 deg C

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38
Q

Min Engine Oil Temp (T/O power)

A

20 deg C

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39
Q

Min Engine Oil Px for T/O (below 72.3% HP)

A

35 psi (T/O), 25 psi (complete flight)

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40
Q

Engine must be shut down if Oil Px drops below

A

25 psi

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41
Q

Min Engine Oil Px for T/O (Above 90.0% HP)

A

45 psi (T/O), 35 psi (complete flight)

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42
Q

All operating fuel boost pumps MUST be ___ for all phases of flight unless fuel balancing in progress

A

ON

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43
Q

Max Fuel tank temp

A

54 deg C

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44
Q

Min Fuel tank temp

A

-37 deg C

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45
Q

Use of TR for power back is

A

NOT APPROVED

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46
Q

Starter duty cycle is ___ starts with a max of ___ per start cycle. Delay _____ between start cycles. After 3 start cycles delay use of starter by _____

A

3, 3 min, 15 sec, 15 min

47
Q

starter my be reengaged at HP RPM speeds up to stater cut out of ____ HP RPM

A

42% HP RPM

48
Q

Max Speed Flaps 10 deg

A

250 KCAS / 0.6 Mt

49
Q

Max speed Flaps 20 deg

A

220 KCAS / 0.6 Mt

50
Q

Max speed Flaps 39 deg

A

170 KCAS / 0.6 Mt

51
Q

Use of speed brakes is not allowed with

A

Landing Gear Extended or full flaps

52
Q

Use of flaps in icing is limited to

A

T/O, Approach, and Landing

53
Q

Ground Spoilers may be inop if

A

Anti-skid is operational,
20 deg Flaps are used,
Cowl and Wing Anti-Ice systems arent used

54
Q

If a touch and go is to be performed

A

GRD SPLR must be off and manual spoiler landing distance taken into account

55
Q

Max Alt to extend the landing gear

A

20,000 ft MSL

56
Q

Max landing gear extension speed

A

225 KCAS / 0.7 Mt

57
Q

Max gear speed (down and locked)

A

250 KCAS / 0.7 Mt

58
Q

Max landing gear extension speed (blow down)

A

175 KCAS

59
Q

Anti-skid my inop if

A

Runway is dry,
GRD SPLR is operational,
20 deg Flaps,
Cowl and Wing Anti-Ice not used

60
Q

g loading (Flaps up)

A

-1 to 2.5 g

61
Q

g loading (flaps 10 or 20)

A

0 - 2.0 g

62
Q

g loading (flaps 39 deg) below 75,300 lbs

A

0 - 2.0 g

63
Q

g loading (flaps 39 deg) above 75,300 lbs

A

0 - 1.5 g

64
Q

when HMG is in operation

A

speed brakes may be used provided 3 seconds for full range of movement

65
Q

Max cabin pressure differential

A

10.48 PSID

66
Q

Max cabin pressure differentail (T/O, Taxi, Landing)

A

0.3 PSID

67
Q

Takeoff in Alt Control mode is

A

Prohibited

68
Q

Max crosswind for engine start

A

30 Kt

69
Q

Max tailwind for engine start

A

20 kt

70
Q

Min height to engage auto-pilot

A

200 ft AGL

71
Q

Single-engine auto-pilot coupled go-around is

A

NOT ALLOWED

72
Q

Min height to disengage the auto-pilot from an ILS or LPV

A

60 ft AGL

73
Q

Min height to disengage the auto-pilot from LNAV/VNAV approach

A

50 ft below DA/MDA

74
Q

Max demonstrated altitude loss for a coupled go-around

A

60 ft

75
Q

Max slope for takeoff and landing

A

-2% to 2%

76
Q

Min Flight crew

A

2 pilots

77
Q

Max passengers

A

19

78
Q

Max occupants

A

22

79
Q

Aircraft width

A

93 ft 6 in

80
Q

Aircraft Height

A

25 ft 11 in

81
Q

Aircraft Length

A

96 ft 5 in

82
Q

Max ground starting TGT

A

700 deg C (Momentary)

83
Q

Max relighting (Airstart) TGT

A

850 deg C (Momentary)

84
Q

Max Takeoff LP % RPM

A

101.1%

85
Q

Max Takeoff HP % RPM

A

99.6%

86
Q

Max Takeoff TGT

A

900 deg C (5 min 2 Engines, 10 min 1 Engine)

87
Q

Max Continuous LP % RPM

A

101%

88
Q

Max Continuos HP % RPM

A

98.9%

89
Q

Max Continuous TGT

A

860 deg C

90
Q

Max Overspeed LP % RPM

A

101.5%

91
Q

Max Overspeed HP % RPM

A

99.8%

92
Q

Max Overspeed TGT

A

905 deg C (20 sec)

93
Q

Max Reverse LP % RPM

A

70.0% (30 sec)

94
Q

Zero Fuel Weight

A

54,500 lbs

95
Q

Max Ramp Weight

A

91,400 lbs

96
Q

Max Takeoff Weight

A

91,000 lbs

97
Q

Max Landing Weight

A

75,300 lbs

98
Q

Max Fuel Imbalance (Takeoff)

A

1,000 lbs

99
Q

Max Fuel Imbalance (In-flight)

A

2,000 lbs

100
Q

Max Fuel

A

41,300 lbs

101
Q

PTU activates

A

L hydro px < 1500 psi
L hydro Res > 1.5 gal
R hydro temp < 104.4 C

102
Q

Max ALT for air start

A

25,000 ft

103
Q

Min speed for windmill start

A

250 KCAS

104
Q

Min Vapp (flaps 20)

A

125 KCAS

105
Q

Max ALT for suction feed

A

20,000 ft

106
Q

Pylon Hot illuminates

A

250 F

107
Q

Aft Equip Hot

A

250 F

108
Q

L/R EER Hot

A

150 F

109
Q

Fuel level low

A

Hopper below 650 lb

110
Q

Maximum speed with the emergency stabilizer trim armed, autopilot engaged and a jammed elevator

A

270 KCAS / 0.8 Mt

111
Q

Max speed with missing vortex generators

A

0.85 Mt

112
Q

Max brake temp

A

650 C

113
Q

Wing anti ice temp

A

130 F +/- 10

g550 (12 decks)

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